Actuator assembly

Patent metadata

Field	Value
Publication number	US-10598265-B2
Application number	US-201715659693-A
Country	US
Kind code	B2
Filing date	Jul 26, 2017
Priority date	Jul 27, 2016
Publication date	Mar 24, 2020
Grant date	Mar 24, 2020

Abstract

An actuator assembly may comprise a screw shaft having a shaft axis; a drive arrangement pivotally supported about the screw shaft axis for driving the screw shaft, e.g., about the shaft axis or along the shaft axis, and a rod mounted to the drive arrangement at a location off the shaft axis for providing a primary function of reacting torque about the shaft axis on the drive arrangement. The rod may comprise a rod axis and provide a load path along the rod axis for reacting torque. The rod may also comprise a device for which provides a secondary function for the actuator assembly based on the load experienced along the load path provided by the rod.

First claim

The invention claimed is:

1. An actuator assembly comprising:
a screw shaft having a shaft axis;
a drive arrangement pivotally supported for rotation around the shaft axis for driving the screw shaft;
a rod mounted to the drive arrangement at a location radial outward from the shaft axis for providing a primary function of reacting against torque applied about the shaft axis on the drive arrangement, the rod having a rod axis and being arranged to provide a load path that experiences load in a direction along the rod axis in reaction to torque on the drive arrangement, wherein the rod comprises a load sensor for detecting at least a direction of the load along the rod load path;
a no-back device, wherein the no-back device is connected with a rotational coupling to a frame and the drive arrangement is supported on bearings permitting the drive arrangement to rotate about the screw shaft axis and about the no-back device; and
a processor configured to receive a movement signal indicating a direction of drive of the screw shaft from a movement sensor and to receive a direction of load signal from the load sensor, wherein the processor is configured to determine, from the direction of load signal and the movement signal, whether or not the drive arrangement is operating in a resistive load quadrant or a load driven quadrant.

2. The actuator assembly as claimed in claim 1 , wherein the device comprises a resilient mechanism.

3. The actuator assembly as claimed in claim 2 , wherein the device comprises a load limiter which activates to limit axial forces in the rod.

4. The actuator assembly as claimed in claim 2 , wherein the resilient mechanism is a spring arrangement.

5. The actuator assembly as claimed in claim 3 , wherein relative movement of a nut along the screw shaft is limited by at least one metal end stop.

6. The actuator assembly as claimed in claim 1 , wherein the device is for detecting a performance of the actuator assembly based on load experienced along the rod load path reacting torque on the drive arrangement, wherein the device comprises a load limiter configured to control a change in length of the rod through axial movement of one portion relative to another when a load along the rod load path exceeds a pre-load of the load limiter, and wherein the device comprises an activation sensor for detecting a change of length of the rod.

7. The actuator as claimed in claim 1 , wherein the load sensor is arranged to transmit load signals to a processor which is programmed with an algorithm to compute parameters comprising a fatigue life consumption or endurance life consumption of one or more components of the actuator assembly.

8. The actuator assembly as claimed in claim 1 , wherein the processor is configured to:
output a performance signal indicating whether the drive arrangement is operating in a resistive load quadrant or a load driven quadrant.

9. The actuator assembly as claimed in claim 1 , wherein the actuator assembly further comprises a second rod for reacting against torque applied to the no-back device into the frame, the second rod being provided with a device which provides a secondary function for the actuator assembly based on load experienced along the second rod.

10. The actuator assembly as claimed in claim 9 , wherein the device in the second rod is a load sensor which provides a load signal for use in monitoring the operation and/or health of the actuator assembly.

Assignees

• Ratier Figeac Sas

Inventors

• Seminel Bruno
• Vermande Frédéric

Classifications

• F16H2025/2037

  Actuator supports or means for fixing piston end, e.g. flanges · CPC title

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• G01L5/0061

  Force sensors associated with industrial machines or actuators (for the specific machine or actuator involved see relevant class, e.g. F01, F04, F16, B66, E21) · CPC title

• B64C13/341

  having duplication or stand-by provisions · CPC title

• F16H2025/2081

  Parallel arrangement of drive motor to screw axis · CPC title