A system for use with a landing gear of an aircraft includes a drag brace assembly having an upper end configured to be rotatably coupled to the aircraft and a lower end configured to be rotatably coupled to a shock strut of the landing gear. The system further includes a jury linkage having a brace portion configured to be pivotally coupled to the drag brace assembly and a strut portion pivotally coupled to the brace portion and configured to be rotatably coupled to the shock strut.
SIDE FOLDING AND REFORMING LINKAGE FOR LANDING GEAR
2021-05-13
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |