Variable geometry diffuser having extended travel and control method thereof
An improved variable geometry diffuser (VGD) mechanism for use with a centrifugal compressor. This VGD mechanism extends substantially completely into the diffuser gap so that the VGD mechanism may be used more fully to control other operational functions. The VGD mechanism may be used to minimize compressor backspin and associated transient loads during compressor shut down by preventing a reverse flow of refrigerant gas through the diffuser gap during compressor shutdown, which is prevented because the diffuser gap is substantially blocked by the full extension of the diffuser ring. During start-up, transient surge and stall also can be effectively eliminated as gas flow through the diffuser gap can be impeded as load and impeller speed increase, thereby alleviating the problems caused by startup loads at low speeds. The VGD mechanism can be used for capacity control as well so as to achieve more effective turndown at low loads.
1. A variable geometry diffuser for a centrifugal compressor, comprising:
a diffuser ring configured to extend into a diffuser gap formed between a nozzle base plate and a diffuser plate, wherein the diffuser ring is disposed within a groove of the nozzle base plate, wherein the diffuser ring has an L-shaped cross-section formed by a first flange and a second flange extending crosswise to the first flange, and wherein the diffuser gap is configured to receive a gas flow and enable at least a portion of the gas flow to enter the groove and surround the second flange; and
an actuator configured to move the diffuser ring between a retracted position and an extended position to control a capacity of the centrifugal compressor without prerotation vanes, wherein the diffuser ring extends across the diffuser gap in the extended position to enable a first surface of the first flange of the diffuser ring to engage with a mating surface of the diffuser plate.
2. The variable geometry diffuser of claim 1 , wherein a radial thickness of the first flange is less than a radial thickness of the second flange, and wherein a radial gap extends between the second flange and the groove.
3. The variable geometry diffuser of claim 2 , wherein the first flange comprises the first surface and the second flange comprises a second surface, a third surface, and a fourth surface, wherein the first flange extends from the second surface of the second flange, the third surface is opposite the second surface, the fourth surface extends between the second surface and the third surface, and the radial gap extends between the fourth surface and the groove.
4. The variable geometry diffuser of claim 1 , comprising a controller communicatively coupled to the actuator, wherein the controller is configured to instruct the actuator to transition the diffuser ring between the retracted position and the extended position based on sensor feedback indicative of an operating parameter of the centrifugal compressor.
5. The variable geometry diffuser of claim 4 , wherein the operating parameter comprises a speed of the centrifugal compressor, an acoustic energy generated by the centrifugal compressor, or both.
6. The variable geometry diffuser of claim 1 , comprising a controller communicatively coupled to the actuator and configured to store a threshold length between the first surface of the diffuser ring and the mating surface of diffuser plate or the nozzle base plate, wherein the controller is configured to determine the extended position of the diffuser ring based on the threshold length.
7. The variable geometry diffuser of claim 1 , comprising a controller communicatively coupled to the actuator, wherein the actuator is configured to provide a first signal to the controller indicative of a first position of the actuator associated with the diffuser ring in the extended position and to provide a second signal to the controller indicative of a second position of the actuator associated with diffuser ring in the retracted position to enable calibration of the controller.
8. The variable geometry diffuser of claim 7 , wherein the calibration of the controller enables the controller to determine a location of the diffuser ring relative to the diffuser gap when the actuator is between the first position and the second position without use of additional sensors.
9. The variable geometry diffuser of claim 1 , wherein the actuator is a linear actuator.
10. A centrifugal compressor, comprising:
a diffuser ring disposed within a groove of a nozzle base plate and configured to move within the groove and into a diffuser gap extending between the nozzle base plate and a diffuser plate, wherein the diffuser ring has an L-shaped cross section formed by a first flange and a second flange extending crosswise to the first flange, wherein the diffuser gap is configured to enable a gas to flow therethrough and to enter the groove and surround the second flange; and
an actuator configured to move the diffuser ring between a retracted position and an extended position, wherein the first flange extends across the diffuser gap to engage with the diffuser plate in the extended position, and wherein the centrifugal compressor is without prerotation vanes.
11. The centrifugal compressor of claim 10 , wherein the first flange is configured to extend into the diffuser gap and toward the diffuser plate in a direction crosswise to a flow direction of the gas through the diffuser gap.
12. The centrifugal compressor of claim 10 , further comprising:
a controller communicatively coupled to the actuator; and
an acoustic sensor configured to provide feedback to the controller indicative of noise related to surge or stall of the centrifugal compressor, wherein the controller is configured to instruct the actuator to transition the diffuser ring to the extended position upon receiving the feedback.
13. The centrifugal compressor of claim 10 , further comprising:
a controller communicatively coupled to the actuator; and
a power source electrically coupled to the controller and the actuator, wherein the power source is configured to supply electrical power to the controller and the actuator upon receiving feedback from a sensor indicating a loss of primary power to the centrifugal compressor, and wherein the controller is configured to instruct the actuator to transition the diffuser ring to the extended position upon receiving the feedback.
14. The centrifugal compressor of claim 10 , wherein a first radial thickness of the first flange is less than a second radial thickness of the second flange.
15. A method for controlling gas flow in a centrifugal compressor, comprising:
directing, via an impeller, a gas through a diffuser gap extending between a diffuser plate and a nozzle base plate of the centrifugal compressor; and
translating, via an actuator, a diffuser ring within a groove formed in the nozzle base plate between a retracted position and an extended position to modulate a capacity of the centrifugal compressor without using prerotation vanes, wherein the diffuser ring includes an L-shaped cross section formed by a first flange extending toward the diffuser gap and a second flange extending crosswise to the first flange, and wherein the groove is configured to receive the gas to enable the gas to surround the second flange.
16. The method of claim 15 , comprising modulating the diffuser ring between the retracted position and the extended position to reduce transient loads on the centrifugal compressor during start up or shut down of the centrifugal compressor.
17. The method of claim 15 , comprising calibrating a controller of the centrifugal compressor to associate an actuator position of the actuator with a position of the diffuser ring, wherein calibrating the controller comprises:
storing a first position of the actuator corresponding to the first flange being in the retracted position; and
storing a second position of the actuator corresponding to the first flange being in the extended position across the diffuser gap.
18. The method of claim 17 , comprising determining the position of the diffuser ring relative to the diffuser gap based on the actuator position.
19. The method of claim 15 , comprising:
monitoring, via a sensor, an operating parameter of the centrifugal compressor to detect an occurrence of a stall or surge condition of the centrifugal compressor; and
translating, via the actuator, the diffuser ring to the extended position upon detection of the stall or surge condition, wherein, in the extended position, the first flange is configured to extend across the diffuser gap to engage with the diffuser plate.