A system (101) for use with a landing gear (100) of an aircraft (10) includes a drag brace assembly (102) having an upper end (108) configured to be rotatably coupled to the aircraft and a lower end (110) configured to be rotatably coupled to a shock strut of the landing gear. The system further includes a jury linkage (114) having a brace portion (116) configured to be pivotally coupled to the drag brace assembly and a strut portion (118) pivotally coupled to the brace portion and configured to be rotatably coupled to the shock strut.
SIDE FOLDING AND REFORMING LINKAGE FOR LANDING GEAR
SEITENFALT- UND -UMFORMUNGSGELENK FÜR FAHRWERK
LIAISON DE PLIAGE ET DE REFORMAGE LATÉRAL POUR TRAIN D'ATTERRISSAGE
2021-05-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |