Redundant integrated liquid cooling system for avionics
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B60H-001/00
F28F-001/00
B64D-013/00
B64D-013/06
출원번호
US-0852567
(2013-03-28)
등록번호
US-9752834
(2017-09-05)
우선권정보
DE-10 2012 006 628 (2012-03-30)
발명자
/ 주소
Schöll, Robert
Terzi, Cherif
출원인 / 주소
AIRBUS OPERATIONS GMBH
대리인 / 주소
Dickinson Wright
인용정보
피인용 횟수 :
0인용 특허 :
6
초록▼
A cooling system cools at least one heat producing device provided in a unit of transport, and a method is provided for cooling at least one heat producing device provided in a unit of transport. The cooling system includes at least one first liquid circuit and at least one first heat exchanger assi
A cooling system cools at least one heat producing device provided in a unit of transport, and a method is provided for cooling at least one heat producing device provided in a unit of transport. The cooling system includes at least one first liquid circuit and at least one first heat exchanger assigned to the first liquid circuit, the first liquid circuit, for cooling the at least one first heat producing device, being configured to absorb heat of the first heat producing device via a cooling liquid circulating in the first liquid circuit and dissipate heat to the first heat exchanger, the first heat exchanger being coupled in such a manner to a first air-guiding system available on board the unit of transport, that exhaust air extracted from the first air-guiding system can be supplied to the first heat exchanger in order to recool the cooling liquid.
대표청구항▼
1. A cooling system for cooling at least one first heat producing device provided on-board a means of transport, the cooling system comprising: at least one first liquid circuit,at least one first heat exchanger assigned to the first liquid circuit,the first liquid circuit, for cooling the at least
1. A cooling system for cooling at least one first heat producing device provided on-board a means of transport, the cooling system comprising: at least one first liquid circuit,at least one first heat exchanger assigned to the first liquid circuit,the first liquid circuit, for cooling the at least one first heat producing device provided on board the means of transport, being configured to absorb heat of the first heat producing device by a cooling liquid circulating in the first liquid circuit and dissipate heat to the first heat exchanger, andone of a first fan and a first pressure regulating valve assigned to the first liquid circuit, the one of the first fan and the first pressure regulating valve being configured to extract first exhaust air by sucking the exhaust air, via a first pipe arrangement, out of a first exhaust air system available on board the means of transport, the extracted first exhaust air flowing through the first heat exchanger in order to recool the cooling liquid, andthe cooling system further comprising:at least one second liquid circuit,at least one second heat exchanger assigned to the second liquid circuit,the second liquid circuit, for cooling at least one second heat producing device provided on board the means of transport, being configured to absorb heat of the second heat producing device by a cooling liquid circulating in the second liquid circuit and dissipate heat to the second heat exchanger, andone of a second fan and a second pressure regulating valve assigned to the second liquid circuit, the one of the second fan and the second pressure regulating valve being configured to extract second exhaust air by sucking the exhaust air, via a second pipe arrangement, out of a second exhaust air system available on board the means of transport, the extracted second exhaust air flowing through the second heat exchanger in order to retool the cooling liquid. 2. The cooling system according to claim 1, the at least one first heat exchanger being arranged in a first region of the means of transport and/or the at least one second heat exchanger being arranged in a second region separated from the first region. 3. The cooling system according to claim 2, the first region comprising a first side of a centre plane running through a longitudinal axis of the means of transport and/or the second region comprising a second side of the centre plane running through the longitudinal axis of the means of transport. 4. The cooling system according to claim 2, at least one of the at least one first liquid circuit, for cooling at least one of the at least one first heat producing device, extending at least partially in the first region and/or at least one of the at least one second liquid circuit, for cooling at least one of the at least one second heat producing device, extending at least partially in the second region. 5. The cooling system according to claim 2, at least one of the at least one first liquid circuit, for cooling at least one of the at least one second heat producing device, extending at least partially in the second region and/or at least one of the at least one second liquid circuit, for cooling at least one of the at least one first heat producing device, extending at least partially in the first region. 6. The cooling system according to claim 2, at least one of the at least one first liquid circuit, for cooling all of the at least one first heat producing device, extending at least partially in the first region and/or at least one of the at least one second liquid circuit, for cooling all of the at least one second heat producing device, extending at least partially in the second region. 7. The cooling system according to claim 2, at least one of the at least one first liquid circuit, for cooling at least one of the at least one first heat producing device, extending at least partially in the first region and, for cooling at least one of the at least one second heat producing device, extending at least partially in the second region and/or at least one of the at least one second liquid circuit, for cooling at least one of the at least one first heat producing device, extending at least partially in the first region and, for cooling at least one of the at least one second heat producing device, extending at least partially in the second region. 8. Cooling system according to claim 1, the cooling system further comprising one or more fans and/or one or more pressure regulating valves which are each arranged in such a manner in the cooling system and so configured as to extract the exhaust air from the first air-guiding system, for example the first exhaust air system, and/or the second air-guiding system, for example the second exhaust air system, and also one or more pipe arrangements which are each configured to supply the extracted exhaust air to the first and/or the second heat exchanger in order to recool the cooling liquid. 9. Cooling system according to claim 1, the cooling system being so configured that outside air surrounding the means of transport and/or inside air present inside the means of transport and surrounding the cooling system can be supplied to the first and/or the second heat exchanger in order to cool the cooling liquid, and the exhaust air extracted from the first air-guiding system, for example the first exhaust air system, and/or the second air-guiding system, for example the second exhaust air system, can be guided past the first and/or second heat exchanger via one or more bypass arrangements. 10. Cooling system according to claim 9, the cooling system further comprising a valve arrangement and/or a pipe stop arrangement which is configured to isolate the supplied outside air and/or the supplied inside air from the exhaust air guided via the bypass arrangement. 11. Cooling system according to claim 1, the cooling system further comprising one or more thermoelectric cooling elements which are each arranged in such a manner in the first and/or in the second liquid circuit and so configured that the one or more thermoelectric cooling elements absorb heat from the cooling liquid in the inflow of the first and/or of the second liquid circuit and dissipate heat to the cooling liquid in the outflow of the first and/or of the second liquid circuit. 12. Use of the cooling system according to claim 1 for cooling at least one first heat producing device provided in a means of transport, for example in an aircraft. 13. Means of transport, for example aircraft, comprising the cooling system according to claim 1.
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이 특허에 인용된 특허 (6)
Scherer, Thomas; Schmidt, Ruediger; Solntsev, Alexander, Air supply for an aircraft.
Thomson Mark W. (Ventura CA) Matulich Dan S. (Rolling Hills Estates CA), Contaminate neutralization system for use with an advanced environmental control system.
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