Aircraft servo unit push:rod guide - has longitudinally split bearing bush fixed in housing by telescopic cone rings supported by compression springs

The guide element is for push rods, esp. in redundant electrohydraulic servo units of aircraft control systems. The guide element consists of a bearing bush, which is split several times in a longitudinal direction. The bearing bush is fixed to the housing of the servo unit via two telescopic cone r...

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Bibliographische Detailangaben
1. Verfasser:	RENNER,ECKHARD
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BEARINGS BLASTING COSMONAUTICS ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The guide element is for push rods, esp. in redundant electrohydraulic servo units of aircraft control systems. The guide element consists of a bearing bush, which is split several times in a longitudinal direction. The bearing bush is fixed to the housing of the servo unit via two telescopic cone rings which accommodate the bush. The cone rings are supported in the longitudinal direction by compression springs. The rings and front faces of the bush are in a drive connection, to be able to move the rings away from each other against the force of the springs.