Method and system for emergency ventilation of an aircraft cabin in the case of a leak in the area of an air mixer
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64D-013/00
B64C-001/18
B64D-013/02
B64C-001/00
출원번호
US-0126544
(2009-09-08)
등록번호
US-9266601
(2016-02-23)
우선권정보
DE-10 2008 058 451 (2008-11-21)
국제출원번호
PCT/EP2009/006510
(2009-09-08)
§371/§102 date
20110826
(20110826)
국제공개번호
WO2010/057548
(2010-05-27)
발명자
/ 주소
Klimpel, Frank
Schmidt, Rüdiger
출원인 / 주소
Airbus Operations GmbH
대리인 / 주소
Wood, Herron & Evans, LLP
인용정보
피인용 횟수 :
1인용 특허 :
27
초록▼
In a method for emergency ventilation of an aircraft cabin, a leak is detected in the area of an air mixer of an aircraft air conditioning system. An emergency air flap, which in a closed position prevents an air exchange between an aircraft area adjacent to the air mixer and the aircraft cabin, is
In a method for emergency ventilation of an aircraft cabin, a leak is detected in the area of an air mixer of an aircraft air conditioning system. An emergency air flap, which in a closed position prevents an air exchange between an aircraft area adjacent to the air mixer and the aircraft cabin, is controlled into an open position. Air from the aircraft area adjacent to the air mixer is conveyed through the open emergency air flap into the aircraft cabin.
대표청구항▼
1. A method for emergency ventilation of an aircraft cabin in an aircraft, comprising: detecting a leak in the area of an air mixer of an aircraft air conditioning system, through which air escapes from the air mixer into an aircraft area, the aircraft area being adjacent to the air mixer and within
1. A method for emergency ventilation of an aircraft cabin in an aircraft, comprising: detecting a leak in the area of an air mixer of an aircraft air conditioning system, through which air escapes from the air mixer into an aircraft area, the aircraft area being adjacent to the air mixer and within the aircraft,electronically controlling an emergency air flap, which in a closed position prevents an air exchange between the aircraft area adjacent the air mixer and the aircraft cabin, into an open position, which allows air escaping from the air mixer to flow out of the aircraft area adjacent the air mixer into the aircraft cabin, andconveying air from the aircraft area adjacent the air mixer through the open emergency air flap into the aircraft cabin. 2. The method according to claim 1, further comprising: controlling an air outlet valve of an aircraft cabin pressure control system into an open position in such a way as to generate in another area of the aircraft that is adjacent to the air outlet valve a pressure that is lower than the pressure in the aircraft area. 3. The method according to claim 1, further comprising: controlling an air conditioning unit of the aircraft air conditioning system in such a way that a maximum air-mass flow is generated by the air conditioning unit and supplied to the air mixer. 4. The method according to claim 1, further comprising: controlling an emergency ram-air inlet flap into an open position so that aircraft ambient air is supplyable through an emergency ram-air inlet to the air mixer. 5. The method according to claim 1, further comprising: controlling recirculation fans of the aircraft air conditioning system in such a way that their operation is interrupted. 6. The method according to claim 1, wherein the emergency air flap is disposed in a cabin trim panel or formed by a cabin trim panel. 7. A system for emergency ventilation of an aircraft cabin in an aircraft, comprising: an electronic control unit, which detects a leak in the area of an air mixer of an aircraft air conditioning system, through which air escapes from the air mixer into an aircraft area, the aircraft area being adjacent to the air mixer and within the aircraft, and which electronically controls an emergency air flap, which in a closed position prevents an air exchange between the aircraft area adjacent the air mixer and the aircraft cabin, into an open position, which allows air escaping from the air mixer to flow out of the aircraft area adjacent the air mixer into the aircraft cabin, anda device that causes air to be conveyed from the aircraft area adjacent the air mixer through the open emergency air flap into the aircraft cabin. 8. The system according to claim 7, wherein the device that causes air to be conveyed from the aircraft area into the aircraft cabin comprises an air outlet valve of an aircraft cabin pressure control system that is adapted to be controlled into an open position in such a way as to generate in another area of the aircraft adjacent to the air outlet valve a pressure that is lower than the pressure in the aircraft area. 9. The system according to claim 7, wherein the electronic control unit is further adapted to control an air conditioning unit of the aircraft air conditioning system in such a way that a maximum air-mass flow is generated by the air conditioning unit and supplied to the air mixer. 10. The system according to claim 7, wherein the electronic control unit is further adapted to control an emergency ram-air inlet flap into an open position so that aircraft ambient air is supplyable through an emergency ram-air inlet to the air mixer. 11. The system according to claim 7, wherein the electronic control unit is further adapted to control recirculation fans of the aircraft air conditioning system in such a way that their operation is interrupted. 12. The system according to claim 7, wherein the emergency air flap is disposed in a cabin trim panel or formed by a cabin trim panel.
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이 특허에 인용된 특허 (27)
Dechow Martin (Hamburg DEX) Scherer Thomas (Hamburg DEX), Air conditioning system for a passenger aircraft.
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Frawley Robert C. (Shelton CT) Perrotta Thomas (Brookfield CT) Barnard Richard S. (Monroe CT), Integrated environmental control system for a helicopter.
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Leland, Bradley C.; Lundy, Brian F.; Klinge, John D., System, method, and apparatus for throat corner scoop offtake for mixed compression inlets on aircraft engines.
Ding, Yigong; Yao, Weizheng; Zhang, Jian; Ruan, Weihua; Wang, Dawei, Circulative cooling system and method for controlling circulation in the cooling system.
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