Invention Grant
- Patent Title: Structural casing for an axial turbine engine
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Application No.: US16263958Application Date: 2019-01-31
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Publication No.: US10907504B2Publication Date: 2021-02-02
- Inventor: Ludovic Bovyn , Eric Englebert , Maxime Peeters
- Applicant: SAFRAN AERO BOOSTERS SA
- Applicant Address: BE Herstal
- Assignee: SAFRAN AERO BOOSTERS SA
- Current Assignee: SAFRAN AERO BOOSTERS SA
- Current Assignee Address: BE Herstal
- Agent James E. Walton
- Priority: BE2018/5063 20180202
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D9/04 ; F01D25/28

Abstract:
A structural casing for an axial turbine engine includes an outer ring, an inner hub, and a plurality of struts extending radially from the hub to the ring, wherein the ring is made of a plurality of angular segments welded together. The segments extend circumferentially of different angles, some segments being larger angularly than others. The structural casing is adapted to be an intermediate casing between two compressors of a turbine engine.
Public/Granted literature
- US20190242271A1 Structural Casing for an Axial Turbine Engine Public/Granted day:2019-08-08
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