Bracelet sensing array
In accordance with at least one aspect of this disclosure, a sensing system includes a sensor mat configured to conform to a component having a central axis, a first sensor cluster disposed on or in the sensor mat configured to sense one or more conditions at a first location on the component, and a second sensor cluster disposed on or in the sensor mat configured to sense one or more conditions at a second location circumferentially spaced to the first location. In embodiments, the second location can be diametrically opposed to the first location.
1. A sensor mat, comprising:
a first substrate configured to wrap about a component to which the sensor mat is configured to attach, the component extending about a central axis and the first substrate having a length extending along a horizontal axis from a first end to a second end;
a plurality of sensors disposed on or within the first substrate at predetermined locations and configured to sense one or more forces acting on the component to which the sensor mat is configured to attach,
wherein the predetermined locations are based on a geometry of the component to which the sensor mat is configured to attach;
and
wherein the horizontal axis of the first substrate is configured to extend parallel to the central axis of the component when the sensor mat is attached to the component; and
wherein the plurality of sensors are arranged in two or more sensor clusters and wherein the two or more sensor clusters are arranged in complimentary pairs disposed at locations defined relative to one another based on the geometry of the component.
2. The sensor mat of claim 1 , wherein at least one sensor in each complimentary pair is axially aligned with the horizontal axis of the sensor mat.
3. The sensor mat of claim 1 , wherein at least one sensor in each complimentary pair is arranged oblique to the horizontal axis of the sensor mat.
4. The sensor mat of claim 1 , wherein the plurality of sensors include Fiber-Bragg Grating sensors configured to sense one or more of shear strain, normal strain, and/or temperature.
5. The sensor mat of claim 1 , wherein the plurality of sensors include foil strain sensors.
6. The sensor mat of claim 1 , wherein the plurality of sensors include carbon nanotube strain sensors.
7. The sensor mat of claim 1 , wherein the sensor mat further includes a second substrate and a third substrate configured to sandwich the first substrate.
8. A system comprising:
a load bearing component; and
the sensor mat of claim 1 conformally attached to the component.
9. The system of claim 8 , wherein at least one sensor of each complimentary pair is axially aligned with a central axis of the component, wherein a first sensor cluster of the complimentary pair is spaced 180 degrees from a second cluster of the complimentary pair in the circumferential direction.
10. The system of claim 8 , wherein at least one sensor of each complimentary pair is obliquely offset from a central axis of the component, wherein a first sensor cluster of the complimentary pair is spaced 90 degrees from a second cluster of the complimentary pair in the circumferential direction.
11. The system of claim 8 , wherein at least one sensor of each sensor cluster is oriented oblique to a central axis of the load bearing component.
12. The system of claim 8 , wherein the load bearing component is an aircraft landing gear component.
13. The system of claim 12 , wherein the landing gear component is a shock, a strut, rod, beam or support column.
14. The system of claim 8 , wherein the load bearing component is symmetrical about at least a longitudinal axis of the load bearing component.
15. The sensor mat of claim 1 , wherein the complimentary pairs are disposed at a linear distance πR or ½πR on the first substrate, wherein R is a radius of the component.
16. A method for installing a sensing system, comprising:
selecting a sensor mat based on a geometry of a load bearing component, the component having a central axis;
applying the sensor mat conformally around the component, the sensor mat comprising:
a first substrate; and
a plurality of sensors disposed on or within the first substrate and configured to sense one or more forces acting on the component;
wherein the plurality of sensors are arranged in two or more sensor clusters and wherein the two or more sensor clusters are arranged in complimentary pairs circumferentially spaced from one another about the central axis of the component; and
wherein the sensor mat is applied to the component such that portions of the substrate on or within which the plurality of sensors are disposed do not overlap.
17. The method of claim 16 , wherein applying the sensor mat includes applying the first substrate via a transfer sheet, wherein the first substrate remains attached to the component upon removal of the transfer sheet.
18. The method of claim 16 , wherein the complimentary pairs are circumferentially spaced 90 degrees or 180 degrees.
19. The method of claim 16 , wherein at least one sensor in each complimentary pair is axially aligned with the central axis of the component.
20. The method of claim 16 , wherein at least one sensor in each complimentary pair is arranged oblique to the central axis of the component.