WO2013170632A1 - 直喷式柴油机双层分流燃烧*** - Google Patents

直喷式柴油机双层分流燃烧*** Download PDF

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Publication number
WO2013170632A1
WO2013170632A1 PCT/CN2013/000574 CN2013000574W WO2013170632A1 WO 2013170632 A1 WO2013170632 A1 WO 2013170632A1 CN 2013000574 W CN2013000574 W CN 2013000574W WO 2013170632 A1 WO2013170632 A1 WO 2013170632A1
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WO
WIPO (PCT)
Prior art keywords
spray
collision
combustion chamber
diesel engine
guiding
Prior art date
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PCT/CN2013/000574
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English (en)
French (fr)
Inventor
隆武强
齐鲲鹏
田江平
张强
盛凯
依平
王一聪
付垚
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大连理工大学
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Application filed by 大连理工大学 filed Critical 大连理工大学
Publication of WO2013170632A1 publication Critical patent/WO2013170632A1/zh
Priority to US14/529,187 priority Critical patent/US20150053172A1/en
Priority to US15/865,296 priority patent/US10563569B2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M29/00—Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture
    • 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
    • F02B23/0645—Details related to the fuel injector or the fuel spray
    • F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
    • F02B23/0651—Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
    • 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
    • F02B23/0672—Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
    • 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
    • F02B23/0678—Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets
    • F02B23/0693—Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets the combustion space consisting of step-wise widened multiple zones of different depth
    • 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 
    • F02F3/24—Pistons  having means for guiding gases in cylinders, e.g. for guiding scavenging charge in two-stroke engines
    • 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
    • F02B1/00—Engines characterised by fuel-air mixture compression
    • F02B1/12—Engines characterised by fuel-air mixture compression with compression ignition
    • 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
    • F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14—Direct injection into combustion chamber
    • 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
    • F02B3/00—Engines characterised by air compression and subsequent fuel addition
    • F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

Definitions

  • the present invention relates to a two-stage split combustion system for a direct injection diesel engine, which belongs to the field of engine mixture formation and combustion.
  • the direct injection diesel engine has a large excess air coefficient, but it is easy to emit black smoke.
  • the main reason is that the porous spray is unevenly distributed in the circumferential direction, and an excessively rich region is generated at the spray drop point.
  • a part of the spray accumulates at or near the landing point, or forms an oil film, and the other part bounces and then spreads to the periphery. Because it is close to the combustion chamber wall, the amount of air entrapped is small, and an excessively concentrated area is formed at the falling point of the spray. This results in low diesel engine air utilization, incomplete combustion, high fuel consumption and high soot emissions.
  • the invention provides a two-stage split combustion system for a direct injection diesel engine.
  • the two-layer split-flow combustion system reduces the space between the top surface of the piston and the bottom surface of the cylinder head. Part of the spray is rebounded by the collision table, and a part of the spray is quickly shunted along the upper and lower sides of the guide surface to realize double-layer splitting, and at the same time, the spray can achieve secondary atomization, improve spray atomization performance, expand the spray space distribution range, and reduce the spray at the falling point. Stacking nearby.
  • a double-split combustion system of a direct-injection diesel engine wherein the fuel injection nozzle sprays high-pressure fuel into a mist-like manner by a cylinder head, a cylinder liner and a piston. In the combustion chamber.
  • the combustion chamber is divided into upper and lower layers, the diameter of the upper layer of the combustion chamber is greater than the diameter D 2 of the lower layer of the combustion chamber, and a spray collision table is provided at the junction of the upper layer of the combustion chamber and the lower layer of the combustion chamber;
  • the misty oil jet sprayed from the injection stage is sprayed onto the spray collision table, and a profile suitable for spray flow is arranged on the spray collision table, a part of the misty oil bundle is rebounded, and a part of the sprayed collision table faces the collision table.
  • the top of the collision and the lower part of the collision table are quickly deployed to achieve double-layer splitting.
  • the spray collision table is composed of a spray collision surface, a spray upper guide surface, and a spray lower guide surface.
  • the structure of the spray collision surface includes a spray collision cone surface, a first upper transition surface, and a first lower transition
  • the structure of the spray collision surface includes a spray collision surface, a second upper transition surface, and a second lower transition surface.
  • the structure of the spray collision surface includes an upper spray collision surface and a lower spray collision surface.
  • the spray upper guiding surface adopts a first upper guiding plane.
  • the spray upper guiding surface adopts a first upper guiding annular surface and a second upper guiding plane.
  • the spray upper guiding surface adopts a first upper guiding annular surface and a second upper guiding annular surface.
  • the spray upper guiding surface adopts an upper guiding annular surface.
  • the spray lower guiding surface adopts a first lower guiding annular surface and a second lower guiding annular surface.
  • the spray lower guiding surface adopts a first lower guiding conical surface and a second lower guiding annular surface.
  • the spray lower guiding surface adopts a third lower guiding annular surface.
  • the first scheme the collision surface is a conical surface; the second scheme: the collision surface is an annular surface; the third scheme: the collision surface is a combination of two conical surfaces.
  • the guiding surface of the upper layer of the double-layer splitting combustion chamber collision table is a plane;
  • the second scheme the guiding surface of the upper layer of the double-layer splitting combustion chamber collision table is a combined surface of a plane and an annular surface.
  • the third scheme The guiding surface of the upper layer of the double-layer splitting combustion chamber collision platform is a combined surface composed of two annular surfaces;
  • the fourth scheme the double-layer splitting combustion chamber collision table The guiding surface of the upper layer is an annular surface.
  • the first scheme the lower guiding surface of the double-layer splitting combustion chamber collision table is composed of two annular surfaces; the second scheme: the lower guiding surface of the double-layer splitting combustion chamber collision table is composed of a conical surface and an annular surface; Solution: The lower guide surface of the double-stage splitter combustion chamber collision table has only one annular surface.
  • the different collision faces of the collision table, the different upper guide faces and the different lower guide faces can be combined to form different types of collision tables.
  • the spray hits the collision table, a part of which is bounced, and a part of which is rapidly diverted to the sides along the upper and lower guide faces of the collision table. Because the spray rapidly splits into the upper and lower layers of the combustion chamber, the spatial extent of the distribution becomes larger, and the air is not close to the wall surface, and the amount of air entrainment is increased, and the air in the upper and lower layers of the combustion chamber can be fully utilized, so that the air can be relatively uniformly formed relatively quickly. Mixture.
  • the beneficial effects of the invention are: the double-split combustion system of the direct injection diesel engine, the porous injector spray
  • the oil beam hits the collision table, a part of the oil beam is rebounded, and a part of the oil beam is rapidly shunted up and down along the guide surface.
  • double-layer splitting the accumulation of spray at and near the drop point is reduced, the diffusion speed is fast, the spatial distribution is wide, and the air entrainment is increased, so that a relatively uniform mixture can be formed relatively quickly, the combustion of the diesel engine is improved, and the economy is improved. Emission performance.
  • the double-phase split combustion system has a 3% reduction in fuel consumption compared to the original combustion system, and the soot emissions have decreased by 50%.
  • Figure 1 is a schematic view showing the structure of a two-stage split combustion system for a direct injection diesel engine.
  • Figure 2 is an enlarged view of a portion A in Figure 1.
  • Figure 3 shows the second collision surface of the collision table.
  • Figure 4 shows the third type of collision surface of the collision table.
  • Figure 5 shows the second upper guide surface of the collision table.
  • Figure 6 shows the third upper guide surface of the collision table.
  • Figure 7 shows the fourth upper guide surface of the collision table.
  • Figure 8 shows the second lower guide surface of the collision table.
  • Figure 9 shows the third lower guide surface of the collision table.
  • a second lower guide annular surface 15, a first upper guide plane, 16, first Upper guiding annular surface, 17, second upper guiding plane, 18, second upper guiding annular surface, 19, upper guiding annular surface, 20, first lower guiding conical surface, 21, third lower guiding annular surface.
  • Figure 1 shows a structural scheme of a two-stage split combustion system for a direct injection diesel engine.
  • the fuel injector 5 sprays the pressurized fuel into the combustion chamber 4 composed of the cylinder head 1, the cylinder liner 2 and the piston 3 in a multi-oil bundle manner, and is provided at the joint portion of the upper and lower layers of the combustion chamber 4.
  • Spray collision table 7. During the injection of the injector, the misty oil jet 6 ejected from the injector is sprayed onto the collision table, and a suitable spray flow is provided on the collision table. Dynamic profile. Some of them are rebounded, and some of them are quickly shunted up and down along the guide surface on the collision table.
  • Figures 2, 3, and 4 show the collision surface scheme for the spray collision table of three double-layer split-flow combustion systems.
  • the misty oil bundle 6 ejected from the injector 5 falls on the spray collision table.
  • the oil beam is rapidly dispersed along the guide on the collision table toward the upper side of the collision table and below the collision table, realizing a two-layer split to form an ideal distribution.
  • FIGS 2, 5, 6, and 7 show the upper guide surface scheme for the four collision tables.
  • FIGS 2, 8, and 9 show the lower guide surface scheme for the three types of collision tables.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Dispersion Chemistry (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

一种直喷式柴油机双层分流燃烧***，喷油嘴（5）以多油束方式把高压燃油以雾状喷入由气缸盖（1）、气缸套（2）和活塞（3）组成的燃烧室（4）中，其特征是：所述燃烧室（4）分成上下两层，燃烧室上层（8）的直径D1大于燃烧室下层（9）的直径D2，在燃烧室上层（8）和燃烧室下层（9）的结合处设有喷雾碰撞台（7）；在所述喷油嘴（5）的主喷油阶段喷出的雾状油束（6）喷射到喷雾碰撞台（7）上，在喷雾碰撞台（7）上设有适合喷雾流动的型面，雾状油束（6）一部分被反弹，一部分沿着喷雾碰撞台（7）的导向面向碰撞台的上方和碰撞台的下方迅速展开，实现双层分流。通过导向分流，减少喷雾在落点及附近的堆积，扩散速度快，空气卷吸量增加，因而能较快地形成相对均匀的混合气，使燃烧迅速和完善。

Description

直喷式柴油机双层分流燃烧***
技术领域
本发明涉及一种直喷式柴油机双层分流燃烧***，其属于发动机混合气形成 和燃烧领域。
背景技术
目前， 直喷式柴油机的过量空气系数大， 却易冒黑烟。 其主要原因是多孔 喷雾在圆周方向上分布不均匀， 以及在喷雾落点处产生过浓区。 一部分喷雾堆 积在落点及附近、 或形成油膜， 另一部分反弹后向四周扩散， 因为紧贴燃烧室 壁， 卷入的空气量少， 而在喷雾的落点处形成过浓区。 这就使得柴油机空气利 用率低， 燃烧不完全， 油耗高、 碳烟排放量大。
发明内容
为了解决多孔喷雾的落点处混合气过浓和燃烧室周向分布不均，以及燃烧室 内空气利用率低的问题。 本发明提供一种直喷式柴油机双层分流燃烧***。 该 双层分流燃烧***减少了活塞顶面和气缸盖底面之间的空间。 喷雾一部分被碰 撞台反弹， 一部分沿着导向面向上下两侧迅速分流， 实现双层分流， 同时使喷 雾实现二次雾化， 提高喷雾雾化性能， 扩大喷雾空间分布范围、 减少喷雾在落 点及附近的堆积。
本发明解决其技术问题所采用的技术方案是： 一种直喷式柴油机双层分流 燃烧***， 喷油嘴以多油束方式把高压燃油以雾状喷入由气缸盖、 气缸套和活 塞组成的燃烧室中。 所述燃烧室分成上下两层， 燃烧室上层的直径 0,大于燃烧 室下层的直径 D2， 在燃烧室上层和燃烧室下层的结合处设有喷雾碰撞台； 在所 述喷油嘴的主喷油阶段喷出的雾状油束喷射到喷雾碰撞台上， 在喷雾碰撞台上 设有适合喷雾流动的型面， 雾状油束一部分被反弹， 一部分沿着喷雾碰撞台的 导向面向碰撞台的上方和碰撞台的下方迅速展开， 实现双层分流。
所述喷雾碰撞台由喷雾碰撞面、 喷雾上导向面和喷雾下导向面组成。
所述喷雾碰撞面的结构包括喷雾碰撞锥面、 第一上过渡曲面和第一下过渡
1
确认本 曲面。
所述喷雾碰撞面的结构包括喷雾碰撞曲面、 第二上过渡曲面和第二下过渡 曲面。
所述喷雾碰撞面的结构包括上喷雾碰撞曲面和下喷雾碰撞曲面。
所述喷雾上导向面采用第一上导向平面。
所述喷雾上导向面采用第一上导向环形面和第二上导向平面。
所述喷雾上导向面采用第一上导向环形面和第二上导向环形面。
所述喷雾上导向面采用上导向环形面。
所述喷雾下导向面采用第一下导向环形面和第二下导向环形面。
所述喷雾下导向面采用第一下导向圆锥面和第二下导向环形面。
所述喷雾下导向面采用第三下导向环形面。
双层分流燃烧室的喷雾碰撞面有三种方案。 第一种方案： 碰撞面为圆锥面； 第二种方案： 碰撞面为环形面； 第三种方案： 碰撞面是由两个圆锥面组合而成。
双层分流燃烧室碰撞台上层的导向面有四种方案。第一种方案： 双层分流燃 烧室碰撞台上层的导向面为平面； 第二种方案： 双层分流燃烧室碰撞台上层的 导向面为平面和环形面组成的组合面。 第三种方案： 双层分流燃烧室碰撞台上 层的导向面为两个环形面组成的组合面； 第四种方案： 双层分流燃烧室碰撞台 上层的导向面为一个环形面。
双层分流燃烧室碰撞台下层的导向面有三种方案。 第一种方案： 双层分流 燃烧室碰撞台的下层导向面为两个环形面组成； 第二种方案： 双层分流燃烧室 碰撞台的下层导向面为圆锥面和环形面组成； 第三种方案： 双层分流燃烧室碰 撞台的下层导向面只有一个环形面。
碰撞台不同的碰撞面、 不同的上层导向面和不同的下层导向面可以进行组 合， 形成不同形式的碰撞台。
燃油喷射过程中， 喷雾撞击到碰撞台上， 一部分被反弹， 一部分沿着碰撞台 的上下导向面迅速向两侧分流。 因为喷雾向燃烧室的上下两层迅速分流， 分布 的空间范围变大， 又不贴近壁面， 空气的卷入量增多， 能充分利用燃烧室上下 两层的空气， 因而能较快地形成相对均匀的混合气。
本发明的有益效果是： 这种直喷式柴油机双层分流燃烧***， 多孔喷油器喷 出的油束撞击到碰撞台上， 油束一部分被反弹， 一部分沿着导向面迅速向上下 两侧分流。 通过双层分流， 减少了喷雾在落点及附近的堆积， 扩散速度快， 空 间分布广， 空气卷吸量增加， 因而能较快地形成相对均匀的混合气， 改善柴油 机燃烧， 提高经济性和排放性能。 在标定工况下， 双层分流燃烧***与原机燃 烧***相比油耗率下降了 3%， 碳烟排放量下降了 50%。
附图说明
下面结合附图和实施例对本发明作进一步说明。
图 1是一种直喷式柴油机双层分流燃烧***的结构示意图。
图 2是图 1 中 A部放大图。
图 3表示碰撞台的第二种碰撞面。
图 4表示碰撞台的第三种碰撞面。
图 5表示碰撞台的第二种上层导向面。
图 6表示碰撞台的第三种上层导向面。
图 7表示碰撞台的第四种上层导向面。
图 8表示碰撞台的第二种下层导向面。
图 9表示碰撞台的第三种下层导向面。
图中： 1、 气缸盖， 2、 气缸套， 3、 活塞， 3a、 活塞顶面， 4、 燃烧室， 5、 喷油器， 6、 雾状油束， 7、 喷雾碰撞台， 8、 燃烧室上层， 9、 燃烧室下层， 10、 喷雾碰撞锥面， 10a、 第一上过渡曲面， 10b、 第一下过渡曲面， 11、 喷雾 碰撞曲面， l la、 第二上过渡曲面， l lb、 第二下过渡曲面， 12a、 上喷雾碰撞曲 面， 12b、 下喷雾碰撞曲面， 13、 第一下导向环形面， 14、 第二下导向环形面， 15、 第一上导向平面， 16、 第一上导向环形面， 17、 第二上导向平面， 18、 第 二上导向环形面， 19、 上导向环形面， 20、 第一下导向圆锥面， 21、 第三下导 向环形面。
具体实施方式
图 1 示出了一种直喷式柴油机双层分流燃烧***的结构方案。 图中， 喷油 嘴 5以多油束方式把髙压燃油以雾状喷入由气缸盖 1、气缸套 2和活塞 3组成的 燃烧室 4中， 在燃烧室 4上下层的结合部设有喷雾碰撞台 7。在喷油嘴的喷射过 程中， 喷油嘴喷出的雾状油束 6 喷射到碰撞台上， 在碰撞台上设有适合喷雾流 动的型面。 一部分被反弹， 一部分沿着碰撞台上的导向面迅速向上下两侧分流。 因为喷雾向燃烧室的上下两层分流， 分布的空间范围变大， 又不贴近壁面， 空 气的卷入量增多。 又因为上层燃烧室的直径较大， 减小了活塞顶 3a与汽缸盖之 间的空间， 能更加充分利用燃烧室上下两层的空气， 因而能较快地形成相对均 匀的混合气。 实验结果表明： 在标定工况下， 双层分流燃烧***与原机燃烧系 统相比， 经济性提高 3%， 碳烟下降 50%。
图 2、 3、 4 示出了三种双层分流燃烧***喷雾碰撞台的碰撞面方案。 在主 喷油阶段， 喷油器 5喷出的雾状油束 6落于喷雾碰撞台上。 油束沿着碰撞台上 的导向面向碰撞台的上方和碰撞台的下方迅速分散， 实现双层分流， 形成理想 分布。
图 2、 5、 6、 7示出了四种碰撞台的上层导向面方案。
图 2、 8、 9示出了三种碰撞台的下层导向面方案。

Claims

1.一种直喷式柴油机双层分流燃烧***， 喷油嘴（5 ) 以多油束方式把高压 燃油以雾状喷入由气缸盖（1 )、 气缸套（2 )和活塞（3 )组成的燃烧室（4)中， 其特征是： 所述燃烧室 （4) 分成上下两层， 燃烧室上层 （8 ) 的直径 大于燃 烧室下层 （9) 的直径 D2， 在燃烧室上层 （8)和燃烧室下层 （9) 的结合处设有 喷雾碰撞台 （7 ); 在所述喷油嘴 （5 ) 的主喷油阶段喷出的雾状油束 （6 ) 喷射 到喷雾碰撞台 （7 ) 上， 在喷雾权碰撞台 （7 ) 上设有适合喷雾流动的型面， 雾状 油束 （6 ) —部分被反弹， 一部分沿着喷雾碰撞台 （7) 的导向面向碰撞台的上 方和碰撞台的下方迅速展开， 实现双层分流； 所述喷雾碰撞台 （7) 由喷雾碰撞 面、 喷雾上导向面和喷雾下导向面组成。
2.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 书
述喷雾碰撞面的结构包括喷雾碰撞锥面 （10)、 第一上过渡曲面 （10a) 和第一 下过渡曲面 (動。
3.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾碰撞面的结构包括喷雾碰撞曲面 （11 )、 第二上过渡曲面 （11a)和第二 下过渡曲面 （l lb)。
4.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾碰撞面的结构包括上喷雾碰撞曲面（12a)和下喷雾碰撞曲面（12b)。
5.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾上导向面采用第一上导向平面（15)。
6.根据权利要求 1 所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾上导向面采用第一上导向环形面 （16 )和第二上导向平面（17)。
7.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾上导向面采用第一上导向环形面（16 )和第二上导向环形面（18)。
8.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾上导向面采用上导向环形面（19)。
9.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾下导向面采用第一下导向环形面 （13)和第二下导向环形面（14)。
5
替換页 （细则第 26条)
10.根据权利要求 1所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾下导向面采用第一下导向圆锥面 （20) 和第二下导向环形面 （14)。
11.根据权利要求 1 所述的直喷式柴油机双层分流燃烧***， 其特征是： 所 述喷雾下导向面采用第三下导向环形面 （21 )。
6
替換页 （细则第 26条)
PCT/CN2013/000574 2012-05-16 2013-05-15 直喷式柴油机双层分流燃烧*** WO2013170632A1 (zh)

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