Ignition System for a turbine engine

An ignition system for a gas turbine engine comprising:

• an energy storage device to store energy;
• a bi-state switch connected in series with the energy storage device, the bi-state switch having a fully conducting state and a non-conducting state, the bi-state switch requiring a transition time period T1 to transition from the non-conducting state to the fully conducting state;
• a sparking device connected in series with the bi-state switch and the energy storage device, the sparking device having a non-conducting state and a conducting state and requiring a transition time period T2 to transition from the non-conducting state to the conducting state;
• and,
• a current limiting network connected in series in any order with the bi-state switch and the sparking device to limit current flow through the sparking device until the sparking device has completed its transition time period T2 and to thereafter permit an increased current to flow through the sparking device to generate sparks.

An exciter for energizing a spark generating device to ignite fuel in a gas turbine engine, the spark generating device having an associated turn-on time period T1 for transitioning from a non-conducting state to a conducting state, the turn-on time period T1 commencing when the spark generating device begins to receive energy from the exciter and terminating when the spark generating device enters the conducting state, the exciter comprising:

• an energy storage device to store energy;
• a controlled switch connected in series with the energy storage device and transitioning from a non-conducting state to a conducting state for selectively discharging the energy from the energy storage device upon receipt of a control signal, the controlled switch having an associated turn-on time period T2 for transitioning from the non-conducting state to the fully conducting state, the turn-on time period T2 commencing when the controlled switch receives the control signal and terminating when the controlled switch enters the fully conducting state;
• an output terminal for removably connecting the spark generating device, the output terminal being connected in series with the energy storage device and the controlled switch to receive the energy discharged from the energy storage device and to output the received energy to the spark generating device;
• and,
• a delay network connected in series with the controlled switch and the output terminal for limiting current flow through the spark generating device for a time period T3 after which the current through the spark generating device is not limited by the delay network, the time period T3 commencing at substantially the same time as the turn-on time period T1 of the spark generating device and ending after the turn-on time period T1 of the spark generating device has terminated, wherein the current through the spark generating device rises to an increased level after the period T3 has terminated.

An exciter for energizing a spark generating device to ignite fuel in a gas turbine engine, the spark generating device having an associated turn-on time period T1 for transitioning from a non-conducting state to a conducting state, the turn-on time period T1 commencing when the spark generating device begins to receive energy from the exciter and terminating when the spark generating device enters the conducting state, the exciter comprising:

• an energy storage device to store energy;
• a bi-state switch connected in series with the energy storage device, the bi-state switch having a fully conducting state and a non-conducting state, the bi-state switch requiring a transition time period T2 to transition from the non-conducting state to the fully conducting state;
• an output terminal for removably connecting the spark generating device to the exciter, the output terminal being connected in series with the energy storage device and the bi-state switch to receive the energy discharged from the energy storage device and to output the received energy to the spark generating device;
• and,
• a current limiting network connected in series in any order with the bi-state switch and the sparking device to limit current flow through the sparking device until the sparking device has completed its transition time period T1 and to thereafter permit an increased current to flow through the sparking device to generate sparks.

An exciter for energizing a spark generating device to ignite fuel in a gas turbine engine, the spark generating device having an associated turn-on time period T1 for transitioning from a non-conducting state to a conducting state, the turn-on time period T1 commencing when the spark generating device begins to receive energy from the exciter and terminating when the spark generating device enters the conducting state, the exciter comprising:

• an energy storage device to store energy;
• a controlled switch connected in series with the energy storage device and transitioning from a non-conducting state to a conducting state for selectively discharging the energy from the energy storage device upon receipt of a control signal;
• an output terminal for removably connecting the spark generating device, the output terminal being connected in series with the energy storage device and the controlled switch to receive the energy discharged from the energy storage device and to output the received energy to the spark generating device;
• and,
• a delay network connected in series with the controlled switch and the output terminal for limiting current flow through the spark generating device for a time period T2 after which the current through the spark generating device is not limited by the delay network, the time period T2 commencing at substantially the same time as the turn-on time period T1 of the spark generating device and ending after the turn-on-time period T1 of the spark generating device has terminated, wherein the current through the spark generating device rises to an increased level after the period T2 has terminated.