A de-icing assembly for a surface of an aircraft includes a carcass with a first layer and a second layer, a plurality of seams sewn into the carcass, and a bonded region. The plurality of seams join the first and second layers of the carcass together. Each of the plurality of seams comprises two or more stitchlines. The bonded region is disposed between the two or more stitchlines and seals a portion of the first layer of the carcass to a portion of the second layer of the carcass.
Sewn alternate inflate pneumatic de-icer
22.09.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse |
SEWN REINFORCEMENT FEATURES FOR PREVENTION OF STITCH BREAKAGE IN A PNEUMATIC DE-ICER
Europäisches Patentamt | 2018
|Sewn reinforcement features for prevention of stitch breakage in a pneumatic de-icer
Europäisches Patentamt | 2020
|SEWN REINFORCEMENT FEATURES FOR PREVENTION OF STITCH BREAKAGE IN A PNEUMATIC DE-ICER
Europäisches Patentamt | 2019
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