Oxidizing fuel in multiple operating modes

• US 8,701,413 B2
• Filed: 12/08/2008
• Issued: 04/22/2014
• Est. Priority Date: 12/08/2008
• Status: Expired due to Fees

• Current Assignee: ReductoNox Corp.
• Original Assignee: Ener-Core Power, Inc. (Ener-Core, Inc.)
• Inventors: Prabhu, Edan
• Primary Examiner(s): Wongwian, Phutthiwat
• Application Number:
  US12/330,151
• Publication Number:
  US 20100139282A1
• Time in Patent Office: 1,961 Days
• Field of Search: 60/391.2, 60/394.65, 60/395, 607/37
• US Class Current: 60/737
• CPC Class Codes: F02C 3/22 the fuel or oxidant being gaseous at standard temperature and pressure F02C3/28 takes precedence
• CPC Class Codes: F02C 6/18 using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10
• CPC Class Codes: F02C 7/08 Heating air supply before combustion, e.g. by exhaust gases
• CPC Class Codes: F02C 7/10 by means of regenerative heat-exchangers
• CPC Class Codes: F02C 7/22 Fuel supply systems
• CPC Class Codes: F02C 9/26 Control of fuel supply F02C9/48 takes precedence; fuel valves F02C7/232
• CPC Class Codes: F02C 9/40 specially adapted to the use of a special fuel or a plurality of fuels

Abstract

A fuel oxidizer system is operated in a first operating mode. In the first operating mode, a mixture that includes fuel from a fuel source is compressed in a compressor of the fuel oxidizer system; the fuel of the compressed mixture is oxidized in a reaction chamber of the fuel oxidizer system; and the oxidized fuel is expanded to generate rotational kinetic energy. The fuel oxidizer system is operated in a second operating mode. In the second operating mode, fuel from the fuel source is directed to bypass the compressor, and the fuel that bypassed the compressor is oxidized in the reaction chamber.

Claims

1. A fuel oxidizer system comprising:

a compressor that has a mixture inlet and a compressed mixture outlet and is configured to compress an air and fuel mixture between the mixture inlet and the compressed mixture outlet;

a reaction chamber configured to receive a compressed mixture from the compressed mixture outlet and oxidize at least a portion of the fuel of the compressed mixture to produce an oxidation product;

a turbine;

a first valve system, comprising a first valve disposed along a first flow path and a second valve disposed along a second flow path, configured to receive fuel from a fuel source and direct the fuel to the reaction chamber (i) by directing the fuel to the mixture inlet of the compressor via the first valve, in a first mode, and (ii) by directing the fuel to bypass the compressor via the second valve, in a second mode; and

a second valve system configured to receive the oxidation product from the reaction chamber and direct the oxidation product (i) to the turbine via a third flow path, in the first mode, and (ii) to an exhaust path, bypassing the turbine via a fourth flow path, in the second mode.

2. The fuel oxidizer system of claim 1, wherein the reaction chamber is configured to receive and oxidize the fuel directed by the first valve system to bypass the compressor.

3. The fuel oxidizer system of claim 1, wherein the turbine is configured to receive the oxidized fuel from the reaction chamber and convert heat energy from the oxidized mixture into rotational movement.

4. The fuel oxidizer system of claim 1, wherein the turbine comprises a turbine inlet, the turbine being configured to receive the oxidized mixture from the reaction chamber through the turbine inlet, and the reaction chamber is configured to maintain a maximum temperature of the mixture in the reaction chamber substantially at or below a temperature of the turbine inlet.

5. The fuel oxidizer system of claim 1, further comprising a blower between the fuel source and the reaction chamber.

6. The fuel oxidizer system of claim 1, the reaction chamber comprising an igniter that is configured to initiate combustion of fuel to bypass the compressor.

7. The fuel oxidizer system of claim 1, wherein the reaction chamber is configured to initiate oxidation of fuel to bypass the compressor substantially independent of an igniter and substantially independent of an oxidation catalyst.

8. The fuel oxidizer system of claim 1, wherein the reaction chamber is configured to initiate oxidation the fuel of the compressed mixture substantially independent of an igniter and substantially independent of an oxidation catalyst.

9. The fuel oxidizer system of claim 1, wherein the first valve system comprises an inlet of the first valve in fluid communication with the fuel source, an outlet of the first valve in fluid communication with the mixture inlet of the compressor, an inlet of the second valve in fluid communication with the fuel source, and an outlet of the second valve in fluid communication with the reaction chamber and configured to direct fuel to bypass the compressor.

10. The fuel oxidizer system of claim 1, wherein the first valve system comprises multiple valves.

11. The fuel oxidizer system of claim 1, further comprising a heat exchanger between the fuel source and the reaction chamber.

12. The fuel oxidizer system of claim 11, wherein, in the second mode, the first valve system is configured to direct the fuel through the heat exchanger.

13. The fuel oxidizer system of claim 11, wherein, in the second mode, the second valve system is configured to direct the oxidation product through the heat exchanger.

14. The fuel oxidizer system of claim 5, wherein, in the second mode, the blower is configured to receive the fuel from the fuel source and air from an air source to provide a flow of a mixture of air and fuel to the reaction chamber.