$\require{mediawiki-texvc}$
  • 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

Thrust vectoring system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-029/00    F02K-001/00   
미국특허분류(USC) 24/402.3A ; 24/402.3D ; 602/28
출원번호 US-0055663 (1998-04-06)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Woodard, Emhardt, Naughton Moriarty & McNett
인용정보 피인용 횟수 : 20  인용 특허 : 25
초록

A thrust directing mechanism to vector thrust and control discharge throat area with a number of vanes mounted across the passage. The mechanism includes a control link pivotally coupled to each of the vanes. The control link is selectively movable to correspondingly pivot the vanes and has at least two degrees of freedom corresponding to a two coordinate position. A desired orientation of the vanes may be determined as a function of the two coordinate position. The discharge exit area is contracted by adjusting convergence of the vanes. During convergen...

대표
청구항

[ What is claimed is:] [1.] A thrust system, comprising:(a) an aircraft having a passage with an outlet configured to discharge working fluid to produce thrust;(b) a number of vanes pivotally mounted across said outlet to direct thrust, said number of vanes including at least a first vane, a second vane mounted adjacent said first vane, and a third vane mounted adjacent said second vane;(c) a thrust control linkage including a control link, said link being spaced apart from said first, second, and third vanes, said linkage further including:a first tie r...

이 특허에 인용된 특허 (25)

  1. Sokhey Jack (Jagdish) Singh ; Crook Andrew James ; Snyder Philip Harold ; Vittal Baily R.. Aircraft thrust vectoring system. USP1998065769317.
  2. Thayer Edward B. (Jupiter FL) Scott Philip R. (Lake Park FL) Roach Thomas A. (Mauldin SC). Area controlled, thrust vectoring vane cascade with nutating control vane. USP1989014798328.
  3. Madden William M. (Palm Springs FL). Area two-dimensional converging/diverging nozzle. USP1986054587806.
  4. Lippmeier William C. (Cincinnati OH). Axisymmetric vectoring exhaust nozzle seal. USP1991085039014.
  5. Thayer Edward B. (Jupiter FL) Stevens Herman L. (West Palm Beach FL). Control vent for diverting exhaust nozzle. USP1989024805401.
  6. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1997055630564.
  7. Carey Lee F. (North Tonawanda NY). Extendible/expandable nozzle for rocket engines and the like and method of making same. USP1979074162040.
  8. Hurley John F. (Huntington CT). Infrared radiation suppressor for gas turbine engine. USP1977044018046.
  9. Nightingale Douglas J. (Jonesboro GA). Mechanism for operating a cascade of variable pitch vanes. USP1996015485958.
  10. Smereczniak Philip (St. Peters MO) Spetnagel David R. (St. Charles MO). Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine eng. USP1997125694766.
  11. Robinson Michael R. ; Ouellette Richard P.. Multi axis thrust vectoring for turbo fan engines. USP1998015706649.
  12. Holowach Joseph (Cincinnati OH) Van Sutherland William (Milford OH) Wooten William Harvey (Cincinnati OH). Multifunction exhaust system for gas turbine engines. USP1997115690280.
  13. Bevilaqua Paul M. (Santa Clarita CA) Shumpert Paul K. (Valencia CA). Propulsion system for a vertical and short takeoff and landing aircraft. USP1993055209428.
  14. Garrett Timothy M. (Florissant MO) Zilz David E. (St. Peters MO). Rotatable arms for thrust vectoring and changing the area of a nozzle throat. USP1994035294055.
  15. Garland Douglas (Rexdale CAX) Farbridge Joseph E. (Thornhill CAX). Segmented vectoring cruise nozzles. USP1990084948072.
  16. Camboulives AndreA. M. L. (Savigny sur Orge FRX). Supersonic nozzle for a turbojet engine. USP1996115571262.
  17. Musgrove Robert G. (Arlington TX). Tandem fan series flow VSTOL propulsion system. USP1984104474345.
  18. Evans Robert C. (Cincinnati OH) Ammer Robert C. (Bright IN). Thrust vectoring apparatus for a VTOL aircraft. USP1980064205813.
  19. Barcza W. Kevin (Stuart FL) Anders Larry E. (West Palm Beach FL). Thrust vectoring ejector nozzle. USP1994075328098.
  20. Pedersen George H. (Indianapolis IN). Variable area exhaust nozzle. USP1980124241876.
  21. Short Malcolm (Bristol GB2). Variable camber vane. USP1995115464175.
  22. Langley ; Jr. David T. (226 S. Main St. Los Angeles CA 90012). Variable throat nozzle. USP1986084606499.
  23. Clifton Robert T. (Houston TX) Cook Woodrow L. (Lake Almanor Peninsula CA). Vertical/short take-off and landing aircraft. USP1989054828203.
  24. Herrick Paul W. (Jupiter FL) Thayer Edward B. (Jupiter FL) Stewart Jim D. (Jupiter FL). Yaw and pitch convergent-divergent thrust vectoring nozzle. USP1989064836451.
  25. Holden Davis C. (Pensacola FL). Yaw and pitch thrust vectoring nozzle. USP1997115687907.

이 특허를 인용한 특허 피인용횟수: 20

  1. Yoeli, Raphael. Apparatus for generating horizontal forces in aerial vehicles and related method. USP2010057717368.
  2. Yoeli, Raphael. Control flows and forces in VTOL vehicles. USP2013078496200.
  3. Yoeli, Raphael. Ducted fan VTOL vehicles. USP2010127857253.
  4. Yoeli, Raphael. Ducted fan VTOL vehicles. USP2010107806362.
  5. Yoeli, Raphael. Ducted fan VTOL vehicles. USP2014018622335.
  6. Yoeli, Raphael. Ducted fan for VTOL vehicles with system and method to reduce roll moments. USP2014118876038.
  7. Evulet, Andrei. Fluidic propulsive system and thrust and lift generator for aerial vehicles. USP20190210207812.
  8. Migliaro, Jr., Edward F.. Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle. USP2013028365515.
  9. Yoeli, Raphael. Ground effect vanes arrangement. USP2011098020804.
  10. Pesyna, Kenneth M.; Henkle, Jeffrey P.. Mechanism for a vectoring exhaust nozzle. USP2010117836681.
  11. Pesyna, Kenneth M.; Henkle, Jeffrey P.. Mechanism for a vectoring exhaust nozzle. USP2012088245495.
  12. Stephan, Volker. Method for the control of aero gas turbine engines. USP2004036712314.
  13. Roberts, Steven D.; Damgaard, Jocelyn Charis. Retainer for suspended thermal protection elements in a gas turbine engine. USP2013118572986.
  14. Sokhey, Jagdish; Kornegay, Brian. Techniques to reduce infrared detection of a gas turbine engine. USP2014078776527.
  15. David Levi Sutterfield ; Von David Baker ; Jagdish Singh Sokhey. Thrust vectoring mechanism. USP2002056382559.
  16. Windisch, D. Anthony. VTOL propulsion for aircraft. USP2015028960592.
  17. Yoeli, Raphael. VTOL vehicle with coaxially tilted or tiltable rotors. USP2013018342441.
  18. Yoeli, Rafi. Vehicles particularly useful as VTOL vehicles. USP2010097789342.
  19. Wood, Victor A.. Vertical take off and landing aircraft system with energy recapture technology. USP2011098016226.
  20. Yoeli, Raphael. Wall effects on VTOL vehicles. USP2014098833692.