Turboprop engine with adjustable pitch propeller

Details Turboprop engine with adjustable pitch propeller Turboprop engine with adjustable pitch propeller

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 7/00 (2006.01) F01D 5/30 (2006.01)

Patent

CA 2619927

Turbopropulseur comportant au moins une hélice formée d'un ensemble de pales pivotantes. Selon l'invention, chaque pale (20) montée pivotante sur un support tournant (19a), comporte un pignon (23a) en engrènement avec un anneau d'actionnement (21a) tournant sur ledit support tournant et couplé à un anneau de commande (25a) par l'intermédiaire d'un mécanisme épicycloïdal (27a).

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