SYSTEM OF TWO COAXIAL MAIN ROTORS OF FLYING VEHICLE

aeronautical engineering; main rotors of flying vehicle. SUBSTANCE: proposed system includes reduction gear with two coaxial shafts, main rotor hubs, main rotor control circuits, two wobble plates and main rotor collective and differential pitch control mechanism. Shaft of upper main rotor is made a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BELJAEV V.V, ZEVIG G.V, VLASOV A.A, PONOMAREV N.N, MALYSHEV B.S, SOLOV'EV A.I, KHRIBKOV V.K, PODNEBESNOV B.JA
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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