Invention Grant
- Patent Title: Anti-icing system for a turbine engine vane
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Application No.: US15748252Application Date: 2016-07-27
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Publication No.: US10683805B2Publication Date: 2020-06-16
- Inventor: Guillaume Claude Georges Philippe Linassier , Morgan Balland , Helene Mazet , Christophe Scholtes , Antoine Robert Alain Brunet , Simon Amodeo
- 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$PriorityClaim@33410f92 com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@7ed65613
- International Application: PCT/FR2016/051953 WO 20160727
- International Announcement: WO2017/017378 WO 20170202
- Main IPC: F02C7/047
- IPC: F02C7/047 ; F01D25/02 ; F01D9/04

Abstract:
An anti-icing system for a turbine engine vane extending between an outer casing and an inner casing defining a passage, the system includes an injector device for injecting a jet of air into the passage upstream from the vane, the injector device including a first injection orifice for injecting the jet of air, the first orifice passing through one member selected from the outer casing and the inner casing, and being located in such a manner that, at a first speed of the engine wherein a stream of air flows generally in the passage along a first direction, the first orifice and a leading edge of the vane are substantially in alignment along the first direction, the first orifice is spaced apart from the junction between the leading edge of the vane and the member through which the first orifice passes by a distance of at least 10 mm, and preferably of about 15 mm.
Public/Granted literature
- US20180216528A1 ANTI-ICING SYSTEM FOR A TURBINE ENGINE VANE Public/Granted day:2018-08-02
Information query
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