Guide vane assembly vane box of an axial turbine engine compressor
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United States of America Patent
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Apr 4, 2017
Grant Date -
Jan 7, 2016
app pub date -
Jul 6, 2015
filing date -
Jul 7, 2014
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Abstract
The invention relates to an angular sector of a bladed stator of a low-pressure compressor of an axial turbine engine. The sector comprises an outer shroud and an inner shroud in the form of circular arcs intended to be mounted in a concentric manner on the outer casing of the turbine engine compressor. The sector likewise comprises a row of stator vanes extending radially and anchored in the shrouds in such a manner as to form a bladed box. The vanes of the box comprise anchoring lugs at their outer ends, the lugs being disposed in the thickness of the outer shroud. The inner shroud comprises stubs for anchoring vanes.
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