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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Bibliographische Detailangaben
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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Beschreibung
Zusammenfassung:	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.