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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0426805 (2009-04-20) |
등록번호 | US-8146868 (2012-04-03) |
우선권정보 | FR-08 02211 (2008-04-21) |
발명자 / 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 | 피인용 횟수 : 0 인용 특허 : 13 |
Disclosed is a mast for the suspension of a bypass turbine engine beneath a wing of an aircraft in which the wing has at least one flap. The mast includes a rear fairing that protrudes rearward of a trailing edge of the wing and is mounted so as to tilt in a deployed downward position as the flap is
1. A mast for the suspension of a bypass turbine engine beneath a wing of an aircraft, said wing being furnished with at least one flap and said mast comprising a rear fairing which protrudes rearward relative to a trailing edge of said wing and which is mounted so as to tilt in a deployed downward
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