AIRCRAFT WITH INJECTION COOLING SYSTEM AND INJECTION COOLING SYSTEM
摘要
<p>An aircraft with aturbofan engine assembly having at least one compressor, a nacelle surrounding the turbine engine and defining an annular bypass duct between the nacelle and the turbine engine, a thrust reverser having at least one moveable control surface, a thrust reverser locking system configured to selectively lock the thrust reverserand an injection cooling system</p>
申请公布号
WO2015096000(A1)
申请公布日期
2015.07.02
申请号
WO2013CN90219
申请日期
2013.12.23
申请人
GENERAL ELECTRIC COMPANY;PANG, QIANG;ZHONG, GUOHUA;YAO, LI