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특허 상세정보

Integrated bleed air and engine starting system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/08    F02C-007/27   
미국특허분류(USC) 600/390.7 ; 600/391.42 ; 454/076
출원번호 US-0390412 (1999-09-03)
발명자 / 주소
  • Lui Clarence
출원인 / 주소
  • AlliedSignal Inc.
대리인 / 주소
    Zak, Jr., Esq.
인용정보 피인용 횟수 : 58  인용 특허 : 11
초록

An integrated bleed air and engine starting system for an engine utilizes an innovative flow multiplier air turbine starter to provide bleed air supply to an ECS as well as starting an engine. The technique reduces bleed air consumption by mixing fan stage air and high stage air for ECS fresh air usage. It also can eliminate or reduce the size of the precooler heat exchanger. The system includes an air turbine starter subsystem and an air flow subsystem. The air turbine starter subsystem includes a compressor, a turbine, and a common shaft fixed between ...

대표
청구항

[ What is claimed is:] [1.]1. An integrated bleed air and engine starting system for an engine, comprising:an air turbine starter subsystem comprising a turbine mechanically coupled to said engine, a compressor mechanically coupled to said turbine, and a variable nozzle upstream of said turbine;said variable nozzle having an open position that allows said bleed air to flow to said turbine; andan air flow subsystem that includes a diverter valve downstream of said turbine and an isolation valve upstream of said variable nozzle;said diverter valve having a...

이 특허를 인용한 특허 (58)

  1. Rosen, Seth E.; Beers, Craig M.; Pragluski, Robert M.; Rowley, Michael P., Air cycle machine air bearing shaft.
  2. McAuliffe, Christopher; Merritt, Brent J.; Beers, Craig M., Air cycle machine for an aircraft environmental control system.
  3. Merritt, Brent J.; Beers, Craig M., Air cycle machine integrated rotor and shaft.
  4. Coffinberry,George Albert, Air turbine powered accessory.
  5. Zawilinski, David J.; Makulec, Jeffrey M.; Ryan, Bradley Thomas; Slayter, Matthew, Air turbine starter.
  6. Zawilinski, David J.; Makulec, Jeffrey M.; Slayter, Matthew, Air turbine starter inlet housing assembly airflow path.
  7. Zawilinski, David J.; Makulec, Jeffrey M.; Slayter, Matthew, Air turbine starter turbine blade airfoil.
  8. Zawilinski, David J.; Makulec, Jeffrey M.; Ryan, Bradley Thomas; Slayter, Matthew, Air turbine starter turbine nozzle airfoil.
  9. Zawilinski, David J.; Makulec, Jeffrey M.; Slayter, Matthew, Air turbine starter turbine nozzle airfoil.
  10. Balan, Chellappa; Sheldon, Karl Edward, Aircraft auxiliary gas turbine engine and method for operating.
  11. Mackin, Steve G.; Foutch, David W.; Landre, Eric G., Aircraft bleed air and engine starter systems and related methods.
  12. Zhou, Rui; Winter, Stephen Francis; Kyriazopoulos, Athanasios; Muller, Jones Ricardo; Parilla, Javier Armando, Aircraft energy management system including engine fan discharge air boosted environmental control system.
  13. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; McCune, Michael E., Apparatus and method for operating a gas turbine engine during windmilling.
  14. Wollenweber,Gary C., Apparatus for operating gas turbine engines.
  15. Sheldon, Karl Edward; Seeley, Charles Erklin; Haber, Ludwig Christian, Auxiliary power unit assembly.
  16. Libera, Tony; Zeiner, Peter, Bi-modal turbine assembly and starter / drive turbine system employing the same.
  17. Sennoun, Mohammed El Hacin, Bleed air and hot section component cooling air system and method.
  18. Foutch, David W.; Mackin, Steve G., Bleed air systems for use with aircraft and related methods.
  19. Foutch, David W.; Mackin, Steve G.; Bowman, Michael D., Bleed air systems for use with aircraft and related methods.
  20. Mackin, Steve G.; Foutch, David W., Bleed air systems for use with aircrafts and related methods.
  21. Mackin, Steve G.; Ludlow, George A., Bleed air systems for use with aircrafts and related methods.
  22. Mackin, Steve G.; Ludlow, George A., Bleed air systems for use with aircrafts and related methods.
  23. Andrew, Philip L., Ceramic matrix composite turbine engine.
  24. Dyer, Gerald P., Combined air turbine starter, air-oil cooler, and fan.
  25. Munsell, Peter M.; Stripinis, Philip S., Compressed air bleed supply for buffer system.
  26. Suciu, Gabriel L.; Merry, Brian D.; Penda, Allan R.; Dye, Christopher M., Constant speed transmission for gas turbine engine.
  27. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; McCune, Michael E., Controllable speed windmill operation of a gas turbine engine through low spool power extraction.
  28. Silet, Fabien; Chevalier, Stephane; Rideau, Jean-Francois, Controlling method and system for compressed air supply to a pneumatic network, in particular in an aircraft.
  29. Strecker, Steven; Liu, Xiaoliu; Logan, Adam, Cooling system for engine and aircraft air.
  30. Ferra, Paul W.; Wang, Yi, Gas cooler and method for cooling gas.
  31. Gustafson,James R., Gas turbine engine system having an electric starter motor with integral clutch.
  32. Olmes, Sven; Reiter, Wilhelm; Zierer, Thomas, Gas turbine with heat exchanger for cooling compressed air and preheating a fuel.
  33. Schwarz, Frederick M.; Suciu, Gabriel L., Geared turbofan engine with low pressure environmental control system for aircraft.
  34. Blewett, Michael R.; Short, Keith E., Integrated accessory gearbox and engine starter.
  35. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Squier, Steve; Welch, Richard; Becker, Arthur Curtis, Integrated air turbine driven system for providing aircraft environmental control.
  36. Dittmar,Kevin S.; Edmonds,David H.; Schenk,Bjoern; Sheoran,Yogendra Y., Integrated gearless and nonlubricated auxiliary power unit.
  37. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Squier, Steven E.; Welch, Richard; Becker, Arthur Curtis, Integrated system for providing aircraft environmental control.
  38. Suciu, Gabriel L.; Penda, Allan R.; Merry, Brian D.; Glahn, Jorn A.; Dye, Christoper M.; Snape, Nathan, Integrated thermal management system and environmental control system for a gas turbine engine.
  39. Makulec, Jeffrey M.; Stadler, Jeffrey A., Interface with mount features for precise alignment.
  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. Rensch, Detlef, Jet engine with at least one emergency drive unit.
  42. Brown, Ryan; Olivarez, Jason; Roberts, Kenneth, Linear quadratic regulator control for bleed air system fan air valve.
  43. Ho, Yu-Hang, Magnetically coupled integrated power and cooling unit.
  44. Youssef, Nashed; Eleftheriou, Andreas; Alecu, Daniel, Method and assembly for providing an anti-icing airflow.
  45. Klimpel, Frank; Schmidt, Rüdiger, Method and system for emergency ventilation of an aircraft cabin in the case of a leak in the area of an air mixer.
  46. Weber, Kent I.; Kyriazopoulos, Athanasios; Hightower, Peter C.; Miller, Lance F.; Soave, Ronald J., Method and system for vehicle thermal management.
  47. Weber, Kent; Kyriazopoulos, Athanasios; Hightower, Peter C.; Burie, Bradley J., Method and systems for bleed air supply.
  48. Weber, Kent; Kyriazopoulos, Athanasios; Hightower, Peter C.; Burie, Bradley J., Method and systems for bleed air supply.
  49. Wollenweber, Gary C., Methods for operating gas turbine engines.
  50. Ammann, Luke J., Non-integral turbine blade platforms and systems.
  51. Stolte, Ralf-Henning, Power distribution system.
  52. Merritt, Brent; McAuliffe, Christopher, RAM fan system for an aircraft environmental control system.
  53. Clarence Lui ; Wai-Pak Wong ; Myron Quan, Recirculating regenerative air cycle.
  54. Huang, He; Kaslusky, Scott F.; Tillman, Thomas G.; DeValve, Timothy D.; Bertuccioli, Luca; Sahm, Michael K.; Spadaccini, Louis J.; Bayt, Robert L.; Lamm, Foster Philip; Sabatino, Daniel R., System and method for thermal management.
  55. Burns, Donald W., System, propulsion system and vehicle.
  56. Burns, Donald W., System, propulsion system and vehicle.
  57. Zeiner, Peter Kenneth; Libera, Tony; Langston, Todd, Turbine drive system with lock-up clutch and method.
  58. Heathco, Craig, Variable cycle gas turbine engine.