Method and apparatus for protecting electrical systems from lightning strike effects

Claim 3

The method of claim 1 further comprising the step of reactively voltage dividing undesirable voltage increases applied to the power distribution bus.

Claim 4

The method of claim 2 wherein one of said power conductors is connected to said common ground and wherein the step of connecting mutually coupled chokes further comprises inducing a voltage from said grounded conductor to the other power conductor that diminishes the lightning current and any induced surge voltage that would otherwise enter said distribution bus through said other conductor.

Claim 5

The method of claim 1 wherein one of said power conductors is connected to said common ground and wherein the step of connecting mutually coupled chokes further comprises inducing a voltage from said grounded conductor to the other power conductor that diminishes the lightning current and any induced surge voltage that would otherwise enter said distribution bus through said other conductor.

Claim 6

A lightning protection device adapted to be connected to an electrical system, said device comprising: first and second parallel wound, magnetically coupled inductors, each of said inductors having first and second terminals, said first terminals being the input terminals of said protection device; a third inductor having first and second terminals, said first terminal of said third inductor connected to said second terminal of said first inductor, said second terminals of said second and third inductors being the output terminals of said device; and a voltage limiting element connected to said first terminal of said third inductor and the second terminal of said second inductor, whereby a voltage or current surge applied to the input terminals of said protective device is reduced substantially at the output terminals.

Claim 7

A lightning protection device adapted to be connected to an electrical system, said device comprising: first and second parallel wound, magnetically coupled inductors, each of said inductors having first and second terminals, said first terminals being the input terminals of said protection device; a third inductor having first and second terminals, said first terminal of said third inductor connected to said second terminal of said first inductor, said second terminals of said second and third inductors being the output terminals of said device; and a voltage limiting element connected to said first terminal of said third inductor and the second terminal of said second inductor, whereby a voltage or current surge applied to the input terminals of said protective device is reduced substantially at the output terminals.

Claim 8

The lightning protection device of claim 5 wherein said voltage limiting device is a varistor.

Claim 9

The lightning protection device of claim 6 wherein each of said first and second inductors are bifilarly wound on an air core and an insulating form.

Claim 10

The lightning protection device of claim 7 wherein said inductors are enclosed in a housing and said third inductor is positioned relative to said first and second inductors to minimize inductive coupling therebetween.

Claim 11

The lightning protection device of claim 8 wherein the inductance of said third inductor is greater than said first or second inductors.

Claim 12

In an aircraft mounted electrical system having a high susceptibility to lightning strikes wherein lightning strike currents are conducted from the electrical system along the electrical power cables to a power distribution bus, a protection apparatus for limiting the magnitude of currents and voltages conducted to said bus, said apparatus including: an electrical ground conductor connected between said electrical system and the main frame portion of said aircraft; and a pair of magnetically coupled choke coils connected in electrical relation with said electrical power cables to increase the impedance thereof above that of said grounding conductor whereby a substantial portion of a lightning strike current is harmlessly conducted along said ground conductor to said aircraft frame.

Claim 13

In an aircraft mounted electrical system having a high susceptibility to lightning strikes wherein lightning strike currents are conducted from the electrical system along the electrical power cables to a power distribution bus, a protection apparatus for limiting the magnitude of currents and voltages conducted to said bus, said apparatus including: an electrical ground conductor connected between said electrical system and the main frame portion of said aircraft; and a pair of magnetically coupled choke coils connected in electrical relation with said electrical power cables to increase the impedance thereof above that of said grounding conductor whereby a substantial portion of a lightning strike current is harmlessly conducted along said ground conductor to said aircraft frame.

Claim 14

The protection apparatus of claim 10 further comprising: a voltage limiting means shunting said electrical power cables at a point between said choke coils and said power distribution bus.

Claim 15

The protection apparatus of claim 11 further comprising: an inductor connected in electrical series relation with one winding of said choke and said power distribution bus, said inductor located between said choke and said bus.

Claim 16

The protection apparatus of claim 12 wherein said aircraft mounted electrical system includes a radome-mounted pitot tube heater circuit with a heater element located within the pitot tube and said electrical power cables provide electrical power to said heater element, said power cables extending along the inner walls of said pitot tube and said radome to a power distribution bus adjacent the radome-fuselage interface.

Claim 17

The protection apparatus of claim 13 further comprising: means limiting the voltage difference between said heater element and said pitot tube.

Claim 18

The protection apparatus of claim 14 wherein said voltage limiting means comprises: a voltage limiting device connected between said pitot tube and one terminal of said heater element; and an electrical short-circuit connection between the other terminal of said heater element and said pitot tube.