IP Library › Granted Patent US 11,209,227
Granted Patent B2
US 11,209,227 · App. 16/161,242 · Granted Dec 28, 2021

Method and a system for regulating a temperature associated with a heat exchanger assembly of a turbine engine

Inventors: Cedrik Djelassi (Moissy-Cramayel, FR); Pierre Cabrera (Moissy-Cramayel, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F28F27/02F01D25/12F02C6/08F02C7/18F02C9/18B64D13/06B64D27/10B64D2013/0618F02C6/04F02C7/143F05D2270/112F05D2270/303F05D2270/44
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Quick Facts
Patent No.
US 11,209,227
App. No.
16/161,242
Granted
Dec 28, 2021
Kind
B2
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.

Claims (16)

1. A regulation method for regulating a temperature associated with a heat exchanger assembly of a turbine engine, the method being for implementing in a regulator system that comprises a temperature sensor for measuring said temperature, a valve controlled electrically by a control unit, the valve having a shutter configured to vary a flow rate of a fluid passing through said heat exchanger assembly in order to influence said temperature, the heat exchanger assembly further comprising a heat exchanger, a first inlet of the heat exchanger being connected to a first pipe bleeding off a first air stream and a second inlet of the heat exchanger being connected to a second pipe bleeding off a second air stream using the valve, a temperature of the second air stream at the second inlet to the heat exchanger being lower than a temperature of the first air stream at the second inlet to the heat exchanger, and the heat exchanger being suitable for lowering the temperature of the first air stream at a first outlet from the heat exchanger by heat exchange with the second air stream, the method comprising during a single regulation cycle:

measuring the temperature of the first air stream at the first outlet from the heat exchanger;

receiving a setpoint temperature for the first air stream at the first outlet from the heat exchanger using a control unit;

estimating a theoretical temperature for the first air stream at the first outlet from the heat exchanger as a function of an estimate of a position of the shutter of the valve using the control unit;

calculating a first temperature difference between the measured temperature and the estimated theoretical temperature using the control unit;

determining a correction current for correcting a control current from the control unit for controlling the valve based on the calculated first temperature difference using the control unit;

determining a second temperature difference between the measured temperature and the setpoint temperature using the control unit; and

determining a control current for controlling the shutter of the valve based on the determined second temperature difference and a preceding correction current determined during a preceding cycle using the control unit,

wherein the position of the shutter of the valve is determined from the control current and the preceding correction current determined during the preceding cycle using the control unit.

2. The method according to claim 1 , wherein determining the correction current comprises amplifying a representative signal representative of the calculated first temperature difference by a gain and by integrating said amplified representative signal using the control unit.

3. The method according to claim 1 , wherein the theoretical temperature results from adding together a static component and a dynamic component:

the static component resulting from the temperature of the first air stream at the first inlet to the heat exchanger to which a regulation term has been added, the regulation term being determined from a product of an efficiency of the heat exchanger multiplied by an inlet temperature difference calculated by subtracting a value of the temperature of the second air stream at the second inlet to the heat exchanger measured using a second temperature sensor from a value of the temperature of the first air stream at the first inlet to the heat exchanger measured using a first temperature sensor; and

the dynamic component corresponding to a first order lowpass function in which a time constant varies as a function of the efficiency of the heat exchanger and of a flow rate of the first air stream at the first inlet to the heat exchanger measured using a first flow rate sensor.

4. The method according to claim 3 , wherein the efficiency of the heat exchanger depends on a flow rate of the second air stream at the second inlet to the heat exchanger measured using a second flow rate sensor and on the flow rate of the first air stream at the first inlet to the heat exchanger measured using the first flow rate sensor, the method further comprising measuring the flow rate of the first air stream at the first inlet to the heat exchanger using the first flow rate sensor and determining the flow rate of the second air stream at the second inlet to the heat exchanger from a maximum value for an air flow rate of cooling air when the shutter of the valve is fully open from a factor depending on the position of the shutter of the valve using the control unit.

5. The method according to claim 4 , wherein the maximum value of the air flow rate of cooling air is determined from a product of a function depending on a ratio of a pressure of the second air stream at the second inlet to the heat exchanger measured using a first pressure sensor divided by a pressure of the second air stream at a second outlet from the heat exchanger measured using a second pressure sensor multiplied by a ratio of said pressure of the second air stream at the second inlet to the heat exchanger divided by a square root of the temperature of the second air stream at the second inlet to the heat exchanger.

6. The method according to claim 1 , further comprising saturating the control current at a maximum value or a minimum value as a function of said second temperature difference using the control unit, the maximum saturation value and the minimum saturation value depending on the correction current.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 16, 2018
From: DJELASSI, CEDRIK; CABRERA, PIERRE
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 047174/0035 →
Priority Claims (1)
FR 17 59906 · Oct 20, 2017 · national
Continuity (1)
Related Publication 20190120576A1 · Apr 25, 2019
Cited By (1)
US 12,464,675