$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Gas turbine engine nacelle assembly 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-029/00
출원번호 US-0185906 (1994-01-21)
우선권정보 GB-0016986 (1991-08-07)
국제출원번호 PCT/GB92/00994 (1992-06-03)
§371/§102 date 19940121 (19940121)
국제공개번호 WO-9302920 (1993-02-18)
발명자 / 주소
  • Newton Arnold C. (Derby GB2)
출원인 / 주소
  • Rolls-Royce plc (London GB2 03)
인용정보 피인용 횟수 : 81  인용 특허 : 0

초록

A gas turbine engine nacelle assembly (10) comprises a pylon (13) for mounting the assembly on an aircraft, a nacelle (11) and a gas turbine engine (12) enclosed within the nacelle (11). Part (15) of the nacelle (11) is structurally integral with the pylon (13) and has the remainder of the nacelle (

대표청구항

A gas turbine nacelle assembly (10) suitable for mounting on an aircraft comprising a pylon (13) for the attachment of said assembly (10) to said aircraft, a gas turbine engine (12) and a nacelle (11), said nacelle (11) enclosing said gas turbine engine (12) and comprising, in axial flow series, an

이 특허를 인용한 특허 (81)

  1. Suciu, Gabriel L.; Chandler, Jesse M., ATR axial V-groove.
  2. Suciu, Gabriel L.; Chandler, Jesse M., ATR full ring sliding nacelle.
  3. Suciu, Gabriel L.; Chandler, Jesse M., ATR guide pins for sliding nacelle.
  4. Chaumeret,Michel; Mazeaud,Georges, Air input device for a turboprop engine.
  5. Klamka Andrew ; Parham Dean Leon, Aircraft engine and associated aircraft engine cowl.
  6. Shutrump, Jeffrey D., Aircraft engine inlet having zone of deformation.
  7. Shutrump, Jeffrey D., Aircraft engine inlet having zone of deformation.
  8. Diochon, Lionel; Sarrato, Michael; Chartier, David; Petrissans, Isabelle, Aircraft jet engine pylon suspension attachment.
  9. Stretton,Richard G; Moore,Alastair D, Aircraft wing and aeroengine arrangement for attenuating engine noise.
  10. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  11. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  12. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian, Axial compressor for tip turbine engine.
  13. Nordeen, Craig A.; Suciu, Gabriel L., Balanced turbine rotor fan blade for a tip turbine engine.
  14. Vauchel, Guy Bernard; Collier, Jerome; Dhainault, Patrice; Conte, Francois; Hillereau, Nicolas; Chouard, Pierre-Alain; Lefort, Guillaume, Bypass turbojet engine nacelle.
  15. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian, Cantilevered tip turbine engine.
  16. Suciu, Gabriel L.; Nordeen, Craig A.; Kramer, Stephen, Combustor for turbine engine.
  17. Merry, Brian; Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Counter-rotating compressor case and assembly method for tip turbine engine.
  18. Suciu, Gabriel; Merry, Brian; McCune, Michael E., Counter-rotating gearbox for tip turbine engine.
  19. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Diffuser aspiration for a tip turbine engine.
  20. Suciu, Gabriel L.; Roberge, Gary D., Ejector cooling of outer case for tip turbine engine.
  21. El Hamel,Karim; Newton,Arnold C, Engine arrangement.
  22. Diochon, Lionel; Cetout, Jean-Michel; LaFont, Laurent, Engine assembly for aircraft.
  23. Diochon, Lionel; El Hammami, Samir; Le Louvetel-Poilly, Julie; Dumas, Jean-Baptiste; Koenig, Nicolas, Engine assembly for aircraft comprising an engine and a mounting device for such an engine.
  24. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B., Engine mount system for a turbofan gas turbine engine.
  25. Suciu, Gabriel L.; Marx, Jon A.; Merry, Brian D.; Nordeen, Craig A.; Dye, Christopher M., Engine mounting configuration for a turbofan gas turbine engine.
  26. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine.
  27. Suciu, Gabriel L.; Chandler, Jesse M.; Bomzer, T. David, Full ring sliding nacelle with thrust reverser.
  28. Suciu, Gabriel L.; Chandler, Jesse M.; Bomzer, T. David, Full ring sliding nacelle with thrust reverser.
  29. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine compressor arrangement.
  30. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine compressor arrangement.
  31. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  32. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  33. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  34. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  35. Nordeen, Craig A.; Norris, James W., Individual inlet guide vane control for tip turbine engine.
  36. Suciu, Gabriel L.; Portlock, Lawrence E.; Merry, Brian, Inflatable bleed valve for a turbine engine.
  37. Suciu, Gabriel L.; Chandler, Jesse M., Integrated nozzle and plug.
  38. Bellabal, Francois Robert; Gallet, Francois; Poisson, Mathieu Ange, Isostatic suspension of a turbojet by rear double support.
  39. Suciu, Gabriel L.; Merry, Brian, Modular tip turbine engine.
  40. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M., Mounting system for a gas turbine engine.
  41. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M., Mounting system for a gas turbine engine.
  42. Suciu, Gabriel L.; Merry, Brian D.; Marx, Jon A.; Dye, Christopher M., Mounting system for a gas turbine engine.
  43. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian, Particle separator for tip turbine engine.
  44. Suciu, Gabriel L.; Chandler, Jesse M.; Bomzer, T. David, Pivot thrust reverser surrounding inner surface of bypass duct.
  45. Suciu, Gabriel L.; Chandler, Jesse M., Pivot thrust reverser with multi-point actuation.
  46. Norris, James W.; Nordeen, Craig A., Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method.
  47. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Regenerative turbine blade and vane cooling for a tip turbine engine.
  48. Garland, Philip Henry; Sakota, Nebojsa, Removal of components from aircraft.
  49. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Seal assembly for a fan rotor of a tip turbine engine.
  50. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Seal assembly for a fan-turbine rotor of a tip turbine engine.
  51. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian, Stacked annular components for turbine engines.
  52. Merry, Brian; Webb, Scot Adams; McCune, Michael, Starter generator system for a tip turbine engine.
  53. Suciu, Gabriel L.; Alvanos, Ioannis, TEC mount redundant fastening.
  54. Chandler, Jesse M.; Suciu, Gabriel L., Tandem thrust reverser with multi-bar linkage.
  55. Suciu, Gabriel L.; Chandler, Jesse M., Tandem thrust reverser with multi-point actuation.
  56. Chandler, Jesse M.; Suciu, Gabriel L., Tandem thrust reverser with sliding rails.
  57. Chandler, Jesse M.; Suciu, Gabriel L., Tandem thrust reverser with sliding rails.
  58. Norris, James W.; Nordeen, Craig A., Tip turbine engine and operating method with reverse core airflow.
  59. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine engine composite tailcone.
  60. Suciu, Gabriel L.; Merry, Brian; Portlock, Lawrence, Tip turbine engine comprising a nonrotable compartment.
  61. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Tip turbine engine comprising turbine blade clusters and method of assembly.
  62. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor.
  63. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine engine integral case, vane, mount and mixer.
  64. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Tip turbine engine integral fan, combustor, and turbine case.
  65. Suciu, Gabriel L.; Merry, Brian, Tip turbine engine support structure.
  66. Suciu, Gabriel L.; Merry, Brian, Tip turbine engine with a heat exchanger.
  67. Norris, James W.; Nordeen, Craig A.; Roberge, Gary, Tip turbine engine with multiple fan and turbine stages.
  68. Norris, James W.; Nordeen, Craig A., Tip turbine engine with reverse core airflow.
  69. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine single plane mount.
  70. Roberge, Gary D., Turbine blow down starter for turbine engine.
  71. Suciu, Gabriel L.; Alvanos, Ioannis; Merry, Brian, Turbine engine case mount and dismount.
  72. Suciu, Gabriel L.; Pagluica, Gino J.; Duong, Loc Quang; Portlock, Lawrence E., Turbine engine with differential gear driven fan and compressor.
  73. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M., Turbine section of high bypass turbofan.
  74. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  75. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  76. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph Brent; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  77. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly for gas turbine engine.
  78. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method.
  79. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method.
  80. Roberge, Gary D., Vectoring transition duct for turbine engine.
  81. Bulumulla, Selaka Bandara; Calder, David Patrick; Dell'Anno, Michael Joseph; Roach, Andrew Michael, Wireless aircraft engine monitoring system.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로