发明名称 Device for determining the pressure and/or mass flow regulation for a spacecraft propulsion unit
摘要 The device (10) has a combination of a piezo-electrically actuated control valve (32) and two magnetically actuated control valves (22,23) for pressure- or mass flow control of the fluid. The control valves are lined with each other and with a line input (11) such that in a normal operation, the pressure and the mass flow of the fluid is adjusted by the former control valve and a connection or isolation of the former control valve with or from the line input is produced by the latter control valves. The pressure and the mass flow of the fluid are adjusted by the latter regulating valves in an emergency operation.
申请公布号 EP2706424(A2) 申请公布日期 2014.03.12
申请号 EP20130004351 申请日期 2013.09.05
申请人 ASTRIUM GMBH 发明人 MAIER, THOMAS
分类号 G05D7/06;G05D16/20 主分类号 G05D7/06
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