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Turboprop engine with an air-oil cooler 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/12
출원번호 US-0983115 (1998-07-06)
우선권정보 DE-0024731 (1995-07-07)
국제출원번호 PCT/EP96/02634 (1996-06-18)
§371/§102 date 19980706 (19980706)
국제공개번호 WO-9702985 (1997-01-30)
발명자 / 주소
  • Steiner Kurt,DEX
출원인 / 주소
  • Bayerische Motoren Werke Aktiengesellschaft, DEX
대리인 / 주소
    Evenson, McKeown, Edwards & Lenahan, P.L.L.C.
인용정보 피인용 횟수 : 42  인용 특허 : 2

초록

A turboprop engine in the pod of which an air-oil cooler is disposed downstream of a cooling air inlet opening. The oil cooler exhaust air is discharged via an air duct with which a cooling air conveying device is associated. In this way it is ensured that there is always a sufficient cooling air fl

대표청구항

[ What is claimed:] [1.] A turboprop engine, comprising:an engine casing defining an interior and defining an cooling air inlet opening into said interior for cooling air;a cooling air guiding duct adjoining said inlet opening, said cooling air guiding duct being directed to at least one assembly to

이 특허에 인용된 특허 (2)

  1. Geidel Helmut (Karlsfeld DEX) Rohra Alois (Mnchen DEX), Propfan turbine engine.
  2. Rd Klaus (Grbenzell DEX) Rohra Alois (Mnchen DEX), Turbo engine.

이 특허를 인용한 특허 (42)

  1. Sennoun, Mohammed El Hacin; Bonar, James Fitzgerald; Levine, Rachel Wyn, Additively manufactured heat exchanger.
  2. Devine, Michael Thomas, Adjustable size inlet system.
  3. Alecu, Daniel; Kostka, Richard, Air cooled air cooler for gas turbine engine air system.
  4. Alecu, Daniel; Kostka, Richard, Air cooled air cooler for gas turbine engine air system.
  5. Todorovic, Predrag, Air ejector nozzle tube for an oil heat exchanger of an aircraft engine.
  6. Schnoor, Martin, Air intake for an auxiliary power unit in an aircraft.
  7. Stearns, Ethan K.; Glahn, Jorn A.; McKaveney, Daniel J., Air oil cooler airflow augmentation system.
  8. Alecu, Daniel T., Air-cooled oil cooler for turbofan engine.
  9. Hoag Michael S. ; Plank Steven K., Auxiliary power unit passive cooling system.
  10. Jones, Anthony; Julien, Andre; Menheere, David; Thomassin, Jean; Ullyott, Richard, Auxiliary power unit with combined cooling of generator.
  11. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M., Bypass air-pump system within the core engine to provide air for an environmental control system in a gas turbine engine.
  12. Suciu, Gabriel L.; Lord, Wesley K.; Chandler, Jesse M., Bypass duct heat exchanger with controlled fan.
  13. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Bilodeau, Jade; Julien, Andre; Legare, Pierre-Yves; Nichols, Jason, Compound engine assembly with coaxial compressor and offset turbine section.
  14. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves, Compound engine assembly with common inlet.
  15. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves, Compound engine assembly with modulated flow.
  16. Suciu, Gabriel L.; Merry, Brian D.; Glahn, Jorn A.; Dye, Christopher M., Constant speed pump system for engine ECS loss elimination.
  17. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M., Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination.
  18. Schwarz, Frederick M., Cooling exchanger duct.
  19. Schwarz, Frederick M., Cooling exchanger duct.
  20. Schwarz, Frederick M.; Glahn, Jorn A., Cooling exchanger ducts.
  21. Beutin Bruno Albert,FRX ; Brossier Pascal Noel,FRX ; Franchet Michel Fran.cedilla.ois Raymond,FRX ; Lecordix Jean-Loic Herve,FRX ; Loubet Marc Georges,FRX, Cooling system for a turbomachine speed reducer.
  22. Jones, Alan R., Cooling systems.
  23. Jones,Alan R, Cooling systems.
  24. Piesker, Markus, Device for cooling hot gas to be discharged from an aircraft.
  25. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M.; Snape, Nathan; Howlett, Matthew J.; Dixon, Matthew G., Distributed lubrication system.
  26. Julien, Andre; Thomassin, Jean; Courtois, Maxime; Villeneuve, Bruno; Dussault, Serge; Ullyott, Richard; LaFortune, Serge; Dionne, Luc; Jones, Anthony; Hagshenas, Behzad; Menheere, David, Engine assembly with combined engine and cooling exhaust.
  27. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves, Engine intake assembly with selector valve.
  28. Verseux, Olivier, Fairing device for aircraft propulsion assembly comprising an internal compartment fitted with a fan.
  29. Whiting,Michael Owen, Forced air cooling system.
  30. Forcier, Matthew J., Gas turbine engine with lower bifurcation heat exchanger.
  31. Nannoni, Fabio; Ballerio, Dante; Scandroglio, Alessandro, Helicopter.
  32. Horn, Mark D., Integral oil system.
  33. Francisco, Jay M.; Napier, James C.; Sapiro, Dan G.; Hagshenas, Behzad, Mixed-flow exhaust silencer assembly.
  34. Mylemans, John A, Oil cooler having adjustable heat transfer effectiveness.
  35. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  36. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  37. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  38. Dionne,Luc, Passive cooling system for auxiliary power unit installation.
  39. Darrow, Jr., David A.; Tully, Thomas L., Propeller gearbox oil cooler for a rotary wing aircract.
  40. Larkin,Michael J.; Eiler,Donald C., Supplemental oil cooler airflow for gas turbine engine.
  41. Junod, Larry Allen, Thermal management system.
  42. Van Der Woude, Matthijs, Turboprop engine with an apparatus for the generation of a cooling airflow.
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