Gas-assisted liguid fuel oxygen reactor

Patent metadata

Field	Value
Publication number	US-10215402-B2
Application number	US-201615087300-A
Country	US
Kind code	B2
Filing date	Mar 31, 2016
Priority date	Mar 31, 2016
Publication date	Feb 26, 2019
Grant date	Feb 26, 2019

Abstract

The present disclosure is directed to systems and methods for low-CO 2 emission combustion of liquid fuel with a gas-assisted liquid fuel oxygen reactor. The system comprises an atomizer that sprays fuel and CO 2 into an evaporation zone, where the fuel and CO 2 is heated into a vaporized form. The system comprises a reaction zone that receives the vaporized fuel and CO 2 . The system includes an air vessel having an air stream, and a heating vessel adjacent to the air vessel that transfers heat to the air vessel. The system comprises an ion transport membrane in flow communication with the air vessel and reaction zone. The ion transport membrane receives O 2 permeating from the air stream and transfers the O 2 into the reaction zone resulting in combustion of fuel. The combustion produces heat and creates CO 2 exhaust gases that are recirculated in the system limiting emission of CO 2 .

First claim

What is claimed is:

1. A gas-assisted liquid fuel oxygen reactor system, comprising:
a CO 2 -assisted atomizer having an inlet adapted to receive a liquid fuel and an outlet adapted to spray atomized fuel and CO 2 ;
an evaporation zone having an inlet adapted to receive the atomized liquid fuel and CO 2 and having an outer wall that is formed of a thermally conductive material such that the evaporation zone is adapted to heat the atomized fuel and CO 2 into a vaporized form;
a reaction zone co-axially aligned with and in flow communication with the evaporation zone, wherein the reaction zone is adapted to receive a flow of the vaporized fuel and CO 2 from the evaporation zone;
an ion transport membrane that is coaxially aligned with the evaporation zone and defines the reaction zone;
an air vessel defined by structure that is disposed about the ion transport membrane and defines a first space between an outer surface of the ion transport membrane and an inner surface of the air vessel structure, wherein the air vessel structure is formed of a thermally conductive material and the air vessel is for receiving an air stream that flows in a counter direction relative to a flow of the vaporized fuel and CO 2 in the reaction zone;
a heating vessel defined by a structure that is disposed about the air vessel structure and defines a second space between an outer surface of the air vessel structure and an inner surface of the heating vessel structure, wherein the heating vessel is for receiving a heated air and gaseous fuel stream such that heat is transferred from the air and gaseous fuel stream to the first space;
wherein the ion transport membrane is adapted to provide O 2 permeating from the air stream and transfer the O 2 into the reaction zone resulting in an O 2 -depleted air stream in the first space of the air vessel structure, and wherein the reaction zone is adapted to combust the vaporized fuel and CO 2 in the presence of O 2 to produce heat and create exhaust gases that are recirculated in the system.

2. The system of claim 1 , further comprising:
a fuel filter situated between the evaporation zone and the reaction zone and adapted to remove unwanted contaminants from the vaporized fuel and CO 2 prior to entry of the vaporized fuel and CO 2 into the reaction zone.

3. The system of claim 1 , further comprising:
a bluff body located within the evaporation zone and adapted to assist in the evaporation of the fuel.

4. The system of claim 1 , wherein the recirculation of the exhaust gases provides energy to the system to maintain an at least substantially constant temperature at the ion transport membrane.

5. The system of claim 4 , wherein a temperature at the ion transport membrane is maintained between 700° C. and 900° C.

6. The system of claim 1 , further comprising:
a heat exchanger located upstream of the CO 2 -assisted atomizer, the heat exchanger being adapted to receive the O 2 -depleted air stream from the air vessel and the liquid fuel, and adapted to transfer heat from the O 2 -depleted air stream to the liquid fuel prior to reception of the liquid fuel in the CO 2 -assisted atomizer.

7. The system of claim 1 , wherein the system has a cylindrical shape with the ion transport membrane, the air vessel structure and the heating vessel structure being concentric to one another, and wherein the reaction zone is located internally to the ion transport membrane.

8. The system of claim 1 , wherein the ion transport membrane comprises first and second planar membranes with the reaction zone disposed there between.

9. The system of claim 8 , wherein the air vessel comprises first and second planar plates with the ion transport membrane disposed there between.

10. The system of claim 9 , wherein the evaporation zone, the ion transport membrane, the air vessel, and the heating vessel define a first reactor unit, and wherein the system further includes at least a second reactor unit, the second reactor unit having an identical construction as the first reactor unit, the first and second reactor units being in a stacked orientation.

Assignees

• Saudi Arabian Oil Co
• Univ King Fahd Pet & Minerals

Inventors

• Ben-Mansour Rached
• Habib Mohamed A
• Jamal Aqil

Classifications

• F23D5/00 Primary

  Burners in which liquid fuel evaporates in the combustion space, with or without chemical conversion of evaporated fuel · CPC title

• F23D23/00 Primary

  Assemblies of two or more burners (gas burners with provision for a retention flame F23D14/26) · CPC title

• F23D11/404

  Flame tubes (not forming part of the burner F23M9/06) · CPC title

• F23D11/44

  Preheating devices; Vaporising devices · CPC title

• F23D5/12

  Details · CPC title