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CN117432340B - A high specific pressure PDC drill bit - Google Patents

A high specific pressure PDC drill bit Download PDF

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Publication number
CN117432340B
CN117432340B CN202311768119.9A CN202311768119A CN117432340B CN 117432340 B CN117432340 B CN 117432340B CN 202311768119 A CN202311768119 A CN 202311768119A CN 117432340 B CN117432340 B CN 117432340B
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drill bit
blade
track
cutting blade
main cutting
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CN117432340A (en
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况雨春
张涛
杨博
杨淇灵
陈心玥
秦超
韩一维
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Chengdu Yanshi Innovation Technology Co ltd
Southwest Petroleum University
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Chengdu Yanshi Innovation Technology Co ltd
Southwest Petroleum University
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    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B10/00Drill bits
    • E21B10/46Drill bits characterised by wear resisting parts, e.g. diamond inserts
    • E21B10/54Drill bits characterised by wear resisting parts, e.g. diamond inserts the bit being of the rotary drag type, e.g. fork-type bits
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B10/00Drill bits
    • E21B10/42Rotary drag type drill bits with teeth, blades or like cutting elements, e.g. fork-type bits, fish tail bits
    • E21B10/43Rotary drag type drill bits with teeth, blades or like cutting elements, e.g. fork-type bits, fish tail bits characterised by the arrangement of teeth or other cutting elements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/10Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Mining & Mineral Resources (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Earth Drilling (AREA)

Abstract

本发明涉及一种高比压PDC钻头,属于钻探设备技术领域,包括接头和钻头体,所述接头与钻头体的一端固定连接,所述钻头体的另一端沿圆周方向分布至少两组高比压刀翼组,所述高比压刀翼组包括一个主切削刀翼以及至少一个同轨切削刀翼,且同轨切削刀翼上安装的同轨切削齿径向位置与同组的主切削刀翼上安装的主切削齿径向位置偏差Pv范围为‑0.5r至0.5r,其中r为主切削齿的半径。本发明通过让主切削刀翼上的切削齿承担切削岩石的工作,增强单齿上的比压,增强钻头的攻击性。同时让同轨切削刀翼承担增加接触点、预破碎、辅助破岩等辅助工作,从而增加钻头的稳定性、抗冲击性以及耐磨性。从而使所述的高比压PDC钻头具有强攻击性和高稳定性。

The invention relates to a high specific pressure PDC drill bit, belonging to the technical field of drilling equipment. Pressure blade group, the high specific pressure blade group includes a main cutting blade and at least one co-rail cutting blade, and the radial position of the co-rail cutting teeth installed on the co-rail cutting blade is consistent with the main cutting blade of the same group. The radial position deviation Pv of the main cutting teeth installed on the blade ranges from ‑0.5r to 0.5r, where r is the radius of the main cutting teeth. The invention allows the cutting teeth on the main cutting blade to take on the work of cutting rocks, thereby enhancing the specific pressure on the single tooth and enhancing the aggressiveness of the drill bit. At the same time, the co-orbital cutting blades are responsible for auxiliary tasks such as increasing contact points, pre-crushing, and auxiliary rock breaking, thereby increasing the stability, impact resistance and wear resistance of the drill bit. As a result, the high specific pressure PDC drill bit has strong aggressiveness and high stability.

Description

一种高比压PDC钻头A high specific pressure PDC drill bit

技术领域Technical Field

本发明涉及一种高比压PDC钻头,属于钻探设备技术领域。The invention relates to a high specific pressure PDC drill bit, belonging to the technical field of drilling equipment.

背景技术Background Art

PDC钻头又称为固定式刀翼钻头,其原因在于钻头的主要切削结构是与钻头体相对固定的刀翼结构。刀翼的固定方式有多种,其中所用最多的方式则是与钻头体一体式的刀翼。但无论固定形式如何变化,PDC钻头的主要切削原件仍然是安装并焊接在刀翼齿孔上的PDC切削齿。当钻压作用于钻头时,钻头体将钻压传递至PDC切削齿,多颗PDC切削齿共同压入岩石并随钻头绕钻头周旋做圆周运动,从而刮切岩石。因此,在相同的钻压下,增大单齿上的钻压配比,使得切削齿压入岩石的深度越大,从现象上来看则是钻头都具有更强的吃入岩石的能力。PDC drill bits are also called fixed blade drill bits because the main cutting structure of the drill bit is a blade structure that is relatively fixed to the drill bit body. There are many ways to fix the blade, and the most commonly used method is the blade that is integrated with the drill bit body. But no matter how the fixing form changes, the main cutting element of the PDC drill bit is still the PDC cutting teeth installed and welded on the blade tooth holes. When the drilling pressure acts on the drill bit, the drill bit body transfers the drilling pressure to the PDC cutting teeth. Multiple PDC cutting teeth are pressed into the rock together and move in a circle around the drill bit with the drill bit, thereby scraping the rock. Therefore, under the same drilling pressure, increasing the drilling pressure ratio on a single tooth, the deeper the cutting teeth are pressed into the rock, and from a phenomenon point of view, the drill bit has a stronger ability to eat into the rock.

现有技术中,不同刀翼数量的钻头吃入能力是不同的。因此设计人员根据地层岩性通常将钻头设计为不同数量的刀翼,从设计原理上来讲,常规技术在刀翼数量超过四刀翼时,便会同时设置有长刀翼和短刀翼。短刀翼的主要作用是增加钻头鼻部和肩部的布齿密度,从而使得钻头的耐磨性增加。同时,刀翼数量越多,钻头与岩石井底的接触点则越多,即支撑点越多,更容易维持钻头平衡。因此,常规设计中,针对浅层通常设计三刀翼钻头,深层研磨性地层通常设计七刀翼或八刀翼钻头。这样设计的目的是为了取舍不同数量刀翼的优缺点,三刀翼取其攻击性,八刀翼取其稳定性和耐磨性。但相对地,伴随着三刀翼钻头的高攻击性的特点,三刀翼钻头钻进时工具面不稳,井眼质量低,钻头寿命短等问题也困扰着施工人员。同样,在复杂难钻地层钻进时,八刀翼钻头展现出很强的耐磨性和稳定性,但同时也展现出比压低,钻速慢,钻时久的问题。In the prior art, the penetration capacity of drill bits with different numbers of blades is different. Therefore, designers usually design drill bits with different numbers of blades according to the lithology of the formation. From the design principle, when the number of blades exceeds four, conventional technology will be equipped with long blades and short blades at the same time. The main function of the short blade is to increase the tooth density of the nose and shoulder of the drill bit, thereby increasing the wear resistance of the drill bit. At the same time, the more blades there are, the more contact points the drill bit has with the bottom of the rock well, that is, the more support points there are, and it is easier to maintain the balance of the drill bit. Therefore, in conventional designs, three-blade drill bits are usually designed for shallow layers, and seven-blade or eight-blade drill bits are usually designed for deep abrasive formations. The purpose of this design is to choose the advantages and disadvantages of different numbers of blades, three blades for their aggressiveness, and eight blades for their stability and wear resistance. But relatively speaking, along with the high aggressiveness of the three-blade drill bit, the three-blade drill bit is unstable when drilling, the wellbore quality is low, and the drill bit life is short. Problems also plague construction personnel. Similarly, when drilling in complex and difficult-to-drill formations, the eight-blade drill bit exhibits strong wear resistance and stability, but also exhibits problems such as low specific pressure, slow drilling speed, and long drilling time.

上述问题的实质是钻头的设计方法。常规钻头的所有刀翼上的切削齿都参与井底全覆盖设计,导致每个刀翼都承担切削工作,钻压分摊给每个刀翼上的所有切削齿。在相同钻压的情况下,参与切削的刀翼越多,布齿密度越大,破碎岩石的切削齿越多,稳定性越高,单颗切削齿上分得的钻压越小,攻击性越小;反之,参与切削的刀翼越少,布齿密度越小,破碎岩石的切削齿越少,稳定性也就越低,单颗切削齿上分得的钻压越高,攻击性越大。因此在常规钻头中,如何同时具备高攻击性和高稳定性是亟待解决的问题。The essence of the above problem lies in the design method of the drill bit. The cutting teeth on all blades of a conventional drill bit participate in the full-coverage design of the bottom hole, which means that each blade is responsible for the cutting work and the drilling pressure is shared by all the cutting teeth on each blade. Under the same drilling pressure, the more blades involved in cutting, the greater the tooth density, the more cutting teeth that break the rock, the higher the stability, the smaller the drilling pressure allocated to a single cutting tooth, and the lower the aggressiveness; conversely, the fewer blades involved in cutting, the smaller the tooth density, the fewer cutting teeth that break the rock, the lower the stability, the higher the drilling pressure allocated to a single cutting tooth, and the greater the aggressiveness. Therefore, in conventional drill bits, how to have both high aggressiveness and high stability is an urgent problem to be solved.

发明内容Summary of the invention

本发明针对现有技术中常规钻头难以同时具备高攻击性和高稳定性的问题,提供一种高比压PDC钻头。Aiming at the problem that conventional drill bits in the prior art are difficult to have both high aggressiveness and high stability, the present invention provides a high specific pressure PDC drill bit.

本发明解决上述技术问题的技术方案如下:一种高比压PDC钻头,包括接头和钻头体,所述接头与钻头体的一端固定连接,所述钻头体的另一端沿圆周方向分布至少两组高比压刀翼组,所述高比压刀翼组包括一个主切削刀翼以及至少一个同轨切削刀翼,且同轨切削刀翼上安装的同轨切削齿径向位置与同组的主切削刀翼上安装的主切削齿径向位置偏差Pv范围为-0.5r至0.5r,其中r为主切削齿的半径,即同轨偏置带的范围是-0.5r-0.5r。The technical solution of the present invention for solving the above technical problems is as follows: a high specific pressure PDC drill bit, comprising a joint and a drill bit body, wherein the joint is fixedly connected to one end of the drill bit body, and at least two groups of high specific pressure blade groups are distributed along the circumferential direction at the other end of the drill bit body, wherein the high specific pressure blade groups include a main cutting blade and at least one co-track cutting blade, and the radial position deviation Pv of the co-track cutting teeth installed on the co-track cutting blade and the radial position deviation Pv of the main cutting teeth installed on the main cutting blade of the same group is in the range of -0.5r to 0.5r, wherein r is the radius of the main cutting tooth, that is, the range of the co-track offset band is -0.5r-0.5r.

此处对所述高比压刀翼组中的同轨切削刀翼和同轨切削齿的定义展开说明。在钻头的俯视图中,钻头绕钻头的中心轴线旋转,以主切削刀翼上的主切削齿的圆心为基点,钻头旋转一周形成的圆为基准圆环,所述基准圆环往径向向内的位置偏置为负值,最大取至-0.5r,即同轨偏差值Pv为负且最大取-0.5r;所述基准圆环往径向向外的位置偏置为正值,最大取至0.5r,即同轨偏差值Pv为正且最大取0.5r。由此Pv的范围形成主切削齿的同轨偏置带。若同轨切削刀翼上的切削齿的圆心旋转一定角度,所形成的轨迹圆弧在上述同轨偏置带范围内,则可以认为是同轨偏置带所属主切削齿的同轨切削齿。在同轨切削刀翼上至少有一颗切削齿在与主切削刀翼上切削齿的同轨偏置带范围内,即同轨切削刀翼上至少有一颗同轨切削齿,则可称该同轨切削刀翼与该主切削刀翼为同组的高比压刀翼组。Here, the definitions of the co-track cutting blades and co-track cutting teeth in the high-ratio pressure blade group are explained in detail. In the top view of the drill bit, the drill bit rotates around the central axis of the drill bit, and the center of the main cutting tooth on the main cutting blade is used as the base point. The circle formed by one rotation of the drill bit is the reference ring, and the radially inward position bias of the reference ring is a negative value, and the maximum is -0.5r, that is, the co-track deviation value Pv is negative and the maximum is -0.5r; the radially outward position bias of the reference ring is a positive value, and the maximum is 0.5r, that is, the co-track deviation value Pv is positive and the maximum is 0.5r. The range of Pv thus forms a co-track offset band for the main cutting tooth. If the center of the cutting tooth on the co-track cutting blade rotates a certain angle, and the trajectory arc formed is within the range of the above-mentioned co-track offset band, it can be considered as the co-track cutting tooth of the main cutting tooth to which the co-track offset band belongs. If at least one cutting tooth on the same-track cutting wing is within the same-track offset band of the cutting teeth on the main cutting wing, that is, if there is at least one same-track cutting tooth on the same-track cutting wing, then the same-track cutting wing and the main cutting wing can be called a high-pressure blade wing group of the same group.

在上述技术方案的基础上,本发明还可以做如下改进:On the basis of the above technical solution, the present invention can also be improved as follows:

所述主切削刀翼上安装的主切削齿数量满足,其中N表示主切削刀翼数量,n i 为第i号主切削刀翼上主切削齿的数量,r为主切削齿的半径,R为钻头的半径。该设置既能够形成井底全覆盖,同时还能够保证每个主切削刀翼具有足够的强度。The number of main cutting teeth installed on the main cutting blade meets and , where N represents the number of main cutting blades, ni is the number of main cutting teeth on the i-th main cutting blade, r is the radius of the main cutting teeth, and R is the radius of the drill bit. This setting can not only form full coverage of the bottom of the well, but also ensure that each main cutting blade has sufficient strength.

进一步的,所述高比压刀翼组中,同轨切削刀翼设置在主切削刀翼的沿圆周的顺时针或者逆时针方向。Furthermore, in the high specific pressure blade group, the same-track cutting blade is arranged in the clockwise or counterclockwise direction along the circumference of the main cutting blade.

进一步的,所述主切削刀翼和同轨切削刀翼的布齿包络线重合或者偏置,偏置距离d满足:-0.2r≤d≤0.2r 。Furthermore, the tooth arrangement envelopes of the main cutting blade and the same-track cutting blade are overlapped or offset, and the offset distance d satisfies: -0.2r≤d≤0.2r.

进一步的,所述同轨切削刀翼上的切削齿布置在钻头的径向外围部分。Furthermore, the cutting teeth on the same track cutting blade are arranged at the radial peripheral part of the drill bit.

进一步的,所述同轨切削刀翼的径向布齿起始位置在0.25R-0.8R的范围之内,R为钻头的半径。Furthermore, the radial tooth arrangement starting position of the same-track cutting blade is within the range of 0.25R-0.8R, where R is the radius of the drill bit.

进一步的,所述主切削刀翼上的主切削齿为宽刃齿。Furthermore, the main cutting teeth on the main cutting blade are wide-edge teeth.

进一步的,所述同轨切削刀翼上的同轨切削齿为非平面齿。Furthermore, the on-track cutting teeth on the on-track cutting blade are non-planar teeth.

进一步的,所述主切削刀翼上布置双排或多排切削齿,和/或所述同轨切削刀翼上布置双排或多排切削齿。Furthermore, the main cutting blade is provided with double or multiple rows of cutting teeth, and/or the same-track cutting blade is provided with double or multiple rows of cutting teeth.

进一步的,同一个钻头上的不同高比压刀翼组的刀翼数量不相同。Furthermore, the number of blades in blade groups with different high specific pressures on the same drill bit is different.

与现有技术相比,本发明的有益效果是:Compared with the prior art, the present invention has the following beneficial effects:

1)本申请通过设置高比压刀翼组,采用主切削刀翼和同轨切削刀翼进行配合,通过设置较少数量的主切削刀翼,增加主切削齿的比压,提升钻头的攻击性;通过设置同轨切削刀翼,增加钻头与岩石的接触部位,防止钻头失稳,增加钻头的稳定性,另一方面,同轨切削刀翼对整个钻头来说,增加了钻头的刀翼数量,从而增加了钻头与井底的接触点数量,进一步确保钻头在钻进过程中保持较高的稳定性,而同轨切削刀翼上的同轨切削齿不会消耗掉同组主切削刀翼上主切削齿的比压,因此钻头的攻击性不会因为增加了同轨切削刀翼而降低。反而同轨切削齿的存在,意味着整个钻头的PDC含量比没有同轨切削齿的钻头更高,岩层需要磨损掉更多的PDC材料才能使钻头失效,工程中反映出的现象则是钻头的寿命明显增长。1) This application sets a high specific pressure blade group, uses main cutting blades and co-track cutting blades to cooperate, sets a smaller number of main cutting blades, increases the specific pressure of the main cutting teeth, and improves the aggressiveness of the drill bit; sets co-track cutting blades to increase the contact area between the drill bit and the rock, prevents the drill bit from becoming unstable, and increases the stability of the drill bit. On the other hand, the co-track cutting blades increase the number of blades of the drill bit for the entire drill bit, thereby increasing the number of contact points between the drill bit and the bottom of the well, further ensuring that the drill bit maintains a high stability during the drilling process, and the co-track cutting teeth on the co-track cutting blades will not consume the specific pressure of the main cutting teeth on the main cutting blades of the same group, so the aggressiveness of the drill bit will not be reduced due to the addition of co-track cutting blades. On the contrary, the presence of co-track cutting teeth means that the PDC content of the entire drill bit is higher than that of a drill bit without co-track cutting teeth, and the rock formation needs to wear away more PDC materials before the drill bit fails. The phenomenon reflected in the project is that the life of the drill bit has been significantly increased.

2)通过将同轨切削刀翼上安装的同轨切削齿与同组的主切削刀翼上安装的对应主切削齿同轨偏差值Pv范围设置在-0.5r至0.5r之内,能够对同轨切削齿的辅助切削功能进行限定,使钻头整体具备攻击性和稳定性,在该偏差范围内可通过调整合理的偏差距离以适应不同地层的工程需要。2) By setting the co-track deviation value Pv range of the co-track cutting teeth installed on the co-track cutting blade and the corresponding main cutting teeth installed on the main cutting blade of the same group within -0.5r to 0.5r, the auxiliary cutting function of the co-track cutting teeth can be limited, so that the drill bit as a whole has aggressiveness and stability. Within this deviation range, a reasonable deviation distance can be adjusted to meet the engineering needs of different formations.

3)通过将同轨切削刀翼的径向布齿起始位置设置在0.25R-0.8R的范围之内,同轨切削刀翼上的切削齿布置在钻头的径向外围部分,可以使其承担较多的磨损量,增强钻头的耐磨性,延长寿命,使得钻头径向外围的接触点变多,有效减小了钻进过程中的多边形效应,增加钻头的稳定性,同时攻击性强。3) By setting the radial tooth layout starting position of the same-track cutting blade within the range of 0.25R-0.8R, the cutting teeth on the same-track cutting blade are arranged on the radial outer part of the drill bit, which can make it bear more wear, enhance the wear resistance of the drill bit, extend its service life, and increase the contact points on the radial outer part of the drill bit, effectively reducing the polygonal effect during drilling, increasing the stability of the drill bit, and at the same time having strong aggressiveness.

4)通过将主切削刀翼和同轨切削刀翼的布齿包络线重合或者偏置距离设置于-0.2r至0.2r的范围之内,能够降低同轨切削齿或主切削齿的磨损程度,并同时确保钻头的攻击性和稳定性。4) By aligning the tooth envelopes of the main cutting blade and the co-track cutting blade or setting the offset distance within the range of -0.2r to 0.2r, the wear degree of the co-track cutting teeth or the main cutting teeth can be reduced while ensuring the aggressiveness and stability of the drill bit.

附图说明BRIEF DESCRIPTION OF THE DRAWINGS

图1为本发明的一种高比压PDC钻头的示意图;FIG1 is a schematic diagram of a high specific pressure PDC drill bit of the present invention;

图2为本发明的一种高比压PDC钻头的俯视同轨示意图;FIG2 is a top view of a high specific pressure PDC drill bit of the present invention;

图3为本发明的一种高比压PDC钻头的径向布齿示意图;FIG3 is a schematic diagram of radial tooth arrangement of a high specific pressure PDC drill bit of the present invention;

图4为本发明的一种高比压PDC钻头的实施例七示意图;FIG4 is a schematic diagram of a seventh embodiment of a high specific pressure PDC drill bit of the present invention;

图5为本发明的一种高比压PDC钻头的实施例八示意图;FIG5 is a schematic diagram of an eighth embodiment of a high specific pressure PDC drill bit of the present invention;

图6为本发明的一种高比压PDC钻头的实施例九示意图;FIG6 is a schematic diagram of a ninth embodiment of a high specific pressure PDC drill bit according to the present invention;

图7为本发明的一种高比压PDC钻头的实施例十示意图;FIG7 is a schematic diagram of a high specific pressure PDC drill bit according to a tenth embodiment of the present invention;

图8为本发明的一种高比压PDC钻头的实施例十二示意图;FIG8 is a schematic diagram of a high specific pressure PDC drill bit according to a twelfth embodiment of the present invention;

图9为本发明的一种高比压PDC钻头的实施例十三示意图;FIG9 is a schematic diagram of a high specific pressure PDC drill bit according to a thirteenth embodiment of the present invention;

图10为本发明的一种高比压PDC钻头的实施例十四示意图;FIG10 is a schematic diagram of a high specific pressure PDC drill bit according to a fourteenth embodiment of the present invention;

图11为本发明的一种高比压PDC钻头的实施例十五示意图;FIG11 is a schematic diagram of a fifteenth embodiment of a high specific pressure PDC drill bit of the present invention;

图12为本发明的一种高比压PDC钻头的实施例十六示意图;FIG12 is a schematic diagram of a high specific pressure PDC drill bit according to a sixteenth embodiment of the present invention;

图中,1、接头;2、钻头体;3、高比压刀翼组;4、钻头的中心轴线;31、主切削刀翼;32、同轨切削刀翼;311、主切削齿;321、同轨切削齿;312、基准圆弧;322、同轨切削齿的圆环轨迹;323、同轨偏置带;314、主切削刀翼的径向布齿包络线;324、同轨切削刀翼的径向布齿包络线;315、主切削刀翼的布齿冠形线;325、同轨切削刀翼的布齿冠形线;316、第一后备齿;326、第二后备齿;Pv为同轨偏差值;R为钻头的半径;r为主切削齿的半径;d为同轨切削刀翼的径向布齿包络线与主切削刀翼的径向布齿包络线之间的偏置距离;Inp为同轨切削刀翼的径向布齿起始位置;A为钻头体的冠部的内锥角。In the figure, 1, joint; 2, drill body; 3, high specific pressure blade group; 4, center axis of drill bit; 31, main cutting blade; 32, same track cutting blade; 311, main cutting tooth; 321, same track cutting tooth; 312, reference arc; 322, circular track of same track cutting tooth; 323, same track offset zone; 314, radial tooth layout envelope of main cutting blade; 324, radial tooth layout envelope of same track cutting blade; 315, The tooth crown line of the main cutting blade; 325, the tooth crown line of the same track cutting blade; 316, the first backup tooth; 326, the second backup tooth; Pv is the same track deviation value; R is the radius of the drill bit; r is the radius of the main cutting tooth; d is the offset distance between the radial tooth envelope line of the same track cutting blade and the radial tooth envelope line of the main cutting blade; Inp is the radial tooth starting position of the same track cutting blade; A is the inner cone angle of the crown of the drill body.

具体实施方式DETAILED DESCRIPTION

为使本发明的上述目的、特征和优点能够更加明显易懂,下面结合附图对本发明的具体实施方式做详细的说明。在下面的描述中阐述了很多具体细节以便于充分理解本发明。但是本发明能够以很多不同于此描述的其它方式来实施,本领域技术人员可以在不违背本发明内涵的情况下做类似改进,因此本发明不受下面公开的具体实施例的限制。In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the specific embodiments of the present invention are described in detail below in conjunction with the accompanying drawings. In the following description, many specific details are set forth to facilitate a full understanding of the present invention. However, the present invention can be implemented in many other ways different from this description, and those skilled in the art can make similar improvements without violating the connotation of the present invention, so the present invention is not limited by the specific embodiments disclosed below.

除非另有定义,本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文在本发明的说明书中所使用的术语只是为了描述具体的实施方式,不是旨在于限制本发明。Unless otherwise defined, all technical and scientific terms used herein have the same meaning as those commonly understood by those skilled in the art of the present invention. The terms used in the specification of the present invention are only for describing specific embodiments and are not intended to limit the present invention.

如图1所示,一种高比压PDC钻头包括接头1和钻头体2,接头1与钻头体2的一端固定焊接在一起,所述钻头体2的另一端、即钻头顶部圆周分布至少两组高比压刀翼组3,所述高比压刀翼组3由一个主切削刀翼31以及至少一个同轨切削刀翼32组成。主切削刀翼31主要承担破岩工作,主切削刀翼31上分布有多个主切削齿311,同轨切削刀翼32主要承担辅助工作,同轨切削刀翼32上分布有至少一个同轨切削齿321。通过设置较少数量的主切削刀翼31,增加主切削齿311的比压,使主切削齿311吃入岩石的性能增强,提升钻头的攻击性。通过设置同轨切削刀翼32,增加钻头与岩石的接触部位,防止钻头失稳,增加钻头的稳定性。同时,同轨切削齿321的设置增加了整个钻头的PDC切削齿数量,即增加了钻头的PDC材料含量,能够大大提高钻头的耐磨性。让主切削刀翼31和同轨切削刀翼32形成高比压刀翼组3,能够极大程度上发挥出高攻击性和高稳定性的优势。As shown in FIG1 , a high specific pressure PDC drill bit includes a joint 1 and a drill body 2. The joint 1 is fixedly welded to one end of the drill body 2. The other end of the drill body 2, i.e., the top of the drill bit, is circumferentially distributed with at least two groups of high specific pressure blade groups 3. The high specific pressure blade group 3 is composed of a main cutting blade 31 and at least one co-track cutting blade 32. The main cutting blade 31 is mainly responsible for rock breaking, and a plurality of main cutting teeth 311 are distributed on the main cutting blade 31. The co-track cutting blade 32 is mainly responsible for auxiliary work, and at least one co-track cutting tooth 321 is distributed on the co-track cutting blade 32. By setting a smaller number of main cutting blades 31, the specific pressure of the main cutting teeth 311 is increased, so that the performance of the main cutting teeth 311 in eating into the rock is enhanced, and the aggressiveness of the drill bit is improved. By setting the co-track cutting blade 32, the contact area between the drill bit and the rock is increased, the drill bit is prevented from being unstable, and the stability of the drill bit is increased. At the same time, the setting of the same track cutting teeth 321 increases the number of PDC cutting teeth of the entire drill bit, that is, increases the PDC material content of the drill bit, which can greatly improve the wear resistance of the drill bit. The main cutting blade 31 and the same track cutting blade 32 form a high specific pressure blade group 3, which can greatly exert the advantages of high aggressiveness and high stability.

主切削齿311的半径和同轨切削齿321的半径可以设置为一致,也可以设置为不一致。当同轨切削齿321的半径大于主切削齿311的半径时,同轨切削刀翼32上的切削齿在数量不变的情况下金刚石当量增加,增加了钻头的耐磨性;当同轨切削齿321的半径小于主切削齿311的半径时,同轨切削刀翼32上的切削齿与岩石的接触长度减小,减少了同轨切削刀翼32承担的比压,使得主切削刀翼31的比压增大,钻头的攻击性增强。当两者相等的时候,钻头兼具耐磨性和攻击性,但由于同轨切削齿321和主切削齿311半径相同,切削岩石形成的岩石槽环形状正好吻合,使得钻头的稳定性得到提升。The radius of the main cutting tooth 311 and the radius of the co-track cutting tooth 321 can be set to be consistent or inconsistent. When the radius of the co-track cutting tooth 321 is larger than the radius of the main cutting tooth 311, the diamond equivalent of the cutting teeth on the co-track cutting blade 32 increases while the number remains unchanged, thereby increasing the wear resistance of the drill bit; when the radius of the co-track cutting tooth 321 is smaller than the radius of the main cutting tooth 311, the contact length between the cutting teeth on the co-track cutting blade 32 and the rock is reduced, thereby reducing the specific pressure borne by the co-track cutting blade 32, thereby increasing the specific pressure of the main cutting blade 31 and enhancing the aggressiveness of the drill bit. When the two are equal, the drill bit has both wear resistance and aggressiveness, but because the radii of the co-track cutting tooth 321 and the main cutting tooth 311 are the same, the shape of the rock groove ring formed by cutting the rock just matches, thereby improving the stability of the drill bit.

如图1和图2所示,钻头绕钻头的中心轴线4旋转,以主切削刀翼31上的主切削齿311的圆心为基点,随钻头旋转一周形成主切削齿311圆环轨迹,图1和图2中取一段圆弧轨迹展示,定义为基准圆弧312;以同轨切削刀翼32上的同轨切削齿321的圆心为基点,随钻头旋转形成同轨切削齿的圆环轨迹322。基准圆弧312和与之匹配的同轨切削齿的圆环轨迹322之间径向距离为同轨偏差值Pv。As shown in Figures 1 and 2, the drill bit rotates around the central axis 4 of the drill bit, with the center of the main cutting tooth 311 on the main cutting blade 31 as the base point, and the main cutting tooth 311 forms a circular track as the drill bit rotates one circle. A section of the circular arc track is shown in Figures 1 and 2, which is defined as the reference arc 312; with the center of the same track cutting tooth 321 on the same track cutting blade 32 as the base point, the circular track 322 of the same track cutting tooth is formed as the drill bit rotates. The radial distance between the reference arc 312 and the circular track 322 of the matching same track cutting tooth is the same track deviation value Pv.

同轨切削齿的圆环轨迹322相对于所述基准圆弧312往径向向内的位置偏置为负值,定义为同轨偏差值Pv为负,最大取至-0.5r,r为主切削齿311的半径;同轨切削齿的圆环轨迹322相对于所述基准圆弧312往径向向外的位置偏置为正值,定义为同轨偏差值Pv为正,最大取至0.5r。由此形成主切削齿311的同轨偏置带323。值得注意的是,当一组高比压刀翼组3内有多个同轨切削刀翼32时,一颗主切削齿311可能分别在多个同轨切削刀翼32上均有与之匹配的同轨切削齿321。与主切削齿311匹配的同轨切削齿321的同轨偏差值Pv可以为0,此时两者完全同轨,但在-0.5r至0.5r范围内的同轨切削齿321都可与主切削齿311匹配。若同轨切削刀翼32上的切削齿的圆心旋转一定角度,所形成的轨迹圆弧在上述同轨偏置带323范围内,则可以认为是同轨偏置带323所属主切削齿311的同轨切削齿321。也就是说,同轨切削刀翼32至少具有一个同轨切削齿321。同轨切削刀翼32上安装的同轨切削齿321与同组的主切削刀翼31上安装的对应主切削齿311同轨偏差值Pv范围为-0.5r至0.5r,所述同轨偏差值Pv范围是对同轨切削齿321辅助切削功能的限定。同轨偏差值Pv的正负号只表示径向向内偏差和径向向外偏差的方向,偏差绝对值越大,同轨切削齿321的辅助切削功能越强,分担的比压越多。但相对地,其对应主切削齿311上的比压减小,从而导致主切削刀翼31的比压减小,整个钻头的攻击性降低,稳定性增加。偏差绝对值越小,同轨切削齿321分担的比压越小,主切削齿311的比压越大,整个钻头的攻击性升高,稳定性降低。当偏差值等于0时,同轨切削齿321不具备辅助切削功能,只起到加强稳定性和耐磨性的作用,此时钻头的攻击性最强。因此可以通过设置上述偏差范围内的合理偏差距离以适应不同地层的工程需要。当同轨切削齿321的同轨偏差值Pv大于0.5r或小于-0.5r时,指同轨切削齿321相对于与之匹配的主切削齿311径向向内或向外偏置超过0.5r的距离,同轨切削齿321与岩石的接触弧长增大,承担了较大的切削量,同轨切削的作用减弱,转变为主切削作用,可能打破原本主切削布齿的平衡设计,导致钻头稳定性降低从而提早失效。The circular track 322 of the co-track cutting tooth is offset to a negative value inwardly in radial direction relative to the reference arc 312, which is defined as the co-track deviation value Pv is negative, and the maximum value is -0.5r, where r is the radius of the main cutting tooth 311; the circular track 322 of the co-track cutting tooth is offset to a positive value in radial direction relative to the reference arc 312, which is defined as the co-track deviation value Pv is positive, and the maximum value is 0.5r. Thus, the co-track offset zone 323 of the main cutting tooth 311 is formed. It is worth noting that when there are multiple co-track cutting blades 32 in a set of high-ratio pressure blade groups 3, a main cutting tooth 311 may have matching co-track cutting teeth 321 on multiple co-track cutting blades 32. The co-track deviation value Pv of the co-track cutting tooth 321 matching the main cutting tooth 311 can be 0, at which time the two are completely co-track, but the co-track cutting teeth 321 in the range of -0.5r to 0.5r can match the main cutting tooth 311. If the center of the cutting tooth on the same-track cutting blade 32 rotates a certain angle, and the resulting trajectory arc is within the above-mentioned same-track offset band 323, it can be considered as the same-track cutting tooth 321 of the main cutting tooth 311 to which the same-track offset band 323 belongs. In other words, the same-track cutting blade 32 has at least one same-track cutting tooth 321. The same-track deviation value Pv range of the same-track cutting tooth 321 installed on the same-track cutting blade 32 and the corresponding main cutting tooth 311 installed on the same group of main cutting blade 31 is -0.5r to 0.5r, and the same-track deviation value Pv range is a limitation on the auxiliary cutting function of the same-track cutting tooth 321. The positive and negative signs of the same-track deviation value Pv only indicate the direction of the radial inward deviation and the radial outward deviation. The larger the absolute value of the deviation, the stronger the auxiliary cutting function of the same-track cutting tooth 321, and the more specific pressure is shared. But relatively speaking, the specific pressure on the corresponding main cutting tooth 311 decreases, which leads to a decrease in the specific pressure of the main cutting blade 31, and the aggressiveness of the entire drill bit decreases, while the stability increases. The smaller the absolute value of the deviation is, the smaller the specific pressure shared by the same-track cutting tooth 321 is, the greater the specific pressure of the main cutting tooth 311 is, the aggressiveness of the entire drill bit increases, and the stability decreases. When the deviation value is equal to 0, the same-track cutting tooth 321 does not have an auxiliary cutting function, but only plays a role in enhancing stability and wear resistance. At this time, the aggressiveness of the drill bit is the strongest. Therefore, a reasonable deviation distance within the above-mentioned deviation range can be set to meet the engineering needs of different strata. When the same-track deviation value Pv of the same-track cutting tooth 321 is greater than 0.5r or less than -0.5r, it means that the same-track cutting tooth 321 is radially offset inward or outward by more than 0.5r relative to the matching main cutting tooth 311. The contact arc length between the same-track cutting tooth 321 and the rock increases, and it bears a larger cutting amount. The effect of the same-track cutting is weakened and transformed into the main cutting effect, which may break the original balanced design of the main cutting tooth arrangement, resulting in reduced stability of the drill bit and thus premature failure.

切削齿的覆盖通常设计为将所有刀翼上的切削齿共同形成井底全覆盖,每一个刀翼都承担着主切削的功能。但这样的布置方式会使得钻头的布齿密度较大,单齿上的比压降低,钻头的攻击性降低。常规的方法会通过减少刀翼来提高单个刀翼分得的钻压,但该设置又会加剧钻头的多边形效应,降低钻头的稳定性,增加钻头受到的冲击载荷。而本发明采用高比压刀翼组3的设计,将刀翼分为主切削刀翼31和同轨切削刀翼32,一方面仅对主切削刀翼31上的主切削齿311形成井底全覆盖,从承担切削功能的切削齿来看,这样降低了布齿密度,提高了切削齿的比压,增强了钻头的攻击性;另一方面,由于同轨切削刀翼32上的同轨切削齿321几乎不承担切削功能,但能增加钻头的金刚石含量和钻头与岩石的接触点,从而减弱钻头的多边形效应,增强钻头的稳定性。具体的,主切削刀翼31上安装的切削齿能够形成井底全覆盖,即满足 ,其中N表示刀翼数量,n i 为第i号主切削刀翼31上切削齿的数量,r为主切削齿311的半径,R为钻头的半径,所有的主切削齿311的半径相加至少要大于等于钻头半径,才能实现井底各位置的岩石都有切削齿负责破碎。同时,为了保证每个主切削刀翼31具有足够的强度,对主切削齿311的总数量范围设置为,即同一个刀翼上的切削齿不能靠的太近,否则会发生干涉,或者两颗齿之间的钻头体材料太少,导致强度不够,工作时容易发生掉齿的情况。The coverage of the cutting teeth is usually designed to form a full coverage of the bottom of the well with the cutting teeth on all blades, and each blade has the function of main cutting. However, such an arrangement will make the drill bit's tooth density larger, the specific pressure on a single tooth lower, and the aggressiveness of the drill bit lower. Conventional methods will increase the drilling pressure allocated to a single blade by reducing the blade, but this setting will aggravate the polygonal effect of the drill bit, reduce the stability of the drill bit, and increase the impact load on the drill bit. The present invention adopts the design of a high specific pressure blade group 3, and divides the blade into a main cutting blade 31 and a co-track cutting blade 32. On the one hand, only the main cutting teeth 311 on the main cutting blade 31 are fully covered at the bottom of the well. From the perspective of the cutting teeth that bear the cutting function, this reduces the tooth density, increases the specific pressure of the cutting teeth, and enhances the aggressiveness of the drill bit; on the other hand, since the co-track cutting teeth 321 on the co-track cutting blade 32 hardly bear the cutting function, but can increase the diamond content of the drill bit and the contact point between the drill bit and the rock, the polygonal effect of the drill bit is weakened and the stability of the drill bit is enhanced. Specifically, the cutting teeth installed on the main cutting blade 31 can form full coverage of the well bottom, that is, meet the requirements of , where N represents the number of blades, ni is the number of cutting teeth on the i-th main cutting blade 31, r is the radius of the main cutting tooth 311, and R is the radius of the drill bit. The sum of the radii of all the main cutting teeth 311 must be at least greater than or equal to the drill bit radius to ensure that the rocks at all positions on the bottom of the well are broken by cutting teeth. At the same time, in order to ensure that each main cutting blade 31 has sufficient strength, the total number of main cutting teeth 311 is set to That is, the cutting teeth on the same blade cannot be too close, otherwise interference will occur, or there is too little drill body material between the two teeth, resulting in insufficient strength and easy tooth loss during operation.

如图3所示为本发明的径向布齿示意图,所述同轨切削刀翼的径向布齿包络线324与主切削刀翼的径向布齿包络线314重合或者偏置,偏置距离d满足:-0.2r≤d≤0.2r。偏置距离等于-0.2r时,同轨切削刀翼32上的同轨切削齿321首先吃入岩石,对井底造成预破碎,钻头的攻击性最强。偏置距离d等于0时,同轨切削刀翼的径向布齿包络线324与主切削刀翼的径向布齿包络线314重合,此时主切削齿311和同轨切削齿321同时接触井底,钻头稳定性最强。随着偏置距离d的增大,最大至0.2r,意味着主切削齿311在吃入岩石0.2r深度后同轨切削齿321才接触岩石,比压主要由主切削齿311承担,此时钻头的攻击性较强。从主切削刀翼的布齿冠形线315和同轨切削刀翼的布齿冠形线325来看,同轨切削刀翼32的径向布齿起始位置Inp在0.25R-0.8R的范围内。由此可见,同轨切削刀翼32上的切削齿布置在钻头的径向外围部分。这是因为径向外围部分的回转半径大,旋转一圈切削过的行程远,使得切削齿极易磨损,将同轨切削齿321布置在外围部分可以承担较多的磨损量,增强钻头的耐磨性,延长寿命。并且,如此布置使得钻头径向外围的接触点变多,有效减小了钻进过程中的多边形效应,增加钻头的稳定性。心部岩石的破碎主要由主切削齿311承担,因此相对来说,主切削刀翼31为长刀翼,同轨切削刀翼32为短刀翼。同轨切削刀翼32的径向布齿起始位置在0.25R时,同轨切削刀翼32最长,在稳定性稍强的基础上,耐磨性大幅增强;同轨切削刀翼32的径向布齿起始位置在0.8R时,同轨切削刀翼32最短,在稳定性稍弱的基础上,攻击性大幅增强。可以根据地层岩性以及工况的不同,调整同轨切削刀翼32的长短以平衡钻头的攻击性和耐磨性。当Inp小于0.25R时,同轨切削刀翼32接近钻头的中心,从而同轨切削刀翼32与相邻的主切削刀翼31之间的流道狭窄,不利于排出岩屑;当Inp大于0.8R时,从布齿设计的角度上来讲,这已经是外肩过度至保径的位置,虽然在常规设计中可以从该位置布置切削齿以增加耐磨性,但同轨切削刀翼32从该位置布齿则丢失了同轨切削齿321该有的同轨辅助切削、增加稳定性等功能。钻头锥部至鼻部再至肩部的主切削齿311均有预支匹配的同轨切削齿321,能够使主切削齿311在承受高比压的同时得到同轨切削齿321的辅助功能,有利于延长钻头寿命。As shown in FIG3 , a schematic diagram of radial tooth arrangement of the present invention is shown. The radial tooth arrangement envelope 324 of the same-track cutting blade coincides with or is offset from the radial tooth arrangement envelope 314 of the main cutting blade, and the offset distance d satisfies: -0.2r≤d≤0.2r. When the offset distance is equal to -0.2r, the same-track cutting teeth 321 on the same-track cutting blade 32 first eat into the rock, causing pre-crushing of the bottom of the well, and the drill bit has the strongest aggressiveness. When the offset distance d is equal to 0, the radial tooth arrangement envelope 324 of the same-track cutting blade coincides with the radial tooth arrangement envelope 314 of the main cutting blade, and at this time the main cutting teeth 311 and the same-track cutting teeth 321 contact the bottom of the well at the same time, and the drill bit has the strongest stability. As the offset distance d increases, it reaches a maximum of 0.2r, which means that the main cutting teeth 311 only contact the rock after the same-track cutting teeth 321 eat into the rock to a depth of 0.2r, and the specific pressure is mainly borne by the main cutting teeth 311, and at this time the drill bit has a stronger aggressiveness. From the tooth crown line 315 of the main cutting blade and the tooth crown line 325 of the same track cutting blade, the radial tooth starting position Inp of the same track cutting blade 32 is within the range of 0.25R-0.8R. It can be seen that the cutting teeth on the same track cutting blade 32 are arranged in the radial peripheral part of the drill bit. This is because the radial peripheral part has a large radius of gyration and a long cutting distance in one rotation, which makes the cutting teeth very easy to wear. Arranging the same track cutting teeth 321 in the peripheral part can bear more wear, enhance the wear resistance of the drill bit, and extend the service life. In addition, such an arrangement increases the contact points of the radial periphery of the drill bit, effectively reduces the polygonal effect during the drilling process, and increases the stability of the drill bit. The crushing of the core rock is mainly borne by the main cutting teeth 311, so relatively speaking, the main cutting blade 31 is a long blade, and the same track cutting blade 32 is a short blade. When the radial tooth arrangement starting position of the same-track cutting blade 32 is 0.25R, the same-track cutting blade 32 is the longest, and the wear resistance is greatly enhanced on the basis of slightly stronger stability; when the radial tooth arrangement starting position of the same-track cutting blade 32 is 0.8R, the same-track cutting blade 32 is the shortest, and the aggressiveness is greatly enhanced on the basis of slightly weaker stability. The length of the same-track cutting blade 32 can be adjusted according to different formation lithology and working conditions to balance the aggressiveness and wear resistance of the drill bit. When Inp is less than 0.25R, the track cutting blade 32 is close to the center of the drill bit, so that the flow channel between the track cutting blade 32 and the adjacent main cutting blade 31 is narrow, which is not conducive to the discharge of cuttings; when Inp is greater than 0.8R, from the perspective of tooth arrangement design, this is already the position where the outer shoulder transitions to the diameter protection. Although cutting teeth can be arranged from this position in conventional design to increase wear resistance, the track cutting blade 32 loses the track auxiliary cutting and increased stability functions of the track cutting teeth 321. The main cutting teeth 311 from the cone part to the nose and then to the shoulder of the drill bit are all pre-supported and matched track cutting teeth 321, which can enable the main cutting teeth 311 to obtain the auxiliary function of the track cutting teeth 321 while bearing high specific pressure, which is beneficial to extend the life of the drill bit.

作为优选,所述高比压刀翼组3的主切削刀翼的径向布齿包络线314的内锥角、即钻头体的冠部的内锥角A的范围是150-180°,采用小内锥角范围是为了发挥主切削刀翼31的高比压优势,使心部的主切削齿311更加易于吃入岩石,将过剩的钻压分配给外部的主切削齿311,从而提高外部的主切削齿311的比压,最终提高钻头整体的攻击性。Preferably, the inner cone angle of the radial tooth arrangement envelope 314 of the main cutting blade of the high specific pressure blade group 3, that is, the inner cone angle A of the crown of the drill bit body, is in the range of 150-180°. The small inner cone angle range is adopted to give full play to the high specific pressure advantage of the main cutting blade 31, so that the main cutting teeth 311 at the center are easier to bite into the rock, and the excess drilling pressure is distributed to the external main cutting teeth 311, thereby increasing the specific pressure of the external main cutting teeth 311, and ultimately improving the overall aggressiveness of the drill bit.

作为优选,高比压刀翼组3的同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针或者逆时针方向,形成双刀翼组。当同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向时,主切削刀翼31在同轨切削刀翼32行进方向的前方,同一个同轨偏置带323范围内岩石首先与主切削刀翼31上的主切削齿311接触,同轨切削刀翼32主要起到提高钻头稳定性和耐磨性的作用。当同轨切削刀翼32设置在主切削刀翼31的沿圆周的逆时针方向时,同轨切削刀翼32在主切削刀翼31行进方向的前方,同一个同轨偏置带323范围内岩石首先与同轨切削刀翼32上的切削齿接触,从而降低了岩石对主切削刀翼31造成的冲击,间接增强了主切削齿311的抗冲击性能,但也一定程度上降低了钻头的攻击性。Preferably, the co-track cutting blade 32 of the high specific pressure blade group 3 is arranged in the clockwise or counterclockwise direction along the circumference of the main cutting blade 31 to form a double blade group. When the co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31, the main cutting blade 31 is in front of the co-track cutting blade 32 in the direction of travel, and the rock within the same co-track offset band 323 first contacts the main cutting tooth 311 on the main cutting blade 31, and the co-track cutting blade 32 mainly plays a role in improving the stability and wear resistance of the drill bit. When the on-track cutting wing 32 is arranged in the counterclockwise direction along the circumference of the main cutting wing 31, the on-track cutting wing 32 is in front of the main cutting wing 31 in the moving direction, and the rock within the same on-track offset band 323 first contacts the cutting teeth on the on-track cutting wing 32, thereby reducing the impact of the rock on the main cutting wing 31, indirectly enhancing the impact resistance of the main cutting teeth 311, but also reducing the aggressiveness of the drill bit to a certain extent.

作为优选,高比压刀翼组3的主切削刀翼31沿圆周的顺时针或者逆时针方向均设置同轨切削刀翼32,形成三刀翼组或多刀翼组。三刀翼组或多刀翼组的设置方式变化形式较多。以三刀翼组为例,包括一个主切削刀翼31和两个同轨切削刀翼32。当两个同轨切削刀翼32都布置在主切削刀翼31的沿圆周的顺时针方向时,钻头的多边形效应更低,稳定性更强,攻击性较强。当两个同轨切削刀翼32都布置在主切削刀翼31的沿圆周的逆时针方向时,钻头的多边形效应更低,稳定性更强,攻击性减弱,抗冲击性增强。当两个同轨切削刀翼32间隔着主切削刀翼31布置时,布置在主切削刀翼31的沿圆周的顺时针方向的同轨切削刀翼32主要起增强稳定性和耐磨性的作用,布置在主切削刀翼31的沿圆周的逆时针方向的同轨切削刀翼32主要起增强稳定性和抗冲击性的作用。Preferably, the main cutting blade 31 of the high specific pressure blade group 3 is provided with a same-track cutting blade 32 along the clockwise or counterclockwise direction of the circumference to form a three-blade group or a multi-blade group. There are many variations in the arrangement of the three-blade group or the multi-blade group. Taking the three-blade group as an example, it includes a main cutting blade 31 and two same-track cutting blades 32. When the two same-track cutting blades 32 are arranged in the clockwise direction of the main cutting blade 31 along the circumference, the polygonal effect of the drill bit is lower, the stability is stronger, and the aggressiveness is stronger. When the two same-track cutting blades 32 are arranged in the counterclockwise direction of the main cutting blade 31 along the circumference, the polygonal effect of the drill bit is lower, the stability is stronger, the aggressiveness is weakened, and the impact resistance is enhanced. When two co-track cutting wings 32 are arranged with the main cutting wing 31 in between, the co-track cutting wing 32 arranged along the clockwise direction of the main cutting wing 31 mainly plays a role in enhancing stability and wear resistance, while the co-track cutting wing 32 arranged along the counterclockwise direction of the main cutting wing 31 mainly plays a role in enhancing stability and impact resistance.

通常,刀翼之间的间隔角度是直接考虑相邻的刀翼之间的流道距离。而本发明中钻头顶部至少包括两组高比压刀翼组3,为了使同组内的同轨切削刀翼32与主切削刀翼31达到良好的同轨切削效果,防止同轨切削齿321重复破碎,所以与常规钻头相比,本发明需要考虑同一高比压刀翼组3内的刀翼间隔。假设同一个钻头上有多组不同刀翼数量的高比压刀翼组3,那么每一个高比压刀翼组3内的刀翼间隔角度范围都应重新计算,也就是说不同的高比压刀翼组3之间,内部刀翼的间隔角度也不一样。当一个高比压刀翼组3中具有多个同轨切削刀翼32时,同一个高比压刀翼组3中每个刀翼之间的间隔角度范围为288°/(N·Nin)<a<540°/(N·Nin),其中,N表示高比压刀翼组3的数量,Nin表示一个高比压刀翼组3内的刀翼数量,该范围的设置是为了保证刀翼之间有足够的流道空间用于排屑,且能够通过调整刀翼之间的间隔优化钻头的不平衡力,使钻头运行更加平稳。同时,该范围不会导致流道太窄而形成钻头泥包,也不会因为间隔距离太大而干涉其他高比压刀翼组3。这与常规设置中的用360°除以钻头刀翼总数量的方法,从设计原理上存在差异。当a<288°/(N·Nin)时,同一高比压刀翼组3内的刀翼之间间隔太近,可能排屑不及时造成重复破碎,影响同轨切削稳定性且加剧钻头磨损。当a>540°/(N·Nin)时,同一高比压刀翼组3内的刀翼间隔过大,加剧钻头的多边形效应,使钻头振动增加,钻头受到的冲击增大,可能造成钻头异常失效。Usually, the spacing angle between blades directly considers the flow path distance between adjacent blades. In the present invention, the top of the drill bit includes at least two groups of high-pressure blade groups 3. In order to make the same-track cutting blades 32 and the main cutting blades 31 in the same group achieve a good same-track cutting effect and prevent the same-track cutting teeth 321 from being repeatedly broken, compared with conventional drill bits, the present invention needs to consider the blade spacing within the same high-pressure blade group 3. Assuming that there are multiple groups of high-pressure blade groups 3 with different numbers of blades on the same drill bit, the blade spacing angle range within each high-pressure blade group 3 should be recalculated, that is, the spacing angles of the internal blades are different between different high-pressure blade groups 3. When a high pressure blade group 3 has multiple blades 32 for cutting on the same track, the interval angle range between each blade in the same high pressure blade group 3 is 288°/(N·N in )<a<540°/(N·N in ), where N represents the number of high pressure blade groups 3, and N in represents the number of blades in a high pressure blade group 3. This range is set to ensure that there is enough flow channel space between the blades for chip removal, and the unbalanced force of the drill bit can be optimized by adjusting the interval between the blades, so that the drill bit runs more smoothly. At the same time, this range will not cause the flow channel to be too narrow to form drill bit mud bags, nor will it interfere with other high pressure blade groups 3 due to too large intervals. This is different from the method of dividing 360° by the total number of drill blades in the conventional setting, in terms of design principle. When a<288°/(N·N in ), the blades in the same high specific pressure blade group 3 are too close to each other, which may cause repeated chip removal due to untimely chip removal, affect the stability of same-track cutting and increase the wear of the drill bit. When a>540°/(N·N in ), the blade spacing in the same high specific pressure blade group 3 is too large, which aggravates the polygonal effect of the drill bit, increases the vibration of the drill bit, increases the impact on the drill bit, and may cause abnormal failure of the drill bit.

进一步优选,钻头上不同的高比压刀翼组3的刀翼数量不相同。例如,钻头具有两个高比压刀翼组3,分别为一个双刀翼组和一个三刀翼组,双刀翼组的主切削刀翼31沿圆周的顺时针设置同轨切削刀翼32,三刀翼组的主切削刀翼31沿圆周的顺时针和逆时针方向均设置同轨切削刀翼32。这样设置可以通过对刀翼数量的调整,选择性平衡或提高钻头的稳定性和攻击性。It is further preferred that the number of blades of different high-specific-pressure blade wing groups 3 on the drill bit is different. For example, the drill bit has two high-specific-pressure blade wing groups 3, one double blade wing group and one triple blade wing group, the main cutting blade 31 of the double blade wing group is provided with the same-track cutting blade 32 along the clockwise direction of the circumference, and the main cutting blade 31 of the triple blade group is provided with the same-track cutting blade 32 along the clockwise and counterclockwise directions of the circumference. Such a setting can selectively balance or improve the stability and aggressiveness of the drill bit by adjusting the number of blades.

作为优选,主切削刀翼31上的主切削齿311为宽刃齿。利用宽刃齿的高比压齿刃,加强钻头的攻击性。此外,宽刃齿的平刃口使得切削齿与岩石为线接触,且接触线为直线,与冠部曲线基本重合,同样的冠部径向范围内用少量的宽刃齿则能实现井底全覆盖,进一步提高单齿上的比压。实际上,具有类似宽刃结构的切削齿也能在一定程度上增加钻头的攻击性。比如大钝角齿或者大曲率齿刃齿或者脊形宽刃齿。大钝角齿和大曲率齿刃切削齿适用于安装于钻头的外肩位置,以此来逼近冠部曲线外肩位置的曲率,从而获得高比压。脊形宽刃齿适用于复杂不均质地层或夹层,利用脊面的缓冲作用提高主切削齿311的抗冲击性,利用宽齿刃提高钻头的攻击性。Preferably, the main cutting teeth 311 on the main cutting blade 31 are wide-blade teeth. The high specific pressure tooth edge of the wide-blade teeth is used to enhance the aggressiveness of the drill bit. In addition, the flat edge of the wide-blade teeth makes the cutting teeth in line contact with the rock, and the contact line is a straight line, which basically coincides with the crown curve. A small number of wide-blade teeth within the same radial range of the crown can achieve full coverage of the bottom of the well, further increasing the specific pressure on a single tooth. In fact, cutting teeth with similar wide-blade structures can also increase the aggressiveness of the drill bit to a certain extent. For example, large obtuse-angle teeth or large-curvature tooth-blade teeth or ridge-shaped wide-blade teeth. Large obtuse-angle teeth and large-curvature tooth-blade cutting teeth are suitable for installation at the outer shoulder position of the drill bit, so as to approach the curvature of the outer shoulder position of the crown curve, thereby obtaining a high specific pressure. Ridge-shaped wide-blade teeth are suitable for complex and heterogeneous formations or interlayers. The buffering effect of the ridge surface is used to improve the impact resistance of the main cutting teeth 311, and the wide tooth edge is used to improve the aggressiveness of the drill bit.

作为优选,同轨切削刀翼32上的同轨切削齿321为非平面齿。根据地层环境的不同选用不同的非平面齿,例如在不均质地层和软硬交错地层,选用脊形非平面齿(屋脊齿、奔驰齿),使切削齿工作面与岩石的接触是连续的过程,从而提高钻头抗冲击性能。又例如,在研磨性地层,选用楔形齿或圆锥齿,提高切削齿的金刚石含量,从而提高钻头的耐磨性。Preferably, the same-track cutting teeth 321 on the same-track cutting blade 32 are non-planar teeth. Different non-planar teeth are selected according to different formation environments. For example, in heterogeneous formations and soft and hard interlaced formations, ridge-shaped non-planar teeth (roof teeth, Mercedes teeth) are selected to make the contact between the working surface of the cutting teeth and the rock a continuous process, thereby improving the impact resistance of the drill bit. For another example, in abrasive formations, wedge-shaped teeth or conical teeth are selected to increase the diamond content of the cutting teeth, thereby improving the wear resistance of the drill bit.

作为优选,主切削刀翼31上的切削齿可设置为双排或者多排,具体的,主切削齿311的后排布置第一后备齿316,所述第一后备齿316可布置一排或多排,其有益效果在于增加主切削刀翼31的金刚石复合片,以此增加金刚石含量,延长主切削刀翼31的寿命。Preferably, the cutting teeth on the main cutting blade 31 can be arranged in double rows or multiple rows. Specifically, the first backup teeth 316 are arranged in the rear row of the main cutting teeth 311. The first backup teeth 316 can be arranged in one row or multiple rows. The beneficial effect is to increase the diamond composite sheet of the main cutting blade 31, thereby increasing the diamond content and extending the life of the main cutting blade 31.

作为优选,同轨切削刀翼32上的切削齿可设置为双排或者多排,具体的,同轨切削齿321的后排布置第二后备齿326。通过该方式,增加同轨切削刀翼32上切削齿与岩石的接触点,增加钻头的稳定性。在此基础上,同轨切削齿321和第二后备齿326可设置为不同的偏置距离d,平衡同轨切削刀翼32的辅助切削功能和保持稳定性的功能,从而使同轨切削刀翼32具有更加综合的性能。同时,同轨切削齿321和第二后备齿326也可以选用不同的切削齿齿形,例如同轨切削刀翼32上的同轨切削齿321选用脊形齿以增加同轨切削刀翼32的抗冲击能力,第二后备齿326选用楔形齿,增强同轨切削刀翼32的耐磨性,从而使同轨切削刀翼32具有更加综合的性能。Preferably, the cutting teeth on the same track cutting blade 32 can be set to double rows or multiple rows. Specifically, the second backup teeth 326 are arranged in the rear row of the same track cutting teeth 321. In this way, the contact points between the cutting teeth on the same track cutting blade 32 and the rock are increased, and the stability of the drill bit is increased. On this basis, the same track cutting teeth 321 and the second backup teeth 326 can be set to different offset distances d to balance the auxiliary cutting function and the function of maintaining stability of the same track cutting blade 32, so that the same track cutting blade 32 has more comprehensive performance. At the same time, the same track cutting teeth 321 and the second backup teeth 326 can also use different cutting tooth shapes. For example, the same track cutting teeth 321 on the same track cutting blade 32 use ridge teeth to increase the impact resistance of the same track cutting blade 32, and the second backup teeth 326 use wedge teeth to enhance the wear resistance of the same track cutting blade 32, so that the same track cutting blade 32 has more comprehensive performance.

基于上述特征,结合以下实施例对具有特定有益效果的实施方案开展说明。Based on the above features, implementation schemes with specific beneficial effects are described in conjunction with the following examples.

实施例一:如图1所示为一种高比压PDC钻头的一个实施方案,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm,主切削刀翼31和同轨切削刀翼32上都布置单排平面圆齿。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于,主切削刀翼31在同轨切削刀翼32行进方向的前方,同一个同轨偏置带323范围内岩石首先与主切削刀翼31上的主切削齿311接触,同轨切削刀翼32主要起到提高钻头稳定性和耐磨性的作用。Embodiment 1: As shown in FIG1 , this is an implementation scheme of a high pressure ratio PDC drill bit, the radius R of the drill bit is 107.95 mm, the radius r of the main cutting tooth 311 is 6.72 mm, and single-row flat round teeth are arranged on the main cutting blade 31 and the co-track cutting blade 32. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31. The radial position deviation (co-track deviation Pv) of the co-track cutting tooth 321 installed on the co-track cutting blade 32 and the radial position deviation of the main cutting tooth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same-track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the main cutting blade 31 is in front of the same-track cutting blade 32 in the direction of travel, and the rock within the same same-track offset band 323 first contacts the main cutting teeth 311 on the main cutting blade 31. The same-track cutting blade 32 mainly plays a role in improving the stability and wear resistance of the drill bit.

实施例二:该方案与实施例一的区别在于,同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上主切削齿311的同轨偏差Pv为-3.36mm。该方案通过增大同轨偏差Pv,增大了同轨切削齿321的破岩作用,降低了主切削齿311的切削作用,降低了主切削齿311上的比压,从而使钻头的攻击性稍弱,但相对地钻头更加稳定,耐磨性更强。Embodiment 2: The difference between this solution and embodiment 1 is that the radial position of the track cutting teeth 321 installed on the track cutting blade 32 and the track deviation Pv of the main cutting teeth 311 on the same group of main cutting blade 31 is -3.36mm. This solution increases the rock breaking effect of the track cutting teeth 321 by increasing the track deviation Pv, reduces the cutting effect of the main cutting teeth 311, and reduces the specific pressure on the main cutting teeth 311, thereby making the drill bit slightly less aggressive, but relatively more stable and more wear-resistant.

实施例三:该方案与实施例一的区别在于,同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上主切削齿311的同轨偏差Pv为3.36mm。该方案通过增大同轨偏差Pv,增大了同轨切削齿321的破岩作用,降低了主切削齿311的切削作用,降低了主切削齿311上的比压,从而使钻头的攻击性稍弱,但相对地钻头更加稳定,耐磨性更强。实施例二与实施例三为两个反向的同轨偏差,其对刀翼产生的不平衡力也是反向的,通过对同轨偏差的调整,能够降低钻头的不平衡力,增强钻头的稳定性。Embodiment 3: The difference between this solution and embodiment 1 is that the radial position of the co-track cutting tooth 321 installed on the co-track cutting blade 32 and the co-track deviation Pv of the main cutting tooth 311 on the same group of main cutting blade 31 is 3.36mm. This solution increases the rock-breaking effect of the co-track cutting tooth 321 by increasing the co-track deviation Pv, reduces the cutting effect of the main cutting tooth 311, and reduces the specific pressure on the main cutting tooth 311, thereby making the drill bit slightly less aggressive, but relatively more stable and more wear-resistant. Embodiments 2 and 3 are two opposite co-track deviations, and the unbalanced force generated on the blade is also opposite. By adjusting the co-track deviation, the unbalanced force of the drill bit can be reduced and the stability of the drill bit can be enhanced.

实施例四:该方案与实施例一的区别在于,同轨切削刀翼32的径向布齿起始位置Inp在64.77mm处。该方案同轨切削刀翼32较短,在稳定性不变的基础上,攻击性增强。Embodiment 4: The difference between this solution and embodiment 1 is that the radial tooth arrangement starting position Inp of the same-track cutting blade 32 is at 64.77 mm. In this solution, the same-track cutting blade 32 is shorter, and the aggressiveness is enhanced on the basis of unchanged stability.

实施例五:该方案与实施例一的区别在于,主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324偏置距离d等于-1.344mm。该方案同轨切削刀翼32上的同轨切削齿321首先吃入岩石,对井底造成预破碎,钻头的攻击性最强。Embodiment 5: The difference between this solution and embodiment 1 is that the radial tooth arrangement envelope 314 of the main cutting blade and the radial tooth arrangement envelope 324 of the co-track cutting blade are offset by a distance d equal to -1.344 mm. In this solution, the co-track cutting teeth 321 on the co-track cutting blade 32 first eat into the rock, causing pre-crushing of the bottom of the well, and the drill bit is the most aggressive.

实施例六:该方案与实施例一和实施例三的区别在于,主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324偏置距离d等于1.344mm。该方案中,主切削齿311在吃入岩石1.344mm深度后同轨切削齿321才接触岩石,比压主要由主切削齿311承担,此时钻头的攻击性较强。Embodiment 6: The difference between this solution and Embodiment 1 and Embodiment 3 is that the radial tooth arrangement envelope 314 of the main cutting blade and the radial tooth arrangement envelope 324 of the same track cutting blade are offset by a distance d of 1.344 mm. In this solution, the main cutting teeth 311 only touch the rock after the same track cutting teeth 321 have penetrated the rock to a depth of 1.344 mm, and the specific pressure is mainly borne by the main cutting teeth 311. At this time, the drill bit is more aggressive.

实施例七:如图4所示为一种高比压PDC钻头的一个实施方案,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm,主切削刀翼31和同轨切削刀翼32上都布置单排平面圆齿。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。与实施例一的区别在于,同轨切削刀翼32设置在主切削刀翼31的沿圆周的逆时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311的同轨偏差为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。同轨切削刀翼32在主切削刀翼31行进方向的前方,同一个同轨偏置带323范围内岩石首先与同轨切削刀翼32上的切削齿接触,从而降低了岩石对主切削刀翼31造成的冲击,间接增强了主切削齿311的抗冲击性能,但也一定程度上降低了钻头的攻击性。Embodiment 7: As shown in FIG4, this is an implementation scheme of a high pressure ratio PDC drill bit, the radius R of the drill bit is 107.95 mm, the radius r of the main cutting tooth 311 is 6.72 mm, and single-row flat round teeth are arranged on the main cutting blade 31 and the co-track cutting blade 32. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The difference from Embodiment 1 is that the co-track cutting blade 32 is arranged in the counterclockwise direction along the circumference of the main cutting blade 31. The radial position of the co-track cutting tooth 321 installed on the co-track cutting blade 32 is 0 with respect to the co-track deviation of the main cutting tooth 311 installed on the main cutting blade 31 of the same group. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same-track cutting blade 32 is at 32.385 mm. The same-track cutting blade 32 is in front of the main cutting blade 31 in the direction of travel, and the rock in the same-track offset zone 323 first contacts the cutting teeth on the same-track cutting blade 32, thereby reducing the impact of the rock on the main cutting blade 31, indirectly enhancing the impact resistance of the main cutting teeth 311, but also reducing the aggressiveness of the drill bit to a certain extent.

实施例八:如图5所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm,主切削刀翼31和同轨切削刀翼32上都布置单排平面圆齿。与实施例一的区别在于,钻头顶部圆周分布两组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及两个同轨切削刀翼32组成。两个同轨切削刀翼32都布置在主切削刀翼31的沿圆周的顺时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于,钻头的多边形效应更低,稳定性更强,攻击性较强。Embodiment 8: A high pressure ratio PDC drill bit as shown in FIG5, the radius R of the drill bit is 107.95 mm, the radius r of the main cutting tooth 311 is 6.72 mm, and single-row flat round teeth are arranged on both the main cutting blade 31 and the co-track cutting blade 32. The difference from Embodiment 1 is that two groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 is composed of a main cutting blade 31 and two co-track cutting blades 32. The two co-track cutting blades 32 are arranged in the clockwise direction along the circumference of the main cutting blade 31. The radial position deviation (co-track deviation Pv) between the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the radial position deviation (co-track deviation Pv) of the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the polygon effect of the drill bit is lower, the stability is stronger, and the aggressiveness is stronger.

实施例九:如图6所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm,主切削刀翼31和同轨切削刀翼32上都布置单排平面圆齿。与实施例一的区别在于,钻头顶部圆周分布两组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及两个同轨切削刀翼32组成。与实施例八的区别在于,两个同轨切削刀翼32都布置在主切削刀翼31的沿圆周的逆时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于,钻头的多边形效应更低,稳定性更强,攻击性减弱,抗冲击性增强。Embodiment 9: A high pressure ratio PDC drill bit as shown in FIG6, the radius R of the drill bit is 107.95 mm, the radius r of the main cutting tooth 311 is 6.72 mm, and single-row flat round teeth are arranged on both the main cutting blade 31 and the co-track cutting blade 32. The difference from Embodiment 1 is that two groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 is composed of a main cutting blade 31 and two co-track cutting blades 32. The difference from Embodiment 8 is that the two co-track cutting blades 32 are arranged in the counterclockwise direction along the circumference of the main cutting blade 31. The radial position deviation (co-track deviation Pv) between the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the radial position deviation (co-track deviation Pv) of the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the polygon effect of the drill bit is lower, the stability is stronger, the aggressiveness is weakened, and the impact resistance is enhanced.

实施例十:如图7所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm,主切削刀翼31和同轨切削刀翼32上都布置单排平面圆齿。与实施例一的区别在于,钻头顶部圆周分布两组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及两个同轨切削刀翼32组成。与实施例八和实施例九的区别在于两个同轨切削刀翼32间隔着主切削刀翼31布置,布置在主切削刀翼31的沿圆周的顺时针方向的同轨切削刀翼32主要起增强稳定性和耐磨性的作用,布置在主切削刀翼31的沿圆周的逆时针方向的同轨切削刀翼32主要起增强稳定性和抗冲击性的作用。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于,钻头的多边形效应更低,且同时增强了钻头的稳定性和抗冲击性。Embodiment 10: A high pressure ratio PDC drill bit as shown in FIG7, the radius R of the drill bit is 107.95 mm, the radius r of the main cutting tooth 311 is 6.72 mm, and single-row flat round teeth are arranged on both the main cutting blade 31 and the co-track cutting blade 32. The difference from Embodiment 1 is that two groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 is composed of a main cutting blade 31 and two co-track cutting blades 32. The difference from Embodiment 8 and Embodiment 9 is that the two co-track cutting blades 32 are arranged with the main cutting blade 31 in between, and the co-track cutting blade 32 arranged along the clockwise direction of the circumference of the main cutting blade 31 mainly plays a role in enhancing stability and wear resistance, and the co-track cutting blade 32 arranged along the counterclockwise direction of the circumference of the main cutting blade 31 mainly plays a role in enhancing stability and impact resistance. The radial position deviation (co-track deviation Pv) between the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth arrangement envelope 314 of the main cutting blade coincides with the radial tooth arrangement envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the co-track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the polygon effect of the drill bit is lower, and at the same time, the stability and impact resistance of the drill bit are enhanced.

实施例十一:该方案与实施例八、实施例九、实施例十的区别在于,该方案顶部分布的两个高比压刀翼组3分别为一个双刀翼组和一个三刀翼组,双刀翼组的主切削刀翼31沿圆周的顺时针方向设置同轨切削刀翼32,三刀翼组的主切削刀翼31沿圆周的顺时针和逆时针方向均设置同轨切削刀翼32。该方案的有益效果在于,通过对组内刀翼数量的调整,选择性提高高比压刀翼组3的攻击性。例如本方案与实施例八、实施例九、实施例十相比,在刀翼数量少的高比压刀翼组3内,单个刀翼上的钻压进一步增大,即比压进一步提高,增强了钻头的攻击性。Embodiment 11: The difference between this solution and Embodiment 8, Embodiment 9 and Embodiment 10 is that the two high pressure blade groups 3 distributed at the top of this solution are respectively a double blade group and a triple blade group, the main cutting blade 31 of the double blade group is provided with a same track cutting blade 32 along the clockwise direction of the circumference, and the main cutting blade 31 of the triple blade group is provided with a same track cutting blade 32 along the clockwise and counterclockwise directions of the circumference. The beneficial effect of this solution is that the aggressiveness of the high pressure blade group 3 is selectively improved by adjusting the number of blades in the group. For example, compared with Embodiment 8, Embodiment 9 and Embodiment 10, in the high pressure blade group 3 with a small number of blades, the drilling pressure on a single blade is further increased, that is, the pressure ratio is further improved, thereby enhancing the aggressiveness of the drill bit.

实施例十二:如图8所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向。同轨切削刀翼32上都布置平面圆齿,为同轨切削齿321。与实施例一的区别在于,主切削刀翼31上布置双排平面圆齿,即主切削齿311和第一后备齿316。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于,主切削刀翼31布置双排切削齿,第一排的主切削齿311主要用于切削岩石,第二排的第一后备齿316主要增强钻头的耐磨性,改善主切削齿311的受力情况,从而增强主切削齿311的寿命。Embodiment 12: A high pressure ratio PDC drill bit as shown in FIG8 , the radius R of the drill bit is 107.95 mm, and the radius r of the main cutting tooth 311 is 6.72 mm. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31. Planar round teeth are arranged on the co-track cutting blade 32, which are co-track cutting teeth 321. The difference from Embodiment 1 is that double rows of planar round teeth are arranged on the main cutting blade 31, namely the main cutting teeth 311 and the first backup teeth 316. The radial position deviation (co-track deviation Pv) between the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth arrangement envelope 314 of the main cutting blade coincides with the radial tooth arrangement envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the co-track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the main cutting blade 31 is arranged with two rows of cutting teeth, the main cutting teeth 311 of the first row are mainly used for cutting rocks, and the first backup teeth 316 of the second row are mainly used to enhance the wear resistance of the drill bit, improve the stress condition of the main cutting teeth 311, and thus enhance the service life of the main cutting teeth 311.

实施例十三:如图9所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向。主切削刀翼31上都布置平面圆齿,即主切削齿311。与实施例一的区别在于,同轨切削刀翼32上布置双排切削齿,即同轨切削齿321和第二后备齿326。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于,同轨切削刀翼32布置双排平面圆齿,增加了同轨切削刀翼32的接触点,一方面起到限制主切削刀翼31吃深的作用,使主切削刀翼31上的主切削齿311载荷波动更小;另一方面增加钻头的稳定性,延长钻头的寿命。Embodiment 13: A high pressure ratio PDC drill bit as shown in FIG9, the radius R of the drill bit is 107.95 mm, and the radius r of the main cutting tooth 311 is 6.72 mm. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31. Planar circular teeth, namely, main cutting teeth 311, are arranged on the main cutting blade 31. The difference from Embodiment 1 is that double rows of cutting teeth, namely, co-track cutting teeth 321 and second backup teeth 326, are arranged on the co-track cutting blade 32. The radial position deviation (co-track deviation Pv) between the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the radial position deviation of the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth arrangement envelope 314 of the main cutting blade coincides with the radial tooth arrangement envelope 324 of the same-track cutting blade. The radial tooth arrangement starting position Inp of the same-track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the same-track cutting blade 32 is arranged with double rows of flat round teeth, which increases the contact points of the same-track cutting blade 32. On the one hand, it plays a role in limiting the depth of the main cutting blade 31, so that the load fluctuation of the main cutting teeth 311 on the main cutting blade 31 is smaller; on the other hand, it increases the stability of the drill bit and prolongs the life of the drill bit.

根据地层和工况特点,本发明的一种高比压PDC钻头的切削齿可以布置非平面齿。According to the characteristics of the formation and working conditions, the cutting teeth of the high specific pressure PDC drill bit of the present invention can be arranged with non-planar teeth.

实施例十四:如图10所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm。与实施例一的区别在于,该方案的主切削刀翼31的主切削齿311布置为单排的宽刃齿。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于利用宽刃齿的高比压齿刃,加强钻头的攻击性;此外,宽刃齿的平刃口使得切削齿与岩石为线接触,且接触线为直线,与冠部曲线基本重合,同样的冠部径向范围内用少量的宽刃齿则能实现井底全覆盖,进一步提高单齿上的比压。Embodiment 14: A high pressure ratio PDC drill bit as shown in FIG10, the radius R of the drill bit is 107.95 mm, and the radius r of the main cutting tooth 311 is 6.72 mm. The difference from embodiment 1 is that the main cutting teeth 311 of the main cutting blade 31 of this scheme are arranged as a single row of wide blade teeth. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31. The radial position deviation (co-track deviation Pv) of the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the radial position deviation of the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 32.385mm. The beneficial effect of this solution is to use the high specific pressure tooth edge of the wide blade tooth to enhance the aggressiveness of the drill bit; in addition, the flat edge of the wide blade tooth makes the cutting tooth and the rock in line contact, and the contact line is a straight line, which basically coincides with the crown curve. In the same radial range of the crown, a small number of wide blade teeth can achieve full coverage of the bottom of the well, further improving the specific pressure on a single tooth.

实施例十五:如图11所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm。与实施例一的区别在于,该方案的主切削刀翼31的主切削齿311布置为单排的脊形齿。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于利用脊形齿工作面与岩石的接触是连续的过程,从而提高钻头抗冲击性能。Embodiment 15: A high pressure ratio PDC drill bit as shown in FIG11, the radius R of the drill bit is 107.95 mm, and the radius r of the main cutting tooth 311 is 6.72 mm. The difference from embodiment 1 is that the main cutting teeth 311 of the main cutting blade 31 of this scheme are arranged as a single row of ridge teeth. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31. The radial position deviation (co-track deviation Pv) of the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the radial position deviation of the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the contact between the ridge-shaped tooth working surface and the rock is a continuous process, thereby improving the impact resistance of the drill bit.

实施例十六:如图12所示的一种高比压PDC钻头,钻头的半径R为107.95mm,主切削齿311的半径r为6.72mm。与实施例一的区别在于,该方案的同轨切削刀翼32的同轨切削齿321布置为单排的脊形齿。钻头顶部圆周分布三组高比压刀翼组3,每组高比压刀翼组3由一个主切削刀翼31以及一个同轨切削刀翼32组成。同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针方向。同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上安装的主切削齿311径向位置偏差(同轨偏差Pv)为0。主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合。同轨切削刀翼32的径向布齿起始位置Inp在32.385mm处。该方案的有益效果在于利用脊形齿工作面与岩石的接触是连续的过程,从而提高同轨切削刀翼32的抗冲击性能,增强钻头的稳定性。Embodiment 16: A high pressure ratio PDC drill bit as shown in FIG12, the radius R of the drill bit is 107.95 mm, and the radius r of the main cutting tooth 311 is 6.72 mm. The difference from the embodiment 1 is that the co-track cutting teeth 321 of the co-track cutting blade 32 of this scheme are arranged as a single row of ridge-shaped teeth. Three groups of high pressure ratio blade groups 3 are distributed circumferentially on the top of the drill bit, and each group of high pressure ratio blade groups 3 consists of a main cutting blade 31 and a co-track cutting blade 32. The co-track cutting blade 32 is arranged in the clockwise direction along the circumference of the main cutting blade 31. The radial position deviation (co-track deviation Pv) of the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the radial position deviation of the main cutting teeth 311 installed on the main cutting blade 31 of the same group is 0. The radial tooth layout envelope 314 of the main cutting blade coincides with the radial tooth layout envelope 324 of the co-track cutting blade. The radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 32.385 mm. The beneficial effect of this solution is that the contact between the ridge-shaped tooth working surface and the rock is a continuous process, thereby improving the impact resistance of the same track cutting blade 32 and enhancing the stability of the drill bit.

对比例一:该方案与实施例一的区别在于,同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上主切削齿311的同轨偏差Pv为-4.12mm。该方案中同轨切削齿321分担的比压偏多,导致主切削刀翼31的比压偏小,使得钻头的攻击性明显偏低。Comparative Example 1: The difference between this solution and Example 1 is that the radial position of the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the co-track deviation Pv of the main cutting teeth 311 on the same group of main cutting blade 31 is -4.12mm. In this solution, the co-track cutting teeth 321 share more specific pressure, resulting in a smaller specific pressure of the main cutting blade 31, which makes the aggressiveness of the drill bit significantly lower.

对比例二:该方案与实施例一的区别在于,同轨切削刀翼32上安装的同轨切削齿321径向位置与同组的主切削刀翼31上主切削齿311的同轨偏差Pv为4.06mm。该方案中同轨切削齿321分担的比压偏多,导致主切削刀翼31的比压偏小,使得钻头的攻击性明显偏低。Comparative Example 2: The difference between this solution and Example 1 is that the radial position of the co-track cutting teeth 321 installed on the co-track cutting blade 32 and the co-track deviation Pv of the main cutting teeth 311 on the same group of main cutting blade 31 is 4.06 mm. In this solution, the co-track cutting teeth 321 share more specific pressure, resulting in a smaller specific pressure of the main cutting blade 31, which makes the aggressiveness of the drill bit significantly lower.

对比例三:该方案与实施例四的区别在于,同轨切削刀翼32的径向布齿起始位置Inp在20.52处。该方案中同轨切削刀翼32偏长,使其攻击性偏差,且不利于排出岩屑。Comparative Example 3: The difference between this solution and Example 4 is that the radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 20.52. In this solution, the same track cutting blade 32 is too long, which makes its aggressiveness biased and is not conducive to the discharge of rock chips.

对比例四:该方案与实施例四的区别在于,同轨切削刀翼32的径向布齿起始位置Inp在90.22处。该方案中同轨切削刀翼32极短,使其稳定性偏差。Comparative Example 4: The difference between this solution and Example 4 is that the radial tooth arrangement starting position Inp of the same track cutting blade 32 is at 90.22. In this solution, the same track cutting blade 32 is very short, which makes its stability deviation.

对比例五:该方案与实施例五的区别在于,主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324偏置距离d等于-2.016mm。该方案中同轨切削刀翼32上的同轨切削齿321首先吃入岩石,但偏置距离d过大导致同轨切削齿321极易被磨损,影响其使用寿命。Comparative Example 5: The difference between this solution and Example 5 is that the offset distance d between the radial tooth arrangement envelope 314 of the main cutting blade and the radial tooth arrangement envelope 324 of the co-track cutting blade is equal to -2.016 mm. In this solution, the co-track cutting teeth 321 on the co-track cutting blade 32 first eat into the rock, but the offset distance d is too large, causing the co-track cutting teeth 321 to be easily worn, which affects their service life.

对比例六:该方案与实施例六的区别在于,主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324偏置距离d等于2.016mm。该方案中主切削齿311首先吃入岩石,但偏置距离d过大导致主切削齿311极易被磨损,影响其使用寿命。Comparative Example 6: The difference between this solution and Example 6 is that the offset distance d between the radial tooth arrangement envelope 314 of the main cutting blade and the radial tooth arrangement envelope 324 of the same track cutting blade is equal to 2.016 mm. In this solution, the main cutting teeth 311 first bite into the rock, but the offset distance d is too large, which makes the main cutting teeth 311 very easy to be worn, affecting its service life.

对实施例一至十六中以及对比例一至六得到的钻头进行钻孔试验,并对实施例一至三、对比例一、二的试验结果进行记录,可得到表1;The drill bits obtained in Examples 1 to 16 and Comparative Examples 1 to 6 were subjected to drilling tests, and the test results of Examples 1 to 3 and Comparative Examples 1 and 2 were recorded, and Table 1 was obtained;

对实施例四、对比例三、四试验结果进行记录,可得到表2;The test results of Example 4, Comparative Examples 3 and 4 are recorded to obtain Table 2;

对实施例五、六、对比例五、六试验结果进行记录,可得到表3;The test results of Examples 5 and 6 and Comparative Examples 5 and 6 are recorded to obtain Table 3;

对实施例七至十一试验结果进行记录,可得到表4;对实施例十二至十六试验结果进行记录,可得到表5,表中对各项性能的优劣排序为:差<较差<一般<稍强<较强<强。By recording the test results of Examples 7 to 11, Table 4 can be obtained; by recording the test results of Examples 12 to 16, Table 5 can be obtained, in which the performance is ranked as follows: poor < poor < general < slightly stronger < stronger < strong.

表1本发明实施例一至三与对比例一、二特征、尺寸和试验结果评价表Table 1 Characteristics, dimensions and test results of Examples 1 to 3 of the present invention and Comparative Examples 1 and 2

由实施例一至三、对比例一、二,结合表1的试验评价可以看出,该方案通过将同轨切削刀翼32上安装的同轨切削齿321与同组的主切削刀翼31上安装的对应主切削齿311同轨偏差值Pv范围设置在-0.5r至0.5r之内,对同轨切削齿321辅助切削功能进行适当的限定,能够使钻头整体的攻击性和稳定性、以及抗冲击性、耐磨性均较为出色,在该偏差范围内可通过调整合理的偏差距离以适应不同地层的工程需要。It can be seen from Examples 1 to 3, Comparative Examples 1 and 2, and the experimental evaluation in Table 1 that the scheme sets the on-track deviation value Pv range of the on-track cutting tooth 321 installed on the on-track cutting wing 32 and the corresponding main cutting tooth 311 installed on the main cutting wing 31 of the same group within -0.5r to 0.5r, and appropriately limits the auxiliary cutting function of the on-track cutting tooth 321, so that the overall aggressiveness and stability of the drill bit, as well as the impact resistance and wear resistance are relatively excellent. Within this deviation range, a reasonable deviation distance can be adjusted to meet the engineering needs of different formations.

表2本发明实施例四与对比例三、四特征、尺寸和试验结果评价表Table 2 Characteristics, dimensions and test results of Example 4 of the present invention and Comparative Examples 3 and 4

由实施例四、对比例三、四,结合表2的试验评价可以看出,该方案通过将同轨切削刀翼32的径向布齿起始位置在0.25R-0.8R的范围之内,同轨切削刀翼32上的切削齿布置在钻头的径向外围部分,可以使其承担较多的磨损量,增强钻头的耐磨性,延长寿命,使得钻头径向外围的接触点变多,有效减小了钻进过程中的多边形效应,增加钻头的稳定性,同时攻击性强。可以根据地层岩性以及工况的不同,调整同轨切削刀翼32的长短以平衡钻头的攻击性和耐磨性。From the fourth embodiment, the third and fourth comparative examples, and the test evaluation in Table 2, it can be seen that the scheme arranges the cutting teeth on the same track cutting blade 32 in the radial peripheral part of the drill bit by setting the radial tooth arrangement starting position of the same track cutting blade 32 within the range of 0.25R-0.8R, so that the same track cutting blade 32 can bear more wear, enhance the wear resistance of the drill bit, extend the service life, increase the contact points on the radial periphery of the drill bit, effectively reduce the polygon effect during drilling, increase the stability of the drill bit, and have strong aggressiveness. The length of the same track cutting blade 32 can be adjusted according to the different formation lithology and working conditions to balance the aggressiveness and wear resistance of the drill bit.

表3本发明实施例五至六与对比例五至六特征、尺寸和试验结果评价表Table 3 Characteristics, dimensions and test results of Examples 5 to 6 of the present invention and Comparative Examples 5 to 6

由实施例五、六、对比例五、六,结合表3的试验评价可以看出,该方案通过将主切削刀翼的径向布齿包络线314和同轨切削刀翼的径向布齿包络线324重合或者偏置距离d设置于-0.2r≤d≤0.2r的范围之内,可以同时确保钻头的攻击性和稳定性,在该距离范围内可通过适当的调整以适应不同地层的工程需要。It can be seen from Examples 5 and 6, Comparative Examples 5 and 6, combined with the experimental evaluation in Table 3, that the scheme can ensure the aggressiveness and stability of the drill bit at the same time by aligning the radial tooth arrangement envelope 314 of the main cutting blade and the radial tooth arrangement envelope 324 of the same-track cutting blade or setting the offset distance d within the range of -0.2r≤d≤0.2r, and within this distance range, appropriate adjustments can be made to adapt to the engineering needs of different formations.

表4本发明实施例七至十一特征、尺寸和试验结果评价表Table 4 Characteristics, dimensions and test results of embodiments 7 to 11 of the present invention

表5 本发明实施例十二至十六特征、尺寸和试验结果评价表Table 5 Characteristics, dimensions and test results of embodiments 12 to 16 of the present invention

由实施例七至十六,结合表4、表5的试验评价可以看出,当同轨偏差值Pv、同轨切削刀翼32的径向布齿起始位置、偏置距离d均设置在适宜的范围之内,同轨切削刀翼32设置在主切削刀翼31的沿圆周的顺时针或者逆时针方向,或高比压刀翼组3的设置数量、设置方位,以及刀翼上的切削齿形态均可根据地层岩性以及工况的不同进行适应性调整,同时能够确保钻头具备较为出色的攻击性和稳定性。From Examples 7 to 16, combined with the test evaluation in Tables 4 and 5, it can be seen that when the on-track deviation value Pv, the radial tooth layout starting position of the on-track cutting blade 32, and the offset distance d are all set within an appropriate range, the on-track cutting blade 32 is set in the clockwise or counterclockwise direction along the circumference of the main cutting blade 31, or the number and orientation of the high-pressure blade group 3, as well as the cutting tooth shape on the blade can be adaptively adjusted according to the different lithology and working conditions, while ensuring that the drill bit has better aggressiveness and stability.

值得注意的是,上述部分实施例中,同一只钻头上的高比压刀翼组3中,组内刀翼结构形式相同,这是因为实施例中介绍具有代表性的特征,若对不同的高比压刀翼组3中的刀翼结构形式进行细微调整导致不同组内的刀翼结构形式不同,即使其使用效果不如上述代表性实施例的有益效果,但仍然属于本发明的保护范围内。如将实施例十二的高比压刀翼组3内刀翼结构(按顺时针排序)更改为两组“主切削刀翼31+同轨切削刀翼32”和一组“同轨切削刀翼32+主切削刀翼31”,如此一来即使调整后方案的有益效果不如实施例十二的有益效果明显,但仍是本发明的保护范围。It is worth noting that in some of the above embodiments, in the high pressure blade group 3 on the same drill bit, the blade structures in the group are the same. This is because the embodiments introduce representative features. If the blade structures in different high pressure blade groups 3 are slightly adjusted to result in different blade structures in different groups, even if the use effect is not as good as the beneficial effects of the above representative embodiments, it still falls within the scope of protection of the present invention. For example, the blade structures in the high pressure blade group 3 of the embodiment 12 (arranged clockwise) are changed to two groups of "main cutting blade 31 + same track cutting blade 32" and one group of "same track cutting blade 32 + main cutting blade 31". In this way, even if the beneficial effects of the adjusted scheme are not as obvious as those of the embodiment 12, it still falls within the scope of protection of the present invention.

以上所述实施例的各技术特征可以进行任意的组合,为使描述简洁,未对上述实施例中的各个技术特征所有可能的组合都进行描述,然而,只要这些技术特征的组合不存在矛盾,都应当认为是本说明书记载的范围。The technical features of the above-described embodiments may be arbitrarily combined. To make the description concise, not all possible combinations of the technical features in the above-described embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

以上所述实施例仅表达了本发明的几种实施方式,其描述较为具体和详细,但并不能因此而理解为对发明专利范围的限制。应当指出的是,对于本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变形和改进,这些都属于本发明的保护范围。因此,本发明专利的保护范围应以所附权利要求为准。The above-mentioned embodiments only express several implementation methods of the present invention, and the descriptions thereof are relatively specific and detailed, but they cannot be understood as limiting the scope of the invention patent. It should be pointed out that, for ordinary technicians in this field, several variations and improvements can be made without departing from the concept of the present invention, and these all belong to the protection scope of the present invention. Therefore, the protection scope of the patent of the present invention shall be subject to the attached claims.

Claims (9)

1.一种高比压PDC钻头,包括接头和钻头体,所述接头与钻头体的一端固定连接,其特征在于:所述钻头体的另一端沿圆周方向分布至少两组高比压刀翼组,所述高比压刀翼组包括一个主切削刀翼以及至少一个同轨切削刀翼,且同轨切削刀翼上安装的同轨切削齿径向位置与同组的主切削刀翼上安装的主切削齿径向位置偏差Pv范围为-0.5r至0.5r,其中r为主切削齿的半径;1. A high specific pressure PDC drill bit, comprising a joint and a drill bit body, wherein the joint is fixedly connected to one end of the drill bit body, and characterized in that: at least two groups of high specific pressure blade groups are distributed along the circumferential direction at the other end of the drill bit body, wherein the high specific pressure blade groups include a main cutting blade and at least one co-track cutting blade, and the radial position deviation Pv of the co-track cutting teeth installed on the co-track cutting blade and the radial position deviation Pv of the main cutting teeth installed on the main cutting blade of the same group is in the range of -0.5r to 0.5r, wherein r is the radius of the main cutting teeth; 所述主切削刀翼上安装的主切削齿数量满足其中N表示主切削刀翼数量,ni为第i号主切削刀翼上主切削齿的数量,r为主切削齿的半径,R为钻头的半径。The number of main cutting teeth installed on the main cutting blade meets and Where N represents the number of main cutting blades, ni is the number of main cutting teeth on the i-th main cutting blade, r is the radius of the main cutting teeth, and R is the radius of the drill bit. 2.根据权利要求1所述的一种高比压PDC钻头,其特征在于:所述高比压刀翼组中,同轨切削刀翼设置在主切削刀翼的沿圆周的顺时针或者逆时针方向。2. A high specific pressure PDC drill bit according to claim 1, characterized in that: in the high specific pressure blade group, the same track cutting blade is arranged in the clockwise or counterclockwise direction along the circumference of the main cutting blade. 3.根据权利要求1所述的一种高比压PDC钻头,其特征在于:所述主切削刀翼和同轨切削刀翼的布齿包络线重合或者偏置,偏置距离d满足:-0.2r≤d≤0.2r。3. A high specific pressure PDC drill bit according to claim 1, characterized in that: the tooth arrangement envelopes of the main cutting blade and the same track cutting blade coincide or are offset, and the offset distance d satisfies: -0.2r≤d≤0.2r. 4.根据权利要求1所述的一种高比压PDC钻头,其特征在于:所述同轨切削刀翼上的切削齿布置在钻头的径向外围部分。4. A high specific pressure PDC drill bit according to claim 1, characterized in that the cutting teeth on the same track cutting blade are arranged on the radial peripheral part of the drill bit. 5.根据权利要求4所述的一种高比压PDC钻头,其特征在于:所述同轨切削刀翼的径向布齿起始位置在0.25R-0.8R的范围之内,R为钻头的半径。5. A high specific pressure PDC drill bit according to claim 4, characterized in that the radial tooth arrangement starting position of the same track cutting blade is within the range of 0.25R-0.8R, where R is the radius of the drill bit. 6.根据权利要求1所述的一种高比压PDC钻头,其特征在于:所述主切削刀翼上的主切削齿为宽刃齿。6. A high specific pressure PDC drill bit according to claim 1, characterized in that the main cutting teeth on the main cutting blades are wide-edge teeth. 7.根据权利要求1所述的一种高比压PDC钻头,其特征在于:所述同轨切削刀翼上的同轨切削齿为非平面齿。7. A high specific pressure PDC drill bit according to claim 1, characterized in that the on-track cutting teeth on the on-track cutting blades are non-planar teeth. 8.根据权利要求1所述的一种高比压PDC钻头,其特征在于:所述主切削刀翼上布置双排或多排切削齿,和/或所述同轨切削刀翼上布置双排或多排切削齿。8. A high specific pressure PDC drill bit according to claim 1, characterized in that: the main cutting blade is arranged with double or multiple rows of cutting teeth, and/or the same track cutting blade is arranged with double or multiple rows of cutting teeth. 9.根据权利要求1所述的一种高比压PDC钻头,其特征在于:同一个钻头上的不同高比压刀翼组的刀翼数量不相同。9. A high specific pressure PDC drill bit according to claim 1, characterized in that the number of blades in different high specific pressure blade groups on the same drill bit is different.
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