A transport element support assembly (300) comprises a front plate (302), a back plate (304), and a grommet (306). The front plate (302) has a first opening (310) and a first set of holes (313). The back plate (304) has a second opening (320) and a second set of holes (323). A chamber is formed by the first opening and the second opening and is configured to hold a transport element. The grommet (306) is positioned within the chamber. The transport element support assembly (300) formed by the front plate (302), the back plate (304), and the grommet (306) is configured to provide electrical isolation between the transport element and an aircraft structure.
TRANSPORT ELEMENT SUPPORT ASSEMBLY
TRANSPORTELEMENTSTÜTZANORDNUNG
ENSEMBLE DE SUPPORT D'ÉLÉMENT DE TRANSPORT
27.04.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16L PIPES , Rohre / H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen |
SUPPORT ELEMENT, SUPPORT ASSEMBLY, BRAKE BOOSTER AND METHOD
Europäisches Patentamt | 2020
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