会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 2. 发明申请
    • INTERNAL COMBUSTION ENGINE WITH PILOT AND MAIN INJECTION
    • 内燃机与引导和主注射
    • US20160298530A1
    • 2016-10-13
    • US15188378
    • 2016-06-21
    • Pratt & Whitney Canada Corp.
    • Edwin SCHULZJean THOMASSIN
    • F02B19/10F02M55/02F02B53/10
    • F02B19/108F01C1/22F02B53/10F02M55/025Y02T10/125Y02T10/17
    • An internal combustion engine with at least two movable bodies each being sealingly and movably received within a respective internal cavity to define at least one combustion chamber of variable volume. A pilot fuel injector and a main fuel injector are provided for each movable body. A first chamber of a common rail is in fluid communication with each main fuel injector, and a second chamber of the common rail in fluid communication with each pilot fuel injector. A first metering or pressure regulating valve is in fluid communication with the first chamber. A second metering or pressure regulating valve provides selective fluid communication between the first and second chambers; the metering or pressure regulating valves are settable at different pressure values from one another. The movable bodies may be reciprocating pistons. A method of combusting fuel in an internal combustion engine is also provided.
    • 具有至少两个可移动体的内燃机各自密封地且可移动地容纳在相应的内腔内,以限定至少一个具有可变体积的燃烧室。 为每个可移动体设置了先导燃料喷射器和主燃料喷射器。 共轨的第一室与每个主燃料喷射器流体连通,并且共轨的第二室与每个引燃燃料喷射器流体连通。 第一计量或压力调节阀与第一腔室流体连通。 第二计量或压力调节阀在第一和第二腔室之间提供选择性的流体连通; 计量或压力调节阀可以彼此设定在不同的压力值。 可移动体可以是往复活塞。 还提供了一种在内燃机中燃烧燃料的方法。
    • 5. 发明申请
    • ROTARY INTERNAL COMBUSTION ENGINE WITH REMOVABLE SUBCHAMBER INSERT
    • 旋转式内燃机带有可拆卸的底座插件
    • US20160252010A1
    • 2016-09-01
    • US15153277
    • 2016-05-12
    • Pratt & Whitney Canada Corp.
    • Bruno VILLENEUVEEdwin SCHULZ
    • F02B53/04F02B55/16F02B53/10
    • A rotary engine having an outer body having an internal cavity with a peripheral wall having an insert opening defined therethrough in communication with the internal cavity, and a plurality of coolant passages defined through the peripheral wall in proximity of the insert opening, a rotor body rotatable within the internal cavity, and an insert removably received in the insert opening of the peripheral wall, the insert having a subchamber defined therein communicating with the internal cavity, with a minimum width of the insert opening being at least 0.75 inches. An outer body for a rotary engine and a method of inspecting in an internal cavity in an outer body of a rotary engine are also discussed; also, a rotary engine including a fuel injector having a tip received in the injector hole of the peripheral wall without protruding in the insert opening.
    • 一种旋转发动机,其具有内部空腔,所述外部主体具有外围壁,所述外部壁具有与所述内部空腔相连通的所述插入开口,以及限定在所述插入开口附近的所述周壁的多个冷却剂通道, 在内部空腔内,以及可移除地容纳在周壁的插入开口中的插入件,插入件具有限定在其中的与室内连通的子室,插入开口的最小宽度为至少0.75英寸。 还讨论了用于旋转发动机的外体和在旋转发动机的外体中的内腔中检查的方法; 还有一种旋转发动机,其包括燃料喷射器,其具有容纳在周壁的喷射器孔中的尖端,而不突出在插入开口中。
    • 6. 发明申请
    • INTERNAL COMBUSTION ENGINE WITH PILOT AND MAIN INJECTION
    • 内燃机与引导和主注射
    • US20140261293A1
    • 2014-09-18
    • US13796216
    • 2013-03-12
    • PRATT & WHITNEY CANADA CORP.
    • Edwin SCHULZJean THOMASSIN
    • F02B53/10
    • F02B19/108F01C1/22F02B53/10F02M55/025Y02T10/125Y02T10/17
    • An internal combustion engine with at least two rotatable bodies each defining at least one combustion chamber of variable volume and, for each rotatable body: a pilot subchamber, a pilot fuel injector having a tip in communication with the pilot subchamber, an ignition element positioned to ignite fuel within the pilot subchamber, and a main fuel injector spaced apart from the pilot fuel injector. The engine includes a common first fuel conduit in fluid communication with each main fuel injector, and a common second fuel conduit in fluid communication with each pilot fuel injector. First and second pressure regulating mechanisms which are settable at different pressure values from one another respectively regulate a fuel pressure in the first and second conduits. A method of combusting fuel in an internal combustion engine is also provided.
    • 一种具有至少两个可旋转体的内燃机,每个至少两个旋转体限定至少一个具有可变体积的燃烧室,并且对于每个可旋转体,导引子室,具有与导向子室连通的尖端的引燃燃料喷射器,点火元件, 在飞行员子舱内点燃燃料,以及与引燃燃料喷射器间隔开的主燃料喷射器。 发动机包括与每个主燃料喷射器流体连通的公共第一燃料管道,以及与每个引燃燃料喷射器流体连通的公共第二燃料管道。 可在彼此不同压力值下设定的第一和第二压力调节机构分别调节第一和第二管道中的燃料压力。 还提供了一种在内燃机中燃烧燃料的方法。