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특허 상세정보

Airplane leading edge de-icing apparatus

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/02   
미국특허분류(USC) 244/134B; 244/134R
출원번호 US-0868410 (2013-04-23)
등록번호 US-8702039 (2014-04-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Del Vecchio and Stadler LLP
인용정보 피인용 횟수 : 1  인용 특허 : 18
초록

An airplane leading edge de-icing apparatus having a heat diffuser for heating the leading edges of an airplane is provided. The heat diffuser has a first heat diffuser side having a concave shape and a second heat diffuser side having a convex shape. The heat diffuser is joined to the leading edge of an airplane. A counter current heat exchanger is provided and heats a heat transfer fluid with heat energy absorbed from hot gases. The heat transfer fluid is pumped in and out of a reservoir tank with a first pump. A second pump pumps the heat transfer flu...

대표
청구항

1. A method of preventing or melting ice-build up on the leading edge of an airplane comprising the acts of: providing a counter current heat exchanger, and providing a reservoir tank for containing a heat transfer fluid;providing a first pump and joining a first reservoir tube to the first pump and to the reservoir tank;providing a first pump tube and a check valve and joining the first pump tube to the check valve and the first pump;providing an inlet tube and joining the inlet tube to the check valve and to the counter current heat exchanger, and join...

이 특허에 인용된 특허 (18)

  1. Whitmire Thomas W. (Winter Park FL) Hightower Edwin C. (Orlando FL). Aircraft deicer fluid heating and propulsion system. USP1993035190249.
  2. Boluk Mehmet Yaman,CAX ; Jarrell Michael Scott ; Brymer Barbara Jane ; Archambault Germain,CAX. Aircraft deicing fluid with improved anti-icing and ice adhesion control properties. USP1999105968407.
  3. Mouton Pierre C. (Grigny FRX). Anti-icing system for a gas turbine engine. USP1995065423174.
  4. Allison Robert A. (Hueytown AL). Apparatus for de-icing the leading edge of an airfoil section of an aircraft. USP1985034505445.
  5. Amako Kiyoo,JPX ; Mizuno Makoto,JPX. Deicer. USP1998125845848.
  6. Cox Dennis Michael ; Cox Joe Allen ; Palmer Richard Wayne ; Holbert James Donald. Deicing fluid recovery system especially adapted for aircraft deicing apparatus. USP1999055904321.
  7. Manda Leo J. (Florissant MO) Lavorando Michael J. (Chesterfield MO). Energy-exchange system incorporating small-diameter tubes. USP1993075228643.
  8. Brigham William D. (Huntington Beach CA) Dinh Nguyen D. (Orange City CA). Flameless deicer. USP1992035098036.
  9. Brigham William D. (Huntington Beach CA) Nguyen Dinh D. (Orange City CA). Flameless deicer. USP1993065222696.
  10. Venkataramani, Kattalaicheri Srinivasan; Moniz, Thomas Ory; Stephenson, Justin P.. Heat transfer system and method for turbine engine using heat pipes. USP2011037900437.
  11. Venkataramani, Kattalaicheri Srinivasan; Moniz, Thomas Ory; Stephenson, Justin P.; Bailey, William Andrew. Heat transfer system and method for turbine engine using heat pipes. USP2010117823374.
  12. Shah Anil D. (Seattle WA). Integrated thermal anti-icing and environmental control system. USP1976093981466.
  13. Zwick Eugene B. (16841 Edgewater La. Huntington Beach CA 92649). Method and apparatus for heating and delivering deicing fluids. USP1993095242133.
  14. Zwick Eugene B. (16841 Edgewater La. Huntington Beach CA 92649). Method and apparatus for heating and delivering deicing fluids. USP1994025282590.
  15. Koethe Terence L. (1021 Oakwood Dr. Keller TX 76248) Wilson Richard M. (Rte. 6 ; Box 918 Burleson TX 76028) Reid Gary L. (6213 Greenlee Fort Worth TX 76112). Method and apparatus for using hot fuels to de-ice aircraft. USP1996095558303.
  16. Baptist,Praba Kharan; Bharath,Keppel Nyron. Nacelle inlet lip anti-icing with engine oil. USP2006117131612.
  17. Rauckhorst ; III Richard Lawrence ; Leffel Kevin Lee. Skin for a deicer. USP1998125845878.
  18. DeSalve Dennis W. (Findlay OH). Turbine exhaust gas anti-ice system. USP1996015484122.