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특허 상세정보

Aerofoil member

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/52    B64C-003/48    H01L-041/09   
미국특허분류(USC) 244/219; 244/201; 244/215; 244/123.1; 244/123.6
출원번호 US-0480223 (2009-06-08)
등록번호 US-8186631 (2012-05-29)
우선권정보 GB-0624580.7 (2006-12-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cooper Legal Group LLC
인용정보 피인용 횟수 : 8  인용 특허 : 17
초록

An aerofoil member is described which provides for a ‘smart Core’and flexible skin. The core comprises sheet material elements forming adjoining cells. The length of the elements can be changed, for example, using the piezo-electric effect, to alter the cross-sectional shape of the aerofoil without changing the peripheral length. Thus, the shape of the aerofoil may be changed to suit different flight conditions, or to mimic the effect of control surfaces.

대표
청구항

1. An aerofoil member, comprising a flexible outer skin supported by an inner structural core, the core comprising a plurality of sheet material elements joined together to form a matrix of adjoining cells, at least one of the elements comprising an actuator actuable to adjust at least one of a size or shape of at least one of the elements and adjust a cross-sectional shape of the aerofoil member, at least one of the elements at a periphery of the core joined to the skin. 2. The aerofoil member of claim 1, at least one of the elements formed of piezo-ele...

이 특허에 인용된 특허 (17)

  1. Kari Appa. Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression. USP2002046375127.
  2. Breitbach Elmar J.,DEX ; Bein Thilo,DEX. Actuator with a triggerable element of variable length made of a multifunctional element. USP1999045891577.
  3. Kota,Sridhar; Hetrick,Joel A.. Adaptive compliant wing and rotor system. USP2008067384016.
  4. Gruenewald Michael,DEX ; Moeser Clemens,DEX ; Steigenberger Josef,DEX ; Mueller Guenther,DEX. Adaptive flow body. USP2001086276641.
  5. Reinhard Andreas,CHX ; To Frederick E.,CHX ; Ramseier Otto,CHX ; Kammer Res,CHX. Adaptive pneumatic wing for fixed wing aircraft. USP2001036199796.
  6. Campanile Lucio Flavio,DEX ; Hanselka Holger,DEX. Aerodynamic structure, for a landing flap, an airfoil, an elevator unit or a rudder unit, with a changeable cambering. USP2000016010098.
  7. Orrison William W. (900 NE. Loop 410 ; Suite E-103 San Antonio TX 78209). Air foil with reversible camber. USP1982074341176.
  8. Dittrich,Kay. Cellular actuator device and methods of making and using same. USP2006067055782.
  9. Hagood ; IV Nesbitt W. ; Bent Aaron A.. Composites for structural control. USP1999025869189.
  10. Dittrich, Kay W.. Cover skin for a variable-shape aerodynamic area. USP2011037896294.
  11. Dorsett Kenneth Merle ; Stewart Christopher Sean. Inflatable structures to control aircraft. USP2000016015115.
  12. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  13. Perez, Juan. Mechanism for at least regionally adjusting the curvature of airfoil wings. USP2003116644599.
  14. Elzey, Dana M.; Wadley, Haydn N. G.. Reversible shape memory multifunctional structural designs and method of using and making the same. USP2010037669799.
  15. Appa Kari. Seamless mission adaptive control surface. USP1999035887828.
  16. Mueller Dietmar,DEX ; Schuermann Helmut,DEX. Skin-rib structure. USP2001016173925.
  17. Voglsinger, Martin; Perez-Sanchez, Juan. Wing, in particular airfoil of an aircraft, with a variable profile shape. USP2011047918421.