CN114718718A - Swing groove drive reciprocating rotary bump rotary engine - Google Patents
Swing groove drive reciprocating rotary bump rotary engine Download PDFInfo
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- CN114718718A CN114718718A CN202210280776.8A CN202210280776A CN114718718A CN 114718718 A CN114718718 A CN 114718718A CN 202210280776 A CN202210280776 A CN 202210280776A CN 114718718 A CN114718718 A CN 114718718A
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- 230000005540 biological transmission Effects 0.000 claims description 14
- 238000001816 cooling Methods 0.000 claims 1
- 230000002596 correlated effect Effects 0.000 claims 1
- 239000007789 gas Substances 0.000 description 6
- 238000007789 sealing Methods 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000000112 cooling gas Substances 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/02—Methods of operating
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/04—Charge admission or combustion-gas discharge
- F02B53/08—Charging, e.g. by means of rotary-piston pump
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/10—Fuel supply; Introducing fuel to combustion space
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/14—Adaptations of engines for driving, or engine combinations with, other devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/02—Pistons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/08—Outer members for co-operation with rotary pistons; Casings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/16—Admission or exhaust passages in pistons or outer members
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Transmission Devices (AREA)
Abstract
一种摆槽传动往复旋转式凸块转子发动机;旋转缸体作往复旋转运动,经摆槽机构转化为单向旋转动力,机器运转时借助一级压缩气,实现自动进,排气,并可实现有限可变行程工作。本发明理论上其体积和重量仅相当于同功率传统发动机的四分之一即25%,有效输出扭矩为传统发动机的2倍以上。
A pendulum-groove drive reciprocating-rotating convex-rotor engine; the rotary cylinder body performs reciprocating rotational motion, and is converted into unidirectional rotational power through the pendulum-groove mechanism; Realize limited variable stroke work. In theory, the volume and weight of the present invention are only 25% of a quarter of that of a traditional engine of the same power, and the effective output torque is more than twice that of a traditional engine.
Description
本发明涉及一种摆槽传动往复旋转式凸块转子发动机,是本人近年来所申请的多项发动机发明专利的最终之大成。也是集本人40余年专注于发动机研究的最终成果。The present invention relates to a pendulum-groove drive reciprocating rotary bump rotary engine, which is the final culmination of a number of engine invention patents that I have applied for in recent years. It is also the final result of my more than 40 years of focus on engine research.
本发明的主要目的是提供一种即能更好的发挥出传统发动机的优势又能很好克服其弊端,体积小重量轻,使用寿命长,执转换效率高的发动机;为未来航空特别是私人航空领域及野外机器人提供理想的动力。The main purpose of the present invention is to provide an engine that can better exert the advantages of traditional engines and overcome its disadvantages, has small size, light weight, long service life and high conversion efficiency; Ideal power for aerospace and field robots.
在所附图中,以非限制性的举例形式说明本发明的一个In the accompanying drawings, one of the inventions is illustrated by way of non-limiting example
实施例:Example:
图1:为四腔室摆槽传动往复式凸块转子发动机局部剖视图Figure 1: A partial cross-sectional view of a four-chamber pendulum-slot drive reciprocating bump rotary engine
图2至图5:为A-A剖视图Figure 2 to Figure 5: A-A sectional view
其图2即A-A-1;图3即A-A-2;图4即A-A-3;图5即A-A-4;是凸块转子逆时针运转完一个工作行程,开始顺时针运转时各个工作腔室的变化状况以及进、排气口的相应关系的展示。Fig. 2 is A-A-1; Fig. 3 is A-A-2; Fig. 4 is A-A-3; Fig. 5 is A-A-4; it is the working chamber of each working chamber when the bump rotor runs counterclockwise after one working stroke and starts to run clockwise The change of the status and the display of the corresponding relationship between the intake and exhaust ports.
图6至图9:为B-B剖视图Figures 6 to 9: B-B sectional views
其图6即B-B-1;图7即B-B-2;图8即B-B-3;图9即B-B-4;是凸块转子逆时针运转完一个行程又开始顺时针运转时摆槽与偏心滚轴以及主传动齿轮在几个关键节点的相互位置关系和工作状态。Fig. 6 is B-B-1; Fig. 7 is B-B-2; Fig. 8 is B-B-3; Fig. 9 is B-B-4; it is the swing groove and eccentric roller when the bump rotor runs counterclockwise for one stroke and then starts to run clockwise. The mutual positional relationship and working state of the shaft and the main drive gear at several key nodes.
图中:In the picture:
1、蜗扇轴;2、蜗扇叶片;3、一级压缩气室;4、轴承; 5、密封圈;6、联结螺栓;7、气缸端盖;8、中隔板;9、转动缸体;10、蜗扇齿轮;11、摆槽;12、偏心滚轴;13、主传动齿轮;14、凸轮同步齿轮;15、高压油泵;16、油封; 17、动力输出轴;18、凸轮轴;19、油泵凸轮;20、油泵箱体;21、主轴承座;22、齿轮箱体;23、蜗扇轴轴承座;24、 IV工作腔;25、喷油嘴;26、火花塞;27、固定缸凸块;28、 I工作腔;29、固定缸体;30、排气孔;31、压缩气气道; 32、转动缸凸块;33、微刻痕;34、II工作腔;35、III工作腔;36、进气孔;1. Worm fan shaft; 2. Worm fan blade; 3. Primary compressed air chamber; 4. Bearing; 5. Sealing ring; 6. Connecting bolt; 7. Cylinder end cover; 8. Middle baffle; 9. Rotating cylinder body; 10, worm fan gear; 11, swing groove; 12, eccentric roller; 13, main drive gear; 14, cam synchro gear; 15, high pressure oil pump; 16, oil seal; 17, power take-off shaft; 18, camshaft ;19, oil pump cam; 20, oil pump box; 21, main bearing seat; 22, gear box body; 23, worm shaft bearing seat; 24, IV working chamber; 25, fuel injector; 26, spark plug; 27, Fixed cylinder bump; 28, I working chamber; 29, fixed cylinder body; 30, exhaust hole; 31, compressed air passage; 32, rotating cylinder bump; 33, micro-scoring; 34, II working chamber; 35 , III working chamber; 36, air inlet;
参阅附图1:本发明的固定缸体29使用联结螺栓6将齿轮箱体22通过中间隔板8联成一体。当旋转缸体逆时针运转时带动摆槽11摆动,并可直接输出摆动动力。摆槽摆动时通过固定在主传动齿轮13上的偏心滚轴12带动主传动齿轮13作单一方向的旋转并输出旋转动力,与此同时安装在动力输出轴17上的同步齿轮14带动凸轮轴18旋转;驱动高压油泵15工作,产生的高压油通过喷油嘴25向工作腔内定时喷射雾化油气。而凸轮轴18另一端则带动增速蜗扇齿轮10旋转;同时通过蜗扇轴1带动蜗扇叶片2高建旋转,实现一级增压气室3增压。Referring to FIG. 1 : the
参阅附图2:A-A-1。如图所示:转动缸体11及转动凸块32与固定缸体29及固定缸体凸块27之间形成I;II; III;IV四个工作腔;II;IV工作腔处于压缩终点时的状态,位于I、III工作腔的进气孔36和排气孔38完全打开,废气排出的状态,此时火花塞点火,燃烧混合气燃烧膨胀II、IV 工作腔作功,推动转动缸体顺时针旋转。See Figure 2: A-A-1. As shown in the figure: I; II; III; IV four working chambers are formed between the rotating cylinder 11 and the
参阅附图3:A-A-2。如图所示,此时进、排气孔完全关闭,I、III工作腔的喷油嘴喷出雾化油气并开始二级压缩。See Figure 3: A-A-2. As shown in the figure, the inlet and exhaust holes are completely closed at this time, and the fuel injectors of the I and III working chambers spray atomized oil and gas and start secondary compression.
参阅附图4:A-A-3。如图所示II、IV工作腔工作完毕进、排气孔完全打开,一级压缩空气通过进气孔将废气通过排气孔压出,同时对缸体内部进气冷却,与此同时I、III工作腔压缩完毕处于左止点位置火花塞26点火,I、III工作腔开始作功推动旋转缸开始逆时针旋转。如此进入下一个工作行程。See Figure 4: A-A-3. As shown in the figure, the inlet and exhaust holes of the working chambers II and IV are completely opened, and the first-stage compressed air presses the exhaust gas through the exhaust holes through the intake holes, and cools the intake air inside the cylinder at the same time. After the compression of the III working chamber is completed, the
参阅附图5:A-A-4。进、排气孔开始同时关闭,废气完全排出,一级压缩气少量从排气孔溢气,同时对缸体内壁起冷却气作用。See Figure 5: A-A-4. The inlet and exhaust holes begin to close at the same time, the exhaust gas is completely discharged, and a small amount of the first-stage compressed air escapes from the exhaust hole, and at the same time acts as a cooling gas for the inner wall of the cylinder.
综上所述:1、转动缸体凸块前后与固定缸体凸块间均形成工作腔,转动缸体顺时针旋转,逆时时针旋转各一个行程就可完成一个工作循环,极大节约了空间提高了运转效率,因此理论上来说同等功率的发动机,本发明的体积和质量只相当于传统发动机的四分之一及25%。2、自动实现各工作腔的进、排气,无需单独的配气系统极大简化了结构,提高了工作可靠性;3、由于本发明旋转缸体与固定缸体覆盖面大且受力及受热均匀,变形小,因此,基于现代流体动压润滑理论在旋转件和静止件的特定部位刻有特别的浅槽33,借助流经压缩气道31及进气孔的压缩空气辅助;发动机在运转时在密封面间形成乱流及气膜,实现非接触式动密封,实现无磨损密封运行。To sum up: 1. A working cavity is formed between the front and rear of the rotating cylinder block and the fixed cylinder block. The rotating cylinder rotates clockwise and rotates counterclockwise to complete a working cycle, which greatly saves money. The space improves the operation efficiency, so theoretically speaking, the volume and mass of the present invention are only 1/4 and 25% of that of the traditional engine for an engine of the same power. 2. The intake and exhaust of each working chamber are automatically realized, without the need for a separate gas distribution system, which greatly simplifies the structure and improves the working reliability; 3. Because the rotating cylinder body and the fixed cylinder body of the present invention have large coverage and are subjected to force and heat Uniform and small deformation, therefore, based on the modern fluid dynamic pressure lubrication theory, special
参阅附图6:B-B-1。如图所示,此时摆槽11处于上止点位置,当转动缸体工作时逆时针旋转,带动摆槽逆时针摆动,其左端上部驱动与左传动齿轮13一体的偏心滚轴12 带动左传动齿轮旋转并通过与其啮合的右传动齿轮带动主传动轴顺时针输出旋转扭矩。See Figure 6: B-B-1. As shown in the figure, the pendulum groove 11 is at the top dead center position. When the rotating cylinder works, it rotates counterclockwise, which drives the pendulum groove to swing counterclockwise, and the upper left end drives the eccentric roller 12 integrated with the
参阅附图7:B-B-2。如图所示,此时摆槽11处于行程中点位置继续带动传动点轮按原有方向旋转。See Figure 7: B-B-2. As shown in the figure, the pendulum groove 11 is at the midpoint of the stroke and continues to drive the transmission point wheel to rotate in the original direction.
参阅附图8:B-B-3。如图所示,此时摆槽11处于下止点位置。See Figure 8: B-B-3. As shown in the figure, the swing groove 11 is at the bottom dead center position at this time.
参阅附图9:B-B-4。如图所示,此时转动缸体开始顺时针转动,带动摆槽边顺时针摆动,其右端上部驱动与右主传动齿轮一体的偏心滚轴带动右主传动齿轮旋转并直接通过主传动轴输出顺时针旋转扭矩。See Figure 9: B-B-4. As shown in the figure, the rotating cylinder starts to rotate clockwise at this time, which drives the side of the swing groove to swing clockwise, and the upper right end drives the eccentric roller integrated with the right main transmission gear to drive the right main transmission gear to rotate and output directly through the main transmission shaft. Rotate torque clockwise.
从以上B-B-1;B-B-2;B-B-3;B-B-4;四图可以看出①通过摆槽不仅将旋转缸的旋转往复运动转变为了主传动齿轮的单向旋转运动,而且从始至终均有较大的输出扭矩,理论上其有效输出扭矩是传动发动机的2倍以上,完全克服了传统发动机,直线往复运动转发为旋转运动时输出扭矩波动范围大,能量损失较多的弱点。②由于摆槽工作时依靠摆槽左右两端上部依次发挥作用,因此,本发明旋转缸体在略小于设计的最大行程时仍可正常工作,也就是可以实现一定范围内的可变行程工作,这不仅更便于发动机启动而且可实现火花塞的位置,转速双控点火,寻求点火的最佳时机实现能量转发效率的最大化。From the above B-B-1; B-B-2; B-B-3; B-B-4; it can be seen that ① through the swing groove, not only the rotary reciprocating motion of the rotary cylinder is converted into the one-way rotary motion of the main drive gear, but also from the beginning to the In the end, it has a large output torque. In theory, its effective output torque is more than 2 times that of the transmission engine, which completely overcomes the traditional engine. ② Since the swing groove works by relying on the upper parts of the left and right ends of the swing groove to play their roles in sequence, the rotating cylinder of the present invention can still work normally when it is slightly smaller than the designed maximum stroke, that is, it can realize variable stroke work within a certain range. This not only makes it easier to start the engine, but also realizes the position of the spark plug and the dual control of the speed of ignition, and seeks the best timing for ignition to maximize the efficiency of energy transfer.
Claims (6)
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210280776.8A CN114718718A (en) | 2022-03-14 | 2022-03-14 | Swing groove drive reciprocating rotary bump rotary engine |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210280776.8A CN114718718A (en) | 2022-03-14 | 2022-03-14 | Swing groove drive reciprocating rotary bump rotary engine |
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| CN114718718A true CN114718718A (en) | 2022-07-08 |
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| CN202210280776.8A Pending CN114718718A (en) | 2022-03-14 | 2022-03-14 | Swing groove drive reciprocating rotary bump rotary engine |
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