A control system for controlling collective and cyclic pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft
The invention is related to a control system 10 for controlling collective and cyclic pitch of rotor blades 1b, 1 c of a multi-blade rotor 1 a in a rotary-wing aircraft 1, said control system 10 comprising a swash plate assembly 11 with at least one non-rotating plate 12a and at least one rotating p...
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| Format: | Patent |
| Sprache: | eng ; pol |
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