Solid state spark device and exciter circuit using such a device

1. A solid state spark device for use in an aircraft ignition system, comprising:

a triggering transformer having first and second coils;

a triggering circuit electrically connected to the first coil, the triggering circuit including circuit elements connected to supply current to the first coil upon charging of the triggering circuit to a triggering voltage, wherein the current through the first coil of the triggering transformer induces an output in the second coil; and

a control circuit that is electrically connected to the second coil and includes a switch controlled by the output from the second coil;

wherein the device is a two terminal device connectable in series between an igniter and a capacitive storage element that charges up to a sparking voltage sufficient to create a spark on the igniter.

2. The solid state spark device of claim 1 , wherein the sparking voltage is in a range of 3,000 volts to 4,200 volts and wherein the circuit elements are configured so that the triggering circuit charges to the triggering voltage when the capacitive storage element is charged to the sparking voltage.

3. The solid state spark device of claim 2 , wherein the sparking voltage is 4,000 volts.

4. The solid state spark device of claim 1 , wherein one of the circuit elements of the triggering circuit is a diode for alternating current (DIAC).

5. The solid state spark device of claim 1 , wherein the circuit elements of the triggering circuit include a capacitor and a plurality of resistive elements wired to charge the capacitor to the triggering voltage.

6. The solid state spark device of claim 1 , wherein the switch is a silicon-controlled rectifier (SCR) having a gate connected to receive the output from the second coil.

7. The solid state spark device of claim 1 , wherein the circuit elements prevent the supply of current to the first coil until the received voltage from the capacitive storage element reaches the sparking voltage.

8. The solid state spark device of claim 1 , wherein the circuit elements include a capacitor charged via an input of the triggering circuit, wherein the triggering circuit is configured to discharge the capacitor via the first coil when the voltage on the capacitor reaches the triggering voltage.

9. A solid state spark device for use in an aircraft ignition system, comprising:

a triggering transformer having first and second coils;

a triggering circuit electrically connected to the first coil, the triggering circuit including circuit elements connected to supply current to the first coil upon charging of the triggering circuit to a triggering voltage, wherein the current through the first coil of the triggering transformer induces an output in the second coil; and

a control circuit that is electrically connected to the second coil and includes a switch controlled by the output from the second coil;

wherein the circuit elements include a capacitor charged via an input of the triggering circuit, wherein the triggering circuit is configured to discharge the capacitor via the first coil when the voltage on the capacitor reaches the triggering voltage, wherein the circuit elements of the triggering circuit include a switch electrically connected between the capacitor and first coil, and wherein upon charging of the capacitor to the triggering voltage, the switch of the triggering circuit discharges the capacitor via the first coil.

10. The solid state spark device of claim 9 , wherein the triggering circuit includes a voltage divider connected between the input of the triggering circuit and the capacitor.