$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Aircraft wing flap

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/18   
미국특허분류(USC) 244/216 ; 244/218
출원번호 US-0593943 (1984-03-27)
발명자 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 2
초록

A support and actuating system for large Fowler-type flaps on the trailing edge of an aircraft wing. Each flap is vertically and laterally supported at diagonally opposite corners, and the remaining leading-edge corner is vertically supported and laterally free to permit smooth and simple actuation. The flap is constructed to be torsionally stiff to eliminate need for conventional multiple flap tracks and support at the remaining trailing-edge corner. Elimination of some or all external tracks on the wing tracks provides a clean low-drag wing when the fl...

대표
청구항

A lift-augmentation system for an aircraft wing, comprising: a lift-augmentation device of generally quadrilateral planform to define four corners; first and second tracks on the aircraft for supporting the device to be movable between extended and retracted positions on the wing, the device having a first spanwise edge which is remote from the wing and a second spanwise edge which is adjacent the wing when the device is in the extended position; first and second couplers disposed at diagonally opposite corners of the device and connecting such corners t...

이 특허를 인용한 특허 피인용횟수: 14

  1. Cerne, Gerd. Aircraft. USP2013048408499.
  2. Shental,Gad; Shental,Nir; Shental,Ran; Pessachis,Lev. Aircraft wing structure and a method for decreasing flight speed of the aircraft. USP2007127311288.
  3. Phillips, Warren F.. Apparatus and method for reducing induced drag on aircraft and other vehicles. USP2005116970773.
  4. Phillips, Warren F.. Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles. USP2011027883060.
  5. Turner, Travis L.; Kidd, Reggie T.; Lockard, David P; Khorrami, Mehdi R.; Streett, Craig L.; Weber, Douglas Leo. Autonomous slat-cove-filler device for reduction of aeroacoustic noise associated with aircraft systems. USP2016019242720.
  6. Rutan, Elbert L.. Dynamic tow maneuver orbital launch technique. USP2014058727264.
  7. Somers, Dan M.. Laminar-flow airfoil. USP2005066905092.
  8. Andreani, Luc. Lateral coupling device for holding and guiding at least one aerodynamic body relative to the main wing of an aircraft, airfoil and aircraft with such a lateral coupling device. USP2013088517315.
  9. Rutan, Elbert L.. Pressure-equalizing cradle for booster rocket mounting. USP2015028960590.
  10. Wallen, Gregory T.; Regan, James M.; Lang, David J.; Crandall-Seibert, Cory M.; Miller, Mark D.; Leden, William E.; Baines, Andrew N.; Jacobs, Jeffrey Paul. Resolver type skew sensor with gimbal attachment. USP2013058438743.
  11. Eglin, Paul. Rotorcraft having a stabilizer device. USP2017049623965.
  12. Pohl Ulrich (Bremen DEX) Renken Juergen (Freyersen DEX). Segmentized flap system. USP1990014892274.
  13. Jamison, Flint M.; Amorosi, Stephen R.; Klein, Michael K.. Slidable divergent trailing edge device. USP2016109463869.
  14. Heintjes, Mark. Wing of an aircraft or spacecraft, comprising a mobile flow body. USP2016019242719.