A retainer assembly (22) is adapted to secure a removable electronic unit (24) within an avionics equipment mounting tray (26). The retainer assembly includes a latch (48) having a base portion (60) and a handle portion (66). The base portion is pivotally coupled to one of the removable electronic unit and the avionics equipment mounting tray. The handle portion projects outward from the base portion. The base portion includes a cam surface (68) adapted to releasably contact the other of the removable electronic unit and the avionics equipment mounting tray.
AVIONICS CAM RETAINER ASSEMBLY
NOCKENHALTERANORDNUNG FÜR AVIONIK
ENSEMBLE DE RETENUE DE CAME AVIONIQUE
2023-10-11
Patent
Elektronische Ressource
Englisch
IPC: | H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
ARTICLE RETAINER ASSEMBLY (OPTIONS) AND AN ARTICLE RETAINER SYSTEM
Europäisches Patentamt | 2019
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