| 摘要 |
The aileron control device 7, 8 comprises a link rod 14 which is integral in rotation with the lateral movements of the control stick 13 and tilting a crank 16 whose two arms 17, 18 actuate crossed link rods 19, 20 manoeuvring the ailerons 7, 8 via levers 23, 24 for control of their incidence with respect to the wings 5, 6. A pulley mechanism 26 is linked by a cable 37 to the crank arms 16; the pulley 26 is mounted so as to pivot about an eccentric axis 30 on a fork joint 31 elastically returned by a spring 33 towards a fixed point 36 of the mast 3 supporting the wing surface 5, 6, 7, 8; this mechanism lends assistance in manoeuvring the ailerons 7, 8. Application in particular to aircraft of the "motorized micro-light" type. <IMAGE>
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