[특허]Method and apparatus for providing an aircraft emergency safety control system

Method and apparatus for providing an aircraft emergency safety control system 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G05D-001/10 B64C-013/20
출원번호	US-0300141 (2002-11-20)
발명자 / 주소	Langston, James Leland
출원인 / 주소	Raytheon Company
대리인 / 주소	Daly, Crowley & Mofford, LLP.
인용정보	피인용 횟수 : 57 인용 특허 : 0

초록 ▼

대표청구항 ▼

A method and apparatus for providing an Aircraft Emergency Safety Control System (AESCS) capable of regaining control of an aircraft that may have been lost due to incapacitation of the crew includes an airborne segment, a ground segment, and a communications segment wherein control of the aircraft is removed from the control of unauthorized person(s) onboard the aircraft, and the aircraft is directed to a destination that is considered a safe location for the aircraft given it's status, and to facilitate a reasonably safe emergency landing. en the spray gun is positioned in the spray gun receptacle, whereby air is provided through the piston air supply conduit at sufficient pressure to move the insertion portion from the closed position to the open position.5. An apparatus according to claim 1 further comprising an radially extending handle on the body portion for rotating the body portion in the receptacle to effect insertion of the gun assembly in the spray bar.6. An apparatus according to claim 5 further comprising a lock post positioned on the spray bar to provide a stop against which the radially extending handle of the spray gun will abut when the spray gun is fully inserted into the spray bar.7. A spray gun subassembly comprising, in combination: a spray gun subassembly constructed and arranged to be received in a spray gun receptacle having a solution inlet conduit and an atomizing air conduit; the spray gun having a body portion adapted to fit in the receptacle and an insertion portion having a sealable orifice at a spraying end thereof, the body portion having an internal void constructed and arranged to be in fluid communication with the solution inlet conduit and the atomizing air conduit when the spray gun is positioned in the spray gun receptacle and the insertion portion is in an open position; the insertion portion being moveable between an open position defining a passage between the body portion void and the spraying end orifice a closed position sealing the insertion portion against the body portion to close said passage; the spray gun further having a piston received in the body portion, the piston operatively associated with the insertion portion to effect movement of the insertion portion between the open and closed position; the insertion portion being biased to the closed position; and the spray bar further having a piston air supply conduit, the piston air supply conduit being in fluid communication with the piston when the spray gun is positioned in the spray gun receptacle, whereby air is provided through the piston air supply conduit at sufficient pressure to move the insertion portion from the closed position to the open position. 8. An apparatus according to claim 7 further comprising an radially extending handle on the body portion for rotating the body portion in the receptacle to effect insertion of the gun assembly in the spray bar.9. An apparatus according to claim 8 further comprising a lock post positioned on the spray bar to provide a stop against which the radially extending handle of the spray gun will abut when the spray gun is fully inserted into the spray bar.

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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

내보내기 구분	파일저장 인쇄 메일전송
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Method and apparatus for providing an aircraft emergency safety control system 원문보기

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Method and apparatus for providing an aircraft emergency safety control system 원문보기

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연구과제 타임라인

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이 특허를 인용한 특허 (57)

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