Invention Grant
- Patent Title: Turbomachine case comprising a central part projecting from two lateral portions in a junction region
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Application No.: US16166435Application Date: 2018-10-22
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Publication No.: US10934872B2Publication Date: 2021-03-02
- Inventor: Nicolas Paul Tableau , Sebastien Serge Francis Congratel , Antoine Claude Michel Etienne Danis , Maurice Guy Judet , Lucien Henri Jacques Quennehen
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1759986 20171023
- Main IPC: F01D11/08
- IPC: F01D11/08 ; F01D9/04 ; F01D25/24 ; F01D25/28 ; F01D5/14 ; F01D5/28 ; F01D11/00 ; F01D25/00

Abstract:
A support case for a turbomachine ring sector includes an annular body around a longitudinal axis of the case, and a downstream edge for attachment of the ring sector. The downstream edge extends from the body radially towards the inside of the case. The downstream edge extends circumferentially along a junction region between the body and a fixed vanes stage. The junction region includes a central portion and two lateral portions located on each side of the central portion, along a circumferential direction of the case with respect to its longitudinal axis. The central portion projects radially outwards from the case with respect to the lateral portions.
Public/Granted literature
- US20190128132A1 TURBOMACHINE CASE COMPRISING A CENTRAL PART PROJECTING FROM TWO LATERAL PORTIONS IN A JUNCTION REGION Public/Granted day:2019-05-02
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