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Holding device for mounting parts installed inside an aircraft fuselage

A holding device for a mounting part installed inside an aircraft fuselage having a lining including an insulating mat, the holding device includes a fastening part attached to the aircraft fuselage and protruding through an opening in the insulating mat; a sealing disk; and a holding part configured to attach the mounting part and being disposed on an inner side of the aircraft fuselage and cooperating with the fastening part configured to attach the mounting part so as to simultaneously fix the insulating mat between the fastening part and the holding part, wherein the holding part extends through the opening in a sealed manner, and wherein a lower surface of the sealing disk contacts and seals an edge region of the opening when the holding part is installed on the fastening part.
Owner:AIRBUS OPERATIONS GMBH

Fiber-reinforced composite hollow structure, method for production thereof, and apparatus therefor

Center cores are formed by extrusion-molding ABS resin. Seven pieces of the center cores, which are juxtaposed to each other in the horizontal direction, are supplied by a pultruder, and reinforcing long-fibers impregnated with an unsaturated polyester resin are allowed to pass through dispersion guides and squeezing nozzles, to thus squeezing-mold a fiber-reinforced composite hollow structure having FRP made legs. A final squeezing nozzle is disposed in a cross head die through a cooling jacket, and the hollow structure thus molded is allowed to pass therethrough to be covered with the ABS resin in a state in which the outer periphery of the hollow structure is heated. The hollow structure thus covered is subjected to cooled-sizing through a plurality of horizontal and vertical pairs of rollers, and then cured in a hot curing tank. The surface covered with the ABS resin is subjected to a surface-treatment of imparting irregularities for giving an antislipping function to the surface. A thermoplastic resin-made protective cap is fitted to an end of the center core. The apparatus for manufacturing a composite hollow structure has a plurality of pairs of rotatable and heat-resisting sizing rollers. The plurality of pairs of the sizing rollers are disposed in the pultruding direction while being gradually cooled in the order from those positioned on the upstream side to those positioned on the downstream side for sizing the softened outer layer covering the outer periphery of the intermediate layer.
Owner:UBE NITTO KASEI CO LTD
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