Abstract: An air separation module (ASM) is described herein that can include an outer shell having a first end, a second end, and a tubular outer wall disposed between the first end and the second end. The ASM can further include a hollow fiber membrane. The hollow fiber member can include a first tubesheet and a second tubesheet. A plurality of hollow fibers can extend between the first tubesheet and the second tubesheet. At least one of the first tubesheet and the second tubesheet can include a hygrophobic material.

Abstract: The composite tube comprises a tubular arrangement of knitted fiber characterized by a plurality of interlocking loops. The tubular knitted pattern allows for variable electrical, mechanical and geometrical tube options. A matrix material is applied over the knitted fiber pattern and is allowed to cure. The matrix material may include a combination of resin and epoxy constituents. The matrix material may be applied by a vacuum bag molding process. The flexible knitted reinforcing layer allows use of an inflatable bladder to hold the reinforcing layer in the desired shape, thereby facilitating tube constructions of varying shapes and diameters. Continuous application of the matrix material avoids overlapping seams that are prone to delamination. Methods are provided for reinforcing the composite tube construction including one or more folded layers of knitted fiber, a reinforcing wrap made of knitted fiber, and an inflatable balloon element in combination with a layer(s) of knitted fiber.

Abstract: The composite tube comprises a tubular arrangement of knitted fiber characterized by a plurality of interlocking loops. The tubular knitted pattern allows for variable electrical, mechanical and geometrical tube options. A matrix material is applied over the knitted fiber pattern and is allowed to cure. The matrix material may include a combination of resin and epoxy constituents. The matrix material may be applied by a vacuum bag molding process. The flexible knitted reinforcing layer allows use of an inflatable bladder to hold the reinforcing layer in the desired shape, thereby facilitating tube constructions of varying shapes and diameters. Continuous application of the matrix material avoids overlapping seams that are prone to delamination. Methods are provided for reinforcing the composite tube construction including one or more folded layers of knitted fiber, a reinforcing wrap made of knitted fiber, and an inflatable balloon element in combination with a layer(s) of knitted fiber.

Abstract: An aircraft (50) with a variable cargo bay (52) includes a frame (60) having an inner surface and an outer skin (64) covering the frame (60). The frame (60) has a pair of faceted fairings (54, 56) coupled to the frame (60) and a door assembly (58) between the pair of faceted fairings (54, 56). The door assembly (58) has an inner surface connected to a linkage mechanism (66). The linkage mechanism (66) couples the inner surface of the frame (60) and the inner surface of the door assembly (58). A conformable surface (70) is connected between the skin (64) of the frame (60) and the door assembly (58).