Invention Grant
- Patent Title: Lubricating oil circuit of a turbomachine, turbomachine and regulation method thereof
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Application No.: US16598491Application Date: 2019-10-10
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Publication No.: US11619141B2Publication Date: 2023-04-04
- Inventor: Christophe Marc Alexandre Le Brun , Sébastien Jean Fernand Deneuve
- Applicant: Safran Aircraft Engines
- Applicant Address: FR Paris
- Assignee: Safran Aircraft Engines
- Current Assignee: Safran Aircraft Engines
- Current Assignee Address: FR Paris
- Agency: Sughrue Mion, PLLC
- Priority: FR1859410 20181011
- Main IPC: F01D25/18
- IPC: F01D25/18 ; F16H57/04 ; F02C7/14

Abstract:
A lubricating oil circuit of a turbomachine includes a distribution valve that distributes an oil flow rate among a first heat exchanger and a bypass duct, connected to an oil duct, which is connected to an heat exchanger positioned against a turbomachine fuel passage duct, and includes a gearbox of a rotation speed reducer that lowers a rotational speed of a first rotary fan shaft of the turbomachine relative to a rotational speed of a second low-pressure compressor rotary shaft of the turbomachine or of a second low-pressure turbine rotary shaft of the turbomachine, and a regulation device. The regulation device includes a local regulation loop that generates an oil flow rate distribution control signal and regulates an oil temperature of the oil duct on a temperature setpoint, and a global regulation loop that generates the temperature setpoint as a function of the temperature and of the temperature setpoint.
Information query