$\require{mediawiki-texvc}$
  • 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

Spillage drag and infrared reducing flade engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/075   
미국특허분류(USC) 60/204 ; 60/2263 ; 60/395
출원번호 US-0131511 (1993-10-04)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 58  인용 특허 : 0
초록

A FLADE aircraft gas turbine engine having a FLADE duct circumscribing a preferably variable cycle inner gas turbine engine and having a FLADE fan disposed in the FLADE duct and radially outward of and drivenly connected to a first fan disposed in a first fan duct of the inner engine. The annular inlet of the first fan duct is sized to receive essentially the full mass airflow of the engine at full power conditions with the annular FLADE duct inlet essentially closed off. The engine is further designed and operable to fully open the inlet of the flade du...

대표
청구항

An aircraft FLADE gas turbine engine comprising: an inner gas turbine engine having at least one inner fan section with at least one row of inner fan blades disposed in an inner fan duct, a FLADE fan duct circumferentially disposed around said inner engine, a FLADE fan disposed in said FLADE duct, said FLADE fan having at least one row of FLADE fan blades radially outward of and drivenly connected to said inner fan section, said inner fan duct having an inner fan duct inlet and said FLADE fan duct having a FLADE fan duct inlet, a FLADE inlet airflow modu...

이 특허를 인용한 특허 피인용횟수: 58

  1. Zsurka, Mark. Aerodynamic track fairing for a gas turbine engine fan nacelle. USP20190310240561.
  2. Johnson,James Edward. Aft FLADE engine. USP2007057216475.
  3. Rupp, George D.; Troia, Trajaen J.. Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching. USP2016059353684.
  4. Orlando, Robert Joseph; Moniz, Thomas Ory; Baughman, John Lewis. Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans. USP2004076763654.
  5. Orlando, Robert Joseph; Moniz, Thomas Ory. Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines. USP2004026684626.
  6. Orlando, Robert Joseph; Moniz, Thomas Ory. Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines. USP2004036711887.
  7. Johnson, James Edward. Apparatus and method for assembling gas turbine engines. USP2010087765789.
  8. Dale Bradley Elliott ; Peter Nicholas Szucs ; Nicholas Damlis ; Kenneth Paul Onderko. Bifurcated splitter for variable bleed flow. USP2002086438941.
  9. Busbey Bruce C. ; Crall David W. ; Toye Michael D.. Blade assembly with splitter shroud. USP1999115988980.
  10. Powell, Brandon Flowers; Tersmette, Trevor Andrew; Spencer, Craig Bradley. Conformal inlet apparatus for a gas turbine engine. USP2017109777631.
  11. Johnson, James Edward. Convertible gas turbine engine. USP2011027877980.
  12. Orlando, Robert Joseph; Moniz, Thomas Ory. Counter rotating fan aircraft gas turbine engine with aft booster. USP2004076763653.
  13. Powell, Brandon Flowers; Decker, John Jared. Double bypass turbofan. USP2009117614210.
  14. Brunet, Edgar; Daris, Thomas; Page, Alain Pierre; Prouteau, Jackie Raymond Julien. Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft. USP2010087784284.
  15. Froemming, Kenneth W.; Lerg, Bryan H.. Exhaust nozzle apparatus and method for multi stream aircraft engine. USP2018019863366.
  16. Wadia, Aspi Rustom; Turner, Alan Glen; Dziech, Aaron Michael; Szucs, Peter Nicholas; Decker, John Jared. FLADE fan with different inner and outer airfoil stagger angles at a shroud therebetween. USP2010077758303.
  17. Giffin, III,Rollin George; Johnson,James Edward. FLADE gas turbine engine with counter-rotatable fans. USP2007077246484.
  18. Lariviere, Erin Lee; Ettorre, Stephen Michael. Flade discharge in 2-D exhaust nozzle. USP2015038984891.
  19. Johnson,James Edward. Flade gas turbine engine with fixed geometry inlet. USP2008077395657.
  20. Johnson,James Edward. Fladed supersonic missile turbojet. USP2009017475545.
  21. Feldmann, Manfred; Schinko, Norbert; Eichler, Christian; Muschkorgel, Sandra. Flow conducting assembly for cooling the low-pressure turbine housing of a gas turbine jet engine. USP2015119194331.
  22. Roberge, Gary D.. Flow path routing within a gas turbine engine. USP2018039909529.
  23. Duge, Robert T.. Gas turbine engine having configurable bypass passage. USP2017099771945.
  24. Roberge, Gary D.. Gas turbine engine including a third flowpath exhaust nozzle. USP20190210197008.
  25. Roberge, Gary D.; Suciu, Gabriel L.. Gas turbine engine systems involving tip fans. USP2013118590286.
  26. Roberge, Gary D.; Suciu, Gabriel L.. Gas turbine engine systems involving tip fans. USP2013038402742.
  27. Hanlon, Christopher J.; Kupratis, Daniel B.; Ledwith, Walter A.. Gas turbine engine with a multi-spool driven fan. USP20181110119477.
  28. Kupratis, Daniel B.. Gas turbine engine with intercooling turbine section. USP2015069057328.
  29. Zamora, Sean P.; Murphy, Michael Joseph. Gas turbine engine with variable area fan nozzle. USP2012038141366.
  30. Christopherson, Charles Kammer. Gas turbine engine with variable pressure ratio fan system. USP2005066901739.
  31. Giffin, Rollin George; Johnson, James Edward. High pressure ratio aft fan. USP2009127631484.
  32. Baughman, John Lewis. Intermediate fan stage. USP2014078777554.
  33. Giffin,Rollin George. Method and apparatus for assembling gas turbine engines. USP2006127144221.
  34. Griffin, III,Rollin George; Morrow,William James. Methods and apparatus for assembling a gas turbine engine. USP2007037185484.
  35. Renggli,Bernard James; Jumper,Matthew Wilson. Methods and apparatus for assembling gas turbine engines. USP2008127464536.
  36. Renggli, Bernard James; Jumper, Matthew Wilson; Price, Kenneth Daniel; Kuchar, Andrew Paul. Methods and apparatus for flade engine nozzle. USP2005096948317.
  37. Dawson, David Lynn; Lariviere, Erin Lee; Petersen, Brian Joseph; Ellerhorst, Robert Jerome. Multi-nozzle flow diverter for jet engine. USP2018039920710.
  38. Giffin, Rollin George; Johnson, James Edward. Multistage tip fan. USP2014048695324.
  39. Sokhey, Jagdish S.; Pierluissi, Anthony F.. Reduced noise gas turbine engine system and supersonic exhaust nozzle system using elector to entrain ambient air. USP2017079714608.
  40. Johnson,James Edward. Self powdered missile turbojet. USP2008117448199.
  41. Petty, Dale William. Sliding ramp nozzle system for a gas turbine engine. USP2014068739548.
  42. Johnson,James Edward. Supersonic missile turbojet engine. USP2008097424805.
  43. Stoia, Lucas John; DiCintio, Richard Martin; Melton, Patrick Benedict; Romig, Bryan Wesley; Slobodyanskiy, Ilya Aleksandrovich. System and method for a multi-wall turbine combustor. USP2018019869279.
  44. Pesyna, Kenneth M.; Pierluissi, Anthony F.; Lerg, Bryan H.; Moore, Justin N.. Three stream, variable area, vectorable nozzle. USP2017129845768.
  45. Baughman,John Lewis; Johnson,James Edward. Thrust vectoring aft FLADE engine. USP2006117134271.
  46. Johnson,James Edward. Thrust vectoring missile turbojet. USP2009037509797.
  47. Hofer, Douglas Carl; Joshi, Narendra Digamber; Idelchik, Michael Solomon. Turbine engine assembly and method of manufacturing. USP20180910077660.
  48. Lipinski, Thomas; LaChapelle, Donald George; Moore, Kenneth Jay; Tracey, Bradford; Waymeyer, Stephen Joseph. Turbine frame cooling systems and methods of assembly for use in a gas turbine engine. USP20181210151217.
  49. Bouiller Philippe Pierre,FRX ; Bourquin Pierre-Yves,FRX ; Kettler Daniel,FRX ; Ruis Jean-Pierre,FRX. Turbo jet engine exhaust nozzle with masked gas jet. USP2001016179225.
  50. Giffin ; III Rollin G. ; Johnson James E. ; Crall David W. ; Salvage John W. ; Szucs Peter N.. Turbofan engine with a core driven supercharged bypass duct. USP1998095809772.
  51. Bartos James W.. Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and a. USP1999025867980.
  52. Wood, Peter John; Zenon, Ruby Lasandra; LaChapelle, Donald George; Mielke, Mark Joseph; Grant, Carl. Turbofan gas turbine engine with variable fan outlet guide vanes. USP2010067730714.
  53. Shafer, Douglas George; Rettig, Mark Gerard; VanderMolen, Robert John. Turbogenerator with cooling system. USP2013088499544.
  54. Schwark, Jr., Fred W.; Atassi, Oliver V.; Owen, William D.. Variable area fan nozzle bearing track. USP2013058443586.
  55. Schirle Steven M. (Boynton Beach FL) Baghdadi Samy (Palm Beach Gardens FL) Khalid Syed J. (Palm Beach Gardens FL) Perkins Gary M. (Palm Beach Gardens FL). Variable cycle engine with enhanced stability. USP1997045623823.
  56. Baughman, John Lewis; Orlando, Robert Joseph; Moniz, Thomas Ory. Variable torque split aircraft gas turbine engine counter rotating low pressure turbines. USP2004076763652.
  57. Baughman, John Lewis; Eheart, Raymond. Variable-cycle gas turbine engine with front and aft FLADE stages. USP2015049016041.
  58. Thomas, Russell H.; Kinzie, Kevin W.. Wet active chevron nozzle for controllable jet noise reduction. USP2011098015819.