发明名称 AIRCRAFT CONTROL AND MONITORING SYSTEM AND METHOD
摘要 <p>A system for bleeding air on an aircraft, including: at least one air bleed valve that can bleed a flow of air on the aircraft, a first temperature information module, a second temperature information module, at least one control module, and at least one data processing module coupled to the control module.</p>
申请公布号 EP2734719(A1) 申请公布日期 2014.05.28
申请号 EP20120738576 申请日期 2012.07.06
申请人 SNECMA 发明人 SEBAA, JÉRÔME GUY, ROGER;BON, FABRICE
分类号 F02C6/10;F02C6/08;F02C9/18 主分类号 F02C6/10
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