Pressure bulkhead for an aircraft and device as well as method for manufacturing an aircraft structural component
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United States of America Patent
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May 2, 2017
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N/A
app pub date -
Nov 24, 2014
filing date -
Nov 27, 2013
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Abstract
A pressure bulkhead made of fiber composite material for an aircraft fuselage for the pressure-tight axial closure of a fuselage region configured to be put under internal pressure. The bulkhead comprises a first area element, at least one second area element and a plurality of core elements. The first area element has a plurality of receptacles. Each receptacle is configured to receive a core element. The core elements are received in the receptacles between surfaces facing one another of the first area element and of the at least one second area element. The surfaces facing one another of the first area element and of the at least one second area element are connected to one another in regions without core elements.
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