Invention Grant
- Patent Title: Discharge flow duct of a turbine engine comprising a VBV grating with variable setting
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Application No.: US15563359Application Date: 2016-03-31
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Publication No.: US10794218B2Publication Date: 2020-10-06
- Inventor: Jean-Frederic Pierre Joseph Bruhat , Philippe Jacques Pierre Fessou , Benjamin Lukowski
- 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: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@18282362
- International Application: PCT/FR2016/050716 WO 20160331
- International Announcement: WO2016/156739 WO 20161006
- Main IPC: F03B1/00
- IPC: F03B1/00 ; F01D17/14 ; F02C6/08 ; F02C9/18 ; F02K3/075 ; F01D9/02 ; F01D25/24

Abstract:
A hub of an intermediate casing for a dual-flow turbine engine includes a discharge flow duct extending between an inner shroud and an outer shroud of the hub, the discharge flow duct leading into the secondary flow space through an outlet opening formed in the outer shroud, the outlet opening included in a discharge plane substantially tangential to the outer shroud; and discharge fins including an upstream fin and a downstream fin. An upstream acute angle between the discharge plane and the skeleton line of the upstream fin is smaller than a downstream acute angle between the discharge plane and the skeleton line of the downstream fin.
Public/Granted literature
- US20180080337A1 DISCHARGE FLOW DUCT OF A TURBINE ENGINE COMPRISING A VBV GRATING WITH VARIABLE SETTING Public/Granted day:2018-03-22
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