<p>A redundant gas supply or oxygen supply for an aircraft comprising two main lines 10, 50 and a group supply line 30 that is connected to one consumer 60 or to a multitude of consumers 60. In each case a connecting line 20, 40 connects the respective one main line 10, 50 to the group supply line 30. Flow limiters and nonreturn valves can be provided in the connecting lines.</p>
申请公布号
WO2008125572(A4)
申请公布日期
2009.06.11
申请号
WO2008EP54302
申请日期
2008.04.09
申请人
AIRBUS DEUTSCHLAND GMBH;BRICARD, PATRICK;COSTAN, EMIN;DEUTSCHER, WALTER;VOGT, THOMAS;WIRTH, MARKUS
发明人
BRICARD, PATRICK;COSTAN, EMIN;DEUTSCHER, WALTER;VOGT, THOMAS;WIRTH, MARKUS