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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Transverse force-connected body with variable profiling, particularly an airplane wing

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/48   
미국특허분류(USC) 244/219 ; 244/214
출원번호 US-0044400 (1979-05-31)
우선권정보 DE-2907912 (1979-03-01)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 3
초록

This invention relates to an improvement in a transverse, force-connected body with variable profiling, particularly an airplane wing, containing flexible upper, lower, and nose skin parts and supporting elements hingedly engaging thereat in conjunction with a control gear, the improvement comprising clamps securing the upper and lower flexible skin parts at a rigid part of the wing, rigid carriers in the upper and lower areas of the wing, and shaped profile elements on the upper and lower carriers, the shaped profile elements having outwardly-pointing s...

대표
청구항

In a transverse, force-connected body with variable profiling, particularly an airplane wing, containing separate, individually flexible upper, lower, and nose skin parts and supporting elements hingedly engaging thereat in conjunction with a control gear, the improvement comprising means clamping the upper and lower flexible skin parts at a rigid part of the wing, said skin parts forming the wing upper side, lower side, and leading edge, rigid carrier means interposed between said upper skin part and said nose skin part, and between said lower skin part...

이 특허를 인용한 특허 피인용횟수: 19

  1. 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.
  2. Grip, Robert Erik. Aircraft with a pressurized vessel. USP2013088500060.
  3. Statkus Frank D. (Woodinville WA). Continuous skin, variable camber airfoil edge actuating mechanism. USP1982094351502.
  4. Rawdon, Blaine K.; Harber, Benjamin A.; Harrison, Neal A.. Dual-rib morphing leading edge. USP2016089415856.
  5. Perez, Juan. Mechanism for at least regionally adjusting the curvature of airfoil wings. USP2003116644599.
  6. Grip, Robert Erik. Mechanism for changing the shape of a control surface. USP2013048418968.
  7. Grip, Robert Erik. Mechanism for changing the shape of a control surface. USP2011118056865.
  8. Pitt, Dale M.; Eckstein, Nicholas Stephen. Method and apparatus for a leading edge slat on a wing of an aircraft. USP2013098534610.
  9. Pitt, Dale M.; Eckstein, Nicholas Stephen. Method for a leading edge slat on a wing of an aircraft. USP2016099446836.
  10. Grip, Robert E.; Brown, John J.; Harrison, Neal A.; Rawdon, Blaine K.; Vassberg, John C.. Morphing airfoil leading edge. USP2017039598167.
  11. Gordon, Jason; Borgstrom, Carl; Fisher, Noah; Fuhrmeister, Cory; Madigan, Nathan; Parkins, Carly. Morphing wing leading edge. USP2015018925870.
  12. Pitt, Dale M.; Eckstein, Nicholas Stephen. Moveable leading edge device for a wing. USP2013098534611.
  13. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  14. Livingston David E. (Huntsville AL) Kornell Thomas J. (Federal Way WA). Single-piece, flexible inlet ramp. USP1991075033693.
  15. Grip, Robert Erik. Solar collector frame. USP2014028650811.
  16. Cole, James B.. Variable-camber airfoil. USP1985114553722.
  17. Lewis George E. (Renton WA) Thomasson Robert E. (Seattle WA) Nelson David W. (Redmond WA). Wing lift/drag optimizing system. USP1990024899284.
  18. Bray, Robert Reginald. Wingsail. USP201412D720280.
  19. Bray, Robert Reginald. Wingsail propelled boat. USP201410D714712.