IP Library › Granted Patent US 9,453,770
Granted Patent B2
US 9,453,770 · App. 14/080,858 · Granted Sep 27, 2016

Strain measurement device and installation of such a device in an element

Inventors: Marc Sartor (Toulouse, FR); Patricia Morgue (Colomiers, FR); Manuel Paredes (Balma, FR)
Assignee: AIRBUS OPERATIONS S.A.S.
G01L1/246G01B11/18G01D5/35316G01M5/0025G01M5/0041G01M5/0091G01M11/086
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Quick Facts
Patent No.
US 9,453,770
App. No.
14/080,858
Granted
Sep 27, 2016
Kind
B2
Abstract

A strain measurement device is provided. The strain measurement device includes at least one filiform strain sensor and a support of longilinear shape on which the filiform strain sensor is positioned. The strain measurement device also includes a stiffener.

Claims (30)

1. A strain measurement device, comprising:

at least one filiform strain sensor;

a support of longilinear shape on which the filiform strain sensor is positioned; and

a stiffener;

wherein the stiffener and a wall of the support are coupled together so as to define a space between the stiffener and the wall of the support so that the support retains a freedom of movement with respect to bending.

2. The device according to claim 1 , wherein the stiffener is at most fixed to the support at one point.

3. The device according to claim 1 , wherein the filiform strain sensor is an optical fibre Bragg grating.

4. The device according to claim 1 , wherein the support is hollow, and has a longitudinal direction and a width, with the support further comprising a wall having a thickness and having an external surface on which the filiform strain sensor is positioned by one or more connecting points, a main strain direction of the filiform strain sensor being arranged parallel to the longitudinal direction of the support.

5. The device according to claim 4 , wherein one end of the support is blocked.

6. The device according to claim 5 , wherein the support is blocked by a cap an end of which extends beyond the end of the support.

7. The device according to claim 1 , wherein the device comprises a thin tube encapsulating at least the filiform strain sensor with a binder.

8. The device according to claim 4 , further comprising an additional strain sensor, free of deformation with respect to the support, and situated in an internal volume defined by the wall of the hollow support.

9. A structural element, comprising:

a first surface;

a hole having a first end that opens onto a first surface;

a strain measurement device received in at least one measurement zone associated with the hole, the strain measurement device including at least one filiform strain sensor, a support of longilinear shape on which the filiform strain sensor is positioned and a stiffener; and

a binder forming a film surrounding the strain measurement device;

wherein the stiffener and a wall of the support are coupled together so as to define a space between the stiffener and the wall of the support so that the support retains a freedom of movement with respect to bending.

10. The structural element according to claim 9 , wherein the hole has a second end which is closed.

11. The structural element according to claim 9 , wherein the hole is at least approximately coaxial with an axis of symmetry of the element.

12. The structural element according to claim 9 , wherein the stiffener is at most fixed to the support at one point.

13. The structural element according to claim 9 , wherein the filiform strain sensor is an optical fibre Bragg grating.

14. The device according to claim 1 , wherein the stiffener is removeably coupled to the support.

15. The structural element according to claim 9 , wherein the stiffener is removeably coupled to the support.

16. A strain measurement device, comprising:

at least one filiform strain sensor;

a support of longilinear shape on which the filiform strain sensor is positioned; and

a stiffener;

wherein the support is hollow, and has a longitudinal direction and a width, with the support further comprising a wall having a thickness and having an external surface on which the filiform strain sensor is positioned by one or more connecting points, a main strain direction of the filiform strain sensor being arranged parallel to the longitudinal direction of the support, and

wherein the stiffener and a wall of the support are coupled together so as to define a space between the stiffener and the wall of the support so that the support retains a freedom of movement with respect to bending.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 25, 2014
From: SARTOR, MARC; MORGUE, PATRICIA; PAREDES, MANUEL
To: AIRBUS OPERATIONS S.A.S.
Reel/Frame 032294/0727 →
Priority Claims (1)
FR 12 61173 · Nov 23, 2012 · national
Continuity (1)
Related Publication 20140153863A1 · Jun 5, 2014