发明名称 |
INTEGRATED THRUST REVERSER DEVICE AND AIRCRAFT ENGINE NACELLE EQUIPPED THEREWITH |
摘要 |
The present disclosure provides a thrust reverser device that is integrated in an aircraft nacelle. Blocking flaps are stored inside a mobile cowl disposed in a downstream section of the nacelle, under deflection cascade assemblies during direct-jet operation of the nacelle. Various devices are provided for executing the passage from direct-jet operation to reverse-jet operation in two stages: the mobile cowl moves in translation towards the downstream end of the nacelle; and each flap is then deployed in the main air flow path. |
申请公布号 |
EP3030774(A1) |
申请公布日期 |
2016.06.15 |
申请号 |
EP20140759034 |
申请日期 |
2014.08.01 |
申请人 |
AIRCELLE |
发明人 |
GUERIN, PHILIPE;KERBLER, OLIVIER;RAMI, JEAN-PAUL |
分类号 |
F02K1/72;F02K1/09;F02K1/76;F02K3/06 |
主分类号 |
F02K1/72 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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