On-line cleaning of turbine hot gas path deposits via pressure pulsations
A method for removing hot gas deposits from a system via pressure pulses is provided. The method includes regulating a flow of a mixture of detonation fluid and oxidizer into an expansion chamber; and generating a detonation within the expansion chamber by igniting the mixture of detonation fluid and oxidizer in the expansion chamber producing a high-pressure wave, the high-pressure wave propagating along a fluid path of the system in a supersonic rate removing hot gas deposits in the fluid path while the system is in fired operation, the expansion chamber directing the high-pressure wave towards the fluid path of the system.
1. An apparatus for removing hot gas deposits from a system via pressure pulses, comprising:
an expansion chamber configured to receive a mixture of detonation fluid and oxidizer;
an initiator;
a first control device configured to regulate flow of detonation fluid; and
a second control device configured to regulate flow of oxidizer, the first control device and the second control device selectively operable in a first mode of operation and a second mode of operation; and
a controller in communication with the initiator, the first control device, and the second control device, the controller configured to:
selectively control operation of the first control device and the second control device in the first mode of operation to regulate flow of detonation fluid and oxidizer periodically into the expansion chamber, or the second mode of operation to provide a continuous flow of detonation fluid, and one of a continuous supply and selective prevention of oxidizer to the expansion chamber, and
control operation of the initiator to ignite the mixture of detonation fluid and oxidizer during the first mode of operation to create a detonation, the detonation configured to create a high pressure wave that substantially removes hot gas deposits while the system is in fired operation, and initially ignites the mixture of detonation fluid and oxidizer in the second mode of operation.
2. The apparatus as in claim 1 , wherein the controller controls the flow of detonation fluid and oxidizer supplied by the first control device and the second control device to vary a frequency and amplitude of the high-pressure waves.
3. The apparatus as in claim 1 , wherein the controller is configured to control the apparatus as one of a torch igniter or a pilot flame for the system in the second mode of operation, wherein the controller controls the first control device and the second control device to be locked in a continuous flow position as the torch igniter, and wherein the controller is configured to control the first control device to flow detonation fluid continuously and the second control device to flow oxidizer continuously or selectively prevent oxidizer to flow as the pilot flame.
4. The apparatus as in claim 1 , wherein the first control device and the second control device are rotary valves.
5. The apparatus as in claim 1 , wherein the system is a gas turbine operating at pressures greater than atmospheric pressure while in fired operation.
6. The apparatus as in claim 1 , wherein the initiator is a spark plug.
7. A system for removing turbine hot gas path deposits from a fluid path of a gas turbine via pressure pulses, comprising:
an expansion chamber disposed within a combustion chamber of the gas turbine, the expansion chamber is configured to receive a mixture of detonation fluid and oxidizer;
an initiator;
a first control device configured to regulate flow of detonation fluid; and
a second control device configured to regulate flow of oxidizer, the first control device and the second control device selectively operable in a first mode of operation and a second mode of operation; and
a controller in communication with the initiator, the first control device, and the second control device, the controller configured to:
selectively control operation of the first control device and the second control device in the first mode of operation to regulate flow of detonation fluid and oxidizer periodically into the expansion chamber, or the second mode of operation to provide a continuous flow of detonation fluid, and one of a continuous supply and selective prevention of oxidizer to the expansion chamber, and
control operation of the initiator to ignite the mixture of detonation fluid and oxidizer during the first mode of operation to create a detonation, the detonation configured to create a high pressure wave that substantially removes hot gas deposits while the system is in fired operation, and initially ignites the mixture of detonation fluid and oxidizer in the second mode of operation.
8. The system as in claim 7 , wherein the mixture of detonation fluid and oxidizer comprises of at least one volatile liquid fuel, at least one hydrocarbon gas or a combination thereof.
9. The apparatus as in claim 5 , wherein an amount of detonation fluid used by the apparatus in the first mode of operation is about 1/50 of a turbine fuel flow.