发明名称 |
Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction |
摘要 |
A supersonic cruise configuration aircraft comprises a fuselage extending on a longitudinal axis from a forward nose to an aft tail, and a wing coupled at an inboard section to the fuselage and extending to an outboard tip, and having a leading edge and a trailing edge. The aircraft further comprises a landing gear that is coupled to the wing and capable of stowing into the wing and fuselage on retraction. The landing gear has a landing gear strut. The wing is gulled with a dihedral at an angle that is increased inboard and aligns with the retracted landing gear. The wing has a minimum thickness sufficient to enclose the landing gear.
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申请公布号 |
US2005067526(A1) |
申请公布日期 |
2005.03.31 |
申请号 |
US20030655707 |
申请日期 |
2003.09.05 |
申请人 |
SUPERSONIC AEROSPACE INTERNATIONAL, LLC |
发明人 |
QUAYLE BRIAN;MORGENSTERN JOHN M.;ARSLAN ALAN E. |
分类号 |
B64C1/00;B64C3/10;B64C3/16;B64C9/24;B64C25/10;B64C30/00;B64C39/12;B64D27/18;(IPC1-7):B64C15/00 |
主分类号 |
B64C1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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