IP Library Granted Patent US 10,443,609
Granted Patent B2
US 10,443,609 · App. 15/137,302 · Granted Oct 15, 2019

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

Inventors: Emmanuel Pierre Dimitri Patsouris (Melun, FR); Olivier Belmonte (Perthes en Gatinais, FR); Clementine Charlotte Marie Mouton (Tournan en Brie, FR); Thomas Julien Nguyen Van (Alfortville, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F04D29/362B64C11/308F02K3/06B64D2027/005Y02T50/66
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Quick Facts
Patent No.
US 10,443,609
App. No.
15/137,302
Granted
Oct 15, 2019
Kind
B2
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.

Claims (8)

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 .

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 5, 2016
From: PATSOURIS, EMMANUEL PIERRE DIMITRI; BELMONTE, OLIVIER; MOUTON, CLEMENTINE CHARLOTTE MARIE; NGUYEN VAN, THOMAS JULIEN
To: SNECMA
Reel/Frame 039074/0807 →