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특허 상세정보

Aircraft cooling duct

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/38   
미국특허분류(USC) 244/117A;
출원번호 US-0093157 (2006-11-07)
등록번호 US-8960601 (2015-02-24)
우선권정보 GB-0523570.0 (2005-11-18)
국제출원번호 PCT/GB2006/004151 (2006-11-07)
§371/§102 date 20080509 (20080509)
국제공개번호 WO2007/057638 (2007-05-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lowe Hauptman & Ham, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 13

An aircraft structure, for example a wing, includes a section of skin, for example a lower wing panel, the panel defining an external (lower) surface that in use is on the exterior of the aircraft and an internal (upper) surface opposite the external surface, and a duct comprising a section of duct for transporting cooling fluid, for example air, between the internal and external surfaces of the panel from a first location in the panel to a second location that is spaced apart from the first location in a direction substantially parallel to the external ...


1. An aircraft structure including a lower skin and an upper skin, comprising: a section of lower skin, the lower skin defining an external surface that in use is on the exterior of the aircraft and an internal surface directly opposite the external surface, and wherein the section of lower skin is defined by one or more panels,a duct comprising a section of duct defined by a region between the internal and the external surfaces of the lower skin, said section of duct transporting cooling fluid along said region from a first location in the lower skin to...

이 특허에 인용된 특허 (13)

  1. Mark D. Ralston. Aircraft auxiliary air intake with ram and flush opening door. USP2002026349899.
  2. Parikh Pradip G. ; Neumann Frank D.. Aircraft boundary layer control system with discharge transpiration panel. USP1998065772156.
  3. Reysa Gary D. ; Swenson Lynn A. ; Hutchison Robert A. ; Fung Kenny L.. Auxiliary power and thrust unit. USP2001066247668.
  4. Byron David E. (Casselberry FL). Cooling method and apparatus for wings and other fuselage components. USP1990104962903.
  5. Altoz Frank E. (Catonsville MD) Buckley John J. (Catonsville MD). Direct air cooling system for airborne electronics. USP1987064674704.
  6. Holland ; Charles L. ; Nicoloff ; George B.. Inflatable air inlet duct. USP1978104121606.
  7. Meyer,Pascal J. Laminar flow nacelle for an aircraft engine. USP2006057048230.
  8. 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.
  9. Horstman Raymond H. (Auburn WA). Perforated wing panel with variable porosity. USP1993115263667.
  10. Rouse, Gordon F.; Dupuis, Paul B.. Sensor for measuring wind angle. USP2004086772976.
  11. Bardagi Thierry Pascal,FRX ; Jourdain Gerard Ernest Andre,FRX. System for the admission of air into a working section of a gas turbine engine. USP2000076082669.
  12. Schulze Carsten (Gtting DEX) Lotter Kurt (Riemerling DEX) Malefakis Jakob (Putzbrunn DEX). Two-dimensional, unilateral oblique shock diffuser as the air inlet for a gas turbine jet engine for the propulsion of h. USP1983124418708.
  13. Bagnall,Adam M. Variable position intake for an aircraft mounted gas turbine engine. USP2006037014145.