Systems and methods are provided for door alignment of an aircraft landing gear door. One embodiment is an apparatus that includes a plurality of adjustable rods configured to temporarily install in an aircraft to stand in place of a final adjustable part, each of the adjustable rods configured to position a block for stopping a door of the aircraft. Each of the adjustable rods includes a telescopic body configured to extend and retract in length, and a spring configured to compress to reduce the length of the telescopic body, and to expand to extend the length of the telescopic body. Each adjustable rod also includes a locking mechanism configured to lock the telescopic body at a fixed length to prevent expansion of the spring, and to unlock the telescopic body to release the spring and adjust the telescopic body to an adjusted length.
DOOR ALIGNMENT FOR AIRCRAFT LANDING GEAR
2020-08-06
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |