Reinforcing component (11), and its manufacturing method, for a structure of an aircraft or spacecraft (1) which comprises a first component region (13), which is in particular elongate, for reinforcing at least one other element (19), and at least one second component region (17), which is permanently connected to the first component region (13). The reinforcing component (11) is formed using a thermoplastic plastics material in each of the first component region (13) and the second component region (17). In the first component region (13), the thermoplastic plastics material forms a matrix in which continuous reinforcing fibres (31) are embedded, and, in the second component region (17), the reinforcing component (11) comprises discontinuous reinforcing fibres (37) or is free of reinforcing fibres.
REINFORCING COMPONENT FOR A STRUCTURE OF AN AIRCRAFT OR SPACECRAFT, AIRCRAFT OR SPACECRAFT, AND METHOD
VERSTÄRKUNGSKOMPONENTE FÜR EINE STRUKTUR EINES LUFT- ODER RAUMFAHRZEUGS, LUFT- ODER RAUMFAHRZEUG UND VERFAHREN
COMPOSANT DE RENFORCEMENT DESTINÉ À UNE STRUCTURE D'UN AÉRONEF OU D'UN ENGIN SPATIAL, AÉRONEF OU ENGIN SPATIAL ET PROCÉDÉ
07.04.2021
Patent
Elektronische Ressource
Englisch
IPC: | B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64G Raumfahrt , COSMONAUTICS / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge |
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