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특허 상세정보

Compression system for turbomachine heat exchanger

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-005/18    F01D-005/08   
미국특허분류(USC) 415/001; 415/115; 415/116; 415/122.1; 415/178; 415/179
출원번호 US-0914976 (2010-10-28)
등록번호 US-8602717 (2013-12-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds P.C.
인용정보 피인용 횟수 : 9  인용 특허 : 31
초록

An example turbomachine cooling arrangement includes a pump configured to pressurize a first turbomachine fluid that is then communicated through a heat exchanger assembly to remove thermal energy from a second turbomachine fluid. A portion of the pump is configured to be housed within a gearbox housing of a turbomachine.

대표
청구항

1. A turbomachine cooling arrangement comprising: a pump configured to pressurize a first turbomachine fluid that is then communicated through a heat exchanger assembly to remove thermal energy from a second turbomachine fluid, wherein at least a portion of the pump is configured to be housed within a gearbox housing of a turbomachine. 2. The turbomachine cooling arrangement of claim 1, wherein the pump is configured to be driven by the turbomachine. 3. The turbomachine cooling arrangement of claim 2, wherein a towershaft of the turbomachine rotatably dr...

이 특허에 인용된 특허 (31)

  1. Miller,Guy Wallace. Apparatus for driving an accessory gearbox in a gas turbine engine. USP2006067055330.
  2. Hoag Michael S. ; Plank Steven K.. Auxiliary power unit passive cooling system. USP2000076092360.
  3. 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. USP1988094773212.
  4. Glahn, Jorn A.. Bearing compartment pressurization and shaft ventilation system. USP2013088516828.
  5. Suciu Gabriel L. (Glastonbury CT). Bleed valve for axial flow compressor. USP1987124715779.
  6. Wakeman Thomas G. (West Chester OH). Compact air-to-air heat exchanger for jet engine application. USP1980024187675.
  7. Elovic Ernest (Cincinnati OH). Cooling air cooler for a gas turbofan engine. USP1981034254618.
  8. Baldwin Jeffrey D. (Rockford IL) Wagle Ellen J. (Indianapolis IN) Lai Jude C. T. (Rockford IL). Cooling arrangement and method for offset gearbox. USP1994105359247.
  9. McArthur Malcolm J. (Escondido CA). Cooling system for auxiliary power unit. USP1992045105875.
  10. Griffin James G. (West Hartford CT) Schwarz Frederick M. (Glastonbury CT). Cooling system for the electrical generator of a turbofan gas turbine engine. USP1984104474001.
  11. Perry Derick A. (Derby). Deicing of a geared gas turbine engine. USP1988114782658.
  12. 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. USP1993115265408.
  13. Noiseux,Noel; Bernard,Martin; Whiting,Michael Owen. Fire shield apparatus and method. USP2006057040576.
  14. Seed Bernard E. (Nottingham GB2). Fluid outlet duct. USP1988124791782.
  15. Shekelton Jack R. (San Diego CA) Johnson Douglas C. (Corona CA). Gas turbine annular combustor with radial dilution air injection. USP1991105058375.
  16. Vermejan Alexander E. (Mason OH) Daiber Paul C. (Cincinnati OH) Morton Scott C. (Cincinnati OH) Taylor Michelle L. (Cincinnati OH). Gas turbine engine fan cooled heat exchanger. USP1993125269135.
  17. Loxley Russell A. (Leicestershire GB2) Clarke Andrew (Nottingham GB2). Heat exchange apparatus for gas turbine fluids. USP1995085438823.
  18. Mortimer, Thomas P.; Suciu, Gabriel L.. Heat exchange system. USP1985104546605.
  19. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  20. Johnston Richard P. (Morrow OH). Method and apparatus for supplying compressed air to auxiliary systems of a vehicle. USP1991085039281.
  21. 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. USP1994025284012.
  22. Parnes Marvin J. (Norwalk CT) Vogel Herman (Newtown CT). Oil cooler for fan jet engines. USP1990044914904.
  23. Rago Giusseppe,CAX. Oil pump. USP2001056237322.
  24. 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. USP1997085655359.
  25. Dionne, Luc. Passive cooling system for auxiliary power unit installation. USP2003116651929.
  26. Dionne, Luc. Passive cooling system for auxiliary power unit installation. USP2005096942181.
  27. Sheoran,Yogendra Y.; Payne,Roger I.. System and method for dumping surge flow into eductor primary nozzle for free turbine. USP2006127152410.
  28. Hagshenas,Bezhad. Thermal management for aircraft auxiliary power unit compartment. USP2008037337605.
  29. Suciu, Gabriel L.; Merry, Brian. Tip turbine engine with a heat exchanger. USP2009127631485.
  30. Rd Klaus (Grbenzell DEX) Rohra Alois (Mnchen DEX). Turbo engine. USP1991034999994.
  31. Mouton Pierre C. (Grigny FRX). Turbojet compressor blow off valves with water collecting and discharge means. USP1991095044153.

이 특허를 인용한 특허 피인용횟수: 9

  1. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M.. Accessory gearbox buffer cooling air pump system. USP2015038967944.
  2. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; McCune, Michael E.. Apparatus and method for operating a gas turbine engine during windmilling. USP2015038978352.
  3. 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. USP2016079394803.
  4. Suciu, Gabriel L.; Merry, Brian D.; Glahn, Jorn A.; Dye, Christopher M.. Constant speed pump system for engine ECS loss elimination. USP2015109163562.
  5. 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. USP2015109151224.
  6. Kupratis, Daniel Bernard; Hanrahan, Paul R.. Cooled cooling air system for a gas turbine engine. USP20181010100739.
  7. Ancuta, Carmen; Beutin, Bruno Albert. Electroformed nickel-chromium alloy. USP20180710036322.
  8. 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. USP2015038978351.
  9. Suciu, Gabriel L.; Chandler, Jesse M.; Staubach, Joseph Brent; Merry, Brian D.. Intercooled cooling air tapped from plural locations. USP20190310221862.