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Aircraft thermal management system with reduced exhaust re-ingestion

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 244/053.B
출원번호 UP-0515020 (2006-09-01)
등록번호 US-7857257 (2011-02-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds PC
인용정보 피인용 횟수 : 7  인용 특허 : 8
초록
▼

A thermal management system includes a cooling duct system that locates a ram air intake and an exhaust through a first aircraft surface above a second aircraft surface which locates a fan intake. During ground operations, an anti-re-ingestion door is open and a ram air door is closed such that the fan system may draw relatively cooler air from below the aircraft and exhaust the heated air above the aircraft to minimize re-ingestion of the heated exhaust. During flight operations, the anti-re-ingestion door is closed and the ram air door is open such tha...

대표
청구항
▼

What is claimed is: 1. An aircraft cooling air duct system comprising: a plenum; a ram air intake in communication with said plenum; a fan intake in communication with said plenum; and an exhaust in communication with said plenum, said exhaust at least partially above said fan intake and transverse to said ram air intake such that a fan airflow direction from said fan intake through said exhaust is generally transverse to a ram air in direction from said ram air intake. 2. The system as recited in claim 1, wherein said fan intake is below an aircraft...

이 특허에 인용된 특허 (8)

  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. Hoag Michael S. ; Plank Steven K.. Auxiliary power unit passive cooling system. USP2000076092360.
  4. McCaughan John A. I.,GB5. Boundary layer control in aerodynamic low drag structures. USP1998045743493.
  5. 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.
  6. Bollinger Robert S. (Newhall CA) Nicolai Leland M. (Castaic CA). Propulsion system for a V/STOL aircraft. USP1994015275356.
  7. Freese Richard A. ; Perez Julio. Rapid response attitude control logic for shaft-driven lift fan STOVL engine. USP2001086270037.
  8. Breit Hubert,DEX. Suction generator system in an aircraft for maintaining a laminar boundary flow. USP1999035884873.

이 특허를 인용한 특허 피인용횟수: 7

  1. Sweet, David H.. Aircraft environmental threat detection and mitigation. USP2014028655508.
  2. Afrianto, Sigit; Brousseau, Jean. Apparatus for protecting aircraft components against foreign object damage. USP20190410253691.
  3. Donovan, Eric S.; Vonderwell, Daniel J.; Heathco, Craig. Gas turbine engine heat exchanger system. USP2018039915202.
  4. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP2018059957889.
  5. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP2018049951690.
  6. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP20180810054050.
  7. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Variable geometry inlet system. USP20190310221764.

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