In an aircraft line or harness fastening system (32), a clamp (2) attaches a line or harness (30) to an aircraft. A collar (1) within the clamp surrounds the line or harness (30). The collar (1) is smaller than the clamp (2) and is circular in shape to enable rotation of the collar (11) within the clamp (2). The collar (1) comprises two separate complementary parts that fit together around the line or harness (30). Each of the two separate complementary parts includes a tab and a recess. The tab of one of the complementary parts fits into the recess on the other of the complementary parts.
AIRCRAFT LINE OR HARNESS FASTENING SYSTEM
FLUGZEUGLEINEN- ODER KABELBAUM-BEFESTIGUNGSSYSTEM
SYSTÈME DE FIXATION DE LIGNE OU DE FAISCEAU DE CÂBLES D'AÉRONEF
2025-04-02
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / 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 |
Safety belt and safety harness separating and fastening system
European Patent Office | 2024
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