FINE ADJUSTMENT CONTROL MECHANISM FOR ORIENTATION AND/OR POSITIONING OF A PAY LOAD

PCT No. PCT/FR90/00498 Sec. 371 Date Dec. 30, 1991 Sec. 102(e) Date Dec. 30, 1991 PCT Filed Jul. 3, 1990 PCT Pub. No. WO91/00976 PCT Pub. Date Jan. 24, 1991.A mechanism for finely adjusting the orientation and/or the position of a payload, characterized in that it comprises: a resilient mechanism co...

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Hauptverfasser:	PANIN, FABIO
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION BLASTING CONTROLLING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS OPTICS PERFORMING OPERATIONS PHYSICS REGULATING STANDS OR SUPPORTS SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES THERMAL INSULATION IN GENERAL TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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Zusammenfassung:	PCT No. PCT/FR90/00498 Sec. 371 Date Dec. 30, 1991 Sec. 102(e) Date Dec. 30, 1991 PCT Filed Jul. 3, 1990 PCT Pub. No. WO91/00976 PCT Pub. Date Jan. 24, 1991.A mechanism for finely adjusting the orientation and/or the position of a payload, characterized in that it comprises: a resilient mechanism constituted by at least one continuous ring (10); a payload support device (15) suitable for transforming deformation of the ring into rotation or into combined rotation and translation; a ring deformation mechanism (11) suitable for directly applying simultaneous deformation forces at two diameterically opposite points of the ring; and a device (14) for varying the orientation of the diametral line of action of the ring deformation mechanism, thereby enabling the orientation and/or the position of the payload to be adjusted finely or coarsely. The mechanism is applicable to the optical industry, to pointing antennas, etc.