Sensing load relief by a secondary path of a flight control actuator

• US 7,866,602 B2
• Filed: 02/08/2008
• Issued: 01/11/2011
• Est. Priority Date: 02/08/2007
• Status: Active Grant

• Current Assignee: Goodrich Actuation Systems SAS (Rtx Corporation)
• Original Assignee: Goodrich Actuation Systems SAS (Rtx Corporation)
• Inventors: Port-Robach, Isabelle, Moalic, Jean-Marc, Raynal, Jean-Pierre
• Primary Examiner(s): Ellis; Christopher P
• Application Number:
  US12/028,150
• Publication Number:
  US 20080265091A1
• Time in Patent Office: 1,068 Days
• Field of Search: 244/99.4, 244/99.3, 244/99.2
• US Class Current: 244/99.4
• CPC Class Codes: B64C 13/341 having duplication or stand-by provisions
• CPC Class Codes: F16H 2025/2037 Actuator supports or means for fixing piston end, e.g. flanges
• CPC Class Codes: F16H 25/2021 with means for avoiding overloading
• CPC Class Codes: F16H 25/205 comprising alternate power paths, e.g. for fail safe back-up
• CPC Class Codes: F16H 25/24 Elements essential to such mechanisms, e.g. screws, nuts F16H25/22 takes precedence

Abstract

Device for sensing load relief by a secondary path of a flight control actuator having a primary path and a secondary path capable of relieving the load of the primary path in the event of a breakdown thereof, the primary path comprising a screw, the screw terminating in a fastener of the primary path, the secondary path comprising an emergency load relief rod passing through the screw, this rod terminating in a male shape which, when the primary path is carrying the load, is accommodated inside of a female shape of a fastener of the secondary path, characterized in that at least one sensing element is disposed on the male shape terminating the rod, on the female shape or between both of these two shapes, this sensing element being designed to wear down due to the friction between the male shape and the female shape, when the secondary path is loaded and is relieving the load, this sensing element being connected or capable of being connected to means capable of sensing wear on this sensing element and of triggering an alarm when such wear is sensed.

Claims

1. Device for sensing load relief by a secondary path of a flight control actuator having a primary path and a secondary path capable of relieving the load of the primary path in the event of a breakdown thereof, the primary path comprising a screw, the screw terminating in a fastener of the primary path, the secondary path comprising an emergency load relief rod passing through the screw, this rod terminating in a male shape which, when the primary path is carrying the load, is accommodated inside of a female shape of a fastener of the secondary path, the male shape, which terminates the rod, and the female shape of the fastener being spherical or rotational,

characterized in that at least one sensing element is disposed on the male shape terminating the rod, on the female shape or between both of these two shapes, this sensing element being designed to wear down due to the friction between the male shape and the female shape, when the secondary path is loaded and is relieving the load, this sensing element being connected or capable of being connected to processing means capable of sensing wear on this sensing element.

2. Device of claim 1, characterized in that a sensing element is a fairlead extending along a circular generating of either of these two shapes.

3. Device of claim 2, characterized in that the male shape, which terminates the rod, and/or the female shape of the fastener has (have) a groove along at least one generating line, which is intended for receiving a fairlead.

4. Device of claim 2, characterized in that the male shape, which terminates the rod, and/or the female shape of the fastener have at least one circular groove perpendicular to the axis of the screw and hollow shaft.

5. Device of claim 4, characterized in that the male shape, which terminates the rod, or the female shape of the fastener have at least two parallel grooves disposed on both of the two hemispheres, respectively.

6. Device of claim 1, characterized in that the sensing element is a cable comprising one or more electrically conductive wires disposed inside an electrically insulating material and in mechanical case ensuring electromagnetic protection.

7. Device of claim 1, characterized in that the processing means comprise means for sensing an incident by sensing that the circuit of a sensing element or grounding thereof has been disconnected.

8. Device of claim 2, characterized in that the cable is a strip comprising a coated wire protruding along an inside circular generating line of the female shape.

9. Device of claim 1, characterized in that wear-sensing element is a point-based element.

10. Device of claim 3, characterized in that the male shape, which terminates the rod, and/or the female shape of the fastener have at least one circular groove perpendicular to the axis of the screw and hollow shaft.

11. Device of claim 10, characterized in that the male shape, which terminates the rod, or the female shape of the fastener have at least two parallel grooves disposed on both of the two hemispheres, respectively.