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특허 상세정보

Four engine VTOL aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-015/12    B64D-027/00   
미국특허분류(USC) 244/56 ; 244/55 ; 244/124 ; 244/125
출원번호 US-0713504 (1991-06-12)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 25  인용 특허 : 0
초록

A VTOL aircraft has a first engine nacelle mounted under the wing on one side of the fuselage and houses two of the aircraft engines. The first engine nacelle is mounted in close proximity with the fuselage. A second engine nacelle is mounted under the wing on the opposite side of the fuselage from the first nacelle and houses the remaining two engines. The second engine nacelle is mounted in close proximity with the fuselage. The first and second nacelles are movable from positions parallel to the wing for normal flight to positions perpendicular to the...

대표
청구항

A VTOL aircraft having a fuselage and a wing on said fuselage, said aircraft comprising aircraft power means; a first engine nacelle mounted under said wing on one side of said fuselage and housing part of said aircraft power means, said first engine nacelle being mounted in close proximity with said fuselage; and a second engine nacelle mounted under said wing on the opposite side of said fuselage from said first nacelle and housing an additional part of said aircraft power means, said second engine nacelle being mounted in close proximity with said fus...

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