Force sensing clevis insert

• US 20090078846A1
• Filed: 09/25/2007
• Published: 03/26/2009
• Est. Priority Date: 09/25/2007
• Status: Active Grant

• Current Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Powell, James, Isebrand, Scott
• Granted Patent: US 7,661,321 B2
• Time in Patent Office: Days
• US Class Current: 248/543
• CPC Class Codes: B64D 29/06 Attaching of nacelles, fairings or cowlings
• CPC Class Codes: E05B 15/0205 Striking-plates, keepers, staples means for reducing friction E05B17/007; electric strikers E05B47/0046; staples for padlocks E05B67/383; strikers for espagnolettes E05C9/1808
• CPC Class Codes: E05B 17/22 Means for operating or controlling lock or fastening device accessories, i.e. other than the fastening members, e.g. switches, indicators E05B39/00 - E05B45/00 take precedence
• CPC Class Codes: E05C 19/145 flush

Abstract

A sensor includes a clevis insert for reception within a first bore of a clevis. The clevis insert is configured to accommodate a latch pin. A strain sensing element is operatively associated with the clevis insert for detecting mechanical strain imparted to the clevis insert when a force acts on the clevis insert through the pin. The invention also provides a method of retrofitting a cowl latch assembly.

Claims

1. A sensor comprising:

a) a clevis insert for reception within a first bore of a clevis, the clevis insert being configured to accommodate a latch pin; and

b) a strain sensing element operatively associated with the clevis insert for detecting mechanical strain imparted to the clevis insert when a force acts on the clevis insert through the pin.

2. A sensor as recited in claim 1, wherein the clevis insert defines a recess configured to receive the strain sensing element and adapted to concentrate mechanical strain on the strain sensing element.

3. A sensor as recited in claim 2, wherein the clevis insert includes a first alignment feature proximate a periphery of the clevis insert, the first alignment feature being configured and adapted to cooperate with a corresponding second alignment feature within the first bore of the clevis to align the clevis insert.

4. A sensor as recited in claim 3, wherein the first and second alignment features are configured and adapted to align the strain sensing element along a load path defined by a force load when the force acts on the clevis insert.

5. A sensor as recited in claim 4, wherein the recess defined by the clevis insert is configured and adapted so that when the force acts on the clevis insert, the force compresses a portion of the clevis insert proximate the strain sensing element.

6. A sensor as recited in claim 5, further comprising an electrical circuit electrically coupled to the strain sensing element to facilitate measurement of strain.

7. A sensor as recited in claim 1, wherein the strain sensing element is a SAW strain sensor configured and adapted to be excited by energy at a first radio frequency and to wirelessly transmit a second radio frequency indicative of strain experienced by the clevis insert.

8. A sensor as recited in claim 7, further comprising an RF transceiver operatively associated with the clevis insert and being configured and adapted to transmit the first radio frequency to the SAW strain sensor, to receive the second radio frequency from the SAW strain sensor, and to transmit status information indicating the status of the latch.

9. A sensor as recited in claim 1, wherein the clevis is mounted on an engine cowl door.

10. A latch assembly comprising:

a) a clevis portion including a wall having a first bore extending therethrough;

b) an annular insert accommodated within the first bore of the wall of the clevis portion and having an aperture extending therethrough;

c) a keeper pin extending through the aperture in the annular insert; and

d) a strain sensing element mounted adjacent the aperture of the annular insert for detecting mechanical strain imparted to the annular insert when a force acts on the annular insert through the keeper pin.

11. A latch assembly as recited in claim 10, wherein the clevis has a second wall having a second bore, and wherein the keeper pin is configured and adapted to extend through the aperture in the annular insert and the second bore in the clevis.

12. A latch assembly as recited in claim 10, wherein the annular insert defines a recess adapted to receive the strain sensing element, and wherein the recess is configured and adapted to concentrate mechanical strain on the strain sensing element.

13. A latch assembly as recited in claim 12, wherein the annular insert includes a first alignment feature proximate a periphery of the annular insert, the first alignment feature being configured and adapted to cooperate with a corresponding second alignment feature within the first bore of the clevis to align the annular insert.

14. A latch assembly as recited in claim 13, wherein the first and second alignment features are configured and adapted to align the strain sensing element along a load path defined by a force load when the force acts on the annular insert.

15. A latch assembly as recited in claim 14, wherein the second alignment feature within the bore includes a notch defined in a periphery of the bore.

16. A latch assembly as recited in claim 15, wherein the second alignment feature is generally cylindrical in shape.

17. A latch assembly as recited in claim 14, wherein the recess defined by the annular insert is configured and adapted so that when the force acts on the annular insert, the force compresses a portion of the annular insert proximate the strain sensing element.

18. A latch assembly as recited in claim 17, further comprising an electrical circuit electrically coupled to the strain sensing element to facilitate measurement of strain.

19. A latch assembly as recited in claim 10, wherein the strain sensing element is a SAW strain sensor configured and adapted to be excited by energy at a first radio frequency and to wirelessly transmit a second radio frequency indicative of strain experienced by the annular insert.

20. A latch assembly as recited in claim 19, further comprising an RF transceiver operatively associated with the annular insert and configured and adapted to transmit the first radio frequency to the SAW strain sensor, to receive the second radio frequency from the SAW strain sensor, and to transmit status information indicating the status of the latch.

21. A latch assembly as recited in claim 10, wherein the clevis portion is mounted on an engine cowl door.

22. A method of retrofitting a latch assembly comprising the steps of:

a) providing a clevis insert having;

i) a clevis insert body dimensioned for reception within a bore in a wall of a clevis, the clevis insert body having an aperture therein for receiving a latch pin; and

ii) a strain sensing element provided on the clevis insert body adjacent the aperture for detecting mechanical strain imparted to the clevis insert when a force acts thereon through the pin;

b) enlarging an existing bore formed in a wall of the clevis; and

c) positioning the clevis insert within the bore in the wall of the clevis.

23. A method of retrofitting a latch assembly as recited in claim 22, wherein the clevis is mounted on an engine cowl door.