CN115163289A - A Swirl Spray Tumble Combustion System for Opposed Piston Compression Ignition Engine - Google Patents
A Swirl Spray Tumble Combustion System for Opposed Piston Compression Ignition Engine Download PDFInfo
- Publication number
- CN115163289A CN115163289A CN202210654832.XA CN202210654832A CN115163289A CN 115163289 A CN115163289 A CN 115163289A CN 202210654832 A CN202210654832 A CN 202210654832A CN 115163289 A CN115163289 A CN 115163289A
- Authority
- CN
- China
- Prior art keywords
- combustion
- opposed
- swirl
- compression ignition
- chamber
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 74
- 239000007921 spray Substances 0.000 title claims abstract description 34
- 238000007906 compression Methods 0.000 title claims abstract description 26
- 230000006835 compression Effects 0.000 title claims abstract description 24
- 239000000446 fuel Substances 0.000 claims description 13
- 230000009471 action Effects 0.000 abstract description 6
- 238000000034 method Methods 0.000 description 7
- 230000008569 process Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 239000012530 fluid Substances 0.000 description 4
- 230000002000 scavenging effect Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- 241000124033 Salix Species 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 238000000889 atomisation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
Images
Classifications
-
- 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
-
- 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0675—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space being substantially spherical, hemispherical, ellipsoid or parabolic
-
- 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
- F02B75/00—Other engines
- F02B75/28—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
- F02F3/26—Pistons having combustion chamber in piston head
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
Description
技术领域technical field
本发明属于对置活塞压燃式发动机技术领域,尤其是涉及一种对置活塞压燃发动机旋流喷雾滚流燃烧系统。The invention belongs to the technical field of opposed-piston compression-ignition engines, in particular to a swirling spray tumble combustion system of an opposed-piston compression-ignition engine.
背景技术Background technique
对置活塞发动机相比于传统的往复活塞式发动机,由于取消了缸盖和配气机构,具有结构紧凑、做功频次高、动平衡好的特点。但由于换气过程通过气缸套上的进排气口实现,换气通过形成螺旋运动方式组织,废气很难快速排出,为保证扫气效率,通常需要提高给气比并加大排气开启相位。同时,由于对置活塞压燃发动机结构紧凑,喷油器通常侧置。燃油侧向喷入缸内,这样,从喷油器出口到撞壁点距离较短,喷雾空间雾化不充分,通常采用撞壁二次破碎的方式形成混合气,导致燃油湿壁量增加。另外,提前排气开启相位,导致缸内混合气形成和燃烧过程的时间进一步压缩。综合以上因素,这类发动机常常出现由于混合不均匀导致燃烧效率低、燃烧不充分的问题。因此,提高喷雾质量、优化缸内流场结构,可以从根源上改善对置活塞压燃式发动机的混合气形成及燃烧特性。常见的优化方式,多集中在进排气口排列布置方式,通过改变气口径向倾角,加强涡流运动,但对喷雾燃烧过程的作用效果有限。Compared with the traditional reciprocating piston engine, the opposed piston engine has the characteristics of compact structure, high power frequency and good dynamic balance due to the cancellation of the cylinder head and the valve train. However, since the ventilation process is realized through the intake and exhaust ports on the cylinder liner, the ventilation is organized by forming a spiral motion, and the exhaust gas is difficult to discharge quickly. In order to ensure the scavenging efficiency, it is usually necessary to increase the air supply ratio and increase the exhaust opening phase. . At the same time, due to the compact structure of the opposed-piston compression ignition engine, the injector is usually placed on the side. The fuel is injected laterally into the cylinder, so that the distance from the injector outlet to the wall collision point is short, and the atomization of the spray space is insufficient. Usually, the secondary crushing of the collision wall is used to form a mixture, resulting in an increase in the amount of fuel wet wall. In addition, the exhaust opening phase is advanced, resulting in further compression of the timing of the in-cylinder mixture formation and combustion process. Combining the above factors, such engines often have problems of low combustion efficiency and insufficient combustion due to uneven mixing. Therefore, improving the spray quality and optimizing the flow field structure in the cylinder can fundamentally improve the mixture formation and combustion characteristics of the opposed-piston compression ignition engine. The common optimization methods are mostly concentrated on the arrangement of the intake and exhaust ports. By changing the radial inclination of the gas port, the vortex motion is enhanced, but the effect on the spray combustion process is limited.
发明内容SUMMARY OF THE INVENTION
有鉴于此,本发明旨在提出一种对置活塞压燃发动机旋流喷雾滚流燃烧系统,以解决发动机燃烧效率低下的问题。In view of this, the present invention aims to propose a swirling spray tumble combustion system for an opposed-piston compression ignition engine to solve the problem of low combustion efficiency of the engine.
为达到上述目的,本发明的技术方案是这样实现的:In order to achieve the above object, the technical scheme of the present invention is achieved in this way:
一种对置活塞压燃发动机旋流喷雾滚流燃烧系统,包括对置活塞、喷油器、燃烧室、缸套、旋流室和导向屏,缸套内部安装对置活塞,对置活塞中间形成燃烧室,缸套两侧对称安装旋流室,每个旋流室与一个导向屏连通,且导向屏的出口切向方向与所述燃烧室形状匹配,每个旋流室内部安装一个喷油器。A swirling spray tumble combustion system for an opposed-piston compression ignition engine, comprising opposed pistons, an injector, a combustion chamber, a cylinder liner, a swirl chamber and a guide screen, an opposed piston is installed inside the cylinder liner, and the middle of the opposed piston A combustion chamber is formed, swirl chambers are installed symmetrically on both sides of the cylinder liner, each swirl chamber is communicated with a guide screen, and the tangential direction of the outlet of the guide screen matches the shape of the combustion chamber, and a nozzle is installed inside each swirl chamber. oiler.
进一步的,所述旋流室形状接近球形,且位于发动机上止点附近。Further, the shape of the swirl chamber is close to a spherical shape, and is located near the top dead center of the engine.
进一步的,所述导向屏自入口至出口呈渐缩流线型。Further, the guide screen is in a tapered streamline shape from the inlet to the outlet.
进一步的,所述燃烧室为半柳叶型。Further, the combustion chamber is a semi-willow shape.
进一步的,所述对置活塞为非对称结构,且相对布置。Further, the opposed pistons are of asymmetrical structure and are arranged oppositely.
进一步的,所述发动机上止点附近,两侧的半柳叶型燃烧室构成一个类椭圆型燃烧室。Further, near the top dead center of the engine, the semi-willow-shaped combustion chambers on both sides form an elliptical-like combustion chamber.
相对于现有技术,本发明所述的对置活塞压燃发动机旋流喷雾滚流燃烧系统具有以下优势:Compared with the prior art, the swirling spray tumble combustion system of the opposed piston compression ignition engine described in the present invention has the following advantages:
(1)本发明所述的对置活塞压燃发动机旋流喷雾滚流燃烧系统,在上止点附近,利用所述对置活塞的非对称半柳叶燃烧室结构特点,结合所述导向屏出口喷雾射流作用下缸内形成滚流运动,加速油气混合,缩短着火滞燃期和燃烧持续期,提高燃烧效率。(1) The swirling spray tumble combustion system of the opposed piston compression ignition engine according to the present invention, near the top dead center, utilizes the structural features of the asymmetric half-willow combustion chamber of the opposed piston, combined with the guide screen Under the action of the outlet spray jet, a tumble movement is formed in the cylinder, which accelerates the mixing of oil and gas, shortens the ignition delay period and combustion duration, and improves the combustion efficiency.
(2)本发明所述的对置活塞压燃发动机旋流喷雾滚流燃烧系统,通过所述对置活塞的非对称半柳叶燃烧室结构在燃烧过程所形成的滚流运动,在排气过程有利于废气排出,提高发动机扫气效率。(2) In the swirling spray tumble combustion system of the opposed piston compression ignition engine according to the present invention, through the tumble motion formed by the asymmetric half willow leaf combustion chamber structure of the opposed piston in the combustion process, the The process is conducive to exhaust gas discharge and improves engine scavenging efficiency.
(3)本发明所述的对置活塞压燃发动机旋流喷雾滚流燃烧系统,对置活塞上止点存在的相位差,配合所述导向屏出口位置,在上止点附近可实现压缩比迅速提高,进一步提高燃烧等容度,提高燃烧效率。(3) In the swirling spray tumble combustion system of the opposed piston compression ignition engine according to the present invention, the phase difference existing at the top dead center of the opposed pistons can be matched with the position of the exit of the guide screen, and the compression ratio can be realized near the top dead center. Rapidly increase, further improve the combustion isovolume, and improve the combustion efficiency.
附图说明Description of drawings
构成本发明的一部分的附图用来提供对本发明的进一步理解,本发明的示意性实施例及其说明用于解释本发明,并不构成对本发明的不当限定。在附图中:The accompanying drawings constituting a part of the present invention are used to provide further understanding of the present invention, and the exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation of the present invention. In the attached image:
图1为本发明实施例所述的对置活塞压燃发动机旋流喷雾滚流燃烧系统的示意图;1 is a schematic diagram of a swirling spray tumble combustion system of an opposed piston compression ignition engine according to an embodiment of the present invention;
图2为本发明实施例所述的压缩过程旋流室旋流喷雾滚流燃烧系统的工质流动示意图;2 is a schematic diagram of the working fluid flow of a swirling chamber swirling spray tumble combustion system in a compression process according to an embodiment of the present invention;
图3是本发明实施例所述的燃烧过程旋流喷雾滚流燃烧系统的工质流动示意图;3 is a schematic diagram of the working fluid flow of the swirling spray tumble combustion system in the combustion process according to the embodiment of the present invention;
图4是本发明实施例所述的上止点附近旋流喷雾滚流燃烧系统的结构示意图。4 is a schematic structural diagram of a swirling spray tumble combustion system near top dead center according to an embodiment of the present invention.
附图标记说明:Description of reference numbers:
1-对置活塞;2-喷油器;3-燃油喷雾;4-燃烧室;5-缸套;6-旋流室;7-导向屏;8-压缩过程工质流线;9-燃烧过程上侧工质流线;10-燃烧过程下侧工质流线;11-导向屏出口。1- Opposed piston; 2- Fuel injector; 3- Fuel spray; 4- Combustion chamber; 5- Cylinder liner; 6- Swirl chamber; 7- Guide screen; The working fluid streamline on the upper side of the process; 10- the working fluid streamline on the lower side of the combustion process; 11- the exit of the guide screen.
具体实施方式Detailed ways
需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。It should be noted that the embodiments of the present invention and the features of the embodiments may be combined with each other under the condition of no conflict.
在本发明的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。此外,术语“第一”、“第二”等仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”等的特征可以明示或者隐含地包括一个或者更多个该特征。在本发明的描述中,除非另有说明,“多个”的含义是两个或两个以上。In the description of the present invention, it should be understood that the terms "center", "portrait", "horizontal", "top", "bottom", "front", "rear", "left", "right", " The orientation or positional relationship indicated by vertical, horizontal, top, bottom, inner, outer, etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and The description is simplified rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should not be construed as indicating or implying relative importance or implying the number of indicated technical features. Thus, a feature defined as "first", "second", etc., may expressly or implicitly include one or more of that feature. In the description of the present invention, unless otherwise specified, "plurality" means two or more.
在本发明的描述中,需要说明的是,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通。对于本领域的普通技术人员而言,可以通过具体情况理解上述术语在本发明中的具体含义。In the description of the present invention, it should be noted that the terms "installed", "connected" and "connected" should be understood in a broad sense, unless otherwise expressly specified and limited, for example, it may be a fixed connection or a detachable connection Connection, or integral connection; can be mechanical connection, can also be electrical connection; can be directly connected, can also be indirectly connected through an intermediate medium, can be internal communication between two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood through specific situations.
下面将参考附图并结合实施例来详细说明本发明。The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
一种对置活塞压燃发动机旋流喷雾滚流燃烧系统,如图1至图4所示,包括对置活塞1、喷油器2、燃烧室4、缸套5、旋流室6和导向屏7,缸套5内部安装对置活塞1,对置活塞1中间形成燃烧室4,缸套5两侧对称安装旋流室6,每个旋流室6与一个导向屏7连通,每个旋流室6内部安装一个喷油器2。A swirl spray tumble combustion system for an opposed piston compression ignition engine, as shown in Figures 1 to 4, includes
所述喷油器2安装在旋流室6内,燃油喷雾在旋流室6内强涡团卷吸作用下加速蒸发。所述旋流室6形状接近球形,位于发动机上止点附近。The
所述导向屏7自入口至出口呈渐缩流线型。燃油蒸气受所述导向屏7流通面积渐缩作用,喷雾在导向屏的出口11形成射流进入缸套5内。导向屏7的出口11切向方向与所述燃烧室4形状匹配。The
每侧的燃烧室4均为半柳叶型;所述对置活塞1为非对称结构,且相对布置。发动机上止点附近,两侧的半柳叶型燃烧室4构成一个类椭圆型大燃烧室,利用所述对置活塞1的非对称半柳叶燃烧室4结构特点,结合所述导向屏出口11喷雾射流作用下缸内形成滚流运动,加速油气混合,缩短着火滞燃期和燃烧持续期,提高燃烧效率。The
所述对置活塞1的非对称半柳叶燃烧室4结构,在燃烧过程所形成的滚流运动,在排气过程有利于废气排出,提高发动机扫气效率。如果对置活塞上止点存在相位差,配合所述导向屏出口11位置,在上止点附近可实现压缩比迅速提高,进一步提高燃烧等容度,提高燃烧效率。The asymmetric half-
一种对置活塞压燃发动机旋流喷雾滚流燃烧系统的工作原理如下:The working principle of a swirling spray tumble combustion system for an opposed piston compression ignition engine is as follows:
1.发动机压缩过程,如图2所示,工质受所述导向屏7负压作用,进入所述旋流室6,形成旋流室6腔内旋流运动。1. In the engine compression process, as shown in FIG. 2 , the working medium is subjected to the negative pressure of the
2.喷油开始,如图1所示,燃油喷雾3在旋流室6内强涡团卷吸作用下加速蒸发;燃油蒸气受所述导向屏7流通面积渐缩作用,喷雾在导向屏出口11形成射流进入气缸内。2. The fuel injection starts, as shown in Figure 1, the
如图3所示,利用对置活塞1的燃烧室4结构特点,两侧半柳叶型燃烧室4构成类椭圆型燃烧室,结合所述导向屏出口11喷雾射流作用下气缸内形成滚流运动,加速油气混合。As shown in FIG. 3, using the structural characteristics of the
3.对置活塞1上止点存在相位差,在上止点附近,如图4所示,导向屏出口11被下侧对置活塞1遮挡,旋流室6与气缸隔离,工作容积迅速缩小,压缩比迅速提高,进一步提高燃烧等容度,提高燃烧效率。3. There is a phase difference at the top dead center of the opposing
4.对置活塞1进一步下行至排气口位置,排气过程开始,在燃烧过程所形成的滚流运动,利于废气排出,提高发动机扫气效率。4. The
以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included in the scope of the present invention. within the scope of protection.
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210654832.XA CN115163289A (en) | 2022-06-10 | 2022-06-10 | A Swirl Spray Tumble Combustion System for Opposed Piston Compression Ignition Engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210654832.XA CN115163289A (en) | 2022-06-10 | 2022-06-10 | A Swirl Spray Tumble Combustion System for Opposed Piston Compression Ignition Engine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN115163289A true CN115163289A (en) | 2022-10-11 |
Family
ID=83484520
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210654832.XA Pending CN115163289A (en) | 2022-06-10 | 2022-06-10 | A Swirl Spray Tumble Combustion System for Opposed Piston Compression Ignition Engine |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115163289A (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102900521A (en) * | 2011-07-26 | 2013-01-30 | 艾克莫特国际公司 | Tumble-flow accelerating combustion chamber |
US20130036999A1 (en) * | 2011-08-08 | 2013-02-14 | Ecomotors International, Inc. | High-Squish Combustion Chamber With Side Injection |
CN103168148A (en) * | 2010-08-16 | 2013-06-19 | 阿凯提兹动力公司 | Fuel injection spray patterns for opposed-piston engines |
CN104018939A (en) * | 2013-03-01 | 2014-09-03 | 优华劳斯汽车系统(上海)有限公司 | Engine with oppositely-arranged pistons and oppositely-arranged cylinders |
US20150300241A1 (en) * | 2014-02-04 | 2015-10-22 | Ronald A. Holland | Opposed Piston Engine |
-
2022
- 2022-06-10 CN CN202210654832.XA patent/CN115163289A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103168148A (en) * | 2010-08-16 | 2013-06-19 | 阿凯提兹动力公司 | Fuel injection spray patterns for opposed-piston engines |
CN102900521A (en) * | 2011-07-26 | 2013-01-30 | 艾克莫特国际公司 | Tumble-flow accelerating combustion chamber |
US20130036999A1 (en) * | 2011-08-08 | 2013-02-14 | Ecomotors International, Inc. | High-Squish Combustion Chamber With Side Injection |
CN104018939A (en) * | 2013-03-01 | 2014-09-03 | 优华劳斯汽车系统(上海)有限公司 | Engine with oppositely-arranged pistons and oppositely-arranged cylinders |
US20150300241A1 (en) * | 2014-02-04 | 2015-10-22 | Ronald A. Holland | Opposed Piston Engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106460635B (en) | The combustion chamber structure of diesel engine | |
US5014663A (en) | Two-stroke internal combustion engine and cylinder head for the latter | |
CN109899174A (en) | A kind of combustion system for using gasoline ignition engine instead on the basis of diesel engine | |
US3335707A (en) | Internal combustion engines | |
CN113669152B (en) | An Ignition Mechanism of a Gasoline Engine Containing a Strong Tumble Pre-chamber | |
US20200182190A1 (en) | Piston combustion chamber structure of engine | |
CN101463753A (en) | Low-discharge two-stroke gasoline engine | |
CN115163289A (en) | A Swirl Spray Tumble Combustion System for Opposed Piston Compression Ignition Engine | |
CN107060986A (en) | One kind is used for the piston-engined combined type combustion chamber of two stroke Heavy End Aviation Fuels | |
CN201206502Y (en) | Small-sized petrol engine cylinder cover | |
CN202946255U (en) | Cylinder end air passage structure | |
US11536221B2 (en) | Piston crown for a combustion system and an associated method thereof | |
US11512663B2 (en) | Engine with combustion chamber | |
CN212927995U (en) | Novel high-efficiency ignition engine | |
CN104632352B (en) | A kind of combined jet oil beam encapsulating type combustion chamber | |
CN111749784A (en) | Novel high-efficiency ignition engine | |
US8826881B2 (en) | Engine and cylinder with gas exchange through the cylinder wall | |
CN208518762U (en) | Piston combustion bowl and automobile | |
CN201972803U (en) | Cylinder cover of motorcycle engine | |
JP2017061901A (en) | piston | |
CN209781048U (en) | engine | |
CN112761750B (en) | Air flow spraying and flow disturbing device in cylinder of internal combustion engine | |
CN111022210B (en) | High Turbulence Piston Combustion Chamber for Diesel Natural Gas Dual Fuel | |
JPS5933879Y2 (en) | internal combustion engine cylinder head | |
KR102378351B1 (en) | Internal combustion engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20221011 |
|
RJ01 | Rejection of invention patent application after publication |