A slat track roller assembly is provided so as to mount a slat track operatively associated with a wing leading edge slat for movements between retracted and deployed conditions relative to a leading edge of an aircraft wing. The slat track roller assembly may include at least forward and aft pairs of roller mechanisms connected to a respective one of opposed wing ribs of the wing leading edge in operatively rolling contact with a respective opposed lateral edge of the slat track. At least one of the roller mechanisms is positionally adjustable relative to the respectively opposed lateral edge of the slat track so as to compensate for mechanical tolerances that may be present.
Lateral roller assemblies for wing leading edge slat tracks
2023-03-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
LATERAL ROLLER ASSEMBLIES FOR WING LEADING EDGE SLAT TRACKS
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