The invention belongs to the technical field of flying control and relates to a nonlinear flaperon linkage mechanism for a plane. The nonlinear flaperon linkage mechanism comprises a folding and unfolding actuation drum (1), a left-side output transmission rocker arm (2), an input transmission rocker arm (3), a right-side output transmission rocker arm (4), a left-side output transmission rod (5), a left-side transmission rod (6), a right-side transmission rod (7) and a right-side output transmission rod (8). The nonlinear flaperon linkage mechanism has the advantages that in a limited space, a nonlinear linkage mechanism is adopted as a transmission mechanism of a flaperon control plane, so that the wing surface driving function is realized in an effective-flexible-reliable-simple manner.
Nonlinear flaperon linkage mechanism for plane
2015-04-01
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Linkage mechanism for linking a flaperon to a droop panel of an aircraft
Europäisches Patentamt | 2021
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