Control unit and a method for controlling blade tip clearance
View Patent ↗A method and system for controlling clearance between the tips of blades of a turbine rotor in a gas turbine airplane engine and a turbine ring of a casing surrounding the blades. A valve is controlled to act on a flow rate and/or a temperature of air directed against the casing. The valve is of the on/off type for switching between an open state and a closed state in a determined reaction time, the valve control module including a corrector for determining a first binary control signal that can take a first value corresponding to an open state and a second value corresponding to a closed state of the valve. The corrector includes a time-delay module for determining a binary control signal, with the duration between two successive changes of state in the control signal being not less than the reaction time of the valve.
1. A control unit for controlling clearance between the tips of blades of a turbine rotor in a gas turbine airplane engine and a turbine ring of a casing surrounding the blades, the control unit comprising a module for controlling a valve of the on/off type suitable for switching between an open state and a closed state in a determined reaction time in order to act on a flow rate and/or a temperature of air directed against the casing, wherein
said control module comprises a corrector suitable for determining a first binary control signal capable of taking a first value corresponding to an open state of the valve and a second value corresponding to a closed state of the valve, said corrector including:
a determination module for determining a correction magnitude as a function of a clearance setpoint and of an estimate of the clearance;
a switch module suitable for determining a second binary control signal as a function of the correction magnitude, said switch module allocating to the second control signal:
said first value when the correction magnitude is greater than a predetermined threshold; and
said second value when the correction magnitude is less than or equal to the predetermined threshold; and
a time-delay module suitable for determining a third binary control signal as a function of the second control signal, said time-delay module allocating to the third control signal, in response to a change in the value of the second control signal:
the value of the second control signal when the duration that has elapsed since the most recent change in the value of the third control signal is longer than a predetermined time-delay duration; and
the preceding value of the third control signal when the duration that has elapsed since the most recent change in the value of the third control signal is less than or equal to the predetermined time-delay duration;
the predetermined time-delay duration being not less than the reaction time of the valve;
said first control signal being determined as a function of said third control signal.
2. A control unit according to claim 1 , wherein the time-delay duration is determined as a function of a flow rate setpoint.
3. A control unit according to claim 1 , wherein said determination module comprises a proportional-integral corrector suitable for determining an initial correction magnitude as a function of a difference between the clearance setpoint and the estimate of the clearance, and a normalizer module suitable for determining said correction magnitude as a function of the initial correction magnitude and of a gain that depends on the estimate of the clearance.
4. An airplane engine including an on/off type valve and a control unit according to claim 1 , wherein said valve is controlled as a function of the first control signal determined by the control unit.
5. A method of controlling clearance between the tips of blades of a turbine rotor in a gas turbine airplane engine and a turbine ring of a casing surrounding the blades, the method comprising controlling a valve of the on/off type suitable for switching between an open state and a closed state in a determined reaction time in order to act on a flow rate and/or a temperature of air directed against the casing, wherein
the control of the valve comprises determining a first binary control signal capable of taking a first value corresponding to an open state of the valve and a second value corresponding to a closed state of the valve, the determination of the first control signal including:
determining a correction magnitude as a function of a clearance setpoint and of an estimate of the clearance;
determining a second binary control signal as a function of the correction magnitude by allocating to the second control signal:
said first value when the correction magnitude is greater than a predetermined threshold; and
said second value when the correction magnitude is less than or equal to the predetermined threshold; and
determining a third binary control signal as a function of the second control signal, by allocating to the third control signal, in response to a change of value in the second control signal:
the value of the second control signal when the duration that has elapsed since the most recent change in the value of the third control signal is longer than a predetermined time-delay duration and switching the valve between the open state or the closed state; and
the preceding value of the third control signal when the duration that has elapsed since the most recent change in the value of the third control signal is less than or equal to the predetermined time-delay duration and not switching the valve between the open state or the closed state;
the duration of the predetermined time-delay being not less than the reaction time of the valve;
said first control signal being determined as a function of said third control signal.