基本信息:
- 专利标题: LARGE BORE FUEL SYSTEM AND FUEL INJECTOR FOR SAME
- 专利标题(中):大孔燃料系统和相同的燃料喷射器
- 申请号:PCT/US2011045817 申请日:2011-07-29
- 公开(公告)号:WO2012016102A2 公开(公告)日:2012-02-02
- 发明人: HANSON CHRISTOPHER D , LEWIS STEPHEN , MOHAMMED QURSHEED HUSSAIN
- 申请人: CATERPILLAR INC , HANSON CHRISTOPHER D , LEWIS STEPHEN , MOHAMMED QURSHEED HUSSAIN
- 专利权人: CATERPILLAR INC,HANSON CHRISTOPHER D,LEWIS STEPHEN,MOHAMMED QURSHEED HUSSAIN
- 当前专利权人: CATERPILLAR INC,HANSON CHRISTOPHER D,LEWIS STEPHEN,MOHAMMED QURSHEED HUSSAIN
- 优先权: US84738610 2010-07-30
- 主分类号: F02M41/00
- IPC分类号: F02M41/00 ; F02D19/06 ; F02M53/04 ; F02M55/02 ; F02M61/16
摘要:
A low leakage large bore fuel system (10) includes a common rail (16) fluidly connected to at least one of a source of heavy fuel oil (12) and a source of distillate diesel fuel (14). A plurality of fuel injectors (30) are fluidly connected to the common rail (16) and each include a cooling inlet (35) and a cooling outlet (36). Each fuel injector (30) also includes an electrical actuator (40) coupled to a direct operated nozzle check valve by a pilot valve member (41) and a control valve member (45). Fuel leakage is reduced between injection events by equalizing pressures in a pilot control chamber (63) and an intermediate control chamber (62) that are separated by a guide surface of the control valve member (45). Also, between injection events the pilot valve member (41) blocks a drain outlet (37) from a common rail inlet (33) of the fuel injector (30).
摘要(中):
低泄漏大孔燃料系统(10)包括与重质燃料油源(12)和馏分柴油燃料源(14)中的至少一个流体连接的共轨(16)。 多个燃料喷射器(30)流体连接到共轨(16)并且每个包括冷却入口(35)和冷却出口(36)。 每个燃料喷射器(30)还包括通过导阀构件(41)和控制阀构件(45)联接到直接操作的喷嘴止回阀的电致动器(40)。 通过均衡由控制阀构件(45)的引导表面分离的先导控制室(63)和中间控制室(62)中的压力,在喷射事件之间减少燃料泄漏。 而且,在喷射过程之间,先导阀构件(41)阻塞排出口(37)与燃料喷射器(30)的共轨入口(33)。
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F02 | 燃烧发动机;热气或燃烧生成物的发动机装置 |
----F02M | 一般燃烧发动机可燃混合物的供给或其组成部分 |
------F02M41/00 | 由一个共同压力源通过分配器依次向两个或更多个喷射器供料的燃料喷射装置 |