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    • 9. 发明授权
    • Combustion chamber structure of a gas engine
    • 燃气发动机的燃烧室结构
    • US6073604A
    • 2000-06-13
    • US135801
    • 1998-08-18
    • Kenro Nakashima
    • Kenro Nakashima
    • F02B19/02F02B19/14F02B19/16F02B19/18F02B43/00F02D19/02F02D41/38F02M21/02
    • F02B19/165F02B19/02F02B19/18Y02T10/125
    • In the combustion chamber structure of the gas engine the combustion chamber members are formed with the sub-communication holes allowing communication between the main combustion chambers and the pre-combustion chambers and also with throat holes in which throat hole valves are installed. This structure avoids excessively high compressed air pressure in the main combustion chambers during the compression stroke and reduces the compression work to improve performance. The sub-communication holes open at the wall surfaces situated in the main combustion chambers and also at the upper wall surfaces of the pre-combustion chambers. The axes of the ports of the sub-communication holes opening to the main combustion chambers extend toward the center axes of the throat holes. The axes of the ports of the sub-communication holes opening to the pre-combustion chambers extend offset from the center axes of the pre-combustion chambers. Hence, this gas engine can reduce the compression work, lower the maximum pressure of the compressed air at the end of the compression stroke, prevent the gas fuel from remaining in the pre-combustion chambers, and enhance the air utilization factor, improving thermal coefficient.
    • 在燃气发动机的燃烧室结构中,燃烧室部件形成有允许主燃烧室和预燃烧室之间连通的副连通孔,并且还具有安装有喉孔阀的喉孔。 这种结构避免了在压缩冲程期间主燃烧室中的过高的压缩空气压力,并且减小了压缩工作以提高性能。 子连通孔在位于主燃烧室中的壁表面以及在预燃烧室的上壁表面处打开。 通向主燃烧室的副连通孔的端口的轴线朝向喉孔的中心轴线延伸。 通向预燃室的子连通孔的端口的轴线偏离预燃烧室的中心轴线。 因此,该气体发动机可以减小压缩作用,降低压缩冲程结束时的压缩空气的最大压力,防止气体燃料残留在预燃烧室中,提高空气利用系数,提高热系数 。