A torque link assembly for a shock strut includes an upper torque link that is selectively retained in a stowed position when uncoupled from a lower torque link. The upper torque link includes first and second coaxial lugs that rotatably couple the upper torque link to an alignment feature. A latch mechanism includes a latch fitting rotatably coupled to either the upper torque link or the alignment feature. The latch mechanism further includes a stop fitting fixedly coupled to the other of the upper torque link and the alignment feature. The latch fitting engages the stop fitting to maintain the upper torque link in the stowed position. At least one of the latch fitting and stop fitting is positioned between the first and second lugs of the upper torque link.
Upper torque link central latch mechanism
02.03.2021
Patent
Elektronische Ressource
Englisch
IPC: | 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 / F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |