AIRCRAFT TURBINE ENGINE COMPRISING VARIABLE PITCH PROPELLER BLADES

An assembly including a propeller blade and a pitch adjustment system for setting the pitch of the blade. A root of the blade has a bulb and the pitch adjustment system for setting the pitch of the blade includes a cup having an upper opening; a retaining ring, which extends around the bulb, is rest...

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Bibliographic Details
Main Authors JOUDON, Vincent, COURTIER, Vivien Mickaël, JABLONSKI, Laurent, SERVANT, Régis Eugène Henri, COTTET, Clément, LANGLOIS, Arnaud
Format Patent
LanguageEnglish
Published 14.09.2023
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