Flap assembly of aircraft
A technology of aircraft and flaps, which is applied in the field of aircraft flap assembly, can solve the problems of complex design, manufacture and installation, adverse effects on normal flight of aircraft, and high control accuracy requirements, so as to reduce manufacturing and maintenance costs and simplify the drive structure assembly. Integrating and improving the effect of control precision
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[0020] figure 1 Is a schematic diagram of the structure of the present invention, figure 2 To rotate the drive output device structure diagram, image 3 for figure 2 An enlarged view at A, as shown in the figure: The aircraft flap assembly of the present invention includes a flap 6 and a drive assembly. The drive assembly includes a rotary drive output device 1, a planar linkage mechanism, and a pull rod 10. The planar linkage The lever mechanism is a swivel drive pair formed by the sequential articulation of the crank 2, the connecting rod 3 and the pressure rod 9. One end of the pull rod 10 is hinged forward to the tail end of the pressure rod 9, and the other end can move according to a set trajectory with a hinge point. The way is hinged to the rear section 62 of the flap 6, the rotary power output end of the rotary drive output device 1 is connected to the head end of the crank 2, and the connecting rod 3 or / and the pressure rod 9 can move according to the set trajectory ...
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