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특허 상세정보

Hybrid missile propulsion system with reconfigurable multinozzle grid

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/00   
미국특허분류(USC) 060/771; 060/770; 060/767; 060/253
출원번호 US-0044227 (2008-03-07)
등록번호 US-8117847 (2012-02-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle & Sklar, LLP
인용정보 피인용 횟수 : 2  인용 특허 : 50
초록

A propulsion system, such as for use in a missile, includes a multinozzle grid having a pair of plates that are separably mechanically coupled together. When coupled together in a first configuration, the plates provide multiple nozzles in a first nozzle configuration (geometry). Separation of the plates, such as by separating an aft plate from a forward plate that remains with the missile, reconfigures the multinozzle grid to a second configuration that has nozzles in a second nozzle configuration (geometry). The nozzle configurations may be suitable fo...

대표
청구항

1. A hybrid propulsion system comprising: a solid rocket motor;a ramjet; anda reconfigurable multinozzle grid;wherein the solid rocket motor and the ramjet both pass pressurized gas through the reconfigurable multinozzle grid;wherein the multinozzle grid includes: a forward plate; andan aft plate;wherein the plates are separably mechanically coupled together;wherein, when the plates are mechanically coupled together, the plates define a plurality of converge-diverge nozzles each having a first configuration;wherein, when the plates are separated, the noz...

이 특허에 인용된 특허 (50)

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