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CN101666326B - Combined impeller - Google Patents

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Publication number
CN101666326B
CN101666326B CN200810176332XA CN200810176332A CN101666326B CN 101666326 B CN101666326 B CN 101666326B CN 200810176332X A CN200810176332X A CN 200810176332XA CN 200810176332 A CN200810176332 A CN 200810176332A CN 101666326 B CN101666326 B CN 101666326B
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blade
ring body
impeller
combination type
ring
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CN101666326A (en
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杨圣安
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Abstract

The invention discloses a combined impeller, which is characterized in that at least one impeller is assembled on an annular seat body; the annular seat body is provided with a flow guide surface, at least one group of annular hole groups is also arranged on the annular seat body, each annular hole group comprises a plurality of concave clamping grooves and a concave annular hole, and each clamping groove is communicated with the annular hole and the flow guide surface; the impeller is provided with a ring body which is embedded in a ring body hole of the ring-shaped base body, a plurality of blades are surrounded around the ring body, a reinforcing sheet for connecting the ring body and the blades is arranged between the inner edge of each blade and the periphery of the ring body, the reinforcing sheet is correspondingly embedded in the clamping groove, the inner edges of the blades are the same as and matched with the flow guide surface in shape, and an interval formed between two adjacent blades and the ring-shaped base body is an air duct; the design can eliminate the weak area formed between the ring body and the blades, so that the impeller is not easy to deform and the precise positioning combination between the impeller and the ring-shaped seat body is facilitated.

Description

组合式叶轮Combined impeller

技术领域technical field

本发明涉及一种组合式叶轮,特别是涉及一种利用组合方式克服模具脱模的干涉,并增加叶轮构件强度、防止变形、进而精确定位提升产品质量的组合式叶轮。The invention relates to a combined impeller, in particular to a combined impeller which overcomes the interference of mold release by using a combined method, increases the strength of the impeller component, prevents deformation, and precisely positions to improve product quality.

背景技术Background technique

现有的散热风扇请参考中国专利号ZL01268180.6“组合式散热风扇”(请结合参考图11),该组合式散热风扇4包含一下风扇体41及一上风扇体42,该下风扇体41具有一顶面突出成锥状的本体411,该本体411顶面中央突设有套轴412,该本体411外周突伸有多数个下叶片413,该本体411顶面由该套轴412周边向外延伸有与该下叶片413对应数量的卡掣槽414,该卡掣槽414外端口与该下叶片413对齐;该上风扇体42具有一扁平套环421,该套环421中央设有套孔422套固于该下风扇体41的套轴412,该套环421周边延伸有与该下叶片413对应数量的上叶片423,该上叶片423底缘恰与该下叶片413的顶缘呈续接状,该上叶片423根部设有卡掣条424,该卡掣条424置入该下风扇体41的卡掣槽414固定。Please refer to Chinese Patent No. ZL01268180.6 "Combined Cooling Fan" for existing cooling fans (please refer to Figure 11). The combined cooling fan 4 includes a lower fan body 41 and an upper fan body 42. It has a body 411 whose top surface protrudes into a cone shape. A sleeve shaft 412 protrudes from the center of the top surface of the body 411. A plurality of lower blades 413 protrude from the outer periphery of the body 411. The top surface of the body 411 extends from the periphery of the sleeve shaft 412 to There are a number of locking slots 414 corresponding to the lower blades 413 extending outward, and the outer ports of the locking slots 414 are aligned with the lower blades 413; the upper fan body 42 has a flat collar 421, and the center of the collar 421 is provided with a sleeve The hole 422 is sleeved on the sleeve shaft 412 of the lower fan body 41, and the periphery of the collar 421 is extended with upper blades 423 corresponding to the number of the lower blades 413. In a continuous shape, the root of the upper blade 423 is provided with a locking bar 424 , and the locking bar 424 is inserted into the locking groove 414 of the lower fan body 41 to be fixed.

然而,该种组合式散热风扇4,因上叶片423有多出对应该导流面415区间长度,而使该上叶片423因长度过长而强度不足,此外该组合式散热风扇4虽具卡掣条424,但是因该卡掣条424是对应锥状本体411的锥度及上叶片423内缘的弧度而设,使得该上叶片423的内缘结构呈中间高往外周渐低,并因此使上叶片423内缘与套环421间产生脆弱区间W,而容易变形,同时也影响上风扇体42与下风扇体41间的精确定位及牢固情形。However, this kind of combined heat dissipation fan 4, because the upper blade 423 has an excess length corresponding to the section length of the guide surface 415, the strength of the upper blade 423 is too long because of the lack of strength. However, because the locking bar 424 is set corresponding to the taper of the conical body 411 and the radian of the inner edge of the upper blade 423, the inner edge structure of the upper blade 423 is gradually lower from the middle height to the outer periphery, and therefore makes A fragile area W is formed between the inner edge of the upper blade 423 and the collar 421 , which is easily deformed, and also affects the precise positioning and firmness of the upper fan body 42 and the lower fan body 41 .

另外,请参考图12,其为一种离心作用的散热风扇6,该散热风扇6包含有一斜面体61及一上叶轮62,其中该斜面体61设有呈突出的锥状的导流面611,该导流面611的中央设圆平面612,该上叶轮62具对应该圆平面612的环体621,该环体621的外周缘设置数片上叶片622,该数片上叶片622具对应导流面611形状的内缘6221。In addition, please refer to FIG. 12, which is a centrifugal cooling fan 6, which includes a sloped body 61 and an upper impeller 62, wherein the sloped body 61 is provided with a protruding conical guide surface 611 The center of the guide surface 611 is provided with a circular plane 612, and the upper impeller 62 has a ring body 621 corresponding to the circular plane 612, and several upper blades 622 are arranged on the outer periphery of the ring body 621, and the upper blades 622 of the several blades have corresponding guides. Inner edge 6221 of face 611 shape.

但是,此一散热风扇的设计虽具离心作用可增加风压,但是该上叶片622的内缘为对应该导流面而设,使得该上叶片622的内缘结构呈中间高往外周渐低,致使上叶片622内缘与环体621间产生脆弱区间W,并且上叶片622与环体621仅以小区域相互连接,以致强度不足,且容易变形,又难以作精确及牢固的定位。However, although the design of this cooling fan has a centrifugal effect to increase the wind pressure, the inner edge of the upper blade 622 is designed to correspond to the guide surface, so that the inner edge structure of the upper blade 622 is gradually lower from the middle to the outer periphery. , resulting in a fragile section W between the inner edge of the upper blade 622 and the ring body 621, and the upper blade 622 and the ring body 621 are only connected to each other in a small area, so that the strength is insufficient, and it is easy to deform, and it is difficult to make accurate and firm positioning.

因此,如何能在可增加散热效能的前提下,设计出一种能够容易且精确制造以节省成本的散热风扇,即为本技术领域要克服解决的重要课题。Therefore, how to design a heat dissipation fan that can be easily and accurately manufactured to save cost on the premise of increasing heat dissipation performance is an important issue to be solved in the technical field.

发明内容Contents of the invention

本发明的目的在于提供一种组合式叶轮结构,尤其是一种能克服上述现有的组合式散热风扇的缺点,增加制造的叶轮、环形座体等构件强度且不易变形,进而能容易并精确的定位及组合的组合式叶轮。The purpose of the present invention is to provide a combined impeller structure, especially one that can overcome the shortcomings of the above-mentioned existing combined cooling fan, increase the strength of the components such as the manufactured impeller and the annular seat body and are not easily deformed, and then can be easily and accurately The positioning and combination of the combined impeller.

为了实现上述目的,本发明提供了一种组合式叶轮,其在一环形座体组设至少一个的叶轮;其中,该环形座体上设有至少一组的凹陷环体孔组,该凹陷环体孔组包括多数个凹设的卡槽及一凹设的环体孔,且各卡槽连通该环体孔及该导流面;该叶轮具有环体嵌设在环形座体的环体孔中,该环体周围环绕数片叶片,该叶片的内缘与环体外周之间设置有连接该环体与该叶片的补强片,该补强片对应嵌设于该卡槽中,又该叶片的内缘与上述的导流面形状相同且配合,并令相邻的两叶片间及环形座体所形成的区间为风道。In order to achieve the above object, the present invention provides a combined impeller, which is provided with at least one impeller on an annular seat; wherein, the annular seat is provided with at least one group of recessed ring hole groups, and the recessed ring The body hole group includes a plurality of recessed card slots and a recessed ring body hole, and each card slot communicates with the ring body hole and the flow guide surface; the impeller has a ring body hole embedded in the annular seat Among them, the ring body is surrounded by several blades, and a reinforcement piece connecting the ring body and the blade is provided between the inner edge of the blade and the outer periphery of the ring body, and the reinforcement piece is correspondingly embedded in the card slot, and The shape of the inner edge of the vane is the same as that of the above-mentioned guide surface and cooperates, and the section formed between two adjacent vanes and the annular seat is an air duct.

本发明的组合式叶轮进一步使该环形座体的轮毂的外周环绕设置下叶片。且该环形座体的叶片与叶轮的叶片对接形成完整的叶片。或是进一步使该环形座体的叶片的外侧端向上设置突出段,使该环形座体的叶片的内侧相对形成凹陷区,该凹陷区为供叶轮的叶片与之对接形成完整的叶片。又或是进一步使该环形座体的叶片位处在该叶轮的二叶片间所形成的风道后缘处,使该环形座体的叶片成为一增压叶片。In the combined impeller of the present invention, the outer circumference of the hub of the annular base body is further provided with lower blades. And the blades of the annular base body are docked with the blades of the impeller to form a complete blade. Or further, the outer end of the blade of the annular seat body is provided with a protruding section upward, so that the inner side of the blade of the annular seat body is opposite to form a recessed area, and the recessed area is for the blade of the impeller to dock with it to form a complete blade. Or further make the blade of the annular base body be located at the trailing edge of the air duct formed between the two blades of the impeller, so that the blade of the annular base body becomes a booster blade.

本发明的组合式叶轮再进一步使该叶轮的环体顶面低于叶片的顶缘的最高处,且该叶轮的环体的顶面与该叶片的顶缘及该环形座体的导流面依流场设计。In the combined impeller of the present invention, the top surface of the ring body of the impeller is lower than the highest point of the top edge of the blade, and the top surface of the ring body of the impeller is connected to the top edge of the blade and the guide surface of the annular seat body. Designed according to the flow field.

本发明还提供了一种组合式叶轮,包含:The present invention also provides a combined impeller, comprising:

一斜面体,其具有导流面及至少一组环体孔组,该环体孔组包括多数个凹设的卡槽及一凹设的环体孔,该环体孔组的各卡槽连通环体孔及导流面;An inclined plane, which has a diversion surface and at least one ring body hole group, the ring body hole group includes a plurality of recessed card slots and a recessed ring body hole, each card slot of the ring body hole group communicates Ring body hole and diversion surface;

至少一个叶轮,其具有设于斜面体的环体孔中的环体,另有数片叶片环设于该环体的周缘处,且各叶片与上述的环体孔组的卡槽对应,该叶片的内缘与该环体的外周间设置一连接该环体与该叶片的补强片,该补强片对应嵌设于上述的环体孔组的卡槽中,又该叶片的底缘与上述的导流面形状相同且配合。At least one impeller, which has a ring body arranged in the ring body hole of the inclined plane body, and several blades are arranged around the periphery of the ring body, and each blade corresponds to the slot of the above-mentioned ring body hole group, the blades A reinforcement sheet connecting the ring body and the blade is provided between the inner edge of the ring body and the outer circumference of the ring body, and the reinforcement sheet is correspondingly embedded in the slot of the above-mentioned ring body hole group, and the bottom edge of the blade and the The above-mentioned guide surfaces have the same shape and fit together.

该结构设计的优点有:可借由补强片消除环体与叶片间所形成的脆弱区间,且更有利于叶轮与环形座体间的精确定位及牢固组设。The advantages of this structural design are: the weak zone formed between the ring body and the blade can be eliminated by the reinforcing piece, and it is more conducive to the precise positioning and firm assembly between the impeller and the ring seat.

附图说明Description of drawings

图1为本发明第一较佳实施例组合式叶轮立体分解图;Fig. 1 is the three-dimensional exploded view of the combined impeller of the first preferred embodiment of the present invention;

图2为本发明第一较佳实施例组合式叶轮的组合图;Fig. 2 is the assembly diagram of the combined impeller of the first preferred embodiment of the present invention;

图3为本发明第二较佳实施例组合式叶轮的立体分解图;Fig. 3 is a three-dimensional exploded view of a combined impeller according to a second preferred embodiment of the present invention;

图4为本发明第三较佳实施例组合式叶轮的侧视分解图;Fig. 4 is a side exploded view of the combined impeller of the third preferred embodiment of the present invention;

图5为本发明第四较佳实施例组合式叶轮的侧视分解图;Fig. 5 is a side exploded view of the combined impeller of the fourth preferred embodiment of the present invention;

图6为本发明第五较佳实施例组合式叶轮的立体组合图;Fig. 6 is a three-dimensional assembled view of the combined impeller of the fifth preferred embodiment of the present invention;

图7为本发明第六较佳实施例组合式叶轮的立体分解图;Fig. 7 is a three-dimensional exploded view of a combined impeller according to a sixth preferred embodiment of the present invention;

图8为本发明第六较佳实施例组合式叶轮的侧视组合图;Fig. 8 is a side view combined view of the combined impeller of the sixth preferred embodiment of the present invention;

图9为本发明第七较佳实施例组合式叶轮的立体分解图;Fig. 9 is a three-dimensional exploded view of the combined impeller of the seventh preferred embodiment of the present invention;

图10为本发明第八较佳实施例组合式叶轮的侧视分解图;Fig. 10 is a side exploded view of the combined impeller according to the eighth preferred embodiment of the present invention;

图11为中国专利号ZL01268180.6组合式散热风扇立体分解图;Figure 11 is a three-dimensional exploded view of the Chinese patent number ZL01268180.6 combined cooling fan;

图12为传统组合式散热风扇立体分解图。Fig. 12 is a three-dimensional exploded view of a traditional combined cooling fan.

主要元件标号说明:Explanation of main component labels:

本发明:this invention:

1    组合式叶轮                11   环形座体1 Combined impeller 11 Annular seat

111  轮毂                      112  导流面111 wheel hub 112 guide surface

113  环体孔组                  1131 卡槽113 Ring body hole group 1131 Card slot

1132 环体孔                    114  增压叶片1132 ring body hole 114 booster vane

115  叶片                      1151 突出段115 Blade 1151 Protruding section

1152 凹陷区                    12   叶轮1152 concave area 12 impeller

121  环体                      1211 外周121 Ring body 1211 Periphery

1212 顶面                      122  叶片1212 top surface 122 blade

1221 内缘                      1222 顶缘1221 inner edge 1222 top edge

123  补强片                    3    组合式叶轮123 Reinforcing piece 3 3 Combined impeller

31   斜面体                    311  导流面31 Inclined body 311 Diversion surface

312  环体孔组                  3121 卡槽312 Ring body hole group 3121 Card slot

3122 环体孔                    32   叶轮3122 ring body hole 32 impeller

321  环体                      3211 外周321 Ring body 3211 Periphery

322  叶片                      3221 内缘322 Blade 3221 Inner edge

323  补强片                    θ    夹角323 Reinforcing sheet θ included angle

H    水平线                    4    组合式叶轮H Horizontal line 4 Combined impeller

41   环形座体                  411  轮毂41 Ring seat body 411 Wheel hub

412  导流面                    413  环体孔组412 diversion surface 413 ring body hole group

4131 卡槽                      4132 环体孔4131 card slot 4132 ring body hole

42   叶轮                      421  环体42 impeller 421 ring body

4211  外周            422  叶片4211 Perimeter 422 Blade

4221  内缘            423  补强片4221 Inner edge 423 Reinforcement sheet

现有技术:current technology:

4   散热风扇           41   下风扇体4 Cooling fan 41 Lower fan body

411 本体               412  套轴411 Body 412 Shaft

413 下叶片             414  卡掣槽413 Lower blade 414 Locking groove

42  上风扇体           421  套环42 Upper fan body 421 Collar

422 套孔               423  上叶片422 Set hole 423 Upper blade

424 卡掣条             415  导流面424 Buckle bar 415 Diversion surface

W   脆弱区间           5    散热风扇W Fragile Zone 5 Cooling Fan

51  轴流向风扇         511  圆形凸块51 Axial flow fan 511 Round bump

512 扇叶               52   离心向风扇512 fan blade 52 centrifugal fan

523 扇叶               522  筒体523 Blade 522 Cylinder

521 圆顶体             6    散热风扇521 dome body 6 cooling fan

61  斜面体             611  导流面61 Inclined body 611 Diversion surface

612 圆平面             62   上叶轮612 Round plane 62 Upper impeller

621 环体               622  上叶片621 ring body 622 upper blade

6221内缘6221 inner edge

具体实施方式Detailed ways

请配合参考图1、图2所示,其为本发明组合式叶轮的第一较佳实施例;该组合式叶轮1包括:一环形座体11及一叶轮12;其中:Please refer to Fig. 1 and Fig. 2, which is the first preferred embodiment of the combined impeller of the present invention; the combined impeller 1 includes: an annular seat 11 and an impeller 12; wherein:

该环形座体11具有轮毂111,该轮毂111上设弧凸状的导流面112,并于该环形座体11上设置一环体孔组113,该环体孔组113包括多数个凹设的卡槽1131及一凹设的环体孔1132,且各卡槽1131连通该环体孔1132及该导流面112;另,该环形座体11可进一步在周缘处设数个增压叶片114(请参考图6),各增压叶片114位在叶轮12两两相邻的叶片122间的风道后缘中;The annular seat body 11 has a hub 111, the hub 111 is provided with an arc-shaped diversion surface 112, and a ring body hole group 113 is arranged on the annular seat body 11, and the ring body hole group 113 includes a plurality of concave holes. The card groove 1131 and a recessed ring body hole 1132, and each card groove 1131 communicates with the ring body hole 1132 and the flow guide surface 112; in addition, the annular seat 11 can further be provided with several booster blades at the periphery 114 (please refer to Fig. 6), each booster vane 114 is positioned in the trailing edge of the air duct between two adjacent blades 122 of the impeller 12;

该叶轮12中间具有一环体121嵌设在该环形座体11的环体孔1132处,数个叶片122环设在该环体121的外周1211,并与环形座体11的各卡槽1131对应,该叶片122的内缘1221与该环体121的外周1211之间形成一区间,在此区间内设置一补强片123,并使该补强片123连接于该环体121与叶片122之间,且对应嵌设于环形座体11的卡槽1131中,使该环形座体11、叶轮12对应组装定位,又该叶片122的内缘1221对应环形座体11的导流面112形状并相配合,并使相邻的两叶片122间及环形座体11所形成的区间为风道。There is a ring body 121 embedded in the ring body hole 1132 of the ring body 11 in the middle of the impeller 12, and several blades 122 are arranged on the outer periphery 1211 of the ring body 121, and are connected with the slots 1131 of the ring body 11. Correspondingly, a section is formed between the inner edge 1221 of the blade 122 and the outer periphery 1211 of the ring body 121, and a reinforcing piece 123 is arranged in this section, and the reinforcing piece 123 is connected to the ring body 121 and the blade 122 between, and correspondingly embedded in the slot 1131 of the annular seat 11, so that the annular seat 11 and the impeller 12 are assembled and positioned correspondingly, and the inner edge 1221 of the blade 122 corresponds to the shape of the guide surface 112 of the annular seat 11 And cooperate, and make the interval formed between two adjacent blades 122 and the annular base 11 be the air duct.

请参考图3,为本发明组合式叶轮的第二较佳实施例;该组合式叶轮1与其一较佳实施例的组合式叶轮1的差异是在:该环形座体11具有环绕该轮毂111的数片叶片115,该叶片115设置的个数对应该环形座体11的卡槽1131的数量;且该叶片115与叶轮12的叶片122对接形成完整的叶片。Please refer to FIG. 3 , which is a second preferred embodiment of the combined impeller of the present invention; the difference between the combined impeller 1 and the combined impeller 1 of a preferred embodiment is that the annular seat 11 has a hub 111 around it. There are several blades 115, the number of the blades 115 corresponds to the number of the slots 1131 of the annular seat 11; and the blades 115 are docked with the blades 122 of the impeller 12 to form a complete blade.

请参考图4,为本发明组合式叶轮的第三较佳实施例;该组合式叶轮1与第二较佳实施例的组合式叶轮1的差异是在:该环形座体11的叶片115接近外侧的一端向外并向上延伸形成延伸突出段1151,且在相对该延伸突出段1151的叶片115的内侧上缘处形成一凹陷区1152,此凹陷区1152供叶轮12的叶片122对应容置配合,使该分列上、下方位的叶片122、115对接后形成完整的叶片。Please refer to Fig. 4, which is the third preferred embodiment of the combined impeller of the present invention; the difference between the combined impeller 1 and the combined impeller 1 of the second preferred embodiment is that the blades 115 of the annular seat 11 are close to One end of the outer side extends outwards and upwards to form an extended protruding section 1151, and a recessed area 1152 is formed at the inner upper edge of the blade 115 opposite to the extended protruding section 1151. , the blades 122, 115 at the upper and lower positions of the arrangement are docked to form a complete blade.

请配合参考图5所示,其为本发明的第四较佳实施例,该第四较佳实施例的组合式叶轮1与第二较佳实施例的差异主要是在:该叶轮12的环体121顶面1212低于叶片122的顶缘1222的最高处,且该叶轮12的环体121的顶面1212与叶片122的顶缘1222及环形座体11的导流面112依流场设计。Please refer to Fig. 5, which is the fourth preferred embodiment of the present invention. The difference between the combined impeller 1 of the fourth preferred embodiment and the second preferred embodiment is mainly: the ring of the impeller 12 The top surface 1212 of the body 121 is lower than the highest point of the top edge 1222 of the blade 122, and the top surface 1212 of the ring body 121 of the impeller 12, the top edge 1222 of the blade 122 and the guide surface 112 of the annular seat 11 are designed according to the flow field .

请配合参考图6所示,其为本发明的第五较佳实施例,其主要在环形座体11的相邻的叶片115间的风道后缘中设增压叶片114。Please refer to FIG. 6 , which is the fifth preferred embodiment of the present invention, which mainly provides booster blades 114 in the trailing edge of the air duct between adjacent blades 115 of the annular seat 11 .

再参考图7、图8,其为本发明的第六较佳实施例,该组合式叶轮3属于一种具离心作用的风扇,该组合式叶轮3包括一斜面体31及一叶轮32;其中:Referring to Fig. 7 and Fig. 8 again, it is the sixth preferred embodiment of the present invention, the combined impeller 3 belongs to a fan with centrifugal effect, and the combined impeller 3 includes a bevel 31 and an impeller 32; wherein :

该斜面体31设有呈凹弧状的导流面311,并在该斜面体31上设有一环体孔组312,该环体孔组312包括多数个凹设的卡槽3121及一凹设的环体孔3122,该环体孔组312的各卡槽3121连通环体孔3122及该导流面311;The slope body 31 is provided with a diversion surface 311 in a concave arc shape, and a ring body hole group 312 is provided on the slope body 31, and the ring body hole group 312 includes a plurality of recessed card slots 3121 and a recessed Ring body hole 3122, each slot 3121 of the ring body hole group 312 communicates with the ring body hole 3122 and the flow guide surface 311;

该叶轮32中间具有一环体321,该环体321具有外周3211,在该外周3211环绕设有数片叶片322,该叶片322的内缘3221对应斜面体31的导流面311形状,使该上叶片322的内缘3221呈中间高往外渐低的造型,并因此与该环体321的外周3211之间形成一区间,于此区间内设置一补强片323,并使该补强片323连接于该环体321与上叶片322之间,该补强片323对应嵌设于斜面体31的卡槽3121中,且该环体321设于斜面体31的环体孔3122中,以将该叶轮32、斜面体31对应组装定位,又该叶片322的内缘3221对应斜面体31的导流面311形状并相配合,并令相邻的两叶片322间及斜面体31所形成的区间为风道。There is a ring body 321 in the middle of the impeller 32, and the ring body 321 has an outer circumference 3211, and several blades 322 are arranged around the outer circumference 3211. The inner edge 3221 of the blade 322 is in the shape of the middle height gradually lowering outward, and therefore forms a section with the outer periphery 3211 of the ring body 321, and a reinforcing piece 323 is arranged in this section, and the reinforcing piece 323 is connected. Between the ring body 321 and the upper blade 322, the reinforcing piece 323 is correspondingly embedded in the slot 3121 of the inclined plane body 31, and the ring body 321 is arranged in the ring body hole 3122 of the inclined plane body 31, so that the The impeller 32 and the inclined plane body 31 are correspondingly assembled and positioned, and the inner edge 3221 of the blade 322 corresponds to the shape of the guide surface 311 of the inclined plane body 31 and matches, and the interval formed between the adjacent two blades 322 and the inclined plane body 31 is air duct.

在该实施例中,该补强片323的底缘可进一步设计成与自环体321底缘延伸而出的水平线H间具一夹角θ(请再参考图8),以增加该补强片323补强区间的结构强度。In this embodiment, the bottom edge of the reinforcement piece 323 can be further designed to have an angle θ with the horizontal line H extending from the bottom edge of the ring body 321 (please refer to FIG. 8 again), so as to increase the reinforcement The sheet 323 reinforces the structural strength of the section.

本发明的组合式叶轮4的第七较佳实施例,包括:一环形座体41、至少一个叶轮42;其中,为利于说明本发明在此是以二个上、下设置的叶轮42与一环形座体41组成该组合式叶轮4进行说明,并请配合参考图9所示。The seventh preferred embodiment of the combined impeller 4 of the present invention comprises: an annular base body 41, at least one impeller 42; The combined impeller 4 composed of the annular seat body 41 will be explained, and please refer to FIG. 9 for reference.

该环形座体41具有轮毂411,该轮毂411上设锥状的导流面412及对应叶轮42个数设置的环体孔组413,该环体孔组413包括多数个凹设的卡槽4131及一凹设的环体孔4132,该环体孔组413的各卡槽4131连通该环体孔4132及该导流面412;The annular seat body 41 has a hub 411, on which a conical guide surface 412 and a ring body hole group 413 corresponding to the number of impellers 42 are provided, and the ring body hole group 413 includes a plurality of recessed clamping grooves 4131 And a recessed ring body hole 4132, each slot 4131 of the ring body hole group 413 communicates with the ring body hole 4132 and the flow guide surface 412;

该叶轮42中间具有一环体421,数个叶片422环设在该环体421的外周4211,并与环形座体41的各卡槽4131对应,该叶片422的内缘4221与该环体421的外周4211之间形成一区间,于此区间内设置一补强片423,并使该补强片423连接于该环体421与叶片422之间,又该环体421设于环形座体41的环体孔4132中,该叶片422的内缘4221对应环形座体41的导流面412形状并相配合,该补强片423对应嵌设于环形座体41的卡槽4131中,以将该叶轮42对应组装定位于该环形座体41上,并使相邻的两叶片422间及环形座体41所形成的区间为风道。There is a ring body 421 in the middle of the impeller 42, and several blades 422 are arranged on the outer periphery 4211 of the ring body 421, and correspond to the slots 4131 of the annular base body 41, and the inner edge 4221 of the blade 422 is in contact with the ring body 421. A section is formed between the outer circumferences 4211 of the ring body, and a reinforcing piece 423 is arranged in this section, and the reinforcing piece 423 is connected between the ring body 421 and the blade 422, and the ring body 421 is arranged on the annular seat body 41 In the ring body hole 4132, the inner edge 4221 of the vane 422 corresponds to the shape of the guide surface 412 of the annular seat 41 and matches, and the reinforcing piece 423 is correspondingly embedded in the slot 4131 of the annular seat 41, so as to The impeller 42 is correspondingly assembled and positioned on the annular seat 41 , and the section formed between two adjacent blades 422 and the annular seat 41 is an air duct.

本实施例的组合式叶轮4可进一步使该上、下设置的二叶轮42的叶片422对接形成完整的叶片。或是进一步使该位处下方的叶轮42的叶片422如图4的环形座体11的叶片115般,即在其外侧端向上设置突出段1151,使该叶片115的内侧相对形成凹陷区1152,供本实施例中位处上方的叶轮42的叶片422与对接形成完整的叶片。或进一步使该位处下方的叶轮42的叶片422位处在该上方叶轮42的二叶片422间所形成的风道后缘处,使该下方叶轮42的叶片422成为一增压叶片(请参考图10)。此外,该组合式叶轮4可再进一步使该上方的叶轮42的环体421顶面低于叶片422的顶缘的最高处,且该叶轮42的环体421的顶面与该叶片422的顶缘及该环形座体41的导流面412依流场设计。The combined impeller 4 of this embodiment can further make the blades 422 of the two upper and lower impellers 42 docked to form a complete blade. Or further make the vane 422 of the impeller 42 below the position as the vane 115 of the annular seat 11 of Fig. 4, that is, a protruding section 1151 is provided upwards at its outer end, so that the inner side of the vane 115 is relatively formed with a recessed area 1152, In this embodiment, the blade 422 of the upper impeller 42 is connected with the blade 422 to form a complete blade. Or further make the blade 422 of the impeller 42 located below be located at the trailing edge of the air duct formed between the two blades 422 of the upper impeller 42, so that the blade 422 of the lower impeller 42 becomes a booster blade (please refer to Figure 10). In addition, the combined impeller 4 can further make the top surface of the ring body 421 of the upper impeller 42 lower than the highest point of the top edge of the blade 422, and the top surface of the ring body 421 of the impeller 42 and the top surface of the blade 422 The edge and the guide surface 412 of the annular seat 41 are designed according to the flow field.

另外,本实施例的环形座体41可如图1所示的环形座体11形状,或如图7所示的锥体形状。In addition, the annular seat 41 of this embodiment can be in the shape of the annular seat 11 shown in FIG. 1 , or in the shape of a cone as shown in FIG. 7 .

经由上述结构特征的详细说明,可清楚看出本发明设计的特点在于:Through the detailed description of the above-mentioned structural features, it can be clearly seen that the characteristics of the design of the present invention are:

1.上叶轮的上叶片的内缘与环体外周之间以补强片连设,可增加上叶片的强度,并防止上叶轮在射出时及射出后变形。1. The inner edge of the upper blade of the upper impeller and the outer circumference of the ring are connected with a reinforcing sheet, which can increase the strength of the upper blade and prevent the deformation of the upper impeller during and after injection.

2.正因上叶轮不致变形,同时补强片及卡槽的搭配,也使上叶轮容易精确定位及组装于下叶轮之上,而利于旋转的平衡。2. Because the upper impeller will not be deformed, and the matching of the reinforcing plate and the card slot also makes it easy to accurately position and assemble the upper impeller on the lower impeller, which is conducive to the balance of rotation.

Claims (14)

1. a combination type blade wheel is characterized in that, described combination type blade wheel includes:
One annular base body, it has wheel hub, and this wheel hub is provided with guide face, and this annular base body also is provided with at least one group of ring body hole group, and this ring body hole group comprises the ring body hole that most the draw-in grooves and that are arranged with are arranged with, and each draw-in groove is communicated with this ring body hole and this guide face; And
At least one impeller, it has ring body, correspondence is embedded in this ring body hole, the peripheral ring winding number sheet blade corresponding of this ring body with this draw-in groove, one reinforcing chip that is connected this ring body and this blade is set between the inner edge of this blade and the periphery of this ring body, this reinforcing chip correspondence is embedded in this draw-in groove, the inner edge of this blade and the above-mentioned identical and cooperation of guide face shape, and between these two adjacent blades and the formed interval of annular base body is the air channel.
2. combination type blade wheel according to claim 1 is characterized in that the periphery of the wheel hub of this annular base body is provided with several pieces blades.
3. combination type blade wheel according to claim 2 is characterized in that, the blade of the wheel hub periphery of this annular base body is corresponding with the draw-in groove of ring body hole group, and docks formation one intact leaf with the blade of this impeller.
4. combination type blade wheel according to claim 3 is characterized in that, in the trailing edge in described air channel, this annular base body has additional the supercharging blade between its adjacent vanes.
5. combination type blade wheel according to claim 2, it is characterized in that, the blade of the wheel hub periphery of this annular base body is corresponding with the draw-in groove of ring body hole group, and this blade outwards also up extends to form the extension nose section near an end in the outside, and form a depressed area at the relative inboard upper limb place of this blade of this extension nose section, this depressed area makes the intact leaf of the blade-shaped one-tenth butt joint of this two upper and lower setting for the corresponding ccontaining cooperation of blade of this impeller.
6. combination type blade wheel according to claim 2 is characterized in that, this blade that is located at the wheel hub periphery is the supercharging blade, and is positioned at trailing edge place, formed air channel between two adjacent blades of this impeller.
7. combination type blade wheel according to claim 1 is characterized in that the ring body end face of this impeller is lower than the highest point of the apical margin of blade, and the guide face of the apical margin of the end face of the ring body of this impeller and this blade and this annular base body is according to flow Field Design.
8. combination type blade wheel according to claim 1 is characterized in that, the guide face below of this annular base body is established second ring body hole group again and established with second impeller sets of arranging in pairs or groups.
9. combination type blade wheel according to claim 8 is characterized in that, the blade of below impeller docks with the blade of the impeller of top and forms an intact leaf, and between two blades that impeller is adjacent below making and the formed interval of annular base body is the air channel.
10. combination type blade wheel according to claim 9 is characterized in that, in the trailing edge of formed air channel, the impeller of below is established the supercharging blade between its adjacent vanes between two adjacent blades of impeller up.
11. combination type blade wheel according to claim 8 is characterized in that, the blade of the impeller of this below is the supercharging blade, and is positioned at trailing edge place, formed air channel between the two adjacent blades of impeller of this top.
12. combination type blade wheel according to claim 8 is characterized in that, the ring body end face of this top impeller is lower than the highest point of the apical margin of its blade, and the guide face of the apical margin of the end face of the ring body of this top impeller and its blade and this annular base body is according to flow Field Design.
13. a combination type blade wheel is characterized in that, described combination type blade wheel comprises:
One clinohedral, it has guide face and at least one group of ring body hole group, and this ring body hole group comprises the ring body hole that most the draw-in grooves and that are arranged with are arranged with, each draw-in groove connected ring body opening and guide face of this ring body hole group;
At least one impeller, it has the ring body in the ring body hole of the clinohedral be located at, other has several pieces blade rings to be located at the peripheral region of this ring body, and each blade is corresponding with the draw-in groove of above-mentioned ring body hole group, one reinforcing chip that is connected this ring body and this blade is set between the inner edge of this blade and the periphery of this ring body, this reinforcing chip correspondence is embedded in the draw-in groove of above-mentioned ring body hole group, again the root edge of this blade and the above-mentioned identical and cooperation of guide face shape.
14. combination type blade wheel according to claim 13 is characterized in that, the root edge of this reinforcing chip and tool one angle between the horizontal line that the root edge of ring body extends.
CN200810176332XA 2008-09-04 2008-11-14 Combined impeller Expired - Fee Related CN101666326B (en)

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CN103386602B (en) * 2012-05-08 2017-04-12 珠海格力电器股份有限公司 Clothes dryer wind wheel shaft ring assembling device and assembling method
DE102015214854A1 (en) * 2015-08-04 2017-02-09 Bosch Mahle Turbo Systems Gmbh & Co. Kg Compressor wheel for an exhaust gas turbocharger
CN206419267U (en) * 2016-09-12 2017-08-18 东莞市卓奇电子科技有限公司 Centrifugal impeller guide vane and centrifugal impeller
CN109083866B (en) * 2018-09-20 2024-06-18 江门市桑尼光电科技有限公司 Ceiling fan
CN112360764B (en) * 2020-09-22 2021-07-13 东风汽车集团有限公司 Turbocharger, adjustment method, engine, and vehicle

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