$\require{mediawiki-texvc}$

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.

Passive cooling system for auxiliary power unit installation

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-033/00
출원번호 US-0608224 (2003-06-30)
발명자 / 주소
  • Dionne, Luc
출원인 / 주소
  • Pratt &
  • Whitney Canada Corp.
대리인 / 주소
    Ogilvy Renault LLP
인용정보 피인용 횟수 : 36  인용 특허 : 40

초록

A passive cooling system for an auxiliary power unit (APU) installation on an aircraft is provided. The system is for an auxiliary power unit having at least a compressor portion of a gas turbine engine and an oil cooler contained separately within a nacelle. The system includes the auxiliary power

대표청구항

1. An auxiliary power unit assembly on an aircraft, the assembly comprising:an auxiliary power unit housed within a compartment of the aircraft, the auxiliary power unit including at least a compressor portion and a gas exhaust end; and an exhaust eductor in communication with the exhaust end of the

이 특허에 인용된 특허 (40)

  1. Lord Thomas J. (Dayton OH), Air inlet control for aircraft or the like.
  2. Gely Jean-Marie L. (Le Havre FRX), Air take-off for a turbojet engine cold flow duct.
  3. Negulescu Dimitrie,DEX, Aircraft gas turbine engine with a liquid-air heat exchanger.
  4. Hain Klaus (Leonberg DEX) Hofbauer August (Pforzheim DEX) Hochknig Manfred (Moglingen DEX), Airplane, preferably a helicopter.
  5. Altoz Frank E. (Baltimore MD) McClure John D. (Annapolis MD), Apparatus for cooling electronic components in aircraft.
  6. Schulze Wallace M. (West Chester OH), Auxiliary air system for gas turbine engine.
  7. Reysa Gary D. ; Swenson Lynn A. ; Hutchison Robert A. ; Fung Kenny L., Auxiliary power and thrust unit.
  8. Hoag Michael S. ; Plank Steven K., Auxiliary power unit passive cooling system.
  9. Griffin James G. (West Hartford CT) McHale Robert J. (Manchester CT) Dreisbach ; Jr. Raymond A. (Old Saybrook CT) Beck John P. (South Windsor CT), Balancing the heat flow between components associated with a gas turbine engine.
  10. 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.
  11. Griffin James G. (West Hartford CT) Schwarz Frederick M. (Glastonbury CT), Cooling system for the electrical generator of a turbofan gas turbine engine.
  12. Perry Derick A. (Derby), Deicing of a geared gas turbine engine.
  13. Bons ; Robert ; Kitaguchi ; Sam S., Eductor muffler.
  14. Sheoran Yogendra Y. (Scottsdale AZ) Schmittenberg Marc (Phoenix AZ) Lyon Craig A. (Mesa AZ) Royalty Charles M. (Tempe AZ) Kenzler Kurt T. (Chandler AZ) Davis Thomas W. (Tempe AZ), Exhaust eductor cooling system.
  15. Rodgers Leonard J. (Spondon GB2), Exhaust mixer for turbofan aeroengine.
  16. Mutch Henry (Chula Vista CA), Gas turbine engine compartment vent system.
  17. Rodgers Leonard John (Spondon EN) Stuart Alan (Ashby-de-la-Zouch EN), Gas turbine engine gas flow ducts.
  18. Ballard John R. (Sarratt GB2) Timmis Peter H. (Kings Langley GB2) Buller Michael J. (Kings Langley GB2), Gas turbine engine infra-red radiation suppressor.
  19. Marsh David N. (Phoenix AZ), Gas turbine engine rear magnetic or foil bearing cooling using exhaust eductor.
  20. Loxley Russell A. (Leicestershire GB2) Clarke Andrew (Nottingham GB2), Heat exchange apparatus for gas turbine fluids.
  21. Mortimer, Thomas P.; Suciu, Gabriel L., Heat exchange system.
  22. Pilarczyk, Karol, Heat recovery system.
  23. Sargisson Donald F. (Cincinnati OH) Lahti Daniel J. (Cincinnati OH), Hybrid mixer for a high bypass ratio gas turbofan engine.
  24. Tedstone Donald (St. Lambert CA) Schaum Hans-Herman (St. Bruno CA) Sanderson John James (St. Bruno CA), Inertial separator.
  25. Sheoran Yogendra Y., Inlet vortex bustor and ice protector for auxiliary power units.
  26. Hurley John F. (Easton CT) Hoffman Paul L. (Stratford CT), Integral infrared radiation suppressor for a turbofan engine.
  27. Mehr-Ayin Kourosh (Vista CA) Bialas W. J. (San Diego CA) Smith James A. (Escondido CA), Integrated APU.
  28. Torkelson Delbert W. (Claremore OK), Jet engine noise suppression system.
  29. Laborie Daniel J. (Cincinnati OH) Marban Joseph R. (Springdale OH) Schulze Wallace M. (West Chester OH) Baumbick Robert J. (West Chester OH), Nacelle cooling and ventilation system.
  30. Laborie Daniel J. (Cincinnati OH) Marban Joseph R. (Springdale OH) Schulze Wallace M. (West Chester OH) Baumbick Robert J. (West Chester OH), Nacelle cooling and ventilation system.
  31. Campbell Thomas A. (Seattle WA) Dummeyer David M. (Snohomish WA) Yahyavi Mohammad (Bellevue WA), Passive cooling device and method for cooling an auxiliary power unit on an airplane.
  32. Nikkanen John P. (West Hartford CT) Griffin James G. (West Hartford CT), Pressurized nacelle compartment for active clearance controlled gas turbine engines.
  33. Geidel Helmut (Karlsfeld DEX) Rohra Alois (Mnchen DEX), Propfan turbine engine.
  34. Thompson Craig E. (Gilbert AZ) Rowse Jack H. (Tempe AZ), Pusher propeller installation for turboprop engines.
  35. Vanderleest Siebold (Seattle WA), Scoop and inlet for auxiliary power units and method.
  36. Greco Robert J. (Tempe AZ) Betterton Jack D. (Mesa AZ), Spinner ducted exhaust for pusher turboprop engines.
  37. Norris Richard M. (Stratford CT) Murphy Joseph P. (Newtown CT), Swinging door particle separator and deicing system.
  38. Rd Klaus (Grbenzell DEX) Rohra Alois (Mnchen DEX), Turbo engine.
  39. Steiner Kurt,DEX, Turboprop engine with an air-oil cooler.
  40. Bubello Robert (Meriden CT) Ream Jeffrey L. (Tollano CT), Ventilation system for a nacelle.

이 특허를 인용한 특허 (36)

  1. Alecu, Daniel; Kostka, Richard, Air cooled air cooler for gas turbine engine air system.
  2. Alecu, Daniel; Kostka, Richard, Air cooled air cooler for gas turbine engine air system.
  3. Todorovic, Predrag, Air ejector nozzle tube for an oil heat exchanger of an aircraft engine.
  4. Napier, James C., Air inlet noise attenuation assembly.
  5. Da Silva, Carlos Roberto Ilário; Roncatto, André Luis; Belém, Antônio Nunes; Da Cunha, Marcelo Faria, Aircraft air inlet diverter assemblies with improved aerodynamic characteristics.
  6. Rupp, George D.; Troia, Trajaen J., Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching.
  7. DeDe, Brian C.; Martinez, David Eugene; Lau, David; Tate, Mark C., Auxiliary power unit fire enclosure.
  8. Schwarz, Frederick M., Cabin air supercharged aircraft internal combustion engine.
  9. Sheoran, Yogendra Yogi; Bouldin, Bruce Dan; Alazraki, Marcos; Kowal, Adam; Robbins, Rob; Reich, Jennifer Ann, Compartment based inlet particle separator system.
  10. 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.
  11. 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.
  12. 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.
  13. Suciu, Gabriel L.; Glahn, Jorn A.; Dye, Christopher M., Compression system for turbomachine heat exchanger.
  14. Stern, Alfred M., Cooled pusher propeller system.
  15. Stern, Alfred M., Cooled pusher propeller system.
  16. Baumgardt, Torben; Stolte, Ralf-Henning; Weber, Carsten; Reynaud, Remy; Mueller, Christian, Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system.
  17. Sheoran, Yogendra Y.; Michalski, Jr., Joseph W.; Asplund, Kyle D., Diffusing air inlet door assembly.
  18. Glahn, Jorn A.; James, Denman H.; Sheridan, William G., Dual mode scavenge scoop.
  19. Dennis,Michael R., Electrical generator fluid-flow-coolant filtration.
  20. 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.
  21. Judd, Z. Daniel, Exhaust eductor system with a recirculation baffle.
  22. Judd, Z. Daniel, Exhaust eductor system with a recirculation baffle.
  23. Francisco, Jay M.; Giddings, Greg R.; Jones, Anthony C.; Thayalakhandan, Nagamany, Exhaust silencer convection cooling.
  24. Francisco, Jay M.; Napier, James C., Exhaust silencer with baffles.
  25. Laborie, Daniel Jean-Louis, Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl.
  26. Agrawal, Rajendra K.; Sirica, Steven J.; Schneider, William F., Gas turbine engine with noise attenuating variable area fan nozzle.
  27. Horn, Mark D., Integral oil system.
  28. Cloft, Thomas G.; Wiley, Richard H., Integral suction device with acoustic panel.
  29. Cloft, Thomas G.; Wiley, Richard H., Integral suction device with acoustic panel.
  30. Francisco, Jay M.; Napier, James C.; Sapiro, Dan G.; Hagshenas, Behzad, Mixed-flow exhaust silencer assembly.
  31. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  32. Gagne, Steven; Rodriguez, Rigoberto J.; Siegel, William L.; Arvin, John R., Phase change material cooling system for a vehicle.
  33. Nager, Eric Andrew; Jones, Anthony C.; Hagshenas, Behzad; Thayalakhandan, Nagamany, Pressure influencing assembly for an aircraft auxiliary system.
  34. Swanson, Timothy A.; Elving, Carl T.; Brooks, Robert T., Single actuator controlled rotational flow balance system.
  35. Hagshenas,Bezhad, Thermal management for aircraft auxiliary power unit compartment.
  36. Junod, Larry Allen, Thermal management 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