Fuel oxygen conversion unit

Patent metadata

Field	Value
Publication number	US-11085636-B2
Application number	US-201816179022-A
Country	US
Kind code	B2
Filing date	Nov 2, 2018
Priority date	Nov 2, 2018
Publication date	Aug 10, 2021
Grant date	Aug 10, 2021

Abstract

A fuel oxygen conversion unit includes a stripping gas flowpath for a vehicle or an engine of the vehicle. The fuel oxygen conversion unit includes a stripping gas boost pump positioned in airflow communication with the stripping gas flowpath for increasing a pressure of a flow of stripping gas through the stripping gas flowpath; a contactor defining a stripping gas inlet in airflow communication with the stripping gas flowpath, a liquid fuel inlet, and a fuel/gas mixture outlet; a fuel gas separator defining a fuel/gas mixture inlet in fluid communication with the fuel/gas mixture outlet of the contactor, a stripping gas outlet, and a liquid fuel outlet; and a connection assembly mechanically coupling the stripping gas boost pump to the fuel gas separator, the connection assembly having a speed change mechanism such that the stripping gas boost pump rotates at a different rotational speed than the fuel gas separator.

First claim

What is claimed is:

1. A fuel oxygen conversion unit defining a stripping gas flowpath for a vehicle, or an engine of the vehicle, the fuel oxygen conversion unit comprising:
a stripping gas boost pump positioned in airflow communication with the stripping gas flowpath for increasing a pressure of a flow of stripping gas through the stripping gas flowpath;
a contactor defining a stripping gas inlet in airflow communication with the stripping gas flowpath, a liquid fuel inlet, and a fuel/gas mixture outlet;
a fuel gas separator defining a fuel/gas mixture inlet in fluid communication with the fuel/gas mixture outlet of the contactor, a stripping gas outlet, and a liquid fuel outlet; and
a connection assembly mechanically coupling the stripping gas boost pump to the fuel gas separator, the connection assembly having a speed change mechanism configured such that the stripping gas boost pump rotates at different faster rotational speed than the fuel gas separator.

2. The fuel oxygen conversion unit of claim 1 , wherein the speed change mechanism is a gearbox.

3. The fuel oxygen conversion unit of claim 2 , wherein the gearbox defines a gear ratio, wherein the gear ratio is greater than 1:1.

4. The fuel oxygen conversion unit of claim 1 , wherein the speed change mechanism is a continuously variable transmission.

5. The fuel oxygen conversion unit of claim 1 , wherein the speed change mechanism is a torque converter.

6. The fuel oxygen conversion unit of claim 1 , wherein the engine comprises an accessory gearbox, and wherein the fuel gas separator and stripping gas boost pump are each driven by the accessory gearbox.

7. The fuel oxygen conversion unit of claim 6 , wherein the accessory gearbox includes a first pad, and wherein the fuel gas separator and the stripping gas boost pump are each driven by the first pad of the accessory gearbox.

8. The fuel oxygen conversion unit of claim 1 , further comprising:
a catalyst in airflow communication with the stripping gas flowpath for removing an amount of oxygen from the flow of stripping gas through the stripping gas flowpath.

9. A gas turbine engine comprising:
a combustion section; and
a fuel delivery system for providing a flow of fuel to the combustion section, the fuel delivery system comprising a fuel oxygen conversion unit defining a stripping gas flowpath, the fuel oxygen conversion unit comprising
a stripping gas boost pump positioned in airflow communication with the stripping gas flowpath for increasing a pressure of a flow of stripping gas through the stripping gas flowpath;
a contactor defining a stripping gas inlet in airflow communication with the stripping gas flowpath, a liquid fuel inlet, and a fuel/gas mixture outlet;
a fuel gas separator defining a fuel/gas mixture inlet in fluid communication with the fuel/gas mixture outlet of the contactor, a stripping gas outlet, and a liquid fuel outlet; and
a connection assembly mechanically coupling the stripping gas boost pump to the fuel gas separator, the connection assembly having a speed change mechanism configured such that the stripping gas boost pump rotates at a faster rotational speed than the fuel gas separator.

10. A gas turbine engine comprising:
an accessory gearbox; and
a fuel oxygen conversion unit defining a stripping gas flowpath and comprising
a stripping gas boost pump positioned in airflow communication with the stripping gas flowpath for increasing a pressure of a flow of stripping gas through the stripping gas flowpath;
a contactor defining a stripping gas inlet in airflow communication with the stripping gas flowpath, a liquid fuel inlet, and a fuel/gas mixture outlet; and
a fuel gas separator defining a fuel/gas mixture inlet in fluid communication with the fuel/gas mixture outlet of the contactor, a stripping gas outlet, and a liquid fuel outlet, the fuel gas separator and the stripping gas boost pump each mechanically coupled to and driven by the accessory gearbox;
wherein the fuel oxygen conversion unit further comprises a connection assembly mechanically coupling the stripping gas boost pump to the fuel gas separator, and wherein the connection assembly includes a speed change mechanism configured such that the stripping gas boost pump rotates at a faster rotational speed than the fuel gas separator.

11. The gas turbine engine of claim 10 , wherein the accessory gearbox includes a first pad and a second pad, wherein the fuel gas separator is driven by the first pad, and wherein the stripping gas boost pump is driven by the second pad.

12. The gas turbine engine of claim 10 , wherein the accessory gearbox includes a first pad, and wherein the fuel gas separator and the stripping gas boost pump are each driven by the first pad of the accessory gearbox.

13. The gas turbine engine of claim 10 , wherein the speed change mechanism is a gearbox.

14. The gas turbine engine of claim 13 , wherein the gearbox defines a gear ratio, wherein the gear ratio is greater than 1:1.

15. The gas turbine engine of claim 10 , wherein the speed change mechanism is a continuously variable transmission.

16. The gas turbine engine of claim 10 , wherein the speed change mechanism is a torque converter.

Assignees

• Gen Electric

Inventors

• O'Connor Ethan Patrick
• Niergarth Daniel Alan
• Miller Brandon Wayne
• Wesling Richard Alan
• Andrews Jr Peter Allen

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• B64D37/34

  Conditioning fuel, e.g. heating (during filling B64D37/18) · CPC title

• F23K5/04

  Feeding or distributing systems using pumps (from a central source to a plurality of burners F23K5/06) · CPC title

• F05D2260/213

  by the provision of a heat exchanger within the cooling circuit · CPC title

• F23K5/10

  Mixing with other fluids · CPC title