DEVICE AND METHOD FOR PRODUCING A FUSELAGE SHELL FORMED FROM COMPOSITE FIBRE MATERIAL FOR AN AIRCRAFT
A device and a method for manufacturing a fiber-reinforced fuselage shell for an aircraft, which fuselage shell for the purpose of reinforcement comprises several stringers that are spaced apart from each other, wherein the device includes a base frame comprising several supporting walls of differen...
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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
17.10.2012
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Subjects | |
Online Access | Get full text |
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Summary: | A device and a method for manufacturing a fiber-reinforced fuselage shell for an aircraft, which fuselage shell for the purpose of reinforcement comprises several stringers that are spaced apart from each other, wherein the device includes a base frame comprising several supporting walls of different lengths for forming a curved mounting surface for the fuselage shell to be manufactured, wherein several actuators that extend radially outwards and that are longitudinally adjustable are affixed to the mounting surface, at the distal ends of which actuators in each case mold channels for receiving the stringers are attached, which mold channels are interconnected by means of flexible intermediate elements and/or further mold channels for forming a vacuum-tight closed mold surface. |
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Bibliography: | Application Number: EP20100794932 |