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

특허 상세정보

Mechanism for changing the shape of a control surface

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44   
미국특허분류(USC) 244/219; 244/201
출원번호 US-0398951 (2009-03-05)
등록번호 US8056865 (2011-11-01)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Yee & Associates, P.C.
인용정보 피인용 횟수 : 9  인용 특허 : 20
초록

An apparatus comprises a structure having a first side, a second side substantially opposite to the first side, a flexible skin, and a plurality of deformable assemblies. The flexible skin is attached to the first side and the second side of the structure. The plurality of deformable assemblies is moveably connected to the structure, in which each deformable assembly in the plurality of deformable assemblies has a vertex and a base. The each deformable assembly in the plurality of deformable assemblies has a height that is capable of changing to change a...

대표
청구항

What is claimed is: 1. An apparatus comprising:a structure having a first side and a second side substantially opposite to the first side;a flexible skin attached to the first side and the second side of the structure; anda plurality of deformable assemblies moveably connected to the structure, in which each deformable assembly in the plurality of deformable assemblies has a vertex and a base, wherein the each deformable assembly in the plurality of deformable assemblies has a height that is capable of changing to change a shape of the structure and a sh...

이 특허에 인용된 특허 (20)

  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. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  3. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  4. Rowarth Ralph (South Cave GB2). Aircraft wing drooping leading edge device. USP1980044200253.
  5. Frost Richard C. (Fort Worth TX) Gomez Eduardo W. (Fort Worth TX) McAnally Robert W. (Fort Worth TX). Airfoil variable cambering device and method. USP1981014247066.
  6. Statkus Frank D. (Woodinville WA). Continuous skin, variable camber airfoil edge actuating mechanism. USP1982094351502.
  7. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  8. Perez, Juan. Mechanism for at least regionally adjusting the curvature of airfoil wings. USP2003116644599.
  9. Beyer, Kevin W.; Fox, Stephen J.; Lacy, Douglas S.; Sakurai, Seiya. Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface. USP2004096796534.
  10. Appa Kari. Seamless mission adaptive control surface. USP1999035887828.
  11. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2008037338018.
  12. Zimmer Herbert (Friedrichshafen DEX). Transverse force-connected body with variable profiling, particularly an airplane wing. USP1981024252287.
  13. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA). Variable camber aircraft wing tip. USP1984024429844.
  14. Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976113994452.
  15. Cole James B. (Mercer Island WA). Variable camber airfoil. USP1977104053124.
  16. Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1984104475702.
  17. Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1987114706913.
  18. Cole, James B.. Variable-camber airfoil. USP1985114553722.
  19. Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
  20. Lonsinger, Hans; Perez-Sanchez, Juan. Wing, especially a carrier wing of an airplane, having an adaptable profile. USP2010047699270.