$\require{mediawiki-texvc}$
  • 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

Trailing edge flap

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/20   
미국특허분류(USC) 244/217; 244/215; 244/213; 244/212; 244/211; 244/216
출원번호 US-0939221 (2010-11-04)
등록번호 US-8567727 (2013-10-29)
우선권정보 GB-0921007.1 (2009-11-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lowe Hauptman & Ham, LLP
인용정보 피인용 횟수 : 9  인용 특허 : 14
초록

A trailing edge flap arrangement for an aircraft wing, comprising an array of flap elements each discretely moveable between a retracted and an extended position by a respective actuator, wherein the flap elements are arranged to be deployed so as to open up a through slot between an adjacent pair of the flap elements only when the aerodynamic leading element of the pair has reached its extended position. Also, a method of operating the trailing edge flap arrangement.

대표
청구항

1. A trailing edge flap arrangement for an aircraft wing, comprising an array of flap elements each discretely moveable between a retracted and an extended position, wherein the flap elements are arranged to be deployed so as to open up a through slot between an adjacent pair of the flap elements only when the aerodynamic leading element of the pair has reached its extended position, and wherein a first hinge point is disposed between the wing and the aerodynamic leading flap element in the array, and a first ram actuator is connected between the wing an...

이 특허에 인용된 특허 (14)

  1. Weiland Richard H. (Seattle WA) Franklin William L. (Bothell WA). Aircraft trailing edge flap apparatus. USP1987104702442.
  2. Reckzeh, Daniel; Dyke, Adrian R.. Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap. USP2009047520471.
  3. Libby, John. High lift longitudinal axis control system. USP2010027661630.
  4. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  5. Arena Aldo (Smithtown NY). Integrated power hinge actuator. USP1992035098043.
  6. Arena Aldo (Smithtown NY). Linear flap drive system. USP1997075651513.
  7. Perez Sanchez, Juan. Pivoted flap mechanism for adjusting an aerodynamic pivoted flap associated with a wing. USP2009107600718.
  8. Lewis Delbert S. (Bellevue WA) Norton David A. (Bellevue WA) Person Robert P. (Mercer Island WA) Schairer George S. (Bellevue WA) Wimpress John K. (Seattle WA). STOL aircraft. USP1976083977630.
  9. Berry Patrick,SEX. Segmented flap with variable camber for aircraft wing. USP2000096123297.
  10. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
  11. Heynatz Johann T. (Immenstaad DEX). Trailing edge flap operation in wings. USP1989014796840.
  12. Sherman ; Irving R.. Variable aerodynamic compression flaps. USP1978104117996.
  13. Dean Roy Delmar (BOTH OFSeattle WA) Weiland Richard Herschel (BOTH OFSeattle WA). Variable pivot trailing edge flap. USP1977094049219.
  14. Brenholt David L. (Menomonie WI). Vertical takeoff aircraft. USP1991105054721.