Apparatus and method for testing combustion
View Patent ↗A sensor 11 detects the acoustic pressure at a first location in a combustion chamber 7 of a test rig 1 and produces an input signal which is a function of the acoustic pressure. A controller 13 receives the input signal and produces an output signal which is a function of the input signal. An acoustic actuator ( 16 - 18 ) receives the output signal and introduces into the combustion chamber 7 at a second location an acoustic pressure which is a function of the output signal. The acoustic actuator may comprise a fuel injector 18 or a loudspeaker. By using an appropriate control algorithm, acoustic boundary conditions corresponding to a particular gas turbine combustion chamber may be produced, at least in a certain frequency range.
1. A test rig for testing the combustion of a fuel, the test rig comprising:
a combustion chamber; and
means for replicating the acoustic impedance of a combustor in the test rig, said replicating means comprising:
a sensor configured and arranged to detect the acoustic pressure at a first location in the combustion chamber and to produce an input signal which is a function of the acoustic pressure;
a controller in communication with the sensor to receive the input signal and configured and arranged to produce an output signal which is a function of the input signal and the acoustic impedance of the combustor; and
an acoustic actuator configured and arranged to receive the output signal and introduce into the combustion chamber at a second location an acoustic pressure which is a function of the output signal.
2. A test rig as claimed in claim 1 , wherein the actuator comprises a loudspeaker.
3. A test rig as claimed in claim 1 , wherein the actuator comprises a fuel valve controlled by the output signal and a fuel injector which is connected to the fuel valve and which injects fuel into the combustion chamber.
4. A test rig as claimed in claim 1 , wherein the controller comprises a digital processor.
5. A test rig as claimed in claim 1 , wherein the controller comprises a band-pass filter.
6. A test rig as claimed in claim 5 , wherein the controller includes an amplifier.
7. A test rig as claimed in claim 6 , wherein the controller includes a time-delay line.
8. A test rig as claimed in claim 7 , wherein the time-delay line is between the band-pass filter and the amplifier.
9. A method of testing the combustion of a fuel in a test rig, in which a combustion chamber is defined downstream of a burner, the method comprising:
adjusting the acoustic boundary conditions of the test rig, so as to at least in part replicate the acoustic impedance of a combustor in the test rig, the test rig comprising at least
a sensor configured and arranged to detect the acoustic pressure at a first location in the combustion chamber and to produce an input signal which is a function of the acoustic pressure;
a controller in communication with the sensor to receive the input signal and configured and arranged to produce an output signal which is a function of the input signal and the acoustic impedance of the combustor; and
an acoustic actuator configured and arranged to receive the output signal and introduce into the combustion chamber at a second location an acoustic pressure which is a function of the output signal;
installing said burner in said test rig; and
testing said burner, including
detecting the acoustic pressure at said first location in the combustion chamber;
producing an input signal which is a function of the acoustic pressure;
producing an output signal which is a function of the input signal; and
introducing an acoustic pressure which is a function of the output signal into the combustion chamber at a second location, to adjust the acoustic impedance of the combustion chamber.