A wing mounting, comprising: ⋅a base (11); ⋅a wing bracket (25) pivotally mounted to the base, configured to rotate relative to the base within an operational angular range; and ⋅at least one biasing element configured to bias the wing bracket away from the boundaries of the operational angular range, wherein the at least one biasing element (120) is configured to bias the wing bracket within a biasing range adjacent the respective boundaries of the operational angular range, but substantially not to bias the wing bracket within an inner angular range including the middle of the operational angular range.
A wing mounting
2023-05-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |