Aircraft fuel deoxygenation system

Patent metadata

Field	Value
Publication number	US-2016167802-A1
Application number	US-201414570152-A
Country	US
Kind code	A1
Filing date	Dec 15, 2014
Priority date	Dec 15, 2014
Publication date	Jun 16, 2016
Grant date	—

Abstract

An aircraft fuel deoxygenation system includes a boost pump, a contactor-separator, and a centrifuge-separator pump. The boost pump is adapted to receive fuel from a fuel source and inert gas from an inert gas source, and is configured to mix the fuel and inert gas and supply a fuel/gas mixture. The contactor-separator is coupled to receive the fuel/gas mixture and is configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel with entrained purge gas and separated purge gas. The centrifuge-separator pump is coupled to receive the deoxygenated fuel with entrained purge gas and is configured to separate and remove the entrained purge gas from the deoxygenated fuel and supply the deoxygenated fuel and additional purge gas.

First claim

What is claimed is:

1 . 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 a 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.

2 . The system of claim 1 , further comprising:
a gas pump coupled to receive the separated purge gas from the contractor-separator and the additional purge gas from the centrifuge-separator pump and configured to supply pressurized purge gas to the inert gas source.

3 . The system of claim 2 , wherein the gas pump comprises a liquid ring vacuum pump.

4 . The system of claim 2 , further comprising:
a coalescing filter coupled to receive the pressurized purge gas from the gas pump and configured to remove fuel aerosol that may be present in the pressurized purge gas.

5 . The system of claim 1 , further comprising:
a heat exchanger coupled between the boost pump and the passive contactor-separator, the heat exchanger coupled to receive the fuel/gas mixture from the pump and a fluid from a fluid source and configured to transfer heat from the fluid to the fuel/gas mixture to thereby increase fuel/gas mixture temperature prior to supplying the fuel/gas mixture to the passive contactor-separator.

6 . The system of claim 5 , further comprising:
a fuel filter coupled between the heat exchanger and the passive contactor-separator, the fuel filter configured to (i) remove particulate from the fuel/gas mixture and (ii) break up inert gas bubbles in the fuel/gas mixture into relatively smaller sized bubbles.

7 . The system of claim 1 , further comprising an inert gas source configured to supply the inert gas to the pump.

8 . The system of claim 1 , wherein the contactor-separator is configured as a passive contactor-separator.

9 . 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 passive 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; a 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; and a gas pump coupled to receive the separated purge gas from the contactor-separator and the additional purge gas from the centrifuge-separator pump and configured to supply pressurized purge gas to the inert gas source.

10 . The system of claim 9 , wherein the gas pump comprises a liquid ring vacuum pump.

11 . The system of claim 9 , further comprising:
a coalescing filter coupled to receive the pressurized purge gas from the gas pump and configured to remove fuel aerosol that may be present in the pressurized purge gas.

12 . The system of claim 9 , further comprising:
a heat exchanger coupled to receive the fuel/gas mixture from the pump and a fluid from a fluid source and configured to transfer heat from the fluid to the fuel/gas mixture to thereby increase fuel/gas mixture temperature prior to supplying the fuel/gas mixture; and a fuel filter coupled between the heat exchanger and the passive contactor-separator, the fuel filter configured to (i) remove particulate from the fuel/gas mixture and (ii) break up inert gas bubbles in the fuel/gas mixture into relatively smaller sized bubbles.

13 . The system of claim 9 , further comprising:
an inert gas source configured to supply the inert gas to the pump.

14 . An aircraft fuel deoxygenation system, comprising:
an inert gas source for supplying inert gas; a boost pump adapted to receive fuel from a fuel source and inert gas from the 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; a 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; and a liquid ring vacuum pump coupled to receive the separated purge gas from the contactor-separator and the additional purge gas from the centrifuge-separator pump and configured to supply pressurized purge gas to the inert gas source.

15 . The system of claim 14 , further comprising:
a coalescing filter coupled between the liquid ring vacuum pump and the inert gas source and configured to remove fuel aerosol that may be present in the pressurized purge gas.

16 . The system of claim 14 , further comprising:
a heat exchanger coupled to receive the fuel/gas mixture from the pump and a fluid from a fluid source and configured to transfer heat from the fluid to the fuel/gas mixture to thereby increase fuel/gas mixture temperature prior to supplying the fuel/gas mixture.

17 . The system of claim 16 , further comprising:
a fuel filter coupled between the heat exchanger and the passive contactor-separator, the fuel filter configured to (i) remove particulate from the fuel/gas mixture and (ii) break up inert gas bubbles in the fuel/gas mixture into relatively smaller sized bubbles.

18 . The system of claim 14 , wherein the contactor-separator is configured as a passive contactor-separator.

Assignees

• Honeywell Int Inc

Inventors

• Lo Charles
• Blumer Eric
• Laboda Dan
• Bershitsky Alexander

Classifications

• B01D19/0047

  Atomizing, spraying, trickling · CPC title

• B01D46/00

  Filters or filtering processes specially modified for separating dispersed particles from gases or vapours (filtering elements B01D24/00-B01D35/00; filtering material B01D39/00; their regeneration outside the filters B01D41/00) · CPC title

• B01D35/02

  Filters adapted for location in special places, e.g. pipe-lines, pumps, stop-cocks, (B01D35/05 takes precedence; {water pipe system filters E03B3/18, E03B7/07; dirt catchers in sewers E03F; filters or strainers for pipe-lines in general B08B, E03F; object or dirt catching devices in sinks or the like E03C1/26; suction strainers or filters for pumps F04B53/005, F04D29/70}) · CPC title

• B01D19/0068

  General arrangements, e.g. flowsheets (B01D19/0063 takes precedence) · CPC title

• B01D19/0057

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