$\require{mediawiki-texvc}$

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.

Aircraft gas turbine engine bleed air energy recovery apparatus 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-013/00
  • B64D-033/00
출원번호 US-0709851 (1991-06-04)
발명자 / 주소
  • Coffinberry George A. (West Chester OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 73  인용 특허 : 0

초록

An environmental control system for supplying aircraft or cabin air to an aircraft is provided with a propulsive engine compressor bleed supply means and an ECS bleed air flow control means which includes an energy recovery means for using the unrequired or unused energy to pump boundary layer air f

대표청구항

An environmental control system (ECS) powered by an aircraft propulsive gas turbine engine having a compressor section, said ECS comprising: a compressor bleed air means to bleed compressor bleed air form the compressor section of the gas turbine engine; a compressor bleed flowrate control means in

이 특허를 인용한 특허 (73)

  1. Dziorny, Paul J.; Sellers, Benjamin D., Air conditioning apparatus.
  2. Coffinberry,George Albert, Air turbine powered accessory.
  3. Saiz Manuel Munoz,ESX, Aircraft air conditioner energy recovery method.
  4. Hara, Nobuhide; Yamada, Osamu, Aircraft and fuselage cooling structure.
  5. Zywiak, Thomas; Bruno, Louis J.; Drew, Diane; Christians, Douglas L., Aircraft galley chiller system.
  6. Zywiak,Thomas; Bruno,Louis J.; Drew,Diane; Christians,Douglas L., Aircraft galley chiller system.
  7. Dessero, Michael J.; Le, Luong Hoang; Moran, Thomas J., Aircraft galley exhaust system and method of assembling same.
  8. Barbara, Olivier; Prat, Damien, Aircraft including an air conditioning system.
  9. Clawson, Burrell E.; Weiss, Richard A., Apparatus and methods for isolating human body areas for localized cooling.
  10. Herchenroder, Anthony; Paul, Douglas; Landers, Stephen, Arrangements and methods for supplying heated air to a wing anti-icing system.
  11. Lo, Charles, Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine.
  12. Sennoun, Mohammed El Hacin, Bleed air and hot section component cooling air system and method.
  13. Monteiro, Oswaldo Barthel; Tin, Vinicius Jorge; da Silva Franco, Bernardo Campos; Barbosa, Ricardo Jose, Bleed airflow balancing control using simplified sensing.
  14. Army, Donald E., Bleed valve module.
  15. Army, Donald E.; DeFrancesco, Gregory L.; Malijanian, John M., Bleed valve module with position feedback and cooling shroud.
  16. Army, Donald E.; DeFrancesco, Gregory L.; Maljanian, John M., Bleed valve module with position feedback and cooling shroud.
  17. Bizzarro, Peter, Contamination free reverse flow fitting.
  18. Liu, Xiaoliu, Cooler in nacelle with radial coolant.
  19. Strecker, Steven; Liu, Xiaoliu; Logan, Adam, Cooling system for engine and aircraft air.
  20. Laborie Daniel J. ; Mc Nulty Michael, Core compartment valve cooling valve scheduling.
  21. Ronan, Michael, Environmental control generator system and apparatus.
  22. Sampson, Bernard Francis, Environmental control system.
  23. Army, Donald E.; Peacos, Frederick; Polifka, John; Zager, Michael, Environmental control system pack pallets.
  24. Sennoun, Mohammed El Hacin; Dinsmore, Nicholas Rowe; Miller, Brandon Wayne, Environmental control system supply precooler bypass.
  25. Severson Mark Hamilton ; Squier Steven Eric, Environmental control system with energy recovery and bleed air assist.
  26. Gray, John C., Environmental control system, method, and computer program product for controlling the interior environment of a pressurized compartment.
  27. Marche, Herve, Exchanger for aircraft air conditioning circuit and integrated propulsion assembly for such an exchanger.
  28. Arcas Noe ; Hutto Frederick M. ; Parente Charles A., Extended reaction acoustic liner for jet engines and the like.
  29. Finney, Adam M., Gas turbine bleed energy recovery via counter rotating generator.
  30. Coffinberry, George Albert, Gas turbine engine fan bleed heat exchanger system.
  31. Khalid, Syed Jalaluddin, Gas turbine engine with ejector.
  32. Khalid, Syed Jalaluddin, Gas turbine engine with ejector.
  33. Suciu, Gabriel L.; Chandler, Jesse M., Gas turbine engine with plural accessory air paths.
  34. Morris, Timothy M.; Spock, Wayne R.; Smith, Peter Gerard; Schryver, Matthew J.; Walther, Ronald S.; Gukeisen, Robert L.; Hagaman, Edward T., Hybrid engine accessory power system.
  35. Morris, Timothy M.; Spock, Wayne R.; Smith, Peter Gerard; Schryver, Matthew J.; Walther, Ronald S.; Gukeisen, Robert L.; Hagaman, Edward T., Hybrid engine accessory power system.
  36. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Elder, James S., Integrated actuator module for gas turbine engine.
  37. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Elder, James S., Integrated actuator module for gas turbine engine.
  38. Lui Clarence, Integrated bleed air and engine starting system.
  39. Weber Kent, Integrated emergency power and environmental control system.
  40. Leamy, Kevin Richard; Breig, Benjamin Paul; Epstein, Michael Jay; Parrilla, Javier Armando; Hurt, Matthew John; Brinson, Thomas Edward; Fleming, Andrew James, Jet engine cold air cooling system.
  41. DeFrancesco, Gregory L., Low pressure bleed architecture.
  42. Schwarz, Frederick M.; Suciu, Gabriel L., Low pressure environmental control system with safe pylon transit.
  43. Jonqueres, Michel A.; Araki, Roy, Low-pressure bleed air aircraft environmental control system.
  44. Albero, Jose; Dussault, Richard; Thompson, Robert G.; Germain, Patrick; Sahm, Michael K.; Tremaine, Eric, Main propulsion engine system integrated with secondary power unit.
  45. Weber, Kent; Kyriazopoulos, Athanasios; Hightower, Peter C.; Burie, Bradley J., Method and systems for bleed air supply.
  46. Weber, Kent; Kyriazopoulos, Athanasios; Hightower, Peter C.; Burie, Bradley J., Method and systems for bleed air supply.
  47. Stephan, Volker, Method for the control of aero gas turbine engines.
  48. Stephan,Volker, Method for the control of aero gas turbine engines.
  49. Kestler, Steven M.; Sundar, Prithvi; Li, Yuan, Method of controlling boundary layer flow.
  50. DeFrancesco, Gregory L., Method of low pressure bleed.
  51. Orlando,Robert Joseph; Moniz,Thomas Ory; Brauer,John C.; Henry,John Leslie; Patt,Raymond Felix; Vondrell,Randy Marinus; Dolan,James Patrick; Krammer,Erich Alois; Kirk,David Cory, Methods and apparatus for assembling gas turbine engines.
  52. Wollenweber, Gary C., Methods for operating gas turbine engines.
  53. Gokhale, Manoj Prakash; Klingbeil, Adam E., Multi-fuel control system and method.
  54. Gokhale, Manoj Prakesh; Klingbeil, Adam E., Multi-fuel control system and method.
  55. Brown, Keith T.; Fowler, Frank J.; Byrne, Stuart J.; Stein, Adam, Nacelle inlet with extended outer barrel.
  56. Booher, Sr., Benjamin V., Parasitic drag induced boundary layer reduction system and method.
  57. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  58. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  59. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  60. Moes, Thierry, Pnuematic system for an aircraft.
  61. Khalid, Syed J., Positionable ejector member for ejector enhanced boundary layer alleviation.
  62. Thompson Robert George, Secondary power integrated cabin energy system for a pressurized aircraft.
  63. Nenmeni, Vijay Anand Raghavendran; Alexander, Michael Joseph; Plummer, Paul William; Janssen, Timothy Lee, System and method for air extraction from gas turbine engines.
  64. Brousseau, Jean; Afrianto, Sigit; Hamel, Remi; Desilets, Valerie, System and method for operating a precooler in an aircraft.
  65. Lo, Charles; Alford, Ted; Anderson, Morris, System for directing air flow to a plurality of plena.
  66. Strasik, Michael; Fouard, Jean-Michel; Wheaton, Christopher, Systems and methods for duct protection.
  67. Gonzales, Michael D.; Strasik, Michael; Hull, John R., Systems and methods for duct protection of a vehicle.
  68. Hull, John Ralph; Strasik, Michael; Voss, Bret A.; Negley, Mark A.; Sweet, William J.; Housen, Kevin R.; Damazo, Jason S.; Gonzales, Michael D.; Ware, Michael Howard-Edward; Firth, Lee Charles, Systems and methods for duct protection of a vehicle.
  69. Zeiner, Peter Kenneth; Libera, Tony; Langston, Todd, Turbine drive system with lock-up clutch and method.
  70. Atkey, Warren A., Turbo-compressor system and method for extracting energy from an aircraft engine.
  71. Pelagatti, Olivier; Deguin, Thomas; Bodet, Ronan, Turbojet comprising a bleeding system for bleeding air in said turbojet.
  72. Wolfe, David; Minh, Nguyen Q.; Meister, Kurt; Matulich, Dan S., Turbomachine-driven environmental control system.
  73. Anderson, Morris G.; Banta, Paul W.; Brackin, James W.; Romano, Robert; Zmora, David W., Variable geometry ejector for a bleed air system using integral ejector exit pressure feedback.
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