发明名称 Hot gas control system
摘要 A hot gas control system includes a pressure vessel defining a chamber in which is disposed a body of solid propellant material that has a leading portion and a trailing portion. A first layer of the body of solid propellant material extends between the leading portion and an intermediate region of the body of solid propellant material, and a second layer extends between the intermediate region and the trailing portion of the body of solid propellant material. The first layer is composed of a first propellant composition that produces a relatively clean gas, and the second layer is composed of a second propellant composition that produces a relatively less clean gas. The body of solid propellant is arranged to burn within the chamber from the leading portion toward the trailing portion and thereby produce a quantity of gas that passes through an outlet port to a ducting path, the first layer having a thickness sufficient to produce enough relatively clean gas to preheat the ducting structure and thereby inhibit contaminant accumulation due to the withdrawal of heat from the less clean gas.
申请公布号 US4807529(A) 申请公布日期 1989.02.28
申请号 US19870118375 申请日期 1987.11.06
申请人 FORD AEROSPACE & COMMUNICATIONS CORPORATION 发明人 FRAZER, ALSON C.
分类号 B01J7/00;C06D5/00;(IPC1-7):C06B45/00 主分类号 B01J7/00
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