发明名称 Liquid management apparatus for spacecraft
摘要 In a liquid storage tank 10 for use on a spacecraft, a transfer apparatus 15 (comprising gathering vanes 33, an elongate array of fins 32, and a sponge structure formed from panels 31) functions to transfer liquid from the inner surface of the tank 10 to the vicinity of an outlet line 40. A screen 23 is disposed between the panels 31 and the outlet line 40. When wetted with liquid, the screen 23 prevents gas and/or vapor in the tank 10 from passing to the outlet line 40. A perforated plate 22 disposed between the screen 23 and the outlet line 40 causes liquid to pass from the tank 10 to the outlet line 40 in a regular and generally unbroken flow.
申请公布号 US5293895(A) 申请公布日期 1994.03.15
申请号 US19930063815 申请日期 1993.05.20
申请人 LOCKHEED MISSILES & SPACE COMPANY, INC. 发明人 GROVE, R. K.;KING, RONALD W.;L'HEUREUX, JULIE M.
分类号 F17C9/00;F17C13/00;F28D15/04;(IPC1-7):B64G1/00 主分类号 F17C9/00
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