Bypass jet engine comprising a thrust reverser

The engine has a thrust reverser (18) e.g. door type thrust reverser, including a deviation unit (20) to divert a part of a gas stream (12) near or downstream of a rear end (11) of a nacelle (10) in a thrust reverse position, such that the diverted gas stream contacting a gas stream (14) reduces spe...

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Bibliographische Detailangaben
Hauptverfasser: Fert, Jérémy, Emprin, Yves, Wesolowski, Jean-Pierre
Format: Patent
Sprache:eng ; fre ; ger
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