Auto-driven plasma actuator for transition from deflagration to detonation combustion regime and method

Patent metadata

Field	Value
Publication number	US-11493207-B2
Application number	US-201816497979-A
Country	US
Kind code	B2
Filing date	Mar 15, 2018
Priority date	Apr 30, 2017
Publication date	Nov 8, 2022
Grant date	Nov 8, 2022

Abstract

An engine that uses detonation for generating energy includes a housing; an inlet configured to inject a fuel mixture into an ignition region of the housing, the inlet being attached to the housing; an ignitor located in the ignition region and configured to ignite the fuel mixture; a deflagration to detonation, DDT, region in fluid communication and downstream from the ignition region; a pair of electrodes located in the DDT region and configured to apply nanosecond repetitive voltage pulses to the DDT region; and a detonation region, within the housing, in fluid communication and downstream from the DDT region. The nanosecond repetitive voltage pulses generate a non-thermal plasma that transition a combustion front propagation through the housing from a deflagration mode to a detonation mode.

First claim

What is claimed is:

1. An engine that uses detonation for generating energy, the engine comprising:
a housing;
an inlet configured to inject a fuel mixture into an ignition region of the housing, the inlet being attached to the housing;
an ignitor located in the ignition region and configured to ignite the fuel mixture;
a deflagration to detonation, DDT, region in fluid communication and downstream from the ignition region;
a pair of electrodes located in the DDT region and configured to apply nanosecond repetitive voltage pulses with an amplitude smaller than a threshold breakdown voltage of the fuel mixture to the ignited fuel mixture in the DDT region; and
a detonation region, within the housing, in fluid communication and downstream from the DDT region, wherein the nanosecond repetitive voltage pulses generate a non-thermal plasma that transition a combustion front propagation, of the ignited fuel mixture, through the housing, from a deflagration mode to a detonation mode, wherein a pressure wave moves ahead of the combustion front in the DDT region, and wherein the nanosecond repetitive voltage pulses are applied between the combustion front and the pressure wave or are applied into the combustion front itself.

2. The engine of claim 1 , wherein the combustion front has a subsonic speed in the DDT region and a sonic speed, with respect to the burnt gases, in the detonation region.

3. The engine of claim 1 , wherein the engine is a gas turbine.

4. The engine of claim 1 , further comprising:
a pulser configured to generate the nanosecond repetitive voltage pulses; and
a control system configured to control the pulser and the pair of electrodes.

5. The engine of claim 4 , wherein the control system includes a processor and a memory, and the processor is configured to turn on the pair of electrodes before the combustion front arrives at a location of the pair of electrodes.

6. The engine of claim 5 , wherein the processor instructs the pulser to generate the nanosecond repetitive voltage pulses.

7. The engine of claim 6 , wherein the processor receives current or voltage measurements indicative of a volume between the electrodes and based on the measurements, determines to switch off the nanosecond repetitive voltage pulses applied by the pair of electrodes.

8. The engine of claim 6 , wherein the processor is configured to switch off the nanosecond repetitive voltage pulses applied by the pair of electrodes after a predetermined number of discharges.

9. A method for driving an engine that uses detonation for generating energy, the method comprising:
injecting a fuel mixture at an inlet, into an ignition region of a housing;
igniting the fuel mixture with an ignitor located in the ignition region;
applying nanosecond repetitive voltage pulses with an amplitude smaller than a threshold breakdown voltage of the fuel mixture to the ignited fuel mixture, with a pair of electrodes located in a deflagration to detonation, DDT, region, which is in fluid communication and downstream from the ignition region; and
initiating a detonation of a combustion front in a detonation region, within the housing, which is in fluid communication and downstream from the DDT region,
wherein the nanosecond repetitive voltage pulses generate a non-thermal plasma that initiate a transition of the combustion front propagation, of the ignited fuel mixture, through the housing from a deflagration mode to a detonation mode, wherein a pressure wave moves ahead of the combustion front in the DDT region, and wherein the nanosecond repetitive voltage pulses are applied between the combustion front and the pressure wave or are applied into the combustion front itself.

10. The method of claim 9 , wherein the combustion front has a subsonic speed in the DDT region and a sonic speed, with respect to the burnt gases, in the detonation region.

11. The method of claim 9 , further comprising:
generating with a pulser the nanosecond repetitive voltage pulses; and
controlling with a control system the pulser and the pair of electrodes to turn on the pair of electrodes before the combustion front arrives at a location of the pair of electrodes.

12. The method of claim 11 , further comprising:
instructing the pulser to generate the nanosecond repetitive voltage pulses with the amplitude smaller than the threshold breakdown voltage of the fuel mixture for a selected pressure and temperature of the gas.

13. The method of claim 12 , further comprising:
receiving current or voltage measurements indicative of a volume between the pair of electrodes; and
based on the measurements, determining to switch off the nanosecond repetitive voltage pulses applied by the pair of electrodes.

14. The method of claim 12 , further comprising:
switching off the nanosecond repetitive voltage pulses applied by the pair of electrodes after a predetermined number of discharges.

15. An auto-driven plasma actuator control system comprising:
a pulser configured to generate nanosecond repetitive voltage pulses;
a pair of electrodes to be located in a deflagration to detonation, DDT, region of an engine, and configured to apply nanosecond repetitive voltage pulses having an amplitude smaller than a threshold breakdown voltage of a fuel mixture to the DDT region; and
a control system configured to control the pulser and the pair of electrodes,
wherein the control system turns on the pair of electrodes before a combustion front of an ignited fuel mixture of the engine arrives at a location of the pair of electrodes and turns the pair of electrodes off after the combustion front has passed, and
wherein the nanosecond repetitive voltage pulses generate a non-thermal plasma that transitions the combustion front propagation, of the ignited fuel mixture, through the engine from a deflagration mode to a detonation mode, wherein a pressure wave moves ahead of the combustion front in the DDT region, and wherein the nanosecond repetitive voltage pulses are applied between the combustion front and the pressure wave or are applied into the combustion front itself.

Assignees

• Univ King Abdullah Sci & Tech

Inventors

• Lacoste Deanna A

Classifications

• H05H1/52

  using exploding wires or spark gaps (H05H1/26 takes precedence) · CPC title

• F23R7/00 Primary

  Intermittent or explosive combustion chambers · CPC title

• F02K7/04

  with resonant combustion chambers · CPC title

• F02C5/00

  Gas-turbine plants characterised by the working fluid being generated by intermittent combustion · CPC title