Methodology for height measurement in pneumatic deicer boots
The present disclosure provides for methodologies for height measurement in pneumatic deicer boots for aircraft, and related models, systems and methods of use. More particularly, the present disclosure provides for methods, models, systems and applications to detect the life or failure of pneumatic deicer boots for aircraft. A method for detecting the life or failure of pneumatic deicer boots for aircraft is provided.
1. A method for detecting life or failure of pneumatic deicer boots comprising:
positioning a colored strip on a pneumatic deicer boot, and installing the pneumatic deicer boot on an aircraft;
detecting variation of a width of the colored strip via a camera at pre-determined time intervals;
plotting and correlating the width of the colored strip against an inflation or deflation height of a tube of the pneumatic deicer boot utilizing a pre-tested graph to determine the height of inflation or deflation of the tube at the pre-determined time intervals; and
utilizing the height of inflation or deflation of the tube at the pre-determined time intervals to detect the life or failure of pneumatic deicer boot.
2. The method of claim 1 , wherein the camera is positioned inside the aircraft.
3. The method of claim 1 , wherein the colored strip includes a first color and the pneumatic deicer boot includes a second color that is different than the first color.
4. The method of claim 1 , wherein the pneumatic deicer boot is positioned on a wing of the aircraft.
5. The method of claim 1 , wherein the colored strip is positioned on a stitched line or area of the tube.
6. The method of claim 1 , wherein the colored strip includes a glued strip and/or comprises paint.
7. The method of claim 1 , wherein determining the height of inflation or deflation of the tube at the pre-determined time intervals comprises contactless inflation or deflation height measurement.
8. The method of claim 1 , wherein the camera is a high definition camera.
9. The method of claim 1 , wherein the colored strip includes a plurality of colors.
10. The method of claim 1 , wherein the pneumatic deicer boot includes a stretchable fabric and a non-stretchable fabric.
11. A pneumatic deicer boot assembly comprising:
a colored strip positioned on a pneumatic deicer boot, the pneumatic deicer boot installed on an aircraft;
a camera positioned on the aircraft, the camera configured to detect variation of a width of the colored strip at pre-determined time intervals;
wherein variation of the width of the colored strip at the pre-determined time intervals operates to determine a height of inflation or deflation of a tube of the pneumatic deicer boot at the pre-determined time intervals to detect the life or failure of the pneumatic deicer boot.
12. The assembly of claim 11 , wherein the camera is positioned inside the aircraft.
13. The assembly of claim 11 , wherein the colored strip includes a first color and the pneumatic deicer boot includes a second color that is different than the first color.
14. The assembly of claim 11 , wherein the pneumatic deicer boot is positioned on a wing of the aircraft.
15. The assembly of claim 11 , wherein the colored strip is positioned on a stitched line or area of the tube.
16. The assembly of claim 11 , wherein the colored strip includes a glued strip and/or comprises paint.
17. The assembly of claim 11 , wherein determining the height of inflation or deflation of the tube at the pre-determined time intervals comprises contactless inflation or deflation height measurement.
18. The assembly of claim 11 , wherein the camera is a high definition camera.
19. The assembly of claim 11 , wherein the colored strip includes a plurality of colors.
20. The assembly of claim 11 , wherein the pneumatic deicer boot includes a stretchable fabric and a non-stretchable fabric.