$\require{mediawiki-texvc}$
  • 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

Tandem fan series flow VSTOL propulsion system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/14   
미국특허분류(USC) 244/53R ; 244/23B ; 244/23D ; 244/125
출원번호 US-0403678 (1982-07-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 3
초록

A propulsion system for vertical take off and landing aircraft includes a forward compressor fan (40) and an aft compressor fan (42) downstream of the forward fan and in series flow communication with the forward fan. The forward and aft fans are positioned in a central duct (26). A gas turbine engine (44) is in series flow with the forward and aft fans for driving the fans. The forward fan, aft fan and turbine engine are interconnected by a common shaft (50). A forward diverter structure (100) is positioned downstream of the forward fan and is movable b...

대표
청구항

A propulsion system for vertical and short take-off and landing aircraft comprising: a duct comprising therein, a forward compressor fan, an aft compressor fan controllably in series with the forward fan, a turbine means controllably in flow series with the forward and aft compressor fans, means interconnecting the forward compressor fan, aft compressor fan, and turbine means, a gas generator means for driving said turbine means, a first diverter means downstream of said forward fan for selectively diverting exhaust from the forward fan downwardly out of...

이 특허를 인용한 특허 피인용횟수: 22

  1. Sokhey Jack (Jagdish) Singh ; Crook Andrew James ; Snyder Philip Harold ; Vittal Baily R.. Aircraft thrust vectoring system. USP1998065769317.
  2. Saiz Manuel Munuoz,ESXITX 28017. Device for lift and to reduce resistance to aircraft advance. USP2000106138946.
  3. Hollimon, Charles; Barber, John; Sherrer, John Herman; Laramee, Robert. Engine exhaust system. USP2012028123159.
  4. Hollimon, Charles; Barber, John; Sherrer, John Herman; Laramee, Robert. Engine exhaust system with directional nozzle. USP2012038132755.
  5. Dickau, John. Heated insulated catalytic converter with air cooling. USP2005106951099.
  6. Suchezky, Mark E.; Simpkins, Lisa M.. Jet engine exhaust nozzle and associated system and method of use. USP2014068746613.
  7. Pesyna, Kenneth M.; Henkle, Jeffrey P.. Mechanism for a vectoring exhaust nozzle. USP2012088245495.
  8. Harrison, Neal A.; Hyde, David C.. Multi-directional control using upper surface blowing systems. USP2018029889924.
  9. Pashea Terry F. ; Williams Donald L.. Multi-function engine air inlet control. USP1999025865398.
  10. Bevilaqua, Paul. Propulsion system for a vertical and short takeoff and landing aircraft. USP2004056729575.
  11. Oatway, Thomas P.; Bollinger, Robert S.; Nicolai, Leland M.. Propulsion system for an aircraft providing V/STOL capability. USP1994065320305.
  12. Kim Kyusik (5026 Rhoads Ave. Santa Barbara CA 93111). Ram constriction vane diffuser for jet engine. USP1987054667900.
  13. David Levi Sutterfield ; Von David Baker ; Jagdish Singh Sokhey. Thrust vectoring mechanism. USP2002056382559.
  14. Ulanoski Michael S. ; Sokhey Jagdish S.. Thrust vectoring system. USP2000086105901.
  15. Ulanoski Michael S. ; Sokhey Jagdish S. ; Vittal Baily R. ; Baker Von D.. Thrust vectoring techniques. USP2001116318668.
  16. Howarth,Nicholas; Freeman,Christopher. Turbine engine arrangements. USP2007017165744.
  17. Lecordix, Jean-Loic Herve. Turbomachine comprising a plurality of fixed radial blades mounted upstream of the fan. USP2017129835044.
  18. Pedigo, Samuel. Unmanned aerial vehicle. USP20180810040547.
  19. Windisch, D. Anthony. VTOL propulsion for aircraft. USP2015028960592.
  20. Nightingale Douglas J. (Jonesboro GA) Ward Benjamin D. (Marietta GA). Valve for diverting fluid flows in turbomachines. USP1986054587803.
  21. Yates Martin H,GBX. Vectorable nozzle for aircraft. USP2000036036142.
  22. Dickau, John Eugene. Vertical takeoff and landing aircraft propulsion systems. USP2005076918244.