Systems and methods for making a fuel tank inert
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0579021
(2009-10-14)
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등록번호 |
US-8192532
(2012-06-05)
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발명자
/ 주소 |
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출원인 / 주소 |
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
5 인용 특허 :
10 |
초록
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A fuel tank safety system includes a heat exchanger in flow communication with a cabin conditioning system, a blower configured to withdraw a quantity of ullage gas from a vehicle fuel tank for routing through the heat exchanger, and conduit interconnecting the fuel tank, the blower, and the heat ex
A fuel tank safety system includes a heat exchanger in flow communication with a cabin conditioning system, a blower configured to withdraw a quantity of ullage gas from a vehicle fuel tank for routing through the heat exchanger, and conduit interconnecting the fuel tank, the blower, and the heat exchanger. The heat exchanger is configured to reduce a temperature of the ullage gas using cooling providing by the cabin conditioning system and thus reduce the fuel content (or fuel-air ratio) of the ullage below threshold required for combustion.
대표청구항
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1. A fuel tank safety system comprising: a heat exchanger in flow communication with a cabin conditioning system;a blower configured to withdraw a quantity of ullage gas from a vehicle fuel tank for routing through said heat exchanger, said blower further configured to compress said withdrawn quanti
1. A fuel tank safety system comprising: a heat exchanger in flow communication with a cabin conditioning system;a blower configured to withdraw a quantity of ullage gas from a vehicle fuel tank for routing through said heat exchanger, said blower further configured to compress said withdrawn quantity of ullage gas, said heat exchanger configured to reduce a temperature of the ullage gas using cooling provided by the cabin conditioning system; andconduit interconnecting the fuel tank, said blower, and said heat exchanger. 2. A fuel tank safety system according to claim 1 further comprising a system controller configured to control operation of said blower. 3. A fuel tank safety system according to claim 1 further comprising: a system controller;an electric motor operable to drive said blower; anda motor controller, said system controller communicatively coupled to said motor controller, said motor controller operable to control operation of said electric motor. 4. A fuel tank safety system according to claim 1 further comprising: a system controller;at least one temperature sensor positioned to provide temperature measurements of cold-air from the cabin conditioning system to said system controller; andat least one temperature sensor positioned to provide temperature measurements of an ullage region of the fuel tank to said system controller, said system controller programmed to operate said blower when the temperature of the ullage region is greater than the temperature of the cold-air from the cabin conditioning system by a defined threshold. 5. A fuel tank safety system according to claim 4 wherein said system controller programmed to shut off said blower when the temperature of the ullage region is less than the temperature of the cold-air from the cabin conditioning system by a defined threshold. 6. A fuel tank safety system according to claim 1 wherein said heat exchanger is in fluid communication with a plurality of cooling pack components associated with the cabin conditioning system. 7. A fuel tank safety system according to claim 1 wherein said conduit and said blower are operative to blow chilled ullage gas over an exposed surface of the fuel within the fuel tank. 8. A fuel tank safety system according to claim 1 further comprising a system controller further comprising a processor, said processor programmed to control operation of said blower such that the ullage gas within the fuel tank is maintained in an inert state. 9. A fuel tank safety system according to claim 1 further comprising: a system controller;at least one temperature sensor positioned to provide temperature measurements of an ullage region of the fuel tank to said system controller; andat least one pressure sensor positioned to provide measurements of pressure within the fuel tank to said system controller, said system controller programmed to determine a desired temperature for the ullage region based on the pressure measurements. 10. A fuel tank safety system according to claim 9 wherein said system controller is programmed to compare an ullage gas temperature received from said at least one temperature sensor with the desired temperature to determine whether ullage gas within the ullage region is within a non-inert range. 11. A fuel tank safety system according to claim 1 further comprising: a system controller; anda user interface communicatively coupled to said system controller, said system controller programmed to transmit a signal to said user interface when ullage gas within the ullage region is within a non-inert range. 12. A fuel tank safety system according to claim 1 further comprising: a system controller; anda user interface communicatively coupled to said system controller, said user interface comprising a manual switch, operation of said switch configured to cause said system controller to operate said fuel tank safety system. 13. A method for making a fuel tank inert, said method comprising: channeling cooling air from a cabin conditioning system through a heat exchanger;channeling a quantity of ullage gas from the fuel tank through the heat exchanger to reduce a temperature of the quantity of ullage gas, said channeling a quantity of ullage gas comprises operating a blower to withdraw the quantity of ullage gas from the fuel tank, compressing the withdrawn quantity of ullage gas with the blower, and routing the withdrawn quantity of compressed ullage gas through the heat exchanger; andreturning the quantity of reduced temperature ullage gas back to the fuel tank. 14. A method according to claim 13 wherein channeling a quantity of ullage gas from the fuel tank through the heat exchanger comprises: comparing temperature measurements of cold-air from the cabin conditioning system with temperature measurements of an ullage region of the fuel tank;causing a blower channel the quantity of ullage gas when the temperature of the ullage region is greater than the temperature of the cold-air from the cabin conditioning system by a defined threshold; andshutting the blower off when the temperature of the ullage region is less than the temperature of the cold-air from the cabin conditioning system by a defined threshold. 15. A method according to claim 13 wherein returning the quantity of reduced temperature ullage gas back to the fuel tank comprises blowing chilled ullage gas over an exposed surface of the fuel within the fuel tank. 16. A method according to claim 13 further comprising determining a desired temperature for the ullage region based on a measured pressure within the ullage region. 17. A vehicle comprising: a vehicle fuel tank, the fuel tank comprising a fuel region configured to hold a quantity of fuel, and an ullage region configured to hold a quantity of ullage gas;a heat exchanger in flow communication with a cabin conditioning system;a blower configured to withdraw a quantity of ullage gas from said vehicle fuel tank for routing through said heat exchanger, said blower further configured to compress said withdrawn quantity of ullage gas, said heat exchanger configured to reduce a temperature of the ullage gas using cooling provided by the cabin conditioning system;a first conduit interconnecting said fuel tank, said blower, and said heat exchanger; anda second conduit interconnecting said heat exchanger and the cabin conditioning system. 18. A vehicle according to claim 17 further comprising: a system controller;an electric motor operable to drive said blower; anda motor controller, said system controller communicatively coupled to said motor controller, said motor controller operable to control operation of said electric motor. 19. A vehicle according to claim 17 further comprising: a system controller;at least one temperature sensor positioned to provide temperature measurements of cold-air from the cabin conditioning system to said system controller; andat least one temperature sensor positioned to provide temperature measurements of an ullage region of said fuel tank to said system controller, said system controller programmed to operate said blower when the temperature of the ullage region is greater than the temperature of the cold-air from the cabin conditioning system by a defined threshold and shut off said blower when the temperature of the ullage region is less than the temperature of the cold-air from the cabin conditioning system by a defined threshold. 20. A vehicle according to claim 17 wherein said conduit and said blower are operative to blow chilled ullage gas over an exposed surface of the fuel within said fuel tank. 21. A vehicle according to claim 17 further comprising: a system controller;at least one temperature sensor positioned to provide temperature measurements of an ullage region of said fuel tank to said system controller; andat least one pressure sensor positioned to provide measurements of pressure within said fuel tank to said system controller, said system controller programmed to determine a desired temperature for the ullage region based on the pressure measurements and operate said blower to achieve the desired temperature as determined by said at least one temperature sensor. 22. A vehicle according to claim 17 further comprising: a system controller; anda user interface communicatively coupled to said system controller, said system controller programmed to transmit a signal to said user interface when ullage gas within the ullage region is within a non-inert range, said user interface comprising a manual switch, operation of said switch configured to cause said system controller to control operation of said blower.
이 특허에 인용된 특허 (10)
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Sauer, Richard A., Aircraft fuel inerting system for an airport.
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Norman P. Martinov, Aircraft fuel tank explosion reduction safety method.
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Runnels, Joe N.; Fagerlund, Kenneth R., Combustibly inert air supply system and method.
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Moravec,Bradford L.; Boggs,Royal E.; Graham,Rodney N.; Grim,Alan; Adkins,David A.; Snow, Jr.,Donald; Haack,Greg A., Commercial aircraft on-board inerting system.
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Bergman Jacob, Fuel ignition arrester system and method.
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Snow, Jr.,Donald R., Method and apparatus for generating an inert gas on a vehicle.
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Loss,Kevin L.; Adkins,David A., Methods and systems for controlling flammability control systems in aircraft and other vehicles.
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Loss,Kevin L.; Adkins,David A., Methods and systems for controlling flammability control systems in aircraft and other vehicles.
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Bryant Billy O. (3737 Gilmore Ave. Bakersfield CA 93308) Bryant Glen C. (3737 Gilmore Ave. Bakersfield CA 93308) Drube Douglas D. (3737 Gilmore Ave. Bakersfield CA 93308) Lowe Shannon L. (3737 Gilmor, Tank vapor pressure control system.
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Wong,Kenneth K., Utilization of compressor surge control air in an aircraft on-board inert gas generating system.
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Roscoe, Paul; Lehuunho, Emmanuel, Aircraft fuel system.
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Couture, Lyndsay Morgan; Kline, Erin G.; Ernst, Jeffrey; Daniele, Antonio G.; Liang, Hong, Flow reduction for bleed air systems.
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Massey, Alan, On board inert gas generation system with rotary positive displacement compressor.
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Cordatos, Haralambos; Rheaume, Jonathan, On-board aircraft reactive inerting dried gas system.
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Zheng, Daguang; Weng, Dacong, Systems and methods for fuel desulfurization.
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