The invention is related to a rotary wing aircraft that comprises a structural arrangement (6) with at least one first fiber reinforced polymer component (7a) and at least one second fiber reinforced polymer component (7b) that are spaced apart from each other by an interspace (11) and that are rigidly attached to an associated structural component (8), wherein the at least one first fiber reinforced polymer component (7a) and the at least one second fiber reinforced polymer component (7b) are at least partly interconnected by means of an electrically conductive connection (9), and wherein the electrically conductive connection (9) comprises at least one sprayed layer (15) of electrically conductive particles (14), the at least one sprayed layer (15) of electrically conductive particles (14) being provided in the interspace (11).
A ROTARY WING AIRCRAFT WITH A STRUCTURAL ARRANGEMENT THAT COMPRISES AN ELECTRICALLY CONDUCTIVE CONNECTION
DREHFLÜGELFLUGZEUG MIT STRUKTURANORDNUNG MIT EINER ELEKTRISCH LEITENDEN VERBINDUNG
AÉRONEF À VOILURE TOURNANTE AVEC UN AGENCEMENT STRUCTUREL COMPRENANT UNE CONNEXION ÉLECTRIQUEMENT CONDUCTRICE
2018-12-12
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B05D PROCESSES FOR APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TO SURFACES, IN GENERAL , Verfahren zum Aufbringen von Flüssigkeiten oder von anderen fließfähigen Stoffen auf Oberflächen allgemein / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64C AEROPLANES , Flugzeuge / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL / H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS |
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