MECHANISM FOR CONNECTION OF FUNCTIONAL UNIT TO FLYING VEHICLE CONTROL CIRCUIT RUN

FIELD: flying vehicle control systems. ^ SUBSTANCE: proposed mechanism has base 1 mounted on flying vehicle case, drive for connection of functional unit 4, input bell crank 2 and output bell crank 3 articulated together and provided with hinges for connection of rod 5 of pilot's command lever...

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Bibliographische Detailangaben
1. Verfasser:	GITIS ABRAM IL'ICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: flying vehicle control systems. ^ SUBSTANCE: proposed mechanism has base 1 mounted on flying vehicle case, drive for connection of functional unit 4, input bell crank 2 and output bell crank 3 articulated together and provided with hinges for connection of rod 5 of pilot's command lever and rod 6 of functional unit. Both bell cranks are articulated with functional unit cut-in drive and radii of arms from articulation of bell cranks to hinge of attachment to base of input bell crank and to hinge of connection of functional unit rod to output bell crank are equal. ^ EFFECT: reduced mass of mechanism; enhanced reliability. ^ 2 dwg