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특허 상세정보

Inlet muff anti-icing system for an auxiliary power unit

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02G-003/00   
미국특허분류(USC) 060/039.093; 060/782
출원번호 US-0920962 (2004-08-18)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 7  인용 특허 : 21
초록

An auxiliary power unit (APU) inlet muff anti-icing system that uses high pressure, high temperature APU compressor delivery air to melt any accumulation of ice and snow near the bottom of the muff with a tracer line coupled to a perforated gull wing fairing mounted within the inlet muff and that uses the compressor delivery air as the primary stream for an ejector to suck ice and snow melt accumulating near the fairing overboard.

대표
청구항

What is claimed is: 1. A system for removing accumulations of ice and snow from the bottom of inlet muff of an auxiliary power unit (APU), comprising: a gull wing fairing mounted within the inlet muff to direct inlet air into an inlet of the APU that has a plurality of perforations to allow air and liquid flow through the fairing into a stagnant air region of the inlet muff below the fairing; a tracer line comprising tubing that is arranged along a surface of the fairing in a general "zigzag" pattern that has an inlet coupled to a primary stream of high...

이 특허에 인용된 특허 (21)

  1. Schulze Wallace M. (West Chester OH). Aircraft engine inlet cowl anti-icing system. USP1992025088277.
  2. DuPont, Henry Morgan. Airfoil anti-icing assembly and method. USP2004036702233.
  3. Norris Richard M. (Stratford CT) Rumford Kimball J. (Fairfield CT) Youd Douglass S. (Shelton CT). Anti-icing valve. USP1989054831819.
  4. Anthony I. Skur, III. Bleed air heat exchanger integral to a jet engine. USP2002096442944.
  5. Perry Derick A. (Derby). Deicing of a geared gas turbine engine. USP1988114782658.
  6. Alain Porte FR; Stephane Viala FR. Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit. USP2002086427434.
  7. Nikkanen John P. (West Hartford CT) Bubello Robert (Meridan CT) Maier Grant P. (Glastonbury CT). Efficient anti-ice exhaust vent. USP1993115257498.
  8. Numbers Keith E.. Forced air aircraft de-icer system. USP1998055755404.
  9. Porte Alain,FRX. Hot air diffuser for a jet engine air inlet cowl with de-icing circuit. USP2000066079670.
  10. Rodgers Leonard J,GBX. Ice protection for porous structure. USP1999085944287.
  11. Linton, Alan. Ice protection system. USP2005026848656.
  12. Sheoran Yogendra Y.. Inlet vortex bustor and ice protector for auxiliary power units. USP2001076264137.
  13. Zachary Richard E. ; Hudson Roger D.. Method and apparatus for achieving power augmentation in gas turbines via wet compression. USP1999085930990.
  14. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L.. Method and apparatus for aircraft inlet ice protection. USP2004026688558.
  15. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel. Method and apparatus for aircraft inlet ice protection. USP2002046371411.
  16. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel. Method and apparatus for aircraft inlet ice protection. USP2002106457676.
  17. Radhakrishna Chilukuri. Passive control of hot air injection for swirling rotational type anti-icing system. USP2002036354538.
  18. Miller Steven M. (Jupiter FL). Side discharge anti-ice manifold. USP1993065220785.
  19. Arnold Michael J. (Bangor GB5) Cole Derek (Bangor GB5). Thermal anti-icing of aircraft structures. USP1995035400984.
  20. McLaren Douglas (Seattle WA) Orr William W. (Mercer Island WA). Thermal anti-icing system for aircraft. USP1991045011098.
  21. Bouiller Philippe (Samoreau FRX) Corbin Claude G. (Voisenon FRX) Franchet Michel (Cesson FRX) Jourdain Gerard E. A. (Saintry Sur Seine FRX). Turbojet equipped with a deicing system on the intake case. USP1997045623821.