- Patent Title: Guide vane assembly vane box of an axial turbine engine compressor
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Application No.: US14792089Application Date: 2015-07-06
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Publication No.: US09611747B2Publication Date: 2017-04-04
- Inventor: Alain Derclaye
- Applicant: Techspace Aero S.A.
- Applicant Address: BE
- Assignee: Safran Aero Boosters SA
- Current Assignee: Safran Aero Boosters SA
- Current Assignee Address: BE
- Agency: Polster Lieder
- Priority: EP14175924 20140707
- Main IPC: F04D9/04
- IPC: F04D9/04 ; F01D9/04

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.
Public/Granted literature
- US20160003073A1 GUIDE VANE ASSEMBLY VANE BOX OF AN AXIAL TURBINE ENGINE COMPRESSOR Public/Granted day:2016-01-07
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