In-line continuous flow liquid-gas separator-pump

Patent metadata

Field	Value
Publication number	US-9897100-B2
Application number	US-201514688484-A
Country	US
Kind code	B2
Filing date	Apr 16, 2015
Priority date	Apr 16, 2015
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

An in-line continuous flow liquid-gas separator-pump includes a housing, a rotor, a plurality of tubular flow passages, and a plurality of gas flow passages. The rotor includes a rotor first end, a rotor second end, an outer surface, and an inner surface that defines an inner chamber in fluid communication with the purge gas outlet. The tubular flow passages are formed in the rotor and extend between the rotor first end and the rotor second end. Each tubular flow passage includes a fluid inlet that is disposed adjacent the rotor first end and in fluid communication with the liquid/gas inlet, and a fluid outlet that is disposed adjacent the rotor second end and is in fluid communication with the liquid outlet. The gas flow passages are formed in the rotor, and each provides fluid communication between one of the tubular flow passages and the inner chamber.

First claim

What is claimed is:

1. An in-line continuous flow liquid-gas separator-pump, comprising:
a housing having a liquid/gas inlet, a liquid outlet, and a purge gas outlet;
a rotor adapted to receive a drive torque and configured, upon receipt thereof, to rotate, the rotor including a rotor first end, a rotor second end, an inner surface, and an outer surface, the inner surface defining an inner chamber in fluid communication with the purge gas outlet;
a plurality of tubular flow passages formed on the rotor, each tubular flow passage extending between the rotor first end and the rotor second end, each tubular flow passage including a fluid inlet and a fluid outlet, the fluid inlet of each tubular flow passage disposed adjacent the rotor first end and in fluid communication with the liquid/gas inlet, the fluid outlet of each tubular flow passage disposed adjacent the rotor second end and in fluid communication with the liquid outlet; and
a plurality of gas flow passages formed in the rotor, each gas flow passage providing fluid communication between only one of the tubular flow passages and the inner chamber, wherein: the rotor has a truncated cone shape; the rotor first end has a smaller diameter than the rotor second end; and the plurality of tubular flow passages extend in a splayed manner between the rotor first end and the rotor second end;
wherein:
the fluid inlet of each tubular flow passage has a fluid inlet diameter;
the fluid outlet of each tubular flow passage has a fluid outlet diameter; and
the fluid outlet diameter is less than the fluid inlet diameter.

2. The in-line continuous flow liquid-gas separator-pump of claim 1 , further comprising:
a drive shaft coupled to the rotor and configured to supply the drive torque thereto, the drive shaft having a purge gas flow passage formed therein, the purge gas flow passage in fluid communication with the inner chamber.

3. The in-line continuous flow liquid-gas separator-pump of claim 1 , wherein the rotor second end is configured as a centrifugal pump impeller extending radially outwardly from the rotor second end.

4. The in-line continuous flow liquid-gas separator-pump of claim 1 , further comprising a plurality of radial vanes extending radially inwardly from the inner surface into the inner chamber.

5. The in-line continuous flow liquid-gas separator-pump of claim 1 , further comprising:
a plurality of liquid flow passages formed in the rotor, each liquid flow passage fluidly communicating the inner chamber downstream of each fluid outlet.

6. The in-line continuous flow liquid-gas separator-pump of claim 5 , further comprising:
a separation gate coupled to the rotor and extending radially into the inner chamber, the gate separating the inner chamber into a first inner chamber and a second inner chamber.

7. The in-line continuous flow liquid-gas separator-pump of claim 1 , further comprising:
a plurality of upstream liquid flow passages formed in the rotor, each upstream liquid flow passage fluidly communicating the inner chamber with one of the tubular flow passages upstream of the fluid outlet; and
a plurality of downstream liquid flow passages formed in the rotor, each downstream liquid flow passage fluidly communicating the inner chamber downstream of each fluid outlet.

8. The in-line continuous flow liquid-gas separator-pump of claim 7 , further comprising:
a separation gate coupled to the rotor and extending radially into the inner chamber, the gate separating the inner chamber into a first inner chamber and a second inner chamber,
wherein:
each upstream liquid flow passage fluidly communicates the first inner chamber with one of the tubular flow passages upstream of the fluid outlet, and
each downstream liquid flow passage fluidly communicates the second inner chamber downstream of each fluid outlet.

9. The in-line continuous flow liquid-gas separator-pump of claim 1 , further comprising:
a pre-swirler disposed within the housing upstream of the rotor first end and configured to rotate fluid entering the liquid/gas inlet.

10. The in-line continuous flow liquid-gas separator-pump of claim 1 , further comprising:
an orifice disposed within the housing upstream of the rotor first end and configured to reduce fluid pressure.

11. A rotor structure, comprising:
a rotor having a truncated cone shape and including a rotor first end, a rotor second end, an inner surface, and an outer surface, the rotor first end having a first diameter, the rotor second end having a second diameter that is smaller than the first diameter, the inner surface defining an inner chamber;
a plurality of tubular flow passages formed on the rotor, in a splayed manner, between the rotor first end and the rotor second end, each tubular flow passage including a fluid inlet and a fluid outlet, the fluid inlet disposed adjacent the rotor first end and in fluid communication with the liquid/gas inlet, the fluid outlet disposed adjacent the rotor second end; the plurality of tubular flow passages extend in a splayed manner between the rotor first end and the rotor second end and
a plurality of gas flow passages formed in the rotor, each gas flow passage providing fluid communication between only one of the tubular flow passages and the inner chamber; wherein: the fluid inlet of each tubular flow passage has a fluid inlet diameter; the fluid outlet of each tubular flow passage has a fluid outlet diameter; and the fluid outlet diameter is less than the fluid inlet diameter.

12. The rotor structure of claim 11 , further comprising:
a drive shaft coupled to the rotor and configured to supply the drive torque thereto, the drive shaft having a purge gas flow passage formed therein, the purge gas flow passage in fluid communication with the inner chamber.

13. The rotor structure of claim 11 , wherein the rotor second end is configured as a centrifugal pump impeller extending radially outwardly from the rotor second end.

14. The rotor structure of claim 11 , further comprising a plurality of radial vanes extending radially inwardly from the inner surface into the inner chamber.

15. The rotor structure of claim 11 , further comprising:
a plurality of liquid flow passages formed in the rotor, each liquid flow passage fluidly communicating the inner chamber downstream of each fluid outlet; and
a separation gate coupled to the rotor and extending radially into the inner chamber, the gate separating the inner chamber into a first inner chamber and a second inner chamber.

16. The rotor structure of claim 11 , further comprising:
a separation gate coupled to the rotor and extending radially into the inner chamber, the gate separating the inner chamber into a first inner chamber and a second inner chamber;
a plurality of upstream liquid flow passages formed in the rotor, each upstream liquid flow passage fluidly communicating the first chamber with one of the tubular flow passages upstream of the fluid outlet; and
a plurality of downstream liquid flow passages formed in the rotor, each downstream liquid flow passage fluidly communicating the second inner chamber downstream of each fluid outlet.

17. 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;

Assignees

• Honeywell Int Inc

Inventors

• Laboda Daniel J
• Rateick Richard
• Gedeon Christopher
• Valencourt Gary A

Classifications

• B01D19/0073

  by a method not covered by groups B01D19/0005 - B01D19/0042 · CPC title

• B01D19/0094

  by using a vortex, cavitation · CPC title

• B04B5/12

  Centrifuges in which rotors other than bowls generate centrifugal effects in stationary containers · CPC title

• F04D31/00

  Pumping liquids and elastic fluids at the same time · CPC title

• F04D29/2288 Primary

  for comminuting, mixing or separating · CPC title