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특허 상세정보

Airfoil construction

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/48   
미국특허분류(USC) 244/219 ; 244/207
출원번호 US-0032438 (1979-04-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 0

A dual-configuration airfoil having a thin profile which is adapted to foster high-speed flight, and having a pivotable portion on the upper surface which is movable upwardly for selectively increasing the thickness of the airfoil. In one embodiment, the pivotable portion pivots about an axis which coincides generally with the leading edge of the airfoil. The thickness of the airfoil when the pivotable portion is fully raised is about twice the thickness of the airfoil when the pivotable portion is fully retracted. A rigid connecting section forms part o...


An airfoil construction, comprising: (a) upper and lower surface structure which connects leading and trailing edges so as to form a relatively thin profile which is adapted to foster high speed flight, with one portion of the upper surface structure being pivotable upward about a hinge line that coincides generally with the leading edge of the airfoil, for increasing the thickness of the airfoil, and the chordwise length of said pivotable portion being substantially less than the chord length; (b) a connecting section which forms part of the airfoil upp...

이 특허를 인용한 특허 피인용횟수: 16

  1. Pabsch Arno,DEX ; Piening Matthias,DEX ; Bein Thilo,DEX. Actuator for generating high regulating forces and large regulating distances. USP1999015860352.
  2. Kota,Sridhar; Hetrick,Joel A.. Adaptive compliant wing and rotor system. USP2008067384016.
  3. Grove,Graham Bond. Aerofoil arrangement. USP2008127461820.
  4. Greenhalgh Samuel (Doylestown PA). Aircraft with single surface membranous airfoils. USP1987054667898.
  5. Caton John Harold ; Hobey Michael James ; Groeneveld John David ; Jacobs Jack Howard ; Wille Robert Henry ; Brase ; Jr. Lawrence Otto. Control surface for an aircraft. USP2001046209824.
  6. Iglesias, Jean Francois. Device for simultaneously and progressively varying the camber and the angle of attack of hydrodynamic and aerodynamic wings. USP20180710035579.
  7. John Cleveland Waldrop, III ES. Elastic ground plane. USP2002016337294.
  8. Carr Robert J. (1023 W. Churchhill Way Mustang OK 73064). Internal wing aircraft. USP1986044579300.
  9. Carr Robert J. (P.O. Box 2012 Oklahoma City OK 73101). Internal wing aircraft. USP1986024568042.
  10. Foreman Kenneth M. (Bellmore NY) Jenkins Richard C. (Smithtown NY). S-shaped jet engine inlet diffuser. USP1991024989807.
  11. Motosko, III, Stephen. Variable air foil and spoiler. USP2012028113470.
  12. Rinn Aaron ; Khamly Somphone ; Hornick David ; Obrigkeit Matthew ; Kota Sridhar. Variable camber airfoil. USP2000046045096.
  13. Nagel, Alexander; Bauminger, Shlomo. Wing and devices therefor. USP2015069061752.
  14. Lewis George E. (Renton WA) Thomasson Robert E. (Seattle WA) Nelson David W. (Redmond WA). Wing lift/drag optimizing system. USP1990024899284.
  15. Santini, Gregory M.. Wing variable camber trailing edge tip. USP2014098844879.
  16. Perez Sanchez, Juan Mauricio. Wing, particularly airfoil of an aircraft, having changeable profile. USP2009057530533.