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특허 상세정보

Core compartment valve cooling valve scheduling

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/12   
미국특허분류(USC) 600/398.3
출원번호 US-0218915 (1998-12-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Hess
인용정보 피인용 횟수 : 11  인용 특허 : 15
초록

A system is provided for cooling the undercowl environment of a gas turbine engine having a high pressure compressor and a core gas stream. An electronically controlled compartment cooling valve is controlled as a function of corrected fan speed, altitude, ambient conditions, extreme hot day temperatures and the aircraft environmental control system. A cooling manifold distributes cooling air in the undercowl environment. A regulator, such as an on-off control valve, modulates the amount of undercowl cooling flows as a function of any of a variety of con...

대표
청구항

[What is claimed is:] [1.]an electronically controlled compartment cooling valve, the valve being controlled as a function of predetermined parameters comprising corrected fan speed, altitude, ambient conditions, a predetermined temperature and an aircraft environmental control system operating state;a control unit connected to the electronically controlled compartment cooling valve for receiving as inputs the predetermined parameters to control the electronically controlled compartment cooling valve; anda cooling manifold for cooling air distribution in...

이 특허에 인용된 특허 (15)

  1. El-Aini Yehia M. ; Benedict Barry K. ; Baghdadi Samy ; Matheny A. Paul. Active rotor stage vibration control. USP2000056055805.
  2. Lenahan Dean T. (Cincinnati OH) Corsmeier Robert J. (Cincinnati OH) Sterman ; deceased Albert P. (late of Cincinnati OH by Florence G. Sterman ; executor). Air modulation apparatus. USP1983114416111.
  3. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  4. Coffinberry George A. (West Chester OH). Aircraft gas turbine engine bleed air energy recovery apparatus. USP1992085137230.
  5. Ream Jeffrey L. (Tolland CT) Bubello Robert (North Meriden CT). Buffer region for the nacelle of a gas turbine engine. USP1991055012639.
  6. Fitton David L. (South Glastonbury CT). Combined turbine power plant blade tip clearance and nacelle ventilation system. USP1984044441314.
  7. Griffin James G. (West Hartford CT) Schwarz Frederick M. (Glastonbury CT). Cooling system for the electrical generator of a turbofan gas turbine engine. USP1984104474001.
  8. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine. USP1998035724806.
  9. Glickstein Marvin R. (North Palm Beach FL) Dixon James T. (Jupiter FL) Podolsky Donald M. (Jupiter FL). High pressure air source for aircraft and engine requirements. USP1996045511374.
  10. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  11. Claeys Henry M. (Lomita CA) Clarke Kathrine J. (Hermosa Beach CA) Matulich Dan S. (Rolling Hills Estates CA). Integrated power and cooling environmental control system. USP1995085442905.
  12. Cronin Michael J. (Sherman Oaks CA). Multi role primary/auxiliary power system with engine start capability for aircraft. USP1985014494372.
  13. Cronin Michael J. (Sherman Oaks CA). Multifunction power system for an aircraft. USP1987084684081.
  14. Miller Franklin E. (Cincinnati OH). Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine. USP1992065123242.
  15. Miller Franklin E. (Cincinnati OH). Turbojet cooling system. USP1994105357742.

이 특허를 인용한 특허 피인용횟수: 11

  1. Sennoun, Mohammed El Hacin. Bleed air and hot section component cooling air system and method. USP2015129222411.
  2. 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.
  3. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M.. Combined pump system for engine TMS AOC reduction and ECS loss elimination. USP2016109470153.
  4. Friedl, Winfried-Hagen; Au, Joerg. Device for air mass flow control. USP2004086779967.
  5. Sennoun, Mohammed El Hacin; Dinsmore, Nicholas Rowe; Miller, Brandon Wayne. Environmental control system supply precooler bypass. USP2013038397487.
  6. Verseux, Olivier. Fairing device for aircraft propulsion assembly comprising an internal compartment fitted with a fan. USP20180910066551.
  7. Cloft, Thomas G.. Gas turbine engine assembly including accessory components within the nacelle. USP2014078769924.
  8. Laborie, Daniel Jean-Louis. Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl. USP2010027665310.
  9. Feeney, Mark Edward; Leslie, Keith John; Syed, Yusuf Razi; Hartropp, Simon John. Method of monitoring gas turbine engine operation. USP2013118594903.
  10. Feeney,Mark Edward; Leslie,Keith John; Syed,Yusuf Razl; Hartropp,Simon John. Method of monitoring gas turbine engine operation. USP2009027487029.
  11. Diaz, Carlos Enrique; Laborie, Daniel Jean-Louis; Geary, Stephen Dennis. Thermally actuated passive gas turbine engine compartment venting. USP2015038991191.