Ignition system of an aircraft turbine engine

Patent metadata

Field	Value
Publication number	US-10697420-B2
Application number	US-201816161941-A
Country	US
Kind code	B2
Filing date	Oct 16, 2018
Priority date	Oct 23, 2017
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

A turbine engine ignition system comprising a spark plug having excitation and return terminals, and a spark plug exciter connected to the excitation terminal. The return terminal is connected to an equipotential reference-forming structure, the exciter device is connected to a command line for a signal to supply an excitation signal to the spark plug. The ignition system comprises a control device comprising current and voltage sensors, a first voltage comparator, a second current comparator, and a microcontroller receiving output from the two comparators. The first comparator compares the voltage sensor signal to a first reference value and the second comparator compares the current sensor signal to a second reference value. The microcontroller generates a signal indicating a malfunction of the ignition system if the current sensor signal is lower than the second reference value while the voltage sensor signal is higher than the first reference value.

First claim

The invention claimed is:

1. An ignition system of a turbine engine, comprising:
an ignition spark plug having an excitation terminal and a return terminal,
a spark plug exciter device connected to the excitation terminal of the ignition spark plug,
the return terminal being, in use, connected to an equipotential reference-forming structure of the turbine engine,
the exciter device being, in use, connected to a command line and to an electrical power source supplying an excitation signal to the ignition spark plug on reception of an excitation signal over the command line,

a control device comprising a current sensor, a voltage sensor, a first comparator receiving as input a signal generated by the voltage sensor, a second comparator receiving as input a signal generated by the current sensor, and a microcontroller receiving an output of the two comparators,
the first comparator being configured to compare a value of an amplitude of the signal generated by the voltage sensor to a first reference value and
the second comparator being configured to compare a value of the signal generated by the current sensor to a second reference value,
the microcontroller configured to implement an AND logic gate whose output is a signal indicative of a malfunction of the ignition system if the value of an amplitude of the signal generated by the current sensor is lower than the second reference value while the value of the amplitude of the signal generated by the voltage sensor is higher than the first reference value.

2. The ignition system according to claim 1 , wherein the current sensor comprises a shunt.

3. The ignition system according to claim 1 , wherein the voltage sensor comprises a voltage transformer.

4. The ignition system according to claim 1 , wherein the first and the second comparator are analogue, the microcontroller is connected to the output of each of the first comparator and of the second comparator via an analogue/digital converter.

5. The ignition system according to claim 1 , wherein the first and the second comparator are digital and produced via a programming of the microcontroller.

6. A method for detecting a malfunction of an ignition system of a turbine engine implemented by a control device, said ignition system comprising an ignition spark plug having an excitation terminal and a return terminal, a spark plug exciter device connected to the excitation terminal of the ignition spark plug, the return terminal being, in use, connected to an equipotential reference-forming structure of the turbine engine, the exciter device being, in use, connected to a command line and to an electrical power source supplying an excitation signal to the ignition spark plug, on reception of an excitation signal over the command line,
the control device comprising a current sensor, a voltage sensor, a first comparator connected to the voltage sensor, a second comparator connected to the current sensor, and a microcontroller receiving the output of the two comparators,
wherein the method comprises the steps:
measuring a voltage by the voltage sensor, said voltage sensor generating a signal that is an image of said voltage;
measuring a current by the current sensor, said current sensor generating a signal that is an image of said current;
comparing, by the first comparator, an amplitude of the signal generated by the voltage sensor with a first reference value and generating an output signal;
comparing, by the second comparator, an amplitude of a signal generated by the current sensor with a second reference value and generating an output signal;
monitoring, by the microcontroller, a state of the output signal of the first comparator and a state of the output signal of the second comparator;
generating, by the microcontroller, a signal indicative of a malfunction of the ignition system if a value of the amplitude of the signal generated by the current sensor is lower than the second reference value while a value of the amplitude of the signal generated by the voltage sensor is higher than the first reference value.

Assignees

• Airbus Operations Sas

Inventors

• Ambroise Richard
• Collas Xavier

Classifications

• F23Q23/10

  electrically · CPC title

• F05D2260/85

  Starting · CPC title

• F02C7/266 Primary

  Electric (sparking plugs H01T) · CPC title

• F05D2260/80

  Diagnostics · CPC title

• F02P2017/121

  by measuring spark voltage · CPC title