Lever arm device for controlling the pitch of fan blades of a turbine engine having an unducted fan

Patent metadata

Field	Value
Publication number	US-10443609-B2
Application number	US-201615137302-A
Country	US
Kind code	B2
Filing date	Apr 25, 2016
Priority date	May 12, 2015
Publication date	Oct 15, 2019
Grant date	Oct 15, 2019

Abstract

A device for controlling the pitch of fan blades in a turbine engine having an unducted fan including at least one set of adjustable pitch fan blades, each fan blade being coupled, for pitch adjustment purposes, to a radial control shaft constrained to rotate with the set of fan blades and suitable for pivoting about a radial pitch axis of the fan blade, the device including a stationary actuator centered on a longitudinal axis of the turbine engine and driving an outer ring of a load transfer bearing in translation, the outer ring of the load transfer bearing being coupled directly to a lever arm of each control shaft via a respective ball joint connection in order to adjust its pivoting.

First claim

The invention claimed is:

1. A device for controlling a pitch of fan blades in a turbine engine having an unducted fan comprising a set of adjustable pitch fan blades, each fan blade being coupled, for pitch adjustment purposes, to a radial control shaft constrained to rotate with the set of adjustable pitch fan blades and suitable for pivoting about a radial pitch axis of said fan blade, the device comprising:
an actuator centered on a longitudinal axis of the turbine engine and driving an outer ring of a load transfer bearing in translation, said outer ring of the load transfer bearing being directly coupled to a lever arm of each radial control shaft via only a single respective ball joint connection in order to adjust a pivoting of the radial control shaft.

2. The device according to claim 1 , wherein each ball joint connection comprises a radial finger co-operating with a sliding ball joint.

3. The device according to claim 2 , wherein the lever arm of each radial control shaft comprises a sliding ball joint co-operating with the radial finger extending radially outwards from the outer ring of the load transfer bearing.

4. The device according to claim 2 , wherein the outer ring of the load transfer bearing comprises a respective sliding ball joint for each radial control shaft, the ball joint co-operating with the radial finger extending radially inwards from the lever arm.

5. The device according to claim 4 , wherein the sliding ball joints of the outer ring of the load transfer bearing are mounted on brackets that are independent of said outer ring of the load transfer bearing and that are fastened against a side face thereof.

6. The device according to claim 1 , each fan blade is mounted on a blade root support that is pivotally mounted on a rotary ring and that is coupled to an outer radial end of a respective radial control shaft.

7. A turbine engine having an unducted fan and a blade pitch control device according to claim 1 .

Assignees

• Safran Aircraft Engines

Inventors

• Patsouris Emmanuel Pierre Dimitri
• Belmonte Olivier
• Mouton Clementine Charlotte Marie
• Nguyen Van Thomas Julien

Classifications

• B64D2027/005

  Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR] · CPC title

• B64C11/308 Primary

  automatic · CPC title

• F05D2260/74

  by turning around an axis perpendicular the rotor centre line · CPC title

• F04D29/362 Primary

  during rotation · CPC title

• F02K3/06

  with front fan · CPC title