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Gas turbine engine fan cooled heat exchanger 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
출원번호 US-0015243 (1993-02-05)
발명자 / 주소
  • Vermejan Alexander E. (Mason OH) Daiber Paul C. (Cincinnati OH) Morton Scott C. (Cincinnati OH) Taylor Michelle L. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 71  인용 특허 : 0

초록 ▼

A fan-jet gas turbine engine heat exchanger is cooled by fan air taken from the fan duct at a relatively high pressure region of the fan nozzle upstream of the fan nozzle\s throat and exhausted into a relatively low pressure region of the fan nozzle upstream of the throat. One embodiment provides a

대표청구항 ▼

A cooling apparatus for a heat exchanger used with an aircraft gas turbine engine having a fan duct including a fan nozzle and fan nozzle throat, said cooling apparatus comprising: a cooling air duct means, said cooling air duct means having a cooling duct inlet at a relatively high pressure region

이 특허를 인용한 특허 (71)

  1. Marini, Remo; Germain, Patrick; Vrljes, Ljubisa, Air cooler system for gas turbine engines.
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  2. Marini, Remo; Germain, Patrick; Vrljes, Ljubisa, Air cooler system for gas turbine engines.
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  3. Cheong, Chee Yuen, Air recovery system for precooler heat-exchanger.
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  7. Lo, Charles, Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine.
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  17. Thies, Robert, Device for the extraction of bleed air and aircraft engine with at least one device for the extraction of bleed air.
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  23. Riehle, Bradford J.; Loebig, James C., Fan by-pass duct for intercooled turbo fan engines.
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  25. Bulin, Guillaume; Stolte, Ralf-Henning, Fluid-cooling device for a turbine engine propulsive unit.
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  28. Coffinberry, George Albert, Gas turbine engine fan bleed heat exchanger system.
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  30. Lo, Charles, Gas turbine engine in-board cooled cooling air system.
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  31. Suciu, Gabriel L., Gas turbine engine thermal management system for heat exchanger using bypass flow.
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  32. Pritchard, Jr., Byron Andrew; Califf, Charles Daniel; Wood, Peter John; Holm, Raymond Gust; van de Wall, Allan George; Pezzi, Peter Alfred, Gas turbine engine variable bleed valve for ice extraction.
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  34. Campbell, Xiaojun; Phillips, Thomas G.; Phillips, Kathleen R., Heat exchanger.
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  44. Snape, Nathan; Suciu, Gabriel L.; Pickford, Simon; Penda, Allan R., Low profile compressor bleed air-oil coolers.
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  45. Storage, Michael Ralph; Leamy, Kevin Richard; Neal, Brian, Method and apparatus for operating gas turbine engine heat exchangers.
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  60. Noureldin, Mahmoud Bahy, System, method, and program product for synthesizing non-thermodynamically constrained heat exchanger networks.
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  61. Noureldin, Mahmoud Bahy, System, method, and program product for targeting and identification of optimal process variables in constrained energy recovery systems.
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  62. Noureldin, Mahmoud Bahy, Systems and program product for heat exchanger network energy efficiency assessment and lifetime retrofit.
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  63. Schwarz, Frederick M.; Gorbounov, Mikhail B., Thermal management system for turbofan engines.
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  64. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M., Thermal management system integrated pylon.
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  65. Kwok, David W.; Huang, James P.; Mauldin, Jack W., Thermoelectric generator in turbine engine nozzles.
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  66. Beutin, Bruno Albert; Llamas Castro, Nuria; Ramos, Bruna, Turbine engine having an element for deflecting foreign objects.
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  67. Yoshinaka Tsukasa, Turbine engine with intercooler in bypass air passage.
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  68. Olver, Bryan; Ciampa, Alessandro; Marrano, Roberto; Trepanier, Richard; Lamarre, Sylvain; Bernard, Martin; Germain, Patrick, Turbofan bypass duct air cooled fluid cooler installation.
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  69. Winter, Michael, Turbofan engine with variable bypass nozzle exit area and method of operation.
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  70. Bulin, Guillaume; Oberle, Patrick, Turbojet for aircraft.
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  71. Bulin, Guillaume; Oberle, Patrick, Turboreactor for aircraft.
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