发明名称 Tieftemperaturflüssigkeitstreibstoff und insbesondere Abkühlen des Tieftemperaturflüssigkeitstreibstoffs
摘要 <p>A system and method for cooling a first cryogenic fluid (16) in a vessel (12) comprises the steps of directing a second cryogenic fluid (30) into the first cryogenic fluid (16) and releasing gas from the vessel (12). The first cryogenic fluid (16) has a boiling point that is higher than the boiling point of the second cryogenic fluid (30). Directing the second cryogenic fluid (30) into the first cryogenic fluid (16) results in the second fluid (30) cooling the first fluid (16) and the second fluid (30) vaporizing. The vaporized fluid is released as a gas from the vessel (12). The vessel (12) may be a propellant tank for a space vehicle (10). The first and second cryogenic fluids (16,30) are delivered from supplies (18,32) located outside of the vehicle (10). The first cryogenic fluid (16) may be oxygen and the second cryogenic fluid (30) may be nitrogen, neon, or helium. In another aspect of the invention, the first cryogenic fluid (12) may be hydrogen and the second cryogenic fluid (30) may be helium. <IMAGE></p>
申请公布号 DE60022246(T2) 申请公布日期 2006.06.29
申请号 DE2000622246T 申请日期 2000.03.03
申请人 THE BOEING CO., CHICAGO 发明人 LAK, TIBOR I.;ROGERS, GENE;WEBER, JAMES F.;MERLIN, MICHAEL V.;GAYNOR III, TIMOTHY L.;DAVIS, JOHN E.;GERHARDT, DAVID L.
分类号 B64G5/00;B64G1/40;B67D7/02;F02K9/42;F02M31/20;F17C5/02;F17C13/00;F25J1/02 主分类号 B64G5/00
代理机构 代理人
主权项
地址