Abstract: 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.

Abstract: A pneumatic deicer assembly includes a first stretch fabric with a first edge opposite a second edge. The first edge is positioned proximate the second edge such that the first stretch fabric forms a tube. A non-stretch fabric covers a seam formed between the first edge and the second edge of the first stretch fabric. A second stretch fabric covers the non-stretch fabric and a portion of the first stretch fabric.

Abstract: 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.

Abstract: A pneumatic deicer assembly includes a first stretch fabric with a first edge opposite a second edge. The first edge is positioned proximate the second edge such that the first stretch fabric forms a tube. A non-stretch fabric covers a seam formed between the first edge and the second edge of the first stretch fabric. A second stretch fabric covers the non-stretch fabric and a portion of the first stretch fabric.

Abstract: A self-cleaning component assembly includes a fluid containment vessel, an ultrasonic transducer fixed to a wall of the fluid containment vessel, and a germicidal light source fixed to the component such that germicidal light is directed to an internal cavity of the fluid containment vessel.

Abstract: A die-welding system for a de-icer assembly includes a die, a die base, a high energy source, and a de-icer assembly. The de-icer assembly includes a first welded-material layer and a second welded-material layer. At least one of the die and the die base includes a welded-portion pattern thereon configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer.

Abstract: A method of manufacturing a de-icer assembly includes disposing a first welded-material layer and a second welded-material layer beneath a horn of a horn-based welding system, controlling the horn to move along a welded-portion pattern configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer, and applying high-frequency energy to the first welded-material layer and a second welded-material layer using the horn such that the first welded-material layer and the second welded-material layer are welded together at areas in the shape of the welded-portion pattern to form a welded de-icer assembly.