Electro-dynamic swirler, combustion apparatus and methods using the same

• US 8,082,725 B2
• Filed: 04/12/2007
• Issued: 12/27/2011
• Est. Priority Date: 04/12/2007
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Younsi, Abdelkrim, Saddoughi, Seyed Gholamali, Herbon, John Thomas, Pintgen, Florian Peter
• Primary Examiner(s): Cuff, Michael
• Assistant Examiner(s): NGUYEN, ANDREW H
• Application Number:
  US11/734,370
• Publication Number:
  US 20090064661A1
• Time in Patent Office: 1,720 Days
• Field of Search: 607/37, 607/38, 607/47, 60/397.6, 607/48, 602/47, 60/393.8, 431/8, 431/9, 431/12, 431/2, 431/354
• US Class Current: 60/39.76
• CPC Class Codes: F23C 15/00 Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass for generating combustion products of high pressure or high velocity F23R7/00; starting devices F23D11/42
• CPC Class Codes: F23D 11/32 by electrostatic means
• CPC Class Codes: F23K 2300/101 Application of magnetism or electricity
• CPC Class Codes: F23R 3/286 having fuel-air premixing devices F23R3/30 takes precedence
• CPC Class Codes: F23R 7/00 Intermittent or explosive combustion chambers

Abstract

In one embodiment, a combustion apparatus comprises: an oxidant inlet, a fuel inlet, a mixing zone configured to mix fuel and oxidant to form a mixture, a combustion zone in fluid communication with the mixing zone and configured to combust the mixture, and an outlet in fluid communication with the combustion zone. The mixing zone, the combustion zone, and/or the outlet comprises an electro-dynamic swirler configured to swirl ionized gas. The electro-dynamic swirler comprises a plurality of electrodes in electrical communication with a power source. In one embodiment, a method of creating thrust comprises: mixing a fuel and an oxidant to form a mixture, igniting the mixture to form an ignited mixture, combusting the ignited mixture to form a flame, and using the flame to create thrust, wherein the flame and/or the fuel and oxidant are electro-dynamically swirled.

Claims

1. A combustion apparatus, comprising:

an oxidant inlet;

a fuel inlet;

a mixing area in fluid communication with the fuel inlet and the oxidant inlet, and configured to mix fuel and oxidant to form a mixture;

a combustion zone in fluid communication with the mixing area and configured to combust the mixture;

a pulse detonation system located downstream from the combustion zone; and

an outlet in fluid communication with the combustion zone;

wherein the mixing area, the combustion zone, and/or the outlet comprise an electro-dynamic swirler configured to swirl ionized gas, and wherein the electro-dynamic swirler comprises a plurality of electrodes in electrical communication with a power source, and wherein the plurality of electrodes are arranged and connected in groups to produce a rotating electric field.

2. The apparatus of claim 1, wherein the pulse detonation system comprises a mixing chamber in fluid communication with the outlet and with additional fuel and/or oxidant, a detonation chamber located downstream of and in fluid communication with the mixing chamber, and a detonation outlet located downstream of and in fluid communication with the detonation chamber.

3. The apparatus of claim 2, wherein the mixing chamber further comprises a second electro-dynamic swirler.

4. The apparatus of claim 3, wherein the detonation chamber further comprises an ignition location and a third electro-dynamic swirler located downstream of the ignition location.

5. The apparatus of claim 2, wherein the detonation outlet further comprises a second electro-dynamic swirler.

7. The apparatus of claim 1, wherein the plurality of electrodes are arranged in groups approximately 180 degrees apart from each other.

8. The apparatus of claim 1, wherein the rotating electric field is produced by spacing a phase of a voltage to the plurality of electrodes by approximately 120 degrees.

9. The apparatus of claim 8, wherein a frequency applied to each electrode is approximately equal.

10. The apparatus of claim 1, wherein the plurality of electrodes are symmetrically arranged.

11. The apparatus of claim 1, wherein the plurality of electrodes are electrically insulated from one another.

12. The apparatus of claim 1, wherein the plurality of electrodes are arranged to form one of a cylinder and a cone.

6. A pulse detonation apparatus, comprising:

a fuel inlet;

an oxidant inlet;

a mixing area in fluid communication with the fuel inlet and the oxidant inlet;

a detonation chamber located downstream of and in fluid communication with the mixing area; and

a detonation outlet located downstream of and in fluid communication with the detonation chamber;

wherein the mixing area, detonation chamber, and/or detonation outlet comprise an electro-dynamic swirler, and wherein the electro-dynamic swirler comprises a plurality of electrodes in electrical communication with a power source.