Dispatch critical fuel tank inerting system for aircraft
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B01D-053/22
B64D-037/32
출원번호
US-0558616
(2009-09-14)
등록번호
US-8147579
(2012-04-03)
발명자
/ 주소
DeFrancesco, Gregory L.
Rebours, Renaud
출원인 / 주소
Hamilton Sundstrand Corporation
대리인 / 주소
Carlson, Gaskey & Olds, PC
인용정보
피인용 횟수 :
3인용 특허 :
11
초록▼
An air inerting system for supplying nitrogen-enriched air to a fuel tank on a vehicle includes an air separation module. The air separation module has an inlet for receiving air to separate oxygen, and an outlet for delivering nitrogen-enriched air to a downstream fuel tank on a vehicle. Downstream
An air inerting system for supplying nitrogen-enriched air to a fuel tank on a vehicle includes an air separation module. The air separation module has an inlet for receiving air to separate oxygen, and an outlet for delivering nitrogen-enriched air to a downstream fuel tank on a vehicle. Downstream parallel flow lines of the outlet are each provided with a flow control valve. The downstream parallel flow lines reconnect downstream of the flow control valves to provide a source of nitrogen-enriched air to the fuel tank. An air supply line upstream of the air separation module supplies air to at least a pair of upstream parallel lines. Each of the upstream parallel lines are provided with a shut-off valve. The upstream parallel lines reconnect downstream of the shut-off valves to supply air to a heat exchanger. Air downstream of the heat exchanger passes to the air separation module.
대표청구항▼
1. An air inerting system for supplying a nitrogen-enriched air to a fuel tank on a vehicle comprising: an air separation module having an inlet for receiving air to separate oxygen and made into a nitrogen-enriched air, and an outlet for delivering nitrogen-enriched air to a downstream fuel tank on
1. An air inerting system for supplying a nitrogen-enriched air to a fuel tank on a vehicle comprising: an air separation module having an inlet for receiving air to separate oxygen and made into a nitrogen-enriched air, and an outlet for delivering nitrogen-enriched air to a downstream fuel tank on a vehicle, and there being downstream parallel flow lines downstream of said outlet, with each of said downstream parallel lines being provided with a flow control valve, and said downstream parallel lines reconnecting downstream of said flow valves to provide a source of nitrogen-enriched air to the fuel tank; andan air supply line upstream of said air separation module, and said air supply line supplying air to at least a pair of upstream parallel lines, each of said upstream parallel lines being provided with a shut-off valve, and said upstream parallel lines reconnecting downstream of said shut-off valves to supply air to a heat exchanger, air downstream of said heat exchanger passing to said air separation module. 2. The system as set forth in claim 1, wherein temperature sensors are provided on at least one of said upstream and downstream parallel lines, with said temperature sensor being provided with a pair of probes. 3. The system as set forth in claim 2, wherein a first temperature sensor is provided upstream of said upstream parallel lines, and a second temperature sensor is provided intermediate said heat exchanger and said air separation module, and a third temperature sensor is provided downstream of said air separation module, with each of said first, second, and third temperature sensors being provided with redundant probes. 4. The system as set forth in claim 3, wherein said third temperature sensor includes a third and fourth temperature sensor, with one of said third and fourth temperature sensors being mounted in each of said downstream parallel lines. 5. The system as set forth in claim 1, wherein said heat exchanger cools the air passing to said air separation module, and said heat exchanger received in a duct. 6. The system as set forth in claim 5, wherein a damper valve controls the amount of cooling air passing through said duct over said heat exchanger, and said valve being provided with a pair of motors. 7. The system as set forth in claim 6, wherein a tap line taps a portion of air leading to said heat exchanger as an injector air to be injected into said duct. 8. The system as set forth in claim 7, wherein a shut-off valve is provided on said tap line, and said shut-off valve being provided with a pair of redundant motors. 9. The system as set forth in claim 1, wherein the shut-off valves in said upstream and downstream flow lines are each failure closed valves which are biased to a closed position when said valve fails. 10. The system as set forth in claim 1, wherein air being delivered to said heat exchanger passes to a compressor mounted in each of said upstream parallel flow lines. 11. The system as set forth in claim 10, wherein said compressors are positioned downstream of said shut-off valves. 12. The system as set forth in claim 11, wherein said compressor includes a pair of compressor stages, with air delivered from a lower compression stage, then being delivered to a higher compression stage in each of said upstream parallel flow lines. 13. The system as set forth in claim 12, wherein air passes from said lower compression stage through a cooler, said cooler being placed in the path of cooling air, such that air in said cooler is cooled before being delivered to said higher compression stage. 14. The system as set forth in claim 13, wherein air from said higher compression stage then passing through said heat exchanger before being delivered into said air separation module. 15. The system as set forth in claim 14, wherein both said cooler and said heat exchanger are positioned in a common duct.
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이 특허에 인용된 특허 (11)
Cass Michael Andrew ; Short Keith Everett, Aircraft engine fuel system mounting assembly.
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