Assembly for a turbine engine

An assembly 50 includes an annular row of stator blades including vanes 6 extending radially which are variable in pitch, with a tubular component mounted around a radially extending pivot 14, the tubular component 26 having at least a first zone 26a, 26c fitted tightly to the pivot, with a second z...

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Hauptverfasser: Benoit Andre Pierre Frossard, Remi Philippe Guy Onfray, Clement Miraton
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creator Benoit Andre Pierre Frossard
Remi Philippe Guy Onfray
Clement Miraton
description An assembly 50 includes an annular row of stator blades including vanes 6 extending radially which are variable in pitch, with a tubular component mounted around a radially extending pivot 14, the tubular component 26 having at least a first zone 26a, 26c fitted tightly to the pivot, with a second zone 26b where the tubular component bulges 28 and does not make contact with the pivot, defining an annular space 30 there between. The bulge of the tubular component may be convex. There may be two tightly fitted zones, which may be at either end of the tubular component. The assembly is for a turbine engine, it may form part of a turbine engine compressor and may be used in a turbojet or turbo prop engine.
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The bulge of the tubular component may be convex. There may be two tightly fitted zones, which may be at either end of the tubular component. 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subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
WEAPONS
title Assembly for a turbine engine
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