Method for low power non-coking liquid hydrocarbon fuel vaporization and supercritical phase change

Patent metadata

Field	Value
Publication number	US-10119703-B2
Application number	US-201313803206-A
Country	US
Kind code	B2
Filing date	Mar 14, 2013
Priority date	Mar 14, 2013
Publication date	Nov 6, 2018
Grant date	Nov 6, 2018

Abstract

Methods for vaporizing hydrocarbon fuel and delivering the hydrocarbon fuel in either a vaporized phase or a supercritical phase to, for example, a combustion chamber are provided herein. A method of vaporizing a hydrocarbon fuel, wherein the hydrocarbon fuel is in a liquid phase at a first temperature and a first pressure, and wherein the first temperature of the liquid phase hydrocarbon fuel is less than its intrinsic oxidation or endothermic reaction temperature, the method may include lowering a pressure of the liquid phase hydrocarbon fuel from the first pressure to a second pressure; and heating the liquid phase hydrocarbon fuel from the first temperature to a second temperature, wherein the hydrocarbon fuel at the second temperature and the second pressure is in a substantially completely vaporized phase substantially without thermally oxidizing the hydrocarbon fuel, and wherein the hydrocarbon fuel in the substantially completely vaporized phase does not form carbonaceous contaminants.

First claim

The invention claimed is:

1. A method of vaporizing a hydrocarbon fuel comprising:
lowering a pressure of the liquid phase hydrocarbon fuel from a first pressure to a second pressure; and
heating the liquid phase hydrocarbon fuel from a first temperature to a second temperature,
wherein the hydrocarbon fuel is in a liquid phase at the first temperature and the first pressure, and wherein the first temperature of the liquid phase hydrocarbon fuel is less than its intrinsic oxidation or endothermic reaction temperature;
wherein the hydrocarbon fuel at the second temperature and the second pressure is in a substantially completely vaporized phase substantially without thermally oxidizing the hydrocarbon fuel, and wherein, in going to the substantially completely vaporized phase, no carbonaceous contaminants are formed in the hydrocarbon fuel; and
wherein thermal oxidation of the hydrocarbon fuel avoided is not combustion.

2. The method of claim 1 , further comprising:
heating the hydrocarbon fuel in the substantially completely vaporized phase from the second temperature to a third temperature while raising the pressure of the hydrocarbon fuel in the substantially completely vaporized phase from the second pressure to a third pressure, wherein the third temperature maintains the hydrocarbon fuel in the substantially completely vaporized phase at the third pressure.

3. The method of claim 1 , further comprising:
heating the hydrocarbon fuel in the substantially completely vaporized phase from the second temperature to a third temperature while raising the pressure of the hydrocarbon fuel in the substantially completely vaporized phase from the second pressure to a third pressure, wherein the hydrocarbon fuel is in a substantially completely supercritical phase at the third temperature and third pressure.

4. The method of claim 1 , wherein the liquid phase hydrocarbon fuel at the second temperature and second pressure is in a substantially completely vaporized phase within a first duration of time substantially without thermally oxidizing the hydrocarbon fuel in order to avoid formation of carbonaceous contaminants.

5. The method of claim 1 , wherein the hydrocarbon fuel is a heavy hydrocarbon fuel.

6. The method of claim 5 , wherein the heavy hydrocarbon fuel is a JP-8fuel.

7. The method of claim 6 , wherein the first temperature is an ambient temperature and the first pressure is an ambient pressure.

8. The method of claim 7 , wherein the hydrocarbon fuel is in a substantially completely vaporized phase at the second temperature of about 120° Celsius (248° Fahrenheit) and the second pressure of about 0.07 bar.

9. The method of claim 8 , wherein the hydrocarbon fuel remains in a substantially completely vaporized phase at a third temperature of about 204° Celsius (400° Fahrenheit) and a third pressure at about the ambient pressure.

10. The method of claim 6 , wherein the first pressure is about 1 bar and the second pressure is between about 0.07 bar and about 1 bar.

11. The method of claim 10 , further comprising heating the JP-8 fuel to a second temperature at the second pressure for a first duration of time, wherein the first duration does not provide sufficient time for the JP-8 fuel to substantially thermally oxidize and form carbonaceous contaminants.

12. The method of claim 11 , wherein the first duration is less than about one second.

13. The method of claim 1 , wherein one of the following sequences of steps occurs:
(a) lowering the pressure of the liquid phase hydrocarbon from the first pressure to the second pressure precedes heating the liquid phase hydrocarbon from the first temperature to the second temperature;
(b) heating the liquid phase hydrocarbon from the first temperature to the second temperature precedes lowering the pressure of the liquid phase hydrocarbon from the first pressure to the second pressure; or
(c) heating the liquid phase hydrocarbon from the first temperature to the second temperature occurs simultaneously with lowering the pressure of the liquid phase hydrocarbon from the first pressure to the second pressure.

14. The method of claim 1 , wherein heating the liquid phase hydrocarbon fuel from the first temperature to the second temperature does not result in combustion of the hydrocarbon fuel.

15. The method of claim 1 , wherein lowering the pressure of the liquid phase hydrocarbon fuel from the first pressure to the second pressure comprises passing the liquid phase hydrocarbon fuel through a pressure reducing device.

16. The method of claim 1 , wherein the hydrocarbon fuel passes from a first thermodynamic point on a pressure vs. enthalpy chart, at the first temperature and the first pressure, to a second thermodynamic point on the pressure vs. enthalpy chart, at the second temperature and the second pressure, without traversing a coking region on the pressure vs. enthalpy chart.

17. The method of claim 16 , wherein the hydrocarbon fuel passes from the second thermodynamic point on the pressure vs. enthalpy chart, at the second temperature and the second pressure, to a third thermodynamic point on the pressure vs. enthalpy chart, at a third temperature and a third pressure, traversing through the coking region quickly enough so that the hydrocarbon fuel does not substantially thermally oxidize and form carbonaceous contaminants.

18. A method of delivering a hydrocarbon fuel to a combustion chamber, comprising:
flowing the hydrocarbon fuel from a hydrocarbon fuel source to at least one of a pressure-reducing device or a heat exchanger, wherein the hydrocarbon fuel is in a liquid phase at a first temperature and a first pressure, and wherein the first temperature of the liquid phase hydrocarbon fuel is less than its intrinsic oxidation temperature or endothermic reaction temperature;
heating the liquid phase hydrocarbon fuel from the first temperature to a second temperature;
flowing the liquid phase hydrocarbon fuel through the pressure-reducing device to reduce a pressure of the liquid phase hydrocarbon fuel from the first pressure to a second pressure, wherein the liquid phase hydrocarbon fuel substantially completely vaporizes at the second temperature and the second pressure within a first duration of time without forming carbonaceous contaminants;
flowing the vaporized hydrocarbon fuel through a compressor to increase the pressure of the vaporized hydrocarbon fuel from the second pressure to a third pressure;
heating the vaporized hydrocarbon fuel to increase a temperature of the vaporized hydrocarbon fuel from the second temperature to a third temperature, wherein the hydrocarbon fuel is either in a vapor phase at the third pressure and the third temperature or in a supercritical phase at the third pressure and the third temperature; and
flowing the completely vaporized hydrocarbon fuel or supercritical hydrocarbon fuel into the combustion chamber where combustion occurs.

19. The method of claim 18 , wherein the hydrocarbon fuel is a JP-8 fuel.

20. The method of claim 19 , wherein the second temperature is about 120 ° Celsius (248° Fahrenheit) and the second pressure is about 0.07 bar.

21. The method of claim 18 , wherein the first temperature is an ambient temperature and the first pressure is an ambient pressure.

22. The method of claim 21 , wherein the third temperature is about 204 ° Celsius (400° Fahrenheit) and the third pressure is the ambient pressure.

23. The method of claim 22 , wherein the first

Assignees

• U S Army Res Laboratory Attn Rdrl Loc I
• Us Army

Inventors

• Clark David A

Classifications

• F22B1/18

  the heat carrier being a hot gas, e.g. waste gas such as exhaust gas of internal-combustion engines · CPC title

• F23D11/445 Primary

  the flame and the vaporiser not coming into direct contact · CPC title