公开(公告)号：US3809027A

公开(公告)日：1974-05-07

申请号：US22973872

申请日：1972-02-28

申请人： BRUNSWICK CORP

发明人： MORGAN E

IPC分类号： F02B15/00 ,  F02B3/06 ,  F02B19/04 ,  F02B75/02 ,  F02F1/22 ,  F02M23/12 ,  F02M39/00 ,  F02M67/00

CPC分类号： F02F1/22 ,  F02B3/06 ,  F02B19/04 ,  F02B2075/025 ,  F02B2720/253 ,  F02M67/00 ,  Y02T10/125

摘要： An improved self-injection reciprocating diesel or stratified charge type engine which utilizes pressure in the cylinder to air inject fuel into an adjacent combustion chamber. The combustion chamber and the cylinder space are connected by three separate passages, a small fuel passage, a primary air passage, and a secondary air passage, the secondary air passage being smaller than the primary but considerably larger than the fuel passage. Fuel is delivered by pump pressure to the fuel passage well before top dead center of the piston. As the piston approaches top dead center, it blocks the primary air passage; the resulting rapid pressure increase in the cylinder over that in the combustion chamber causes air from the cylinder to flow through the secondary air passage and create a swirl in the combustion chamber, and air to flow through the fuel passage which atomizes part and ejects the remainder of the fuel onto the wall of the combustion chamber from where it evaporates and burns. The secondary air passage, subsequent to the blocking of the primary air passage, provides the flow path for most of the air flowing from the cylinder to the combustion chamber and hence, controls the pressure differential between the cylinder and combustion chamber. Because the fuel passage is substantially smaller than the secondary air passage, it may be cooled without excessive heat losses and at the same time prevent premature evaporation and decomposition of the fuel. This separation and function of the secondary air and fuel passages in combination with selfinjection, swirl creation in the combustion chamber, initial atomization of a small fraction of the fuel, and surface deposition of most of the fuel followed by evaporation are the distinguishing features of this invention.

摘要翻译： 改进的自喷式往复式柴油或分层充气式发动机，其利用气缸中的压力将燃料喷射到相邻的燃烧室中。 燃烧室和气缸空间通过三个单独的通道，小燃料通道，一次空气通道和二次空气通道相连接，二次空气通道小于主要空气通道，但大大大于燃料通道。 在活塞的上止点之前，燃油通过井筒压力输送到燃油通道。 当活塞接近上止点时，它阻塞主空气通道; 气缸中的燃烧室内的快速压力增加导致来自气缸的空气流过二次空气通道并在燃烧室中产生涡流，并且空气流过燃料通道，雾化部分并喷射其余部分 的燃料到燃烧室的壁上，从那里它蒸发和燃烧。 二次空气通道在一次空气通道的堵塞之后为从气缸流向燃烧室的大部分空气提供流路，因此控制气缸和燃烧室之间的压力差。 因为燃料通道基本上小于二次空气通道，所以它可以被冷却而没有过多的热损失，并且同时防止燃料的过早蒸发和分解。 二次空气和燃料通道的分离和功能与自喷射，燃烧室中的涡流产生，燃料的一小部分的初始雾化以及大部分燃料的表面沉积随后蒸发相结合是区别特征 的本发明。

公开(公告)号：US3804114A

公开(公告)日：1974-04-16

申请号：US22973672

申请日：1972-02-28

申请人： BRUNSWICK CORP

发明人： MORGAN E

IPC分类号： F16K15/02 ,  F16K15/12

CPC分类号： F16K15/12 ,  Y10T137/7856 ,  Y10T137/786 ,  Y10T137/7938

摘要： A low inertia, rapid response, low volume check valve utilizes two body members positioned in end-to-end alignment. The valve bodies have end faces which are clamped into sealing engagement with each other. A shallow cylindrical chamber is formed in one of the end faces and carries a very thin, disc like valve closure member which floats between a closed position against the face of the inlet body and an open position against the face of the outlet body. The closure member is relieved to permit fluid flow therearound and into depressions in the face of the outlet body. Preferably the outlet passage is formed by stainless steel tubing such as hypodermic tubing carried in the outlet body to provide an inexpensive outlet passage with a minimum of contained volume.

摘要翻译： 低惯量，快速响应，体积小的止回阀利用位于端对端对准中的两个主体构件。 阀体具有彼此密封接合的端面。 在一个端面中形成浅圆柱形室，并且承载非常薄的盘状阀闭合构件，其在相对于入口主体的表面的关闭位置和相对于出口主体的表面的打开位置之间漂浮。 封闭构件被释放以允许流体在其周围流动并且在出口体的表面处形成凹陷。 优选地，出口通道由不锈钢管形成，例如承载在出口本体中的皮下注射管，以提供具有最小容纳体积的便宜的出口通道。