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114 条记录 (耗时 0.023 秒)

    Device for feeding natural compressed gas to a diesel engine
    14.
    发明授权
    Device for feeding natural compressed gas to a diesel engine 失效
    将天然压缩气体送入柴油发动机的装置

    公开(公告)号：US06250261B1

    公开(公告)日：2001-06-26

    申请号：US09514175

    申请日：2000-02-28

    申请人： Hector Francisco Santarossa

    发明人： Hector Francisco Santarossa

    IPC分类号： F02M2104

    CPC分类号： F02M21/042 ,  F02B1/04 ,  F02B3/06 ,  F02B43/00 ,  F02B69/00 ,  F02M21/0215 ,  F02M21/029 ,  Y02T10/32

    摘要： Diesel engine conversion kit wherein said kit arranged at the engine air inlet of a diesel engine to be transformed, comprises three different pieces defining an air inlet means, gas feeding means and flux regulating means. Said air inlet means comprises a hollow cylindrical piece with a central narrowed position affixed to said gas feeding means. Said gas feeding means comprises passages whose arrangement coincides with the arrangement of the above cited inlet. Inside said passages feeding gas tubes including long gas exit grooves, are lodged. Finally said flux regulating means comprises a plate with two feeding passages in coincidence with the above cited passages of gas feeding means, each including choker plates with a common regulating means.

    摘要翻译： 柴油发动机转换套件，其中所述套件布置在要变形的柴油发动机的发动机空气入口处，包括限定空气入口装置，气体供给装置和通量调节装置的三个不同的部件。 所述空气入口装置包括中空圆柱形件，其具有固定到所述气体供给装置的中心变窄位置。 所述气体供给装置包括与上述引入口的布置重合的通道。 在包括长气体出口槽的气体管道的所述通道内部被放置。 最后，所述助焊剂调节装置包括具有两个进料通道的板，所述进料通道与上述引气通道一致，每个进料装置包括具有共同调节装置的砧板。

    Apparatus and method for converting conventionally fueled engines to operate on an alternative fuel
    15.
    发明授权
    Apparatus and method for converting conventionally fueled engines to operate on an alternative fuel 失效
    用于转换常规燃油发动机以替代燃料进行操作的装置和方法

    公开(公告)号：US5150685A

    公开(公告)日：1992-09-29

    申请号：US758894

    申请日：1991-09-11

    申请人： Fred C. Porter ,  Garth J. Schultz

    发明人： Fred C. Porter ,  Garth J. Schultz

    IPC分类号： F02B1/04 ,  F02B69/00 ,  F02D19/02 ,  F02D35/00 ,  F02D41/30 ,  F02M21/02

    CPC分类号： F02M21/029 ,  F02B69/00 ,  F02D19/024 ,  F02D19/027 ,  F02D35/00 ,  F02D41/30 ,  F02M21/0254 ,  F02B1/04 ,  F02D2200/0606 ,  F02M21/0278 ,  Y02T10/32

    摘要： An apparatus and method for converting a fuel injected internal combustion engine normally operated with a conventional fuel such as gasoline to operate with an alternative fuel are disclosed. The apparatus comprises an alternative fuel introduction assembly having at least one alternative fuel injector, a temperature sensor, and an electronic translator. The electronic translator is adapted to receive conventional fuel injector control signals generated by an electronic control module, and to receive an output signal from the temperature sensor. The electronic translator then calculates an alternative fuel injector control signal to facilitate the supply of a required energy amount of the alternative fuel. The calculation is based upon the energy content of the alternative fuel, the temperature of the alternative fuel, and the flow and operating characteristics of the alternative fuel injector relative to a conventional fuel injector. Preferably, the alternative fuel is natural gas.

    摘要翻译： 公开了一种用于将通常用常规燃料（例如汽油）操作的燃料喷射内燃机转换为用替代燃料操作的装置和方法。 该装置包括具有至少一个备选燃料喷射器，温度传感器和电子转换器的替代燃料引入组件。 电子转换器适于接收由电子控制模块产生的常规燃料喷射器控制信号，并接收来自温度传感器的输出信号。 电子转换器然后计算替代燃料喷射器控制信号，以便于供应所需能量的替代燃料。 该计算基于替代燃料的能量含量，替代燃料的温度，以及替代燃料喷射器相对于常规燃料喷射器的流动和操作特性。 优选地，替代燃料是天然气。

    SPLIT-CYCLE AIRCRAFT ENGINE
    17.
    发明申请
    SPLIT-CYCLE AIRCRAFT ENGINE 审中-公开

    公开(公告)号：US20090255491A1

    公开(公告)日：2009-10-15

    申请号：US12366048

    申请日：2009-02-05

    申请人： Clifford D. Heaton

    发明人： Clifford D. Heaton

    IPC分类号： F02B75/22 ,  F02B25/00

    CPC分类号： F01B17/025 ,  B64D27/24 ,  B64D2027/026 ,  F02B59/00 ,  F02B69/00 ,  Y02T50/44 ,  Y02T50/64

    摘要： A split-cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.

    SPLIT-CYCLE AIRCRAFT ENGINE
    18.
    发明申请
    SPLIT-CYCLE AIRCRAFT ENGINE 审中-公开

    公开(公告)号：US20090145129A1

    公开(公告)日：2009-06-11

    申请号：US12370644

    申请日：2009-02-13

    申请人： Clifford D. Heaton

    发明人： Clifford D. Heaton

    IPC分类号： F01B29/04 ,  B64C3/34

    CPC分类号： F01B17/025 ,  B64D27/24 ,  B64D2027/026 ,  F02B59/00 ,  F02B69/00 ,  Y02T50/44 ,  Y02T50/64

    摘要： A split-cycle aircraft engine includes a crankshaft rotatable about a crankshaft axis. A power piston is slidably received within a power cylinder and is operatively connected to the crankshaft such that the power piston reciprocates through an expansion stroke and an exhaust stroke during a single rotation of the crankshaft. A compression piston is slidably received within a compression cylinder and is operatively connected to the crankshaft such that the compression piston reciprocates through an intake stroke and a compression stroke during a single rotation of the crankshaft. A gas crossover passage operatively interconnects the compression cylinder and the power cylinder. An air reservoir is operatively connected to the gas crossover passage by a reservoir passage. The air reservoir is selectively operable to receive and deliver compressed air. The engine is mounted to an aircraft and the air reservoir is disposed within the aircraft.