Electronic arrangement for an aircraft and method for providing such an electronic arrangement

An opening completely arranged in a skin panel of a structural portion of the aircraft is formed in the outer skin of the skin panel, and for each of the skin panels with one of the openings, an associated structural element of an electronic arrangement is separately provided. The structural element...

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Bibliographic Details
Main Authors Schaupmann, Christian, Altmann, Markus
Format Patent
LanguageEnglish
Published 12.12.2023
Subjects
AEROPLANES
AIRCRAFT
ANTENNAS, i.e. RADIO AERIALS
AVIATION
BASIC ELECTRIC ELEMENTS
COSMONAUTICS
ELECTRICITY
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An opening completely arranged in a skin panel of a structural portion of the aircraft is formed in the outer skin of the skin panel, and for each of the skin panels with one of the openings, an associated structural element of an electronic arrangement is separately provided. The structural element is designed and detachably fastened by a frame thereof to the outer skin in the corresponding skin panel on the side of the outer skin opposite the outer surface, such that it seals the corresponding opening such that the skin panel has at least the same pressure-tightness and at least the same strength relative to tension, pressure and shear forces which act in the skin panel in the extension direction of the outer skin as the same skin panel without the corresponding opening.
Bibliography:Application Number: US202017606849