ABSTRACT 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. 19 Date Recue/Date Received 2020-10-30
SIDE FOLDING AND REFORMING LINKAGE FOR LANDING GEAR
2021-05-11
Patent
Electronic Resource
English