F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 7/00 (2006.01) F01D 17/16 (2006.01) F04D 29/32 (2006.01) F04D 29/54 (2006.01) B63H 7/00 (2006.01) B63H 11/08 (2006.01)
Patent
CA 2434213
A turbine engine, particularly for aircrafts, of the type comprising a rotor and at least two stages of stator blade rows positioned upstream and downstream of the rotor, wherein the rotor blades (8) are of the variable pitch type and have a drop shape, are of the twisted type (1) or of the constant deflection type (2) and the stator blades (25), positioned downstream of the rotor, are of the twisted type.
L'invention concerne un moteur de turbine, en particulier pour des aéronefs, d'un type comportant un rotor et au moins deux phases de rangs de pale de stator placées en amont et en aval du rotor. Les pales de rotor (8) sont de type de pas variable, possèdent une forme de goutte et sont de type vrillé (1) ou du type de braquage permanent (2) et les pales de stator (25) placées en aval du rotor, sont de type vrillé.
Pietricola Paolo
Ridout & Maybee Llp
LandOfFree
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