초록 ▼

A non-rotating actuating system for pitch control of a fan in a bypass turbine engine in which the actuating sleeve, that rotates with a fan and is moved axially to change to the pitch ofthe fan blade, is supported by a part of the fixed structure thereby to minimize loading of the disc supporting s

A non-rotating actuating system for pitch control of a fan in a bypass turbine engine in which the actuating sleeve, that rotates with a fan and is moved axially to change to the pitch ofthe fan blade, is supported by a part of the fixed structure thereby to minimize loading of the disc supporting structure.

대표청구항 ▼

A variable pitch control for a bypass fan in a turbine engine installation including: a row of fan blades, each having at its inner end a crank arm by which the pitch of the fan may be changed, a supporting ring for the fan blades, each blade being mounted at its base in the ring and in a position t

A variable pitch control for a bypass fan in a turbine engine installation including: a row of fan blades, each having at its inner end a crank arm by which the pitch of the fan may be changed, a supporting ring for the fan blades, each blade being mounted at its base in the ring and in a position to rotate on a radial axis, a fixed support structure for the ring, a first bearing supporting the ring to rotate on the fixed structure, a translatable sleeve splined to the support ring to rotate therewith and to slide axially relative thereto, a row of links connecting said sleeve with the crank arms and the blades, and each link being pivotally attached to the sleeve at one end and to the crank arm at the other end, a non-rotating translatable actuating sleeve within said first sleeve, a second bearing between said sleeves to cause said sleeves to move axially in unison, splines between the fixed structure and said second sleeve to support the second sleeve against rotation and means for actuating said second sleeve axially to change the pitch of the blades in unison.