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    Turbine engine with solid fuel starter
    1.
    发明授权
    Turbine engine with solid fuel starter 有权
    具有固体燃料起动器的涡轮发动机

    公开(公告)号：US06374592B1

    公开(公告)日：2002-04-23

    申请号：US09612162

    申请日：2000-07-07

    申请人： John William Box ,  Alberto Francisco Araujo

    发明人： John William Box ,  Alberto Francisco Araujo

    IPC分类号： F02C726

    CPC分类号： F02C7/264 ,  F23R5/00

    摘要： A quantity of solid fuel is attached to the inside of the combustion chamber of the turbine. When the engine begins a starting sequence, a starter begins spinning the compressor and an air flow is pumped through the engine. The solid fuel is then heated by a heater element until the solid fuel begins to burn. The combustion of the solid fuel increases the temperature of the combustion chamber so that when, thereafter, an atomized or vaporized liquid fuel is injected, the temperature within the combustion chamber is sufficient to allow the liquid fuel to burn in a self-sustaining manner.

    摘要翻译： 一定数量的固体燃料附着在涡轮机的燃烧室的内部。 当发动机开始起动顺序时，起动器开始旋转压缩机，空气流被泵送通过发动机。 固体燃料然后被加热元件加热直到固体燃料开始燃烧。 固体燃料的燃烧增加了燃烧室的温度，使得当其后注入雾化或蒸发的液体燃料时，燃烧室内的温度足以允许液体燃料以自维持的方式燃烧。

    Solid fuel afterburner and method of using the same to improve thrust and starting capabilities of a turbojet engine
    4.
    发明授权
    Solid fuel afterburner and method of using the same to improve thrust and starting capabilities of a turbojet engine 有权
    固体燃料加力燃烧器及其使用方法来改善涡轮喷气发动机的推力和起动能力

    公开(公告)号：US06370861B1

    公开(公告)日：2002-04-16

    申请号：US09612161

    申请日：2000-07-07

    申请人： John William Box

    发明人： John William Box

    IPC分类号： F02C1310

    CPC分类号： F02K3/10 ,  F02C7/26 ,  F02K9/08 ,  F02K9/74

    摘要： A turbojet engine includes a housing having a forward inlet nozzle, an aft exhaust nozzle, a combustion chamber therebetween, a compressor between the inlet nozzle and the combustion chamber, and a turbine between the combustion chamber and the exhaust nozzle. A liquid fuel injector is provided to inject atomized or vaporized fuel into the chamber for combustion therein. In addition, a solid fuel is provided in the aft exhaust nozzle. The solid fuel may be used to assist the starting of the engine, particularly useful under adverse starting conditions. That is, when the compressor begins to spin up to pump air through the engine, the solid fuel in the exhaust nozzle is ignited by an igniter which begins to combust with the oxygen rich air introduced by the compressor. This combustion increases the temperature in the entire engine, such that when liquid fuel is injected in the combustion chamber, the temperature is sufficiently high to allow the liquid fuel to burn in a self-sustaining manner. Thus, the engine is ignited from the back, and after ignition, the solid fuel continues to burn providing an afterburner effect boosting the thrust until the solid fuel is depleted. Alternatively, the solid fuel can be ignited after the liquid fuel is undergoing a self-sustained burn to provide an afterburner effect.

    摘要翻译： 涡轮喷气发动机包括具有正向入口喷嘴，后排气喷嘴，其间的燃烧室，入口喷嘴和燃烧室之间的压缩机以及燃烧室和排气喷嘴之间的涡轮机的壳体。 提供液体燃料喷射器以将雾化的或蒸发的燃料喷射到室中以在其中燃烧。 此外，在后排气喷嘴中设置固体燃料。 可以使用固体燃料来辅助发动机起动，在不利的起动条件下特别有用。 也就是说，当压缩机开始旋转以泵送空气通过发动机时，排气喷嘴中的固体燃料被开始与由压缩机引入的富氧空气燃烧的点火器点燃。 这种燃烧增加了整个发动机的温度，使得当液体燃料被喷射到燃烧室中时，温度足够高以允许液体燃料以自维持的方式燃烧。 因此，发动机从后部点燃，并且在点燃之后，固体燃料继续燃烧，提供加力作用，促进推力直到固体燃料耗尽。 或者，固体燃料可以在液体燃料经历自身持续燃烧之后被点燃以提供加力燃烧效应。