CN2732998Y - H type concave three lobe rotor piston engine - Google Patents
H type concave three lobe rotor piston engine Download PDFInfo
- Publication number
- CN2732998Y CN2732998Y CN200420030646.6U CN200420030646U CN2732998Y CN 2732998 Y CN2732998 Y CN 2732998Y CN 200420030646 U CN200420030646 U CN 200420030646U CN 2732998 Y CN2732998 Y CN 2732998Y
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- arc surface
- cylinder
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- 238000007789 sealing Methods 0.000 claims abstract description 21
- 238000002485 combustion reaction Methods 0.000 claims abstract description 6
- 239000000446 fuel Substances 0.000 abstract description 4
- 230000006835 compression Effects 0.000 abstract description 2
- 238000007906 compression Methods 0.000 abstract description 2
- 238000003915 air pollution Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
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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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Abstract
一种H型凹三角转子活塞发动机,它包括气缸和三角转子,三角转子侧面为H型,其相邻两角之间为行星轨迹的内凹形弧面,弧面上前半段开有凹道,气缸内凸处设有弹性密封片,其中一个密封片的前端为燃烧室、后端装有单向排气阀门并与进油管路相通,另一个密封片的前端为吸气口、后端为排气口。本实用新型在排气口和吸气口之间安装有密封片,防止油汽随废气排出;当燃烧室点火的瞬间,转子内凹弧面的后半部顶开单向排气阀门,将这一部分做负功的压力释放并将油汽排放回进油系统。在排气量、压缩比相同的情况下,耗油量下降46%,尾气排污量下降51%,最大扭距和功率提高2.6倍,重量和体积降低了2/3,成本降低1/4,使用寿命为原来的两倍。
An H-shaped concave triangular rotor piston engine, which includes a cylinder and a triangular rotor. The side of the triangular rotor is H-shaped, and the inner concave arc surface of the planetary track is between two adjacent corners. The first half of the arc surface has a groove , there is an elastic sealing piece at the convex part of the cylinder, the front end of one of the sealing pieces is the combustion chamber, the rear end is equipped with a one-way exhaust valve and communicated with the oil inlet pipeline, the front end of the other sealing piece is the suction port, and the rear end is for the exhaust port. The utility model is equipped with a sealing sheet between the exhaust port and the suction port to prevent oil vapor from being discharged with the exhaust gas; when the combustion chamber is ignited, the rear half of the concave arc surface of the rotor pushes open the one-way exhaust valve, and the This part does negative work to release the pressure and discharge the oil vapor back into the oil inlet system. In the case of the same exhaust volume and compression ratio, the fuel consumption is reduced by 46%, the exhaust emission is reduced by 51%, the maximum torque and power are increased by 2.6 times, the weight and volume are reduced by 2/3, and the cost is reduced by 1/4. The service life is doubled.
Description
技术领域technical field
本实用新型是一种发动机,特别是一种H型凹三角转子活塞发动机。The utility model relates to an engine, in particular to an H-shaped concave triangular rotor piston engine.
背景技术Background technique
2001年11月的东京车展上展出了被称为世界上独一无二的凸三角转子发动机配置的RX8跑车。这种发动机的输出功率高,但是由于在转子的每一个工作周期,吸气口与排气口之间都会有瞬间的连通,使进入的油汽随废气排出,造成耗油量的增大和对空气的污染;或者使应该排出的废气进入吸气口,降低油汽的比例,影响发动机的效率。其次是由于转子上的密封片与气缸内壁之间为线接触,象三把尖刀在气缸内壁上刮,很快就在气缸内壁上出现波状振纹磨损,使气缸的使用寿命短。At the Tokyo Motor Show in November 2001, the RX8 sports car, known as the world's unique convex triangular rotor engine configuration, was exhibited. The output power of this kind of engine is high, but because there will be an instant connection between the suction port and the exhaust port in each working cycle of the rotor, the oil vapor entering will be discharged with the exhaust gas, resulting in an increase in fuel consumption and damage to the engine. Air pollution; or let the exhaust gas that should be discharged enter the intake port, reduce the ratio of oil and gas, and affect the efficiency of the engine. Secondly, due to the linear contact between the sealing plate on the rotor and the cylinder inner wall, scraping on the cylinder inner wall like three sharp knives, there will be wavy vibration pattern wear on the cylinder inner wall soon, so that the service life of the cylinder is short.
发明内容Contents of the invention
本实用新型的目的是提供一种新型的发动机,它可以克服现有技术中所存在的缺点,降低耗油率,其次提高使用寿命。The purpose of this utility model is to provide a new type of engine, which can overcome the shortcomings of the prior art, reduce fuel consumption, and secondly increase the service life.
本实用新型的目的是这样实现的:它包括气缸和三角转子,气缸内腔带有两处内凸,三角转子的角端部设有弹性密封片,其特征在于三角转子侧面为H型,其相邻两角之间为行星轨迹的内凹形弧面,弧面上前半段开有凹道,气缸内凸处设有弹性密封片,其中一个密封片的前端为燃烧室、后端装有单向排气阀门并与进油管路相通,另一个密封片的前端为吸气口、后端为排气口。The purpose of this utility model is achieved in the following way: it includes a cylinder and a triangular rotor, the inner chamber of the cylinder has two protrusions, and the corner end of the triangular rotor is provided with an elastic sealing piece, which is characterized in that the side of the triangular rotor is H-shaped, and its Between two adjacent corners is the concave arc surface of the planetary track, the front half of the arc surface has a groove, and the inner convex part of the cylinder is provided with an elastic sealing sheet, and the front end of one sealing sheet is the combustion chamber, and the rear end is equipped with The one-way exhaust valve communicates with the oil inlet pipeline, and the front end of the other sealing sheet is the suction port, and the rear end is the exhaust port.
本实用新型的上述结构有如下优点:由于在排气口和吸气口之间安装有密封片,防止了油汽随废气排出;转子上的内凹形弧面使转子的力臂加长;当燃烧室点火的瞬间,转子内凹弧面的后半部在高压推动下,顶开单向排气阀门,将这一部分做负功的压力释放并将油汽排放回进油系统。所以在排气量、压缩比和主轴转速相同的情况下,本实用新型的耗油量下降46%,尾气排污量下降51%,最大扭距和功率提高2.6倍,重量和体积降低了2/3,成本降低1/4,使用寿命为原来的两倍。The above-mentioned structure of the utility model has the following advantages: because a sealing sheet is installed between the exhaust port and the suction port, oil vapor is prevented from being discharged along with the exhaust gas; the inner concave arc surface on the rotor lengthens the arm of the rotor; At the moment when the combustion chamber is ignited, the second half of the concave arc surface of the rotor is driven by high pressure to open the one-way exhaust valve, releasing the pressure of this part of the negative work and discharging the oil vapor back into the oil system. Therefore, in the case of the same displacement, compression ratio and spindle speed, the fuel consumption of the utility model is reduced by 46%, the exhaust emission is reduced by 51%, the maximum torque and power are increased by 2.6 times, and the weight and volume are reduced by 2/ 3. The cost is reduced by 1/4, and the service life is doubled.
附图说明Description of drawings
图1是本实用新型的断面剖视图。Fig. 1 is a sectional view of the utility model.
图2是本实用新型的侧面剖视图。Fig. 2 is a side sectional view of the utility model.
图3是图1和图2中所示的侧向密封的放大视图。FIG. 3 is an enlarged view of the side seal shown in FIGS. 1 and 2 .
图4是图3中的A向视图。Fig. 4 is a view from direction A in Fig. 3 .
图5是图1中所示的转子上的凹道的断面图。FIG. 5 is a cross-sectional view of a groove on the rotor shown in FIG. 1 .
具体实施方式Detailed ways
下面结合实施例及其附图对本实用新型做进一步详细的说明。Below in conjunction with embodiment and accompanying drawing, the utility model is described in further detail.
图2中1是曲轴,在曲轴上安装有轴承9,并装有外齿轮2和转子7,内齿轮3与转子固定连接并与外齿轮2相啮合,8是飞轮,4是气缸。由图可见,转子的侧面为H型,中间部分为转子的工作面,如图3和图4所示的密封条12和波型弹簧13安装在气缸工作面的两端。1 is crankshaft among Fig. 2, and bearing 9 is installed on crankshaft, and
由图1可见,H型转子7的工作段的横截面为内凹三角形,即三角形的两个相邻角之间为行星轨迹组成的内凹弧面,同时在弧面的前半段上开有如图5所示的凹道5,在转子7的三个顶点上安装有密封片11和实现密封片弹性伸缩的波型弹簧12。为减小对气缸内壁的刮伤,密封片的接触面设计为弧面,与气缸之间为弧面接触。气缸4的内壁带有两个对称布置的内凸,在突起处设有密封,安装有密封片11和弹簧12,在图中上面的突起K处密封片的前端为燃烧室,安装有火花塞14,后端开有通孔,安装有单向排气阀门6。下面的突起Q处前端为吸气口,后端为排气口。It can be seen from Figure 1 that the cross-section of the working section of the H-
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200420030646.6U CN2732998Y (en) | 2004-03-05 | 2004-03-05 | H type concave three lobe rotor piston engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200420030646.6U CN2732998Y (en) | 2004-03-05 | 2004-03-05 | H type concave three lobe rotor piston engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2732998Y true CN2732998Y (en) | 2005-10-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200420030646.6U Expired - Fee Related CN2732998Y (en) | 2004-03-05 | 2004-03-05 | H type concave three lobe rotor piston engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2732998Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103615312A (en) * | 2013-11-22 | 2014-03-05 | 姜地 | Telescopic cylindrical rotor type engine |
| CN104234828A (en) * | 2014-09-04 | 2014-12-24 | 霍勇贤 | Three-cylinder four-stroke rotor engine |
| WO2015165199A1 (en) * | 2014-04-30 | 2015-11-05 | 郭远军 | Rotor high and low pressure power device and work-doing method therefor |
-
2004
- 2004-03-05 CN CN200420030646.6U patent/CN2732998Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103615312A (en) * | 2013-11-22 | 2014-03-05 | 姜地 | Telescopic cylindrical rotor type engine |
| WO2015165199A1 (en) * | 2014-04-30 | 2015-11-05 | 郭远军 | Rotor high and low pressure power device and work-doing method therefor |
| US9726046B2 (en) | 2014-04-30 | 2017-08-08 | Yuanjun GUO | Rotor high-and-low pressure power apparatus and working method thereof |
| CN104234828A (en) * | 2014-09-04 | 2014-12-24 | 霍勇贤 | Three-cylinder four-stroke rotor engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |