Droplet catcher for centrifugal compressor

1. A method of improving the performance of a centrifugal compressor through liquid droplet removal, the method comprising:

positioning a liquid droplet catching device in a portion of a centrifugal impeller comprising a plurality of impeller blades effective to capture the liquid droplet at a point of impact with the centrifugal impeller, wherein the liquid droplet catching device comprises an aperture disposed on a surface of at least one of the plurality of impeller blades, and a channel disposed beneath the aperture within the at least one of the plurality of impeller blades and in fluid communication with the aperture;

capturing the liquid droplet in the aperture of the liquid droplet catching device; and removing the liquid droplet from the at least one of the plurality of impeller blades of the centrifugal compressor by directing the liquid droplet from the aperture to the channel of the liquid droplet catching device.

2. The method of claim 1 , further comprising disposing, a groove disposed on a surface of the at least one of the plurality of impeller blades upstream of the liquid droplet catching device, wherein the groove is configured to direct the liquid droplet to the aperture.

3. The method of claim 1 , wherein when the method of claim 1 is performed, a global volume fraction of a liquid phase in the centrifugal compressor is reduced.

4. A liquid droplet catching device, the device comprising:

a compressor impeller compressing a plurality of impeller blades;

a first aperture disposed on a surface of at least one of the plurality of compressor impeller blades and configured to receive the liquid droplet; and

a channel disposed within the at least one of the plurality of compressor impeller blades and beneath and in fluid communication with the first aperture, wherein in the channel is configured to direct the liquid droplet away from the first aperture and out of the at least one of the compressor impeller blades.

5. The device of claim 4 , wherein the surface of the at least one of the compressor impeller blades further comprises a plurality of grooves disposed thereon configured to direct the liquid droplet toward the first aperture.

6. The device of claim 1 , wherein the first aperture has a slot shape.

7. The device of claim 4 , further comprising a second aperture disposed downstream of the first aperture, wherein the second aperture comprises an upstream end and a downstream end, wherein the surface of the at least one of the compressor impeller blades at the upstream end bends down from and travels beneath the surface of the at least one of the compressor impeller blades at the downstream end to form the second aperture,

wherein the second aperture is configured to direct a liquid film down the bend of the at least one of the compressor impeller blades surface and through the second aperture.

8. The device of claim 4 , wherein the first aperture is disposed in a location of the at least one of the compressor impeller blades surface at a droplet impact area.

9. The device of claim 4 , wherein the first aperture is disposed at a root portion of the at least one compressor impeller blades of the compressor impeller.

10. The device of claim 4 , wherein the compressor impeller is disposed in an industrial compressor.

11. The device of claim 4 , wherein the compressor impeller is disposed in a gas turbine engine.

12. The device of claim 4 , wherein the liquid droplet catching device comprises:

a first surface; and

a second surface,

wherein the first surface faces away from the at least one of the plurality of the compressor impeller blades and the second surface faces in the opposite direction of the first surface, and

wherein the first aperture extends from the first surface of the liquid droplet catching device through the liquid droplet catching device and to the second surface of the liquid droplet catching device.

13. A centrifugal compressor, comprising:

a centrifugal impeller comprising:

a plurality of rotating integral blades, each of the plurality of rotating integral blades having a root portion and a tip portion, wherein the plurality of rotating integral blades are configured to compress air in a centrifugal gravitational field; and

at least one liquid droplet catching device disposed on at least one of the plurality of rotating integral blades, wherein the liquid droplet catching device comprises an aperture disposed on a surface of the at least one of the rotating integral blades, wherein the at least one liquid droplet catching device is configured to receive the liquid droplet, and a channel disposed beneath the aperture within the at least one rotating integral blades and in fluid communication with the aperture, wherein the channel is configured to direct the liquid droplet away from the aperture and out of the centrifugal compressor.

14. The compressor of claim 13 , wherein the liquid droplet catching device further comprises a drainage line in fluid communication with the channel.

15. The compressor of claim 13 , wherein one or more of the liquid droplet catching devices are disposed on a surface of each of the plurality of rotating integral blades.

16. The compressor of claim 15 , wherein each of the surfaces of the plurality of rotating integral blades further comprises a plurality of grooves disposed thereon configured to direct the liquid droplet toward the aperture.

17. The compressor of claim 13 ; wherein the aperture has a slot shape.

18. The compressor of claim 13 , further comprising a second aperture disposed downstream of the first aperture, wherein the second aperture comprises an upstream end and a downstream end, wherein the surface of the at least one of the rotating integral blades at the upstream end bends down from and travels beneath the surface of the at least one of the rotating integral blades at the downstream end to form the second aperture, wherein the second aperture is configured to direct a liquid film down the bend of the at least one of the rotating integral blades impeller surface and through the second aperture.

19. The compressor of claim 13 , wherein the plurality of liquid droplet catching devices are disposed at a droplet impact area.

20. The compressor of claim 19 , wherein the plurality of liquid droplet catching devices are disposed at the root portion of the plurality of rotating integral blades.

21. A gas turbine engine comprising the centrifugal compressor of claim 13 .