FUEL DELIVERY SYSTEM

Abstract

A fuel delivery system includes a turbine, a pump, and an oxygen removal unit. The turbine is adapted to receive and expel fuel at different pressures. The pump is in fluid communication with, and mechanically coupled to, the turbine, and is configured to expel and receive the fuel at about the respective different pressures. The turbine is configured to convert pressure energy of the fuel to kinetic energy to drive the pump. The oxygen removal unit is in fluid communication with at least one of the turbine and the pump, and is configured to remove oxygen from the fuel.

Claims

1. A fuel delivery system comprising: a turbine adapted to receive and expel fuel at different pressures; a pump in fluid communication with and mechanically coupled to the turbine, and configured to expel and receive the fuel at about the respective different pressures, wherein the turbine is configured to convert pressure energy of the fuel to kinetic energy to drive the pump; and an oxygen removal unit in fluid communication with at least one of the turbine and the pump and configured to remove oxygen from the fuel.

2. The fuel delivery system set forth in claim 1, wherein the oxygen removal unit is located between the turbine and the pump for receiving the fuel from the turbine and expelling the fuel to the pump.

3. The fuel delivery system set forth in claim 2, wherein the turbine is adapted to receive fuel in an oxygenated condition and at a high pressure and expel the fuel in the oxygenated condition and at a low pressure to the oxygen removal unit, and the pump is adapted to receive the fuel in a deoxygenated condition and at the low pressure and expel the fuel in the deoxygenated condition and at the high pressure.

4. The fuel delivery system set forth in claim 3, further comprising: a turbine inlet conduit in fluid communication with the turbine, and adapted to flow the fuel in the oxygenated condition and at the high pressure; a turbine outlet conduit extending between and in fluid communication with the turbine and the oxygen removal unit, and adapted to flow the fuel in the oxygenated condition and at the low pressure; a pump inlet conduit extending between and in fluid communication with the oxygen removal unit and the pump, and adapted to flow the fuel in the deoxygenated condition and at the low pressure; and a pump outlet conduit in fluid communication with the pump, and adapted to flow the fuel in the deoxygenated condition and at a high pressure.

5. The fuel delivery system set forth in claim 1, wherein the oxygen removal unit is a membrane type.

6. The fuel delivery system set forth in claim 1, further comprising: a fuel filter in fluid communication between the turbine and the pump, wherein the fuel filter receives fuel at a high pressure of the different pressures from the pump and expels the fuel at about the high pressure to the turbine, and the oxygen removal unit receives the fuel at a low pressure of the different pressures from the turbine.

7. The fuel delivery system set forth in claim 6, wherein the pump receives the fuel at about the low pressure.

8. The fuel delivery system set forth in claim 1, wherein the fuel delivery system is a jet fuel delivery system.

9. A fuel delivery system comprising: a turbine configured to receive fuel at a high pressure and expel the fuel at a low pressure; a pump coupled to and in fluid communication with the turbine and configured to receive the fuel at about the low pressure and expel the fuel at about the high pressure, wherein the turbine is adapted to convert pressure energy of the fuel to kinetic energy to drive the pump; and a fuel conditioning unit disposed between and in fluid communication with the turbine and the pump, wherein the fuel conditioning unit is configured to operate more effectively at one of the high and low pressures.

10. The fuel delivery system set forth in claim 9, wherein the fuel conditioning unit is a filter unit constructed to remove particulate in the fuel.

11. The fuel delivery system set forth in claim 10, wherein the filter unit operates more effectively at the high pressure.

12. The fuel delivery system set forth in claim 11, wherein the filter unit is disposed downstream from the pump and upstream from the turbine.

13. The fuel delivery system set forth in claim 9, wherein the fuel conditioning unit is an oxygen removal unit constructed to remove oxygen from the fuel.

14. The fuel delivery system set forth in claim 13, wherein the oxygen removal unit operates more effectively at the low pressure.

15. The fuel delivery system set forth in claim 14, wherein the oxygen removal unit is disposed upstream from the pump and downstream from the turbine.

16. The fuel delivery system set forth in claim 15, wherein the fuel delivery system is an aviation fuel delivery system and the oxygen removal unit is configured to reduce coking.

17. The fuel delivery system set forth in claim 16, wherein low pressure is less than 150 psia.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Various features will become apparent to those skilled in the art from the following detailed description of the disclosed non-limiting embodiments. The drawings that accompany the detailed description can be briefly described as follows:

[0023] FIG. 1 is a schematic of a deoxygenating fuel delivery system according to one, non-limiting, exemplary embodiment of the present disclosure; and

[0024] FIG. 2 is a schematic of a second embodiment of a deoxygenating fuel delivery system.

DETAILED DESCRIPTION

[0025] Referring to FIG. 1, a fuel delivery system 20 (e.g., deoxygenating fuel delivery system) includes a turbine 22, a pump 24, and a fuel conditioning unit 26 (e.g., oxygen removal unit). In one embodiment, the turbine 22 is mechanically attached to the pump 24 via a rotating shaft 28. The oxygen removal unit 26 is adapted to remove oxygen from hydrocarbon fuel to reduce, or eliminate, undesirable oxidation reactions that may, for example, producing coking effects. The oxygen removal unit 26 may operate most effectively at relatively low fuel pressures. Non-limiting examples of the oxygen removal unit 26 include those disclosed in U.S. Pat. No. 6,315,815, issued Nov. 13, 2001, and U.S. Pat. No. 7,153,343, issued Dec. 26, 2006, both incorporated herein by reference in their entirety. One, non-limiting, application of the deoxygenating fuel delivery system 20 is that of a jet engine. One example of fuel, is jet fuel, however any other type of hydrocarbon fuel may be applicable to the present disclosure. One, non-limiting, example of an oxygen removal unit 26 may be of a membrane type with limited capability of operating under high fuel pressure conditions (e.g., greater than 150 psia).

[0026] The deoxygenating fuel delivery system 20 may further include a turbine inlet conduit 30, a turbine outlet conduit 32, a pump inlet conduit 34, and a pump outlet conduit 36. The oxygen removal unit 26 is disposed between and is in fluid communication with the turbine outlet conduit 32 and the pump inlet conduit 34. In one embodiment, the turbine inlet conduit 30 and the pump outlet conduit 36 flow the fuel at a high pressure, and the turbine outlet conduit 32 and the pump inlet conduit 34 may flow the fuel at a relatively low fuel pressure. Moreover, the fuel in the turbine inlet and outlet conduits 30, 32 may be in an oxygenated condition, and the fuel in the pump inlet and outlet conduits 34, 36 may be in a deoxygenated condition. The term low pressure means any pressure or pressure range suitable for effective and efficient operation of the oxygen removal unit 26, and the term high pressure means any pressure that is higher than the low pressure and is generally not ideal for proper and efficient operation of the oxygen removal unit 26. As one example, low pressure is less than 150 psia, and high pressure is greater than 150 psia.

[0027] During operation, high pressure fuel, in an oxygenated condition, enters the turbine 22 via the turbine inlet conduit 30. The turbine 22 is constructed to convert pressure energy of the incoming fuel to kinetic energy, thus enabling rotation of the shaft 28 and operation of the pump 24. Conversion of the pressure energy, causes the high pressure fuel entering the turbine 22 to exit via the turbine outlet conduit 32 at the low pressure. The low pressure fuel then enters the oxygen removal unit 26 that alters the fuel from the oxygenated condition to the deoxygenated condition. The fuel at the low pressure and in the deoxygenated condition then enters the pump 24. The pump 24 works the fuel, and the fuel exits the pump 24 via the pump outlet conduit 36 at the high pressure and in the deoxygenated condition for combustion within an engine (not shown). In one embodiment, the oxygenated condition represents oxygen in fuel at about 70 ppm and the deoxygenated condition at about 10 ppm.

[0028] Referring to FIG. 2, a second embodiment of a fuel delivery system is illustrated where like elements to the first embodiment have like identifying numerals except with the addition of a prime symbol suffix. A deoxygenating fuel delivery system 20 includes a turbine 22, a pump 24, a fuel conditioning unit 26 (e.g., particulate filter unit), a rotating shaft 28, and an oxygen removal unit 40. The fuel delivery system 20 may further include a turbine inlet conduit 30, a turbine outlet conduit 32, a pump inlet conduit 34, a pump outlet conduit 36 and an oxygen removal unit outlet conduit 42.

[0029] In this embodiment, the fuel conditioning unit 26 may a filter unit adapted to filtrate particulates from the fuel. The filter unit 26 is disposed between and is in fluid communication with the pump outlet conduit 36 and the turbine inlet conduit 30. Like the first embodiment, the turbine inlet conduit 30 and the pump outlet conduit 36 flow the fuel at a high pressure, and the turbine outlet conduit 32 and the pump inlet conduit 34 may flow the fuel at a relatively low fuel pressure.

[0030] Further to this second embodiment, the fuel in the conduits 30, 32, 34, 36, the pump 24, the filter unit 26, and the turbine 22 is in an oxygenated condition, and the fuel in the oxygen removal unit outlet conduit 42 is in a deoxygenated condition. The term high pressure means any pressure or pressure range suitable for effective and efficient operation of the filter unit 26, and the term low pressure means any pressure that is lower than the high pressure and is generally not ideal for proper and efficient operation of the filter unit 26, but may be optimal for efficient operation of the oxygen removal unit 40.

[0031] Advantages and benefits of the present disclosure include placement of oxygen removal units in high pressure fuel systems where previously not available. Another advantage is the ability to place oxygen removal units in high pressure lines while minimizing the amount of energy loss, and increasing fuel performance as a heatsink. Yet further, the present disclosure provides a more robust and efficiently operating system with an increase in design options.

[0032] While the present disclosure is described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the scope of the present disclosure. In addition, various modifications may be applied to adapt the teachings of the present disclosure to particular situations, applications, and/or materials, without departing from the essential scope thereof. The present disclosure is thus not limited to the particular examples disclosed herein, but includes all embodiments falling within the scope of the appended claims.