发明名称 Aircraft fuel tank flammability reduction methods and systems
摘要 An aircraft fuel tank flammability reduction method includes feeding pressurized air into an air separation module containing an oxygen separation membrane. The method includes contacting the separation membrane with the air feed, permeating oxygen from the air feed through the separation membrane, and producing nitrogen-enriched air from the air separation module as a result of removing oxygen from the air feed. The NEA from the air separation module is substantially cooled in a NEA flow heat exchanger and the substantially cooled, nitrogen-enriched air is fed into the fuel tank on board the aircraft. An aircraft fuel tank flammability reduction system includes a NEA flow heat exchanger configured to cool substantially the nitrogen-enriched air from the air separation module and a fuel tank on board the aircraft configured to receive the cooled nitrogen-enriched air.
申请公布号 US9327243(B2) 申请公布日期 2016.05.03
申请号 US201414477058 申请日期 2014.09.04
申请人 THE BOEING COMPANY 发明人 Jojic Ivana;Snow, Jr. Donald R;Grim Alan;Hart Colin W
分类号 B01D53/22;B01D63/02;B01D71/02;B64D37/32 主分类号 B01D53/22
代理机构 Parsons Behle & Latimer 代理人 Parsons Behle & Latimer
主权项 1. An aircraft fuel tank flammability reduction method comprising: feeding pressurized air into an air separation module containing an oxygen separation membrane; contacting the separation membrane with the air feed, permeating oxygen from the air feed through the separation membrane, and producing nitrogen-enriched air from the air separation module as a result of removing oxygen from the air feed; substantially cooling the nitrogen-enriched air (NEA) from the air separation module in a NEA flow heat exchanger downstream of the air separation module; and feeding the substantially cooled, nitrogen-enriched air into the fuel tank on board the aircraft.
地址 Chicago IL US