sistema de comando, notadamente de vôo para aeronave

A control system, in particular an aircraft flight control system, having a linkage with a force-transmission link (3), the link having a body (5) having at least one end housing (8) slidably receiving a coupling rod (9) for coupling the link to an adjacent element of the linkage, the housing being...

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Hauptverfasser:	BRUNO TILLY, FRANÇOIS GUILLOT, ARNAUD DUYCK, JERÔME PIATON
Format:	Patent
Sprache:	por
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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creator	BRUNO TILLY FRANÇOIS GUILLOT ARNAUD DUYCK JERÔME PIATON
description	A control system, in particular an aircraft flight control system, having a linkage with a force-transmission link (3), the link having a body (5) having at least one end housing (8) slidably receiving a coupling rod (9) for coupling the link to an adjacent element of the linkage, the housing being closed by an elastically-deformable test member (10) through which the rod passes and that has an inner periphery fastened to the rod and an outer periphery fastened to a wall defining the end housing, and the end housing receiving at least one sensor (11) for sensing relative movement between the rod and the body.
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subjects	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
title	sistema de comando, notadamente de vôo para aeronave
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