Fan module having variable-pitch blades

Patent metadata

Field	Value
Publication number	US-12428966-B2
Application number	US-202218292611-A
Country	US
Kind code	B2
Filing date	Aug 1, 2022
Priority date	Aug 4, 2021
Publication date	Sep 30, 2025
Grant date	Sep 30, 2025

Abstract

A fan module having variable-pitch blades is configured for use with for a propulsion unit having a longitudinal axis. The fan module includes a rotary casing carrying the blades and a pitch-changing system. The pitch-changing system includes a control device that includes an annular actuator having a stationary body added onto the rotary casing and a body configured to translate with respect to the stationary body along the longitudinal axis. A linking mechanism includes a synchronizing ring coupled to the mobile body, connected to the blades and configured to be translated along the longitudinal axis by the mobile body so as to change the pitch of the blades. A feathering device includes fly-weights coupled to the ring by a connecting rod of which the ends include ball-and-socket joints.

First claim

The invention claimed is:

1. A fan module having variable pitch blades for a propulsion assembly having a longitudinal axis (X), the module comprising:
a rotary casing which rotates about the longitudinal axis (X) and carries the blades,
a system configured to change the pitch of the blades, the system comprising a control device and a connection mechanism, the control device comprising an annular actuator centered on the longitudinal axis (X) having a stationary body fitted to the rotary casing and a body movable in translation relative to the stationary body along the longitudinal axis (X), the movable body being coupled to a synchronizing ring gear of the connection mechanism, said synchronizing ring gear being connected to the blades and configured to be driven in translation along the longitudinal axis (X) by the movable body so as to change the pitch of the blades; and
a feathering device configured to feather the blades, said feathering device comprising an annular row of fly-weights carried by the rotary casing,
wherein the annular row of fly-weights is coupled to the synchronizing ring gear, each of the fly-weights being connected to the synchronizing ring gear by a connecting rod, a first and a second end of which comprise ball-and-socket joints, and the fly-weights being capable, under the centrifugal effect, of being displaced into a position in which the synchronizing ring gear imposes a feathered position on the blades, and wherein the system configured to change the pitch of the blades is devoid of a load transfer bearing.

2. The fan module according to claim 1 , wherein the ball-and-socket joints connecting the first end of the connecting rod to the synchronizing ring gear and connecting the second end of the connecting rod to the fly-weights ( 43 ) have perpendicular axes.

3. The fan module according to claim 1 , wherein the feathering device comprises levers, each articulated about an axis (A) stationary relative to the rotary casing arranged between a first and a second arms of the lever, the first arm being secured to a fly-weight and the second arm being connected to the second end of the connecting rod by one of the ball-and-socket joints, the two arms being stationary relative to each other.

4. The fan module according to claim 3 , wherein each lever is articulated relative to the rotary casing by a pivot connection.

5. The fan module according to claim 4 , wherein at least one of the pivot connections is formed by a needle bearing or by two ball bearings.

6. The fan module according to claim 3 , wherein said rotary casing comprises an annular cap, and at least one lever is articulated about said axis (A) relative to the cap.

7. The fan module according to claim 6 , wherein the cap comprises at least one orifice for passage of the second arm of the at least one lever articulated with respect to the cap, the first arm of the lever being situated radially outside the cap.

8. The fan module according to claim 7 , wherein at least one of said at least one orifice in the cap comprises a deflector extending radially inwardly around a periphery of the orifice.

9. A propulsion assembly with a longitudinal axis (X) comprising at least one fan module with variable pitch blades according to claim 1 .

10. The fan module according to claim 1 , wherein the feathering device feathers the blades in the event of failure of said control device.

11. The fan module according to claim 1 , wherein the connection mechanism further comprises a connecting rod connecting the synchronization ring gear to each of the blades.

Assignees

• Safran Aircraft Engines

Inventors

• Beljambe Ceddric
• Charier Gilles Alain Marie
• Roda Jean Charles Olivier

Classifications

• F05D2260/79

  Bearing, support or actuation arrangements therefor · CPC title

• B64C11/385

  comprising feathering, braking or stopping systems · CPC title

• F01D7/00 Primary

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title

• B64C11/346

  actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces · CPC title

• F05D2260/77

  the adjusting mechanism driven or triggered by centrifugal forces · CPC title