Pitch actuation system for a turbomachine propeller

Patent metadata

Field	Value
Publication number	US-10870481-B2
Application number	US-201716094449-A
Country	US
Kind code	B2
Filing date	Apr 10, 2017
Priority date	Apr 20, 2016
Publication date	Dec 22, 2020
Grant date	Dec 22, 2020

Abstract

A pitch actuation system for a turbomachine propeller, comprising an actuator with a movable portion configured to be connected to blades of the propeller in order to rotate them relative to the blade-pitch setting axes, wherein the actuator is an electromechanical actuator and comprises: blade-pitch control having a transmission screw rotated about an axis; a nut through which the transmission screw passes; and a member configured to engage with the blades in order to move the blades, wherein the nut is connected to the member via a decoupler configured such that a translational movement of the nut causes a translational movement of the member, but rotational movement of the member does not cause rotational movement of the nut.

First claim

The invention claimed is:

1. A pitch actuation system for a turbomachine propeller, comprising:
an actuator having a movable portion configured to be connected to blades of the propeller in order to rotate the blades relative to blade-pitch setting axes, wherein the actuator is an electromechanical actuator, and comprises:
a blade-pitch control comprising at least one electric motor arranged to drive a rotor about an axis, and a transmission screw arranged to be driven in rotation about the axis by said rotor;
a nut through which said transmission screw passes and cooperating with the screw so as to move in translation along the axis;
a member movable both in translation along the axis and in rotation about the axis, the member configured to cooperate with the blades in order to move the blades,
wherein the nut is connected to the movable member such that a translational movement of the nut causes translational movement of the member but a rotational movement of the member does not cause rotational movement of the nut, and
wherein the system further comprises decoupling means for operatively associating the nut with the member, wherein said decoupling means comprise at least one ring and two angular contact roller bearings, a first angular contact bearing being mounted between the ring and the nut and a second angular contact bearing being mounted between the ring and the member.

2. The system according to claim 1 , wherein the second angular contact bearing comprises an inner ring mounted on a sleeve comprising a blind orifice for receiving an end of the member.

3. The system according to claim 1 , wherein a second electric motor is mounted between the ring and the nut and comprises a rotor secured to the ring and a stator secured to the nut.

4. The system according to claim 1 , wherein a sensor is mounted between the ring and the nut and comprises a first element secured to the ring and a second element secured to the nut.

5. The system according to claim 4 , wherein said sensor is of the inductive or Hall effect type.

6. A method for verifying the condition of the angular contact bearings of the system according to claim 4 , comprising the steps of:
when said blade-pitch control is inactive
actuating a second electric motor mounted between the nut and the ring in such a way as to set in rotation the ring about the nut, and
controlling the rotation of the ring by output of the sensor.

7. The system according to claim 1 , further comprising means for blocking the nut in rotation.

8. The system according claim 7 , wherein the means for blocking in rotation are carried by a casing of the actuator and cooperate with the nut.

9. A turbomachine, comprising:
a propeller with blades of a variable pitch, and
a system according to claim 1 , wherein the member cooperates with eccentrics provided on plates for supporting and rotating the blades.

Assignees

• Safran Aircraft Engines

Inventors

• De Wergifosse Huguette

Classifications

• F05D2260/74

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

• F05D2270/09

  to cope with emergencies · CPC title

• B64C11/44 Primary

  electric · CPC title

• F01D7/02

  having adjustment responsive to speed · CPC title

• F02C6/20

  Adaptations of gas-turbine plants for driving vehicles · CPC title