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公开(公告)号：US06189315B1
公开(公告)日：2001-02-20
申请号：US09350412
申请日：1999-06-18
IPC分类号： F02K942
摘要： A gas generator and ignitor assembly for powering a turbine of a turbopump assembly for a rocket engine comprises an injector and a combustion chamber, the injector having a body member including a fuel inlet and an oxidizer inlet spaced one from the other and communicating with respective radially spaced apart annular members in the body member. Three annuli communicate with the fuel inlet and two annuli communicate with the oxidizer inlet, the annuli which communicates with the oxidizer being positioned between pairs of the other annuli. The body member is enclosed by a plate having an array of bores arranged in two series with three radially spaced apart groups of circular rows in each series. The outer series has 28 groups of triplet bores while the inner series has 14 groups of triplet bores. The annuli which communicate with oxidizer feed bores of each series that are between the other bores of a triplet, the latter bores communicating with annuli that communicate with fuel. The inner and outer bores of the triplets of each series are inclined relatively to each other and to the third bore of the triplet so that fuel and oxidizer atomizes as it is sprayed into the inlet of the combustion chamber where the propellants are mixed, and burned. The burning of the propellants is effected by ignition of a plug of solid propellant fuel mounted to communicate with the interior of the combustion chamber.
摘要翻译： 用于为涡轮发动机的涡轮泵组件的涡轮机供电的气体发生器和点火器组件包括喷射器和燃烧室，所述喷射器具有主体构件，该主体构件包括彼此间隔开并与径向相连的燃料入口和氧化剂入口 间隔开的环形构件在主体构件中。 三个环与燃料入口连通，两个环与氧化剂入口连通，与氧化剂连通的环与位于另一个环之间。 主体部件由具有排列成两个系列的孔阵列的板包围，每个系列具有三个径向间隔开的圆形排的组。 外部系列具有28组三重孔，而内部系列具有14组三重孔。 与三联体的其他孔之间的每个系列的氧化剂进料孔进行通气的环路，后者孔与与燃料连通的环路连通。 每个系列的三联体的内孔和外孔相对于彼此倾斜并相对于三联体的第三孔倾斜，使得燃料和氧化剂在其被喷射到燃烧室的入口处时雾化，其中推进剂被混合并燃烧 。 推进剂的燃烧通过点燃安装成与燃烧室内部连通的固体推进剂燃料的塞子来实现。
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