- Patent Title: Method for manufacturing an annular casing equipping a turbomachine
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Application No.: US16303555Application Date: 2017-05-18
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Publication No.: US11293296B2Publication Date: 2022-04-05
- Inventor: Hubert Jean Marie Fabre , Pauline Nathalie Six , Marc-Emmanuel Jean Francois Techer
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Womble Bond Dickinson (US) LLP
- Priority: FR1654606 20160524
- International Application: PCT/FR2017/051197 WO 20170518
- International Announcement: WO2017/203134 WO 20171130
- Main IPC: B29C63/00
- IPC: B29C63/00 ; F01D11/12 ; F01D25/24

Abstract:
The invention relates to a method for manufacturing a carrying casing (12) provided with a collar (18) for supporting at least one cartridge of abradable material for a turbomachine, said carrying casing (12) comprising at least one bare annular casing (16) and one block of honeycomb material (20) that comprises an outer face (22) configured to be secured to an inner face (24) of said bare annular casing (16), said block being covered with a skin (26), characterized in that it comprises successively: —a step in which the outer face (22) of the block (20) is secured to the inner face (24) of the bare annular casing (16), —a step in which the circularity of San inner face (32) of the block (20) is monitored and in which, if necessary, the inner face (32) of the block (20) is machined to round, —a step in which, simultaneously, said skin (26) is produced and is secured to said block (20).
Public/Granted literature
- US20200025017A1 METHOD FOR MANUFACTURING AN ANNULAR CASING EQUIPPING A TURBOMACHINE Public/Granted day:2020-01-23
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