发明名称 DEVICE AND METHOD FOR MEASURING THE LEAKAGE RATE OF REFERENCE PRESSURE LINES ONBOARD AN AIRCRAFT
摘要 The invention relates to a device for testing pneumatic circuits and for measuring the leakage rate of reference lines in an aircraft, said device being connected to a plenum chamber and including: a multi-pressure module (20) including a plurality of sensors, each of which is connected to a reference pressure line; first solenoid valves (EV1...EV15) which are arranged on the intake paths of said multi-pressure module (20), and which are connected to the reference pressure lines (21) via first couplings (24); second solenoid valves (EVP1...EVP15) which are arranged on the reference pressure lines (21); a pressure-adjustment module which is connected to all of the first solenoid valves via a second coupling (25); an electronic board (26) which controls the solenoid valves and the calibration of the multi-pressure module (20); and a check member. The invention also relates to a method implementing said device.
申请公布号 WO2012045968(A1) 申请公布日期 2012.04.12
申请号 WO2011FR52303 申请日期 2011.10.04
申请人 AIRBUS OPERATIONS;AIRBUS;DOS-REIS, MICHEL;BACOU, MICHEL;ARRUTI, CHRISTOPHE;GIRARD, PATRICK 发明人 DOS-REIS, MICHEL;BACOU, MICHEL;ARRUTI, CHRISTOPHE;GIRARD, PATRICK
分类号 G01M3/28;B64F5/00;F15B19/00;G01L27/00 主分类号 G01M3/28
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