CPC F01D 7/00 (2013.01) [B64C 11/38 (2013.01); B64C 11/44 (2013.01); F01D 25/16 (2013.01); F02K 3/06 (2013.01); F04D 29/36 (2013.01); F05D 2220/32 (2013.01); F05D 2240/30 (2013.01); F05D 2240/54 (2013.01); F05D 2250/231 (2013.01); F05D 2260/40311 (2013.01); F05D 2270/52 (2013.01); F05D 2270/56 (2013.01)] | 10 Claims |
1. A turbine engine with a longitudinal axis (X), comprising:
a rotor supporting at least one variable pitch blade and an inlet cone, the rotor being guided in rotation relative to a fixed structure of the turbine engine via a first bearing and a second bearing;
a controlling system for controlling the pitch of the at least one blade, the controlling system being secured to the rotor and having at least one first actuator set in motion by an energy, the controlling system being arranged axially upstream of the first and second bearings; and
a transferring device for transferring the energy disposed axially between the first bearing and the second bearing, the transferring device having a fixed member secured to the fixed structure and a moving member secured to the rotor,
wherein the rotor is annular and defines a downstream portion of an inner space, wherein the inlet cone defines an upstream portion of the inner space that fluidly connected with the downstream portion of the inner space, and wherein the controlling system is positioned inside of the inner space.
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