A de-icer is provided and includes first and second structural layers that each include centerline and a non-inflatable edge angled with respect to the centerline, edge sealing material disposed to adhere the first and second structural layers together to form a non-inflatable edge area extending along at least the non-inflatable edge and surrounding a central area and stitching. The stitching is disposed to stitch the first and second structural layers together in the central area to form tubes. The tubes include an outermost tube which is closest to and parallel with the non-inflatable edge.
PNEUMATIC DE-ICER WITH REDUCED NON-INFLATABLE AREA AT DE-ICER EDGE
2022-12-01
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Pneumatic de-icer with reduced non-inflatable area at de-icer edge
European Patent Office | 2022
|PNEUMATIC DE-ICER WITH REDUCED NON-INFLATABLE AREA AT DEICER EDGE
European Patent Office | 2024
|Engineering Index Backfile | 1944
|SAE Technical Papers | 1944
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