Invention Grant
- Patent Title: Sector of an annular nozzle of a turbine of a turbomachine
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Application No.: US16110255Application Date: 2018-08-23
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Publication No.: US11021979B2Publication Date: 2021-06-01
- Inventor: Lucien Henri Jacques Quennehen , Sébastien Serge Francis Congratel , Antoine Claude Michel Etienne Danis , Clément Jarrossay , Nicolas Paul Tableau
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR1758011 20170830
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D11/00 ; F01D25/24 ; F01D11/08

Abstract:
A sector of a sectorized annular nozzle of a turbine of a turbomachine comprises an outer platform having an outer wall connected to a coaxial inner wall via at least one straightening fixed blade. The outer platform includes hooking means that hook the outer platform to a turbine fixed casing. The outer platform includes an outer circular shell, axially offset with respect to the outer wall and integrally formed with the outer wall, and the outer shell is intended to surround an angular portion of a rotor wheel. The hooking means includes an upstream circular edge and a downstream circular edge extending axially, said upstream and downstream edges being respectively configured to attach to an upstream hook and a downstream hook of said turbine casing, and said upstream and downstream edges being oriented in the downstream direction.
Public/Granted literature
- US20190063244A1 SECTOR OF AN ANNULAR NOZZLE OF A TURBINE OF A TURBOMACHINE Public/Granted day:2019-02-28
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