CN102562261A - Annular double-piston engine - Google Patents
Annular double-piston engine Download PDFInfo
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- CN102562261A CN102562261A CN2012100502988A CN201210050298A CN102562261A CN 102562261 A CN102562261 A CN 102562261A CN 2012100502988 A CN2012100502988 A CN 2012100502988A CN 201210050298 A CN201210050298 A CN 201210050298A CN 102562261 A CN102562261 A CN 102562261A
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Abstract
一种环形双活塞发动机,包括壳体、端盖、活塞、主轴,壳体为圆形筒体,壳体与前端盖、前活塞构成前缸压气室,壳体与后端盖、后活塞构成后缸燃烧室,壳体中部位置还开有导向槽,前活塞和后活塞通过连接件连接,连接件上装有导向片和导轮,导向片设在导向槽中,主轴贯穿于整个壳体,且处于中心轴线位置,主轴在壳体内部有一凸柱,凸柱上开有沿圆柱侧面呈正弦曲线形状的凹槽,凹槽把凸柱分成了前凸柱和后凸柱,导轮放置在凹槽内,可在凹槽内运动。本发明的环形双活塞发动机主要的特点是:散热效果好,可以简化水冷系统或风冷系统;结构紧凑,零件数量少;扭矩大,转速低,中间主轴的凸轮部分就是减速器,不需要另外的减速器。
An annular double-piston engine, including a housing, an end cover, a piston, and a main shaft. In the combustion chamber of the rear cylinder, there is a guide groove in the middle of the shell. The front piston and the rear piston are connected by a connecting piece. The connecting piece is equipped with a guide piece and a guide wheel. The guide piece is set in the guide groove, and the main shaft runs through the whole shell. And in the central axis position, the main shaft has a convex column inside the shell, and the convex column has a sinusoidal groove along the side of the cylinder. The groove divides the convex column into the front convex column and the rear convex column. The guide wheel is placed on the In the groove, it can move in the groove. The main features of the annular double-piston engine of the present invention are: good heat dissipation effect, which can simplify the water cooling system or the air cooling system; reducer.
Description
技术领域 technical field
本发明属于一种环形双活塞发动机。 The invention belongs to an annular double-piston engine.
背景技术 Background technique
目前,活塞式航空发动机仍广泛地应用于中小型飞机,特别是作为通用航空的动力装置。随着航空器的设计和制造技术的不断发展,对其动力装置提出了更高的要求。而当前大多数活塞式航空发动机是采用水冷系统和减速器减速,这必然增加发动机的重量,降低发动机的功率重量比,从而降低发动机的经济性。在“为减轻每一克重量而奋斗”的航空技术领域里,减轻每一克重量就象金子一样宝贵。 At present, piston aeroengines are still widely used in small and medium-sized aircraft, especially as power devices for general aviation. With the continuous development of aircraft design and manufacturing technology, higher requirements are put forward for its power plant. However, most of the current piston-type aero-engines use water-cooling systems and reducers to decelerate, which will inevitably increase the weight of the engine and reduce the power-to-weight ratio of the engine, thereby reducing the economy of the engine. In the field of aviation technology that "strives for every gram of weight reduction", every gram of weight reduction is as precious as gold.
发明内容 Contents of the invention
本发明的目的就是提供一种结构紧凑、制造简单、运行平稳,具有良好的散射性能,而且活塞工作产生的扭矩大的环形活塞发动机。 The object of the present invention is to provide a ring piston engine with compact structure, simple manufacture, stable operation, good scattering performance and large torque generated by the piston working.
本发明的环形双活塞发动机,包括壳体、前端盖、后端盖、前活塞、后活塞、主轴,壳体为圆形筒体,壳体与前端盖、前活塞构成前缸压气室,壳体与后端盖、后活塞构成后缸燃烧室,壳体中部位置还开有四个导向槽,前活塞和后活塞通过连接件连接,连接件上装有导向片和导轮,导向片设在导向槽中,并可在导向槽内左右移动,主轴贯穿于整个壳体,且处于中心轴线位置,主轴在壳体内部有一凸柱,凸柱上开有沿圆柱侧面呈正弦曲线形状的凹槽,其上共有两个峰谷,凹槽把凸柱分成了前凸柱和后凸柱,前凸柱和后凸柱构成的整体作为发动机的减速器,导轮放置在凹槽内,可在凹槽内运动,推动主轴产生扭矩,前缸压气室与后缸燃烧室通过主轴中心通孔或壳体的外管连通。 The annular dual-piston engine of the present invention comprises a housing, a front end cover, a rear end cover, a front piston, a rear piston, and a main shaft. The body, the rear end cover and the rear piston form the combustion chamber of the rear cylinder. There are four guide grooves in the middle of the housing. The front piston and the rear piston are connected through a connecting piece. In the guide groove, and can move left and right in the guide groove, the main shaft runs through the entire shell, and is at the central axis position, the main shaft has a convex column inside the shell, and the convex post has a sinusoidal groove along the side of the cylinder , there are two peaks and valleys on it, and the groove divides the convex column into the front convex column and the rear convex column. The whole body composed of the front convex column and the rear convex column is used as the reducer of the engine. Movement in the groove pushes the main shaft to generate torque, and the front cylinder compression chamber communicates with the rear cylinder combustion chamber through the central through hole of the main shaft or the outer tube of the housing.
本发明的环形双活塞发动机,燃气在后缸燃烧室燃烧,推动后活塞向前运动,从而带动前活塞压缩前缸压气室气体,与此同时,导轮在曲线凹槽内运动,使主轴产生扭矩,活塞一个来回,主轴转动半圈,使得主轴扭矩很大,前活塞压缩后的气体又可通过主轴中心通孔或壳体的外管流到后缸燃烧室,为后缸燃烧室提供压缩气体。 In the annular double-piston engine of the present invention, gas is burned in the combustion chamber of the rear cylinder, which pushes the rear piston to move forward, thereby driving the front piston to compress the gas in the compression chamber of the front cylinder. At the same time, the guide wheel moves in the curved groove to make the main shaft generate Torque, the piston goes back and forth, and the main shaft rotates half a circle, so that the main shaft torque is very large, and the gas compressed by the front piston can flow to the rear cylinder combustion chamber through the through hole in the center of the main shaft or the outer tube of the housing, providing compression for the rear cylinder combustion chamber gas.
本发明的环形双活塞发动机主要的特点是:1、散热效果好,可以简化水冷系统或风冷系统;2、结构紧凑,零件数量少;3、扭矩大,转速低,中间主轴的凸轮部分就是减速器,不需要另外的减速器。 The main features of the annular double-piston engine of the present invention are: 1. good heat dissipation effect, which can simplify the water cooling system or air cooling system; 2. compact structure and small number of parts; 3. large torque and low speed. reducer, no additional reducer is required.
附图说明 Description of drawings
图1为本发明的结构示意图。 Fig. 1 is a structural schematic diagram of the present invention.
具体实施方式 Detailed ways
一种环形双活塞发动机,包括壳体2、前端盖15、后端盖7、前活塞13、后活塞6、主轴1,壳体2为圆形筒体,壳体2与前端盖15、前活塞13构成前缸压气室14,壳体2与后端盖7、后活塞6构成后缸燃烧室8,壳体2中部位置还开有四个导向槽12,前活塞13和后活塞6通过连接件4连接,连接件4上装有导向片3和导轮5,导向片3设在导向槽12中,并可在导向槽12内左右移动,主轴1贯穿于整个壳体2,且处于中心轴线位置,主轴1在壳体2内部有一凸柱,凸柱上开有沿圆柱侧面呈正弦曲线形状的凹槽10,其上共有两个峰谷,凹槽10把凸柱分成了前凸柱11和后凸柱9,前凸柱11和后凸柱9构成的整体作为发动机的减速器,导轮5放置在凹槽10内,可在凹槽10内运动,推动主轴1产生扭矩,前缸压气室14与后缸燃烧室8通过主轴1中心通孔或壳体2的外管连通。
An annular double-piston engine comprises a housing 2, a
当后缸燃烧室8的气体燃烧后,化学能转化为机械能,推动后活塞6运动,带动前活塞13压缩前缸压气室14的气体,与此同时,连接件4上的导轮5在凹槽10内运动,推动前凸柱11和后凸柱9转动,使主轴1产生扭矩,前活塞13运动一个来回,主轴1转动半圈,前活塞13压缩后的气体又可通过主轴1的中心通孔或者壳体2的外管流到后缸燃烧室8,为后缸燃烧室8提供压缩气体。
After the gas in the
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104100372A (en) * | 2014-06-23 | 2014-10-15 | 上海长辛实业有限公司 | Opposed piston guide rail rolling type engine/compressor and working method thereof |
CN107110021A (en) * | 2016-06-01 | 2017-08-29 | 上海长辛实业有限公司 | A kind of novel air pressing transmission device |
Citations (5)
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US1572068A (en) * | 1921-08-31 | 1926-02-09 | Advanced Engine Co Inc | Engine |
US5442913A (en) * | 1992-12-29 | 1995-08-22 | Goldstar Co., Ltd. | Stirling cycle system driving device |
DE19824703A1 (en) * | 1998-06-03 | 1999-12-16 | Elmer Schmidt | Internal combustion cylinder motor |
CN1902388A (en) * | 2003-11-26 | 2007-01-24 | 格雷登·奥伯瑞·谢佛德 | Reciprocating engine |
CN101983278A (en) * | 2008-03-17 | 2011-03-02 | 安塔尔·达乌克 | Engines with variable volume chambers |
-
2012
- 2012-03-01 CN CN2012100502988A patent/CN102562261A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1572068A (en) * | 1921-08-31 | 1926-02-09 | Advanced Engine Co Inc | Engine |
US5442913A (en) * | 1992-12-29 | 1995-08-22 | Goldstar Co., Ltd. | Stirling cycle system driving device |
DE19824703A1 (en) * | 1998-06-03 | 1999-12-16 | Elmer Schmidt | Internal combustion cylinder motor |
CN1902388A (en) * | 2003-11-26 | 2007-01-24 | 格雷登·奥伯瑞·谢佛德 | Reciprocating engine |
CN101983278A (en) * | 2008-03-17 | 2011-03-02 | 安塔尔·达乌克 | Engines with variable volume chambers |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104100372A (en) * | 2014-06-23 | 2014-10-15 | 上海长辛实业有限公司 | Opposed piston guide rail rolling type engine/compressor and working method thereof |
CN107110021A (en) * | 2016-06-01 | 2017-08-29 | 上海长辛实业有限公司 | A kind of novel air pressing transmission device |
WO2017206108A1 (en) * | 2016-06-01 | 2017-12-07 | 上海长辛实业有限公司 | Novel air-compressed transmission device |
CN107110021B (en) * | 2016-06-01 | 2019-12-17 | 上海长辛实业有限公司 | Novel pneumatic transmission device |
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