Invention Grant
- Patent Title: Device for cooling oil for a turbine engine
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Application No.: US14904206Application Date: 2014-07-10
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Publication No.: US10233798B2Publication Date: 2019-03-19
- Inventor: Jean-Louis Muller , Pierre Charles Mouton
- Applicant: Snecma
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Blank Rome LLP
- Priority: FR1356913 20130712
- International Application: PCT/FR2014/051775 WO 20140710
- International Announcement: WO2015/004394 WO 20150115
- Main IPC: F02C6/08
- IPC: F02C6/08 ; F01M5/00 ; F01D25/12 ; F02C7/06 ; F02C7/14 ; F01P1/00 ; F01P11/12
Abstract:
The invention relates to a device (11) for cooling oil for a turbine engine, such as an aircraft turbojet or turboprop engine, characterized in that it comprises a duct (12) for circulating a flow of cold air (F1), means (16) for injecting oil into the duct, and means (19) for extracting the oil mixed with the flow of cold air (F1), located in the duct (12), downstream from the injection means (16).
Public/Granted literature
- US20160153326A1 DEVICE FOR COOLING OIL FOR A TURBINE ENGINE Public/Granted day:2016-06-02
Information query
IPC分类:
