发明名称 TURBOJET ENGINE WITH ATTENUATED JET NOISE
摘要 <p>A plurality of hatches are distributed on the rear periphery of an engine cowl. The hatches are opened only when turbojet engine power is greater than cruising power. In an open position, the hatches draw hot air jets passing through an intermediate chamber before ejecting the jets through longitudinally-distributed communication components.</p>
申请公布号 EP1937954(A1) 申请公布日期 2008.07.02
申请号 EP20060820223 申请日期 2006.10.17
申请人 AIRBUS FRANCE 发明人 PORTE, ALAIN
分类号 F02K1/34;F02K1/38 主分类号 F02K1/34
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