IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0347381
(1982-02-09)
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발명자
/ 주소 |
- Jenkins Donald S. (Tarzana CA)
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출원인 / 주소 |
- The United States of America as represented by the Secretary of the Air Force (Washington DC 06)
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인용정보 |
피인용 횟수 :
9 인용 특허 :
0 |
초록
▼
A gas generator which is structurally and functionally integrated with a fluid heat exchanger. A liquid which is to be heated, vaporized, and used as pressurized gas is introduced into the integrated apparatus where the liquid absorbs heat from the adjacent, but separated, hot gas flow from the gas
A gas generator which is structurally and functionally integrated with a fluid heat exchanger. A liquid which is to be heated, vaporized, and used as pressurized gas is introduced into the integrated apparatus where the liquid absorbs heat from the adjacent, but separated, hot gas flow from the gas generator. Unlike the prior art, this integrated gas generator/fluid heat exchanger is useable to pressurize an oxidizer tank of a liquid engine missile.
대표청구항
▼
An integrated solid propellant gas generator and fluid heat exchanger, comprising: a. a housing; b. means, within said housing, for encasing a solid propellant therein, wherein this means comprises a casing surrounding said solid propellant, with said casing supported within said housing; c. means f
An integrated solid propellant gas generator and fluid heat exchanger, comprising: a. a housing; b. means, within said housing, for encasing a solid propellant therein, wherein this means comprises a casing surrounding said solid propellant, with said casing supported within said housing; c. means for igniting and burning said solid propellant, thereby generating a hot flow of gas, wherein this means is operably connected to, and is disposed adjacent to an opening of, said solid propellant encasing means; d. means, within said housing, for containing said hot gas flow of said propellant gas and for directing said hot gas flow out of said housing, wherein this means includes: a chamber in which flows said hot gas generated by the burning of said solid propellant; and means, in communication with said chamber, for ducting said hot gas flow of solid propellant gas out of said housing and into machinery capable of utilizing said hot gas flow; e. means for receiving a liquid propellant therein, with said liquid propellant being capable of vaporizing upon absorbing heat from said hot flow of said propellant gas and thereby forming a pressurized gas, wherein this means is disposed within said housing, surrounds said casing, and is located adjacent to said means for containing said said hot flow of solid propellant gas, and wherein said liquid propellant receiving means includes a housing inlet which connects said housing and said liquid propellant receiving means to a source of liquid propellant, and also wherein said liquid propellant receiving means and the external surface of said casing form said chamber in which flows said hot gas generated by the burning of said solid propellant, and further wherein said liquid propellant receiving means defines the flow path of said liquid propellant into, within, and out of said housing, with the flow of said liquid propellant directed by this means such as to be adjacent to and separated from said hot gas flow of burning solid propellant; and f. means, operably connected to said liquid propellant receiving means, for allowing said pressurized gas in said liquid propellant receiving means to exit therefrom and from said housing, wherein said means for allowing said pressurized gas to exit includes a housing outlet connected to machinery which requires pressurized gas.
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