首页> 外国专利> METHOD FOR OPERATING A PISTON PISTON COMBUSTION ENGINE AND PISTON PISTON COMBUSTION ENGINE FOR CARRYING OUT THIS METHOD

METHOD FOR OPERATING A PISTON PISTON COMBUSTION ENGINE AND PISTON PISTON COMBUSTION ENGINE FOR CARRYING OUT THIS METHOD

机译:实施该方法的活塞活塞式燃烧发动机和活塞活塞式燃烧发动机的操作方法

摘要

1. A method of operating a reciprocating-piston internal combustion engine having a combustion chamber (17), in which air is compressed by the stroke of the piston (1), into which fuel is injected through an injection nozzle (4) arranged in alignment with the cylinder axis and in which the fuel and the compressed air form a fuel-air mixture, wherein the combustion chamber (17) includes a toroid-like space (6) disposed in the region of the piston's perimeter and also a trough (8) disposed in the cylinder head (3), and wherein the combustion of the fuel-air mixture takes place in stages, characterized in that the entire quantity of fuel is fed - shortly prior to the piston (1) reaching its top dead-centre during the ignition lag - into the trough (8) and forms a rich mixture therein, that, when the piston (1) has reached a position in the region of its top dead-centre, the only link between the trough (8) and the toroid-like space (6) is the one provided by the smallest essentially required piston clearance (11), that the fuel-air mixture is ignited during the first stage at a predeterminable ignition point in the trough (8) so that a flame front moves during the second stage through the rich mixture which, as a result thereof, expands and intensifies a radially outwardly directed squeezed stream from the trough (8), that the partly burnt mixture reaches during the third stage the toroid-like space (6) which, due to its particular shape, causes the mixture to be whirled, that combustion with a surplus of oxygen continues in this whirl, and in that the combustion gas flows during the fourth stage as a squeeze-relieving stream from the whirl into the - by the piston's downward stroke - expanding volume towards the ignition point and thus terminates the combustion.
机译:1.一种操作具有燃烧室(17)的往复式活塞内燃机的方法,其中,空气通过活塞(1)的冲程而被压缩,燃料通过布置在该燃烧室中的喷嘴(4)被喷射到该燃烧室中。燃烧室(17)包括一个环形空间(6),该空间设置在活塞周边区域内,并且还包括一个槽( 8)布置在汽缸盖(3)中,其中燃料-空气混合物的燃烧是分阶段进行的,其特征在于,在活塞(1)到达其上止点之前不久就输送了全部燃料。在点火滞后期间居中-进入凹槽(8)并在其中形成丰富的混合物,这样,当活塞(1)到达其上止点区域时,凹槽(8)之间的唯一连接环形空间(6)是由最小的基本要求提供的空间红色的活塞间隙(11),表示在第一阶段在槽(8)中的预定点火点处点燃了燃油-空气混合物,从而使火焰前锋在第二阶段通过浓混合物移动,其结果是,膨胀并增强了来自水槽(8)的径向向外挤压的水流,部分燃烧的混合物在第三阶段到达环形空间(6),由于其特殊的形状,导致混合物旋转,在此涡流中继续有多余的氧气燃烧,并且在第四阶段,燃烧气体以从涡流进入的挤压释放流的形式(通过活塞的向下冲程)向点火点扩展,从而终止了燃烧。燃烧。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号