Self-aspirated flow control system for centrifugal compressors
A flow control system for a centrifugal compressor includes a plurality of suction holes provided in a diffuser and configured to facilitate suction of a flow control stream from a boundary layer fluid from the diffuser. A plurality of blowing holes are provided in a first interconnecting duct coupled to a de-swirl vane unit and configured to facilitate blowing of the flow control stream into the first interconnecting duct. The blowing holes may also be provided in a suction side or an end wall side of the de-swirl vane unit or in a second interconnecting duct coupled between the de-swirl vane unit and an impeller or an upstream diffuser of another compression stage. A manifold is coupled between the suction holes and the blowing holes and configured to direct flow of the flow control stream from the suction holes to the blowing holes.
1. A flow control system for a centrifugal compressor, comprising:
a plurality of suction holes provided in a diffuser and configured to facilitate suction of a flow control stream from a boundary layer fluid of the diffuser;
a plurality of blowing holes provided in an interconnecting duct coupled to a de-swirl vane unit and configured to facilitate blowing of the flow control stream into a boundary layer fluid of the interconnecting duct;
a manifold coupled between the suction holes and the blowing holes and configured to direct flow of the flow control stream from the suction holes to the blowing holes; and
a fluidic oscillator provided juxtaposed to the blowing holes and configured to facilitate pulsed blowing of the flow control stream into the boundary layer fluid in the interconnecting duct via the blowing holes.
2. The flow control system of claim 1 , wherein the plurality of suction holes are juxtaposed to a location of incipient boundary layer fluid separation in the diffuser.
3. The flow control system of claim 1 , further comprising a flow-metering device provided in the manifold and configured to monitor the flow of the flow control stream.
4. The flow control system of claim 3 , wherein the flow-metering device comprises at least one orifice.
5. The flow control system of claim 3 , wherein the flow-metering device comprises a plenum.
6. The flow control system of claim 1 , wherein the plurality of blowing holes are juxtaposed to a location of incipient boundary layer fluid separation in the interconnecting duct.
7. A flow control system for a centrifugal compressor, comprising:
a plurality of suction holes provided in a diffuser and configured to facilitate suction of a flow control stream from a boundary layer fluid of the diffuser;
a plurality of blowing holes provided in an interconnecting duct coupled between a de-swirl vane unit and an impeller; wherein the blowing holes are configured to facilitate blowing of the flow control stream into a boundary layer fluid in the interconnecting duct; and
a manifold coupled between the suction holes and the blowing holes and configured to direct flow of the flow control stream from the suction holes to the blowing holes.
8. The flow control system of claim 7 , wherein the plurality of suction holes are juxtaposed to a location of incipient boundary layer fluid separation in the diffuser.
9. The flow control system of claim 7 , wherein the plurality of blowing holes are juxtaposed to a location of incipient boundary layer fluid separation in the interconnecting duct.
10. The flow control system of claim 7 , further comprising a fluidic oscillator provided juxtaposed to the blowing holes and configured to facilitate pulsed blowing of the flow control stream into the boundary layer fluid in the interconnecting duct via the blowing holes.
11. A flow control system for a centrifugal compressor, comprising:
a plurality of suction holes provided in a diffuser and configured to facilitate suction of a flow control stream from a boundary layer fluid of the diffuser;
a plurality of blowing holes provided in a de-swirl vane unit and configured to facilitate blowing of the flow control stream into a boundary layer fluid in the de-swirl vane unit; and
a manifold coupled between the suction holes and the blowing holes and configured to direct flow of the flow control stream from the suction holes to the blowing holes.
12. The flow control system of claim 11 , wherein the plurality of suction holes are juxtaposed to a location of incipient boundary layer fluid separation in the diffuser.
13. The flow control system of claim 11 , wherein the plurality of blowing holes are juxtaposed to a location of incipient boundary layer fluid separation in a suction side of the de-swirl vane unit.
14. The flow control system of claim 11 , wherein the plurality of blowing holes are juxtaposed to a location of incipient boundary layer fluid separation in an end wall side of the de-swirl vane unit.
15. The flow control system of claim 11 , further comprising a fluidic oscillator provided juxtaposed to the blowing holes and configured to facilitate pulsed blowing of the flow control stream into the boundary layer fluid in the de-swirl vane unit via the blowing holes.
16. A flow control system for a centrifugal compressor, comprising:
a plurality of suction holes provided in a downstream diffuser and configured to facilitate suction of a flow control stream from a boundary layer fluid of the downstream diffuser;
a plurality of blowing holes provided in an upstream diffuser coupled to a de-swirl vane unit and configured to facilitate blowing of the flow control stream into a boundary layer fluid in the upstream diffuser; and
a manifold coupled between the suction holes and the blowing holes and configured to direct flow of the flow control stream from the suction holes to the blowing holes.
17. The flow control system of claim 16 , wherein the plurality of suction holes are juxtaposed to a location of incipient boundary layer fluid separation in the downstream diffuser.
18. The flow control system of claim 16 , wherein the plurality of blowing holes are juxtaposed to a location of incipient boundary layer fluid separation in the upstream diffuser.
19. A method for controlling fluid flow in a centrifugal compressor, comprising:
intaking a flow control stream from a boundary layer fluid via a plurality of suction holes provided in a diffuser;
directing flow of the flow control stream from the suction holes to a plurality of blowing holes provided in an interconnecting duct coupled to a de-swirl vane unit; and
blowing the flow control stream into a fluid boundary layer in the interconnecting duct coupled to a de-swirl vane unit, via the plurality of blowing holes.
20. The method of claim 19 , wherein intaking a flow control stream comprises intaking fluid via the plurality of suction holes juxtaposed to a location of incipient boundary layer fluid separation in the diffuser.
21. The method of claim 19 , wherein directing flow of the flow control stream from the suction holes to the plurality of blowing holes comprises directing flow of the flow control stream from the suction holes to the plurality of blowing holes via a manifold.
22. The method of claim 21 , further comprising monitoring the flow of the flow control stream via a flow-metering device provided in the manifold.
23. The method of claim 19 , wherein blowing the flow control stream into the first interconnecting duct comprises blowing the flow control stream into the first interconnecting duct via the plurality of blowing holes juxtaposed to a location of incipient boundary layer fluid separation in the interconnecting duct.
24. The method of claim 19 , wherein blowing the flow control stream into the interconnecting duct comprises facilitating pulsed blowing via a fluidic oscillator provided juxtaposed to the blowing holes.
25. A method for controlling fluid flow in a centrifugal compressor, comprising:
intaking a flow control stream from a fluid boundary layer via a plurality of suction holes provided in a diffuser;
directing flow of the flow control stream from the suction holes to a plurality of blowing holes provided in an interconnecting duct coupled between a de-swirl vane unit and an impeller; and
blowing the flow control stream into the interconnecting duct, via the plurality of blowing holes.
26. The method of claim 25 , wherein intaking a flow control stream comprises intaking fluid via the plurality of suction holes juxtaposed to a location of incipient boundary layer fluid separation in the diffuser.
27. The method of claim 25 , wherein blowing the flow control stream into the interconnecting duct comprises blowing the flow control stream into the interconnecting duct via the plurality of blowing holes juxtaposed in a location of incipient boundary layer fluid separation in the interconnecting duct.
28. A method for controlling fluid flow in a centrifugal compressor, comprising:
intaking a flow control stream from a fluid boundary layer via a plurality of suction holes provided in a diffuser;
directing flow of the flow control stream from the suction holes to a plurality of blowing holes provided in a de-swirl vane unit; and
blowing the flow control stream into the de-swirl vane unit, via the plurality of blowing holes.
29. The method of claim 28 , wherein intaking a flow control stream comprises intaking fluid via a plurality of suction holes juxtaposed to a location of incipient boundary layer fluid separation in the diffuser.
30. The method of claim 28 , wherein blowing the flow control stream into the de-swirl vane unit comprises blowing the fluid boundary layer into the de-swirl vane unit via the plurality of blowing holes juxtaposed in a location of incipient fluid boundary layer separation in the suction side of the de-swirl vane unit.
31. The method of claim 28 , wherein blowing the flow control stream into the de-swirl vane unit comprises blowing the fluid boundary layer into the de-swirl vane unit via the plurality of blowing holes juxtaposed in a location of incipient boundary layer fluid separation in an end wall side of the de-swirl vane unit.