Invention Grant
- Patent Title: Method and a system for regulating a temperature associated with a heat exchanger assembly of a turbine engine
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Application No.: US17452978Application Date: 2021-10-29
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Publication No.: US11674760B2Publication Date: 2023-06-13
- Inventor: Cedrik Djelassi , Pierre Cabrera
- 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: FR 59906 2017.10.20
- The original application number of the division: US16161242 2018.10.16
- Main IPC: F28F27/02
- IPC: F28F27/02 ; F02C6/08 ; F02C9/18 ; F02C7/18 ; F01D25/12 ; B64D13/06 ; B64D27/10 ; F02C6/04 ; F02C7/143

Abstract:
A method of regulating a temperature associated with a heat exchanger assembly of a turbine engine, the method includes, in a single cycle: measuring the temperature of an air stream at the outlet from a heat exchanger; receiving a setpoint temperature for the air stream at the outlet from the heat exchanger; estimating a theoretical temperature for the air stream at the outlet from the heat exchanger as a function of an estimate of the shutter position of a controlled valve bleeding off a cooling air stream for the heat exchanger; determining a correction current from the difference between the measured temperature and the theoretical temperature; and determining a control current for the shutter from the difference between the measured temperature and the setpoint temperature and the correction current determined during the preceding cycle, the shutter position being determined from the control and correction currents determined during the preceding cycle.
Information query