Turbine engine ignition system and method

Patent metadata

Field	Value
Publication number	US-11519335-B1
Application number	US-202117459128-A
Country	US
Kind code	B1
Filing date	Aug 27, 2021
Priority date	Aug 27, 2021
Publication date	Dec 6, 2022
Grant date	Dec 6, 2022

Abstract

An ignition system for igniting fuel in a gas turbine engine includes a power supply and an energy storage network electrically connected to the power supply. The energy storage network includes a first stage having a first capacitor and a second stage having a second capacitor. The ignition system further includes an engine igniter electrically coupled to the energy storage network.

First claim

What is claimed is:

1. An ignition system for igniting fuel in a gas turbine engine, comprising:
a power supply;
an energy storage network electrically connected to the power supply and having a network power output capable of providing output power, the energy storage network comprising:
a first stage having a first capacitor and a first switch, with the first switch having an open state and a closed state;
a second stage having a second capacitor and a second switch, with the second switch having an open state and a closed state;
a parallel electrical connection defined between the power supply, the first capacitor, and the second capacitor when each of the first switch and the second switch are in the open state; and
a series electrical connection defined between the first capacitor, the second capacitor, and the network power output when each of the first switch and the second switch are in the closed state, the series electrical connection defining the output power;

an inductor electrically coupled to the network power output and configured to form a modified output power based on the output power received from the network power output; and
an engine igniter electrically coupled to the inductor and configured to produce an ignition spark upon receiving the modified output power.

2. The ignition system of claim 1 , wherein the energy storage network further comprises a first resistor electrically connected to the first capacitor and the first switch.

3. The ignition system of claim 2 , wherein the energy storage network further comprises a second resistor electrically connected to the second capacitor and the second switch.

4. The ignition system of claim 1 , further comprising an ignition lead electrically coupled to the engine igniter and to the network power output, with the ignition lead comprising the inductor.

5. The ignition system of claim 1 , wherein the inductor comprises an inductor coil electrically coupled to the network power output and wound about a magnetically-saturable core.

6. The ignition system of claim 1 , wherein at least one of the first switch or the second switch comprises one of a controllable switch or a semicontrollable switch.

7. The ignition system of claim 6 , wherein the inductor comprises a saturable reactor.

8. The ignition system of claim 1 , wherein the first switch and the second switch each comprise a controllable switch, and wherein the inductor comprises a saturable reactor.

9. The ignition system of claim 1 , further comprising a comparison module electrically coupled to the energy storage network and configured to compare an overall voltage of the energy storage network with a predetermined threshold voltage.

10. The ignition system of claim 1 , further comprising a clamp rectifier electrically coupled to the inductor.

11. The ignition system of claim 1 , wherein the modified output power comprises at least one of a pulse voltage between 800 V and 25,000 V, a pulse current between 200 A and 2000 A, a pulse duration between 1 microsecond and 300 microseconds, or a pulse width between 1 microsecond and 10 microseconds.

12. A gas turbine engine, comprising:
a combustor; and
an ignition system coupled to the combustor for igniting fuel therein, the ignition system comprising:
an energy storage network electrically connectable with a power supply and having a network power output capable of providing output power, the energy storage network comprising:
a first stage having a first capacitor and a first switch, with the first switch having an open state and a closed state;
a second stage having a second capacitor and a second switch, with the second switch having an open state and a closed state;
a parallel electrical connection defined between the power supply, the first capacitor, and the second capacitor when each of the first switch and the second switch are in the open state; and
a series electrical connection defined between the network power output, the first capacitor, and the second capacitor when each of the first switch and the second switch are in the closed state, the series electrical connection defining the network power output;

an inductor electrically coupled to the network power output and configured to form a modified output power based on the output power received from the network power output; and
an engine igniter electrically coupled to the inductor and configured to produce an ignition spark upon receiving the modified output power.

13. The gas turbine engine of claim 12 , wherein the inductor comprises an inductor coil electrically coupled to the network power output and wound about a magnetically-saturable core.

14. The gas turbine engine of claim 12 , wherein at least one of the first switch or the second switch comprises one of a controllable switch or a semicontrollable switch.

15. The gas turbine engine of claim 14 , wherein the inductor comprises a saturable reactor.

16. The gas turbine engine of claim 15 , wherein the first switch and the second switch each comprise the controllable switch, and wherein the inductor comprises the saturable reactor.

17. A method of operating a turbine engine ignition system, the method comprising:
operating an energy storage network of the turbine engine ignition system in a first configuration enabling a parallel electrical connection between a power source, a first capacitor, and a second capacitor for charging the first capacitor and the second capacitor;
operating the energy storage network in a second configuration enabling a series electrical connection between the first capacitor and the second capacitor for generating a summated power output; and
modifying, by way of a inductor, the summated power output to form a modified power output for an igniter in the turbine engine ignition system.

18. The method of claim 17 , wherein the turbine engine ignition system further comprises a first switch and a second switch, each of the first switch and the second switch having an open state and a closed state, and wherein the first configuration is at least partially defined by each of the first switch and the second switch being in the open state.

19. The method of claim 18 , wherein the second configuration is at least partially defined by each of the first switch and the second switch being in the closed state.

20. The method of claim 17 , further comprising directing the summated power output through a coil of the inductor to saturate a core of the inductor, thereby modifying an inductance of the inductor to form the modified power output.

Assignees

• Unison Ind Llc

Inventors

• Carpenter Jay Joseph
• Dolmovich Bruce Edward

Classifications

• H01F38/12 Primary

  Ignition, e.g. for IC engines · CPC title

• F02P15/003

  Layout of ignition circuits for gas turbine plants (ignition of gas turbine plants per se F02C7/26) · CPC title

• F05D2260/99

  Ignition, e.g. ignition by warming up of fuel or oxidizer in a resonant acoustic cavity · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F02C7/266 Primary

  Electric (sparking plugs H01T) · CPC title