Ground fault detection and measurement system for airfield lighting system

• US 5,638,057 A
• Filed: 05/09/1994
• Issued: 06/10/1997
• Est. Priority Date: 05/09/1994
• Status: Expired due to Fees

• Current Assignee: Adb-Alnaco Incorporated
• Original Assignee: Adb-Alnaco Incorporated
• Inventors: Williams, Harold R.
• Primary Examiner(s): Hofsass, Jeffery
• Assistant Examiner(s): Lee, Benjamin C.
• Application Number:
  US08/239,478
• Time in Patent Office: 1,128 Days
• Field of Search: 340/953, 340/947, 340/642, 340/931, 315/130, 315/125, 315/126, 324/500, 324/509, 324/512
• US Class Current: 340/947
• CPC Class Codes: H05B 47/235 with communication between the lamps and a central unit

Abstract

The present invention includes an airfield lighting and control system for energizing at least one airfield control device and containing a ground fault detection system, comprising: (1) at least one airfield control device; (2) an AC electrical circuit conducting an AC signal and connected to said at least one airfield control device; (3) an inductive device, in electrical contact with said AC electrical circuit, which comprises (a) an inductive coil having an input pole and an output pole, and being loaded by a capacitor; (b) a driver winding for the inductive coil, the driver winding adapted to sense AC current flow through the inductor coil; (c) a sampling resistor connected to the driver winding and adapted to detect AC current in the form of a voltage across the sampling resistor; (d) signal processing circuitry comprising: (1) an inverting amplifier adapted to amplify the voltage; and (2) a phase shifter adapted to shift the phase of the voltage; and (e) a power amplifier connected to the signal processing circuitry and to the driver winding.

Claims

1. An airfield lighting system including a ground fault detection system, comprising:

a. at least one airfield control device;

b. an AC electrical circuit adapted to conduct an AC signal and connected to said at least one airfield control device;

c. an inductive device in electrical contact with said AC electrical circuit, said inductive device comprising;

i. an inductive coil having an input pole and an output pole, said inductive coil having a capacitor connected to said output pole so as to load said inductive coil, said input pole connected to said AC electrical circuit so as to receive said AC signal and provide AC current flow through said inductive coil;

ii. a driver winding, having a pair of terminals, coupled to said inductive coil so as to sense said AC current flow through said inductor coil;

iii. a sampling resistor connected to one of said driver winding terminals so as to detect said AC current flow in the form of a voltage across said sampling resistor;

iv. signal processing circuitry comprising;

(1) an inverting amplifier coupled to said sampling resistor so as to amplify said voltage; and

(2) a phase shifter coupled to said inverting amplifier so as to shift the phase of said voltage; and

v. a power amplifier coupled to said signal processing circuitry and also coupled to the other of said driver winding terminals;

d. a DC voltage source connected to said output pole of said inductive coil; and

e. a DC current measuring device adapted to measure DC current flowing to said circuit from said DC voltage source so as to determine the presence of a ground fault condition in said circuit.

2. An airfield lighting system according to claim 1 additionally comprising a corrective feedback device that is coupled to said signal processing circuitry and to said DC current measuring device, whereby a resultant voltage is obtained from a corrective feedback voltage across said corrective feedback device and from said voltage across said sampling resistor and applied to said signal processing circuitry whereby DC bias occurring in said inductor coil is compensated.

3. An airfield lighting system according to claim 1 wherein said DC voltage source is adapted to produce at least two voltage levels.

4. An airfield lighting system according to claim 1 wherein said DC voltage source is adapted to produce voltage levels of about 50 and about 500 volts.

5. An AC electrical circuit for use in an airfield lighting system, said AC electrical circuit having an inductive device comprising:

a. an inductive coil having an input pole and an output pole, said inductive coil having a capacitor connected to said output pole so as to load said inductive coil, said input pole adapted to connect to an AC electrical circuit so as to receive an AC signal therefrom and thereby provide AC current flow through said inductive coil;

b. a driver winding, having a pair of terminals, coupled to said inductive coil so as to sense said AC current flow through said inductor coil;

c. a sampling resistor connected to one of said driver winding terminals so as to detect said AC current flow in the form of a voltage across said sampling resistor;

d. signal processing circuitry comprising;

i. an inverting amplifier coupled to said sampling resistor so as to amplify said voltage; and

ii. a phase shifter coupled to said inverting amplifier so as to shift the phase of said voltage; and

e. a power amplifier coupled to said signal processing circuitry and also coupled to the other of said driver winding terminals.

6. An AC electrical circuit according to claim 5 additionally comprising a corrective feedback device that is coupled to said signal processing circuitry, whereby a resultant voltage is obtained from a corrective feedback voltage across said corrective feedback device and from said voltage across said sampling resistor and applied to said signal processing circuitry whereby DC bias occurring in said inductor coil is compensated.

7. An AC electrical circuit including ground fault detection circuitry for use in an airport lighting system, said circuit comprising:

a. at least one electric light;

b. an AC electrical circuit conducting an AC signal and connected to said at least one electric light;

c. an inductive device in electrical contact with said AC electrical circuit, said inductive device comprising;

i. an inductive coil having an input pole and an output pole, said inductive coil having a capacitor connected to said output pole so as to load said inductive coil, said input pole connected to said AC electrical circuit so as to receive said AC signal and provide AC signal flow through said inductive coil;

ii. a driver winding, having a pair of terminals, coupled to said inductive coil so as to sense said AC current flow through said inductor coil;

iii. a sampling resistor connected to one of said driver winding terminals so as to detect said AC current flow in the form of a voltage across said sampling resistor; and

iv. signal processing circuitry comprising;

(1) an inverting amplifier coupled to said sampling resistor so as to amplify said voltage; and

(2) a phase shifter coupled to said inverting amplifier so as to shift the phase of said voltage; and

d. a power amplifier coupled to said signal processing circuitry and also coupled to the other of said driver winding terminals;

e. a DC voltage source connected to said output pole of said inductive coil; and

f. a DC current measuring device adapted to measure DC current flowing to said circuit from said DC voltage source so as to determine the presence of a ground fault condition in said circuit.

8. An AC electrical circuit according to claim 7 additionally comprising a corrective feedback device that is coupled to said signal processing circuitry and to said DC current measuring device, whereby a resultant voltage is obtained from a corrective feedback voltage across said corrective feedback device and from said voltage across said sampling resistor and applied to said signal processing circuitry whereby DC bias occurring in said inductor coil is compensated.