FIELD: aviation.
SUBSTANCE: invention relates to aviation. Aircraft (AC) contains one separate part – a module representing the chassis, and another separate part – a module representing all the other parts of the AC, which is attached to the hinge to a separate part – the chassis module. Separate part – the module, the rest of the AC is rotatable in the longitudinal plane around the hinge axis with respect to a separate part – the chassis module. Separate part – the module of the chassis is made inseparable from the individual part – the module the rest of the AC after take-off of the AC. Between the controls of the AC, located on a separate part – the module, the rest of the AC, and a separate part-the chassis module-has a kinematic connection. Separate part – the module the rest of the AC is rotatable with respect to a separate part – the chassis module due to the impact on the controls of the AC.
EFFECT: invention is aimed at reducing weight.
8 cl, 2 dwg
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Authors
Dates
2018-11-13—Published
2017-08-01—Filed