In-line centrifuge-separator pump

Patent metadata

Field	Value
Publication number	US-9724625-B2
Application number	US-201514686165-A
Country	US
Kind code	B2
Filing date	Apr 14, 2015
Priority date	Apr 14, 2015
Publication date	Aug 8, 2017
Grant date	Aug 8, 2017

Abstract

An in-line centrifuge-separator pump includes a shaft, a shroud, and a plurality of spaced-apart corrugated, and concentrically disposed separator structures. The shaft is adapted to receive a drive torque and is configured, upon receipt thereof, to rotate. The shroud is spaced apart from and is coupled to the shaft to be rotated thereby. The separator structures are at least partially disposed within the shroud and are coupled to both the shroud and the shaft to simultaneously rotate therewith. Each separator structure has a plurality of perforations formed therein.

First claim

What is claimed is:

1. An in-line centrifuge-separator pump, comprising:
a shaft adapted to receive a drive torque and configured, upon receipt thereof, to rotate;
a shroud spaced apart from and coupled to the shaft to be rotated thereby; and
a plurality of spaced-apart corrugated, and concentrically disposed, separator structures at least partially disposed within the shroud and coupled to both the shroud and the shaft to simultaneously rotate therewith, each separator structure having a plurality of perforations formed therein.

2. The in-line centrifuge-separator of claim 1 , wherein:
each separator structure includes a plurality of corrugation peaks and a plurality of corrugation valleys; and
the each of the perforations is disposed on only a corrugation peak or on a corrugation valley.

3. The in-line centrifuge-separator of claim 1 , wherein:
the separator structures include an innermost separator structure, an outermost separator structure, and a plurality of intermediate separator structures between the innermost and outermost separator structures; and
the separator structures successively increase in length from the innermost structure to the outermost structure.

4. The in-line centrifuge-separator of claim 1 , wherein the shroud and each of the separator structures have a truncated cone shape.

5. The in-line centrifuge-separator of claim 4 , wherein:
the shroud includes an inlet end and outlet end, the inlet end having a smaller diameter than the outlet end.

6. The in-line centrifuge-separator of claim 1 , further comprising:
a plurality of vanes extending radially from the shaft, each vane coupled to the shroud and to each of the separator structures.

7. The in-line centrifuge-separator of claim 6 , wherein the vanes extend axially beyond the outlet end of the shroud to implement a pump impeller.

8. The in-line centrifuge-separator of claim 1 , wherein:
the shaft has a first end and a second end; and
the shaft is tapered along at least a portion of the shaft between its first end and its second end.

9. An in-line centrifuge-separator pump, comprising:
a shaft adapted to receive a drive torque and configured, upon receipt thereof, to rotate;
a shroud spaced apart from and coupled to the shaft to be rotated thereby; and
a plurality of spaced-apart corrugated, and concentrically disposed, separator structures at least partially disposed within the shroud, each separator structure including a plurality of corrugation peaks and a plurality of corrugation valleys and having a plurality of perforations formed therein, each of the perforations disposed on only a corrugation peak or on a corrugation valley; and
a plurality of vanes extending radially from the shaft, each vane coupled to the shroud and to each of the separator structures.

10. The in-line centrifuge-separator of claim 9 , wherein:
the shroud and each of the separator structures have a truncated cone shape; and
the shroud includes an inlet end and outlet end, the inlet end having a smaller diameter than the outlet end.

11. The in-line centrifuge-separator of claim 9 , wherein the vanes extend axially beyond the outlet end of the shroud to implement a pump impeller.

12. The in-line centrifuge-separator of claim 9 , wherein:
the shaft has a first end and a second end; and
the shaft is tapered along at least a portion of the shaft between its first end and its second end.

13. An aircraft fuel deoxygenation system, comprising:
a boost pump adapted to receive fuel from a fuel source and inert gas from an inert gas source, the boost pump configured to mix the fuel and inert gas and supply a fuel/gas mixture;
a contactor-separator coupled to receive the fuel/gas mixture and configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel with entrained purge gas and separated purge gas; and
an in-line centrifuge-separator pump coupled to receive the deoxygenated fuel with entrained purge gas and configured to separate and remove the entrained purge gas from the deoxygenated fuel and supply the deoxygenated fuel and additional purge gas, the centrifuge-separator pump comprising:
a shaft adapted to receive a drive torque and configured, upon receipt thereof, to rotate,
a shroud spaced apart from and coupled to the shaft to be rotated thereby, and
a plurality of spaced-apart corrugated, and concentrically disposed, separator structures at least partially disposed within the shroud and coupled to both the shroud and the shaft to simultaneously rotate therewith, each separator structure having a plurality of perforations formed therein.

14. The system of claim 13 , wherein:
each separator structure includes a plurality of corrugation peaks and a plurality of corrugation valleys; and
the each of the perforations is disposed on only a corrugation peak or on a corrugation valley.

15. The system of claim 13 , wherein:
the separator structures include an innermost separator structure, an outermost separator structure, and a plurality of intermediate separator structures between the innermost and outermost separator structures; and
the separator structures successively increase in length from the innermost structure to the outermost structure.

16. The system of claim 13 , wherein the shroud and each of the separator structures have a truncated cone shape.

17. The system of claim 16 , wherein:
the shroud includes an inlet end and outlet end, the inlet end having a smaller diameter than the outlet end.

18. The system of claim 13 , further comprising:
a plurality of vanes extending radially from the shaft, each vane coupled to the shroud and to each of the separator structures.

19. The system of claim 18 , wherein the vanes extend axially beyond the outlet end of the shroud to implement a pump impeller.

20. The system of claim 13 , wherein:
the shaft has a first end and a second end; and
the shaft is tapered along at least a portion of the shaft between its first end and its second end.

Assignees

• Honeywell Int Inc

Inventors

• Lo Charles

Classifications

• B01D19/0005

  with one or more auxiliary substances · CPC title

• F04D7/02

  of centrifugal type · CPC title

• B01D19/0057 Primary

  the centrifugal movement being caused by a vortex, e.g. using a cyclone, or by a tangential inlet · CPC title

• B01D45/14

  generated by rotating vanes, discs, drums or brushes · CPC title

• B64D37/32

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title