IP Library Granted Patent US 10,408,069
Granted Patent B2
US 10,408,069 · App. 15/150,832 · Granted Sep 10, 2019

Radial control shaft for a device for controlling the pitch of fan blades of a turbine engine having an unducted fan, and a method of mounting such a shaft

Inventors: Olivier Belmonte (Perthes en Gatinais, FR); Emmanuel Pierre Dimitri Patsouris (Melun, FR); Thomas Julien Nguyen Van (Alfortville, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F01D7/00B64C11/306F02K3/072F04D29/323F16C3/02B64D2027/005F05D2220/32F05D2260/74
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Quick Facts
Patent No.
US 10,408,069
App. No.
15/150,832
Granted
Sep 10, 2019
Kind
B2
Abstract

A radial control shaft for a device for controlling the pitch of fan blades of a turbine engine having an unducted fan, is disclosed. The shaft includes an external portion that is designed to be mounted in the control device from its outside and to be coupled to at least one fan blade in order to adjust its pitch, and an internal portion, independent of the external portion, that is designed to be mounted from the inside of the control device, to be connected to a load transfer bearing in order to pivot the shaft about a radial axis, and to close an oil enclosure in which the bearing is housed, the external and internal portions of the shaft being coupled to each other. A method of mounting such a shaft and a control device including such a shaft are also disclosed.

Claims (22)

1. A radial control shaft for a control device for controlling a pitch of fan blades of a turbine engine having an unducted fan, said control shaft comprising:

an external portion that is designed to be mounted to an outer portion of the control device and to be coupled to at least one fan blade in order to adjust the pitch of the at least one fan blade; and

an internal portion, independent of the external portion, that is designed to be mounted to an inner portion of the control device, to be connected to a load transfer bearing in order to pivot said control shaft about a radial axis,

wherein the external and internal portions of the control shaft are coupled to each other,

wherein the internal portion of the control shaft is designed to be mounted through a hub casing with a ball bearing interposed between the internal portion of the control shaft and the hub casing,

wherein for closing an oil enclosure in which said load transfer bearing is housed, a shoulder of the internal portion and a shoulder of the hub casing are designed to act as a plug that limits any risk of oil leaking out from the oil enclosure, and

wherein the internal portion of the control shaft has a first shoulder designed to come radially into abutment against the ball bearing while the internal portion is being mounted to the inner portion of the control device, and the shoulder of the internal portion that is radially offset outwards relative to the first shoulder is designed to come into abutment against the shoulder of the hub casing while mounting the internal portion to the inner portion of the control device, and a nut being interposed between the ball bearing and the shoulder of the hub casing.

2. The control shaft according to claim 1 , wherein the external and internal portions of the control shaft are coupled to each other by fluting of complementary shapes.

3. The control shaft according to claim 1 , wherein the internal portion of the control shaft includes a lever arm designed to be coupled to an outer ring of the load transfer bearing.

4. The control shaft according to claim 3 , wherein the lever arm includes a finger extending radially inward which cooperates with a sliding ball joint carried by the outer ring of the load transfer bearing.

5. The control shaft according to claim 1 , wherein the external portion of the control shaft includes a coupling system for coupling to the at least one fan blade.

6. The control shaft according to claim 1 , wherein the external portion of the control shaft is designed to be mounted on a rotary ring and to be held thereon by a nut.

7. The control shaft according to claim 1 , wherein the radial axis of the control shaft is offset in at least one of an axial direction or tangential direction relative to a pitch axis of the at least one fan blade that the control shaft controls.

8. A method of mounting the radial control shaft according to claim 1 , the method comprising:

mounting the external portion of the control shaft to the outer portion of the control device;

mounting the internal portion of the control shaft to the inner portion of the control device; and

coupling together the internal and external portions of the control shaft.

9. The control shaft according to claim 1 , wherein the external portion is removable from the internal portion without removing the oil enclosure.

10. A device for controlling the pitch of fan blades of a turbine engine having an unducted fan, the device comprising:

the radial control shaft according to claim 1 , the external portion of the control shaft being coupled to one of the fan blades, and the internal portion of the control shaft being mechanically linked to a load transfer bearing designed to enable said control shaft to pivot about the radial axis.

11. The device according to claim 10 , wherein a rotary ring holds the external portion of the control shaft radially and leaves the control shaft free to turn.

12. The device according to claim 10 , further comprising a hub casing that serves to hold the internal portion of the control shaft radially and leaves the control shaft free to turn.

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 Mar 8, 2017
From: BELMONTE, OLIVIER; PATSOURIS, EMMANUEL PIERRE DIMITRI; NGUYEN VAN, THOMAS JULIEN
To: SNECMA
Reel/Frame 041495/0820 →
Priority Claims (1)
FR 15 54280 · May 12, 2015 · national
Continuity (1)
Related Publication 20160333709A1 · Nov 17, 2016
Cited By (1)
US 12,497,901