Invention Grant
- Patent Title: Turbomachine designed to operate in turning gear mode
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Application No.: US15025638Application Date: 2014-09-29
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Publication No.: US10753280B2Publication Date: 2020-08-25
- Inventor: Romain Thiriet , Vincent Poumarede , Camel Serghine
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@31b2194f
- International Application: PCT/FR2014/052444 WO 20140929
- International Announcement: WO2015/044614 WO 20150402
- Main IPC: F02C7/06
- IPC: F02C7/06 ; F01D25/10 ; F01D25/18 ; F01D25/36 ; F02C3/04 ; F02C7/268 ; F02C6/18

Abstract:
A field of turbine engines, and more particularly to an engine including a compressor; a combustion chamber; a first turbine connected to the compressor by a first rotary shaft; an actuator device for actuating the first rotary shaft in order to keep the first turbine and the compressor in rotation while the combustion chamber is extinguished; and a lubrication circuit for lubricating the engine. The circuit passes through at least one heat source suitable for heating the lubricant in the lubrication circuit while the first turbine and the compressor are rotating with the combustion chamber extinguished.
Public/Granted literature
- US20160237900A1 TURBOMACHINE DESIGNED TO OPERATE IN TURNING GEAR MODE Public/Granted day:2016-08-18
Information query
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