Sensor system for laminated structures

Patent metadata

Field	Value
Publication number	US-2016370238-A1
Application number	US-201514740984-A
Country	US
Kind code	A1
Filing date	Jun 16, 2015
Priority date	Jun 16, 2015
Publication date	Dec 22, 2016
Grant date	—

Abstract

A sensor system for a laminated structure may include a sensor assembly disposed between a first layer and a second layer of the laminated structure. The sensor assembly may include a first anchor member and a second anchor member spaced at a predetermined distance from one another. A sensor chamber is formed between the first and second anchor members. The sensor assembly may also include a sensing line extending through the anchor members and the sensor chamber. The sensing line may include a configuration within the sensor chamber for sensing one of stress forces within the laminated structure, temperature or temperature changes within the laminated structure. A first transport tube may extend from the first anchor member opposite the sensor chamber and a second transport tube may extend from the second anchor member opposite the sensor chamber. The sensing line extends through the first and second transport tubes.

First claim

What is claimed is:

1 . A sensor system ( 100 , 200 ) for a laminated structure ( 102 , 202 , 300 , 400 ), comprising:
a sensor assembly ( 108 , 108 a , 208 , 402 , 502 ) disposed between a first layer ( 104 , 204 ) of the laminated structure and a second layer ( 106 , 206 ) of the laminated structure, the second layer of the laminated structure being disposed on the first layer, the sensor assembly comprising:
a first anchor member ( 310 , 410 );
a second anchor member ( 312 , 412 ) spaced at a predetermined distance (D) from the first anchor member;
a sensor chamber ( 314 , 414 ) formed between the first anchor member and the second anchor member; and
a sensing line ( 112 , 212 , 316 , 416 ) extending between the first anchor member and the second anchor member through the sensor chamber and the sensing line extending through the first anchor member and the second anchor member, the sensing line comprising a configuration within the sensor chamber for sensing one of stress forces within the laminated structure, temperature or temperature changes within the laminated structure;
a first transport tube ( 110 , 210 , 318 , 422 ) extending from the first anchor member opposite the sensor chamber and between the first layer of the laminated structure and the second layer of the laminated structure; and a second transport tube ( 110 , 210 , 320 , 424 ) extending from the second anchor member opposite the sensor chamber and between the first layer of the laminated structure and the second layer of the laminated structure, the sensing line extending through the first transport tube and the second transport tube.

2 . The sensor system of claim 1 , wherein the sensing line extends through the first transport tube and the second transport tube without any tension on the sensing line to prevent any stress on the sensing line within the first transport tube and the second transport tube in response to forces being applied to the laminated structure.

3 . The sensor system of claim 1 , wherein the sensing line is held within the sensor chamber by the first anchor member and the second anchor member at a preset tension to form a stress sensor ( 304 ), wherein a physical stress applied to the laminated structure causes a corresponding change to the preset tension of the sensing line within the sensor chamber.

4 . The sensor system of claim 3 , further comprising a detection device ( 116 ) connected to the sensing line, the detection device being configured to detect the corresponding change to the preset tension of the sensing line within the sensor chamber caused by movement of the first anchor member and the second anchor member in response to one more forces being applied to the laminated structure.

5 . The sensor system of claim 4 , wherein the sensing line comprises an optical fiber and the detection device comprises:
an optical signal generator ( 118 , 214 ) that transmits an optical signal through the optical fiber optic; an optical signal detector ( 120 , 218 ) that measures one or more properties of the transmitted optical signal at an output ( 130 ) of the optical fiber; a signal processing module ( 124 , 224 ) that determines a stress on the laminated structure at a location of the stress sensor based on the measured one or more properties of the transmitted optical signal; and a display ( 126 , 226 ) to present the determined stress on the laminated structure.

6 . The sensor system of claim 4 , wherein the sensing line comprises an electrically conductive wire and the detection device comprises:
a radio frequency (RF) signal generator ( 118 , 214 ) that transmits an RF signal through the electrically conductive wire; an RF receiver ( 120 , 218 ) that measures one or more properties of the transmitted RF signal at an output ( 130 ) of the electrically conductive wire; a signal processing module ( 124 , 224 ) that determines a stress on the laminated structure at a location of the stress sensor based on the measured one or more properties of the transmitted RF signal; and a display ( 126 , 226 ) to present the stress on the laminated structure.

7 . The sensor system of claim 1 , wherein the sensor assembly further comprises a thermally sensitive plate ( 418 ) disposed within the sensor chamber and a selected portion ( 420 ) of the sensing line is attached to the thermally sensitive plate to form a thermal sensor ( 404 ) and the sensing line extends from the thermally sensitive plate respectively to the first anchor member and the second anchor member without any tension or a predetermined amount of slack, wherein changes in temperature in the sensor chamber cause the thermally sensitive plate to distort which causes stress in the sensing line corresponding to the temperature or changes in temperature.

8 . The sensor system of claim 7 , further comprising a detection device ( 116 ) connected to the sensing line, the detection device being configured to detect changes in stress in the sensing line within the sensor chamber, the changes in stress in the sensing line corresponding to the temperature or changes in temperature in the sensor chamber.

9 . The sensor system of claim 8 , wherein the sensing line comprises an optical fiber and the detection device comprises:
an optical signal generator ( 118 , 214 ) that transmits an optical signal through the optical fiber optic; an optical signal detector ( 120 , 218 ) that measures one or more properties of the transmitted optical signal at an output ( 130 , 220 ) of the optical fiber; a signal processing module ( 124 , 224 ) that determines a temperature at a location of the thermal sensor ( 404 ) based on the measured one or more properties of the transmitted optical signal; and a display ( 126 , 226 ) for presenting the temperature or temperature changes at the location of the thermal sensor.

10 . The sensor system of claim 8 , wherein the sensing line comprises an electrically conductive wire and the detection device comprises:
a radio frequency (RF) signal generator ( 118 , 214 ) that transmits an RF signal through the electrically conductive wire; an RF receiver ( 120 , 218 ) that measures one or more properties of the transmitted RF signal at an output of the electrically conductive wire; a signal processing module ( 124 , 224 ) that determines a temperature at a location of the thermal sensor based on the measured one or more properties of the transmitted RF signal; and a display ( 126 , 226 ) to present the temperature or temperature changes at the location of the thermal sensor.

11 . The sensor system of claim 1 , further comprising:
a plurality of sensor assemblies ( 108 , 108 a , 208 , 208 a ) distributed at predetermined locations in the laminated structure between the first layer of the laminated structure and the second layer of the laminated structure, the sensing line comprising a configuration within each sensor assembly to provide one of a stress sensor ( 304 ) that senses stress forces within the laminated structure or a thermal sensor ( 404 ) that senses temperature or temperature changes within the laminated structure; a plurality of transport tubes ( 110 , 210 ), one of the plurality of transport tubes extending between adjacent sensor assemblies of the plurality of sensor assemblies, the plurality of sensor assemblies being connected in series by the transport tubes, and another one ( 110 a ) of the transport tubes extending from each end sensor assembly ( 108 a , 208 a ) of the series connected sensor assemblies to an edge ( 114 , 213 ) of the laminated structure, the sensing line extending through the plurality of transport tubes witho

Assignees

• Boeing Co

Inventors

• Peck Jr James L
• Muley Arun

Classifications

• G01L1/241 Primary

  by photoelastic stress analysis · CPC title

• G01K1/08

  Protective devices, e.g. casings · CPC title

• G01L1/246

  using integrated gratings, e.g. Bragg gratings · CPC title

• G01K11/3206

  at discrete locations in the fibre, e.g. using Bragg scattering · CPC title

• G01L1/247

  using distributed sensing elements, e.g. microcapsules (along a single optical fibre G01L1/242) · CPC title