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특허 상세정보

Aircraft wing

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/42DA ; 244/113
출원번호 US-0632468 (1975-11-17)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 47  인용 특허 : 0
초록

An aircraft wing having a relatively thin airfoil cross section including a main body portion and a plurality of auxiliary airfoil sections disposed at the trailing edge of the wing and movable relative to the main body portion and to one another. In a normal cruise position the auxiliary sections and the main body portion form a complete airfoil having a substantially contiguous and unbroken exterior airfoil surface which preserves the high speed characteristics of the wing. At least two of the auxiliary sections comprising a leading auxiliary section a...

대표
청구항

An aircraft wing comprising in combination a main body portion, a plurality of movable auxiliary sections disposed at the trailing edge of said main body portion, said movable auxiliary sections comprising a leading auxiliary section and a trailing auxiliary section, hinge means operably connecting said auxiliary sections and said main body portion, said hinge means including a fixed hinge member disposed on said main body portion and connecting said leading and trailing auxiliary sections to the main body portion, said leading and trailing auxiliary sec...

이 특허를 인용한 특허 피인용횟수: 47

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  15. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2013108567726.
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  30. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  31. Beyer,Kevin W.; Fox,Stephen J.; Lacy,Douglas S.; Meredith,Paul T.; Prow,Clayton A.; Sakurai,Seiya; Wells,Stephen L.. Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface. USP2007087258308.
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