IP Library Granted Patent US 10,151,653
Granted Patent B2
US 10,151,653 · App. 14/843,161 · Granted Dec 11, 2018

System for reproducing a dry friction torque applied to an actuator of a valve located in a hydraulic line of an engine of a spacecraft including an electrical actuator controlling orthogonal forces of plates on a disc to apply resistive torque to a shaft of the actuator

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Quick Facts
Patent No.
US 10,151,653
App. No.
14/843,161
Granted
Dec 11, 2018
Kind
B2
Abstract

A system for reproducing a dry friction torque applied to an actuator on a valve of a hydraulic line including a disc coupled to a power transmission shaft; a disc brake including a caliper mounted on a frame and plates adapted to be put into contact with the disc; and an electric actuator configured to control the force of application of the plates onto the disc so as to apply a controlled resistive torque to the power transmission shaft, is provided.

Claims (24)

1. A system for reproducing a dry friction torque applied to a valve actuator to be tested, comprising:

a disc coupled to a power transmission shaft of the valve actuator to be tested;

a disc brake including a caliper mounted on a frame and plates adapted to be put into contact with the disc so as to apply an orthogonal force to the disc; and

an electrical actuator configured to control a force of application of the plates on the disc so as to apply a controlled resistive torque to the power transmission shaft of the valve actuator to be tested,

wherein the disc is movable in rotation about an axis, the system including a device for measuring forces tangent to the rotation of the disc that the caliper transmits to the frame,

wherein the caliper is mounted on the frame, so as to be movable about an axis of rotation, and said device for measuring tangent forces includes instruments for measuring an angular displacement of the caliper about the axis of rotation,

wherein said device for measuring tangent forces includes two identical springs, mounted in opposition, so that each spring opposes the rotation of the power transmission shaft of the valve actuator to be tested and of the disc about the axis of rotation in a distinct direction, the system further including sensors adapted to measure an angular displacement of the power transmission shaft of the valve actuator to be tested and of the disc about its axis of rotation so as to determine the resistive torque on the power transmission shaft of the valve actuator to be tested,

wherein a first end of each spring is mounted on a support on which the caliper is mounted to the frame, the support being movable about the axis of rotation, and a second end of each spring is mounted to one of the sensors, and

wherein the resistive torque on the power transmission shaft of the valve actuator to be tested is determined based on the angular displacement of the power transmission shaft of the valve actuator to be tested and of the disc about its axis of rotation, and stiffness values of the two identical springs.

2. The system according to claim 1 , wherein the electrical actuator is a piezoelectric actuator.

3. The system according to claim 2 , wherein said electrical actuator is configured so as to generate at least one of a displacement and a force proportional to a control voltage or a current which is applied to the electrical actuator.

4. The system according to claim 1 , wherein the caliper is fixedly mounted to the frame, and said device for measuring tangent forces includes strain gauges measuring strains applied to a fixing of the caliper on the frame.

5. A method for reproducing a dry friction torque applied to a power transmission shaft of a valve actuator to be tested, the method comprising:

applying an orthogonal force to plates of a disc brake rubbing on a disc to generate a resisting torque on the power transmission shaft of the valve actuator to be tested, the power transmission shaft of the valve actuator to be tested being coupled to the disc,

wherein an electrical actuator controls a force of application of the plates on the disc,

wherein the disc is movable in rotation about an axis,

wherein forces tangent to the rotation of the disc are measured, which a caliper bearing the plates of the disc brake transmits to a frame,

wherein the caliper is mounted on the frame, so as to be movable about an axis of rotation,

wherein an angular displacement of the caliper about the axis of rotation is measured using a device including two identical springs, mounted in opposition, so that each spring opposes the rotation of the power transmission shaft of the valve actuator to be tested and of the disc about the axis of rotation in a distinct direction,

wherein an angular displacement of the power transmission shaft of the valve actuator to be tested and of the disc about its axis of rotation is measured using sensors so as to determine the resistive torque on the power transmission shaft of the valve actuator to be tested,

wherein a first end of each spring is mounted on a support on which the caliper is mounted to the frame, the support being movable about the axis of rotation, and a second end of each spring is mounted to one of the sensors, and

wherein the resistive torque on the power transmission shaft of the valve actuator to be tested is determined based on the angular displacement of the power transmission shaft of the valve actuator to be tested and of the disc about its axis of rotation, and stiffness values of the two identical springs.

6. The method according to claim 5 , wherein closed loop control of the braking force is accomplished by acting on the electrical actuator based on measurement of the force applied to the disc through the plates accomplished to the caliper of the disc brake.

7. The method according to claim 5 , wherein open loop control of the braking force is accomplished by acting on the electrical actuator based on filtered or estimated information on the force applied to the caliper of the disc brake.

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 Oct 15, 2015
From: FAYE, OLIVIER; CARON, ANTHONY; NOMERANGE, PHILIPPE; LEGONIDEC, SERGE
To: SNECMA
Reel/Frame 036801/0466 →