Testing an inductive load of a device using a modulated signal

• US 20100259274A1
• Filed: 05/31/2007
• Published: 10/14/2010
• Est. Priority Date: 05/31/2007
• Status: Active Grant

• Current Assignee: Woodward HRT Incorporated (Woodward Incorporated)
• Original Assignee: HR Textron, Inc.
• Inventors: Chung, Estella C., Lee, Joon, Liu, Raymond Y.
• Granted Patent: US 7,956,619 B2
• Time in Patent Office: Days
• US Class Current: 324/502
• CPC Class Codes: G01R 31/34 Testing dynamo-electric machines
• CPC Class Codes: G01R 31/346 Testing of armature or field windings

Abstract

A device has built-in inductive load testing capabilities. The device includes a device housing, an inductive load disposed within the device housing; and test circuitry disposed within the device housing. The test circuitry is constructed and arranged to effectuate application of a modulated test signal to the inductive load, and obtain a result signal in response to the application of the modulated test signal to the inductive load. The test circuitry is further constructed and arranged to generate an output signal indicating that the inductive load is in one of (i) a shorted inductive load state, (ii) a normal inductive load state, and (iii) an abnormally high inductive load state, based on the result signal. Such test circuitry is well-suited for testing a variety of devices having inductors/coils which are susceptible to defects (e.g., a solenoid, a motor winding, various actuator components, etc.).

Claims

1. A method for testing an inductive load of a device, the method comprising:

effectuating application of a modulated test signal to the inductive load of the device;

obtaining a result signal in response to the application of the modulated test signal to the inductive load of the device; and

based on the result signal, generating an output signal indicating that the inductive load of the device is in one of (i) a shorted inductive load state, (ii) a normal inductive load state, and (iii) an abnormally high inductive load state.

2. A method as in claim 1 wherein the device is a guidable projectile;

wherein the inductive load is a motor winding involved in steering the guidable projectile while the guidable projectile is in flight; and

wherein effectuating application of the modulated test signal to the inductive load of the device includes driving a switching circuit, which is disposed between the motor winding and a power rail, with a pulse width modulated control signal to apply the modulated test signal from the power rail to the motor winding involved in steering the guidable projectile.

3. A method as in claim 1 wherein the device is a guidable projectile;

and

wherein the method further comprises enabling launch of the guidable projectile when the output signal indicates that the inductive load of the device is in the normal inductive load state, and disabling launch of the guidable projectile when the output indicates that the inductive load is in either of (i) the shorted inductive load state, and (ii) the abnormally high inductive load state.

4. A method as in claim 1 wherein obtaining the result signal includes acquiring, as the result signal, (i) a first voltage when the inductive load is in the shorted inductive load state, (ii) a second voltage when the inductive load is in the normal inductive load state, and (iii) a third voltage when the inductive load is the abnormally high inductive load state;

wherein the absolute value of the second voltage is greater than the absolute value of the first voltage; and

wherein the absolute value of the third voltage is greater than the absolute value of the second voltage.

5. A device, comprising:

a device housing;

an inductive load disposed within the device housing;

test circuitry disposed within the device housing, the test circuitry being constructed and arranged to;

effectuate application of a modulated test signal to the inductive load,

obtain a result signal in response to the application of the modulated test signal to the inductive load, and

generate an output signal indicating that the inductive load is in one of (i) a shorted inductive load state, (ii) a normal inductive load state, and (iii) an abnormally high inductive load state, based on the result signal.

6. A device as in claim 5 wherein the device is a guidable projectile;

wherein the inductive load is a motor winding involved in steering the guidable projectile while the guidable projectile is in flight; and

wherein the test circuitry includes a switching circuit and a controller, the switching circuit being disposed between the motor winding and a power rail, the controller being constructed and arranged to drive the switching circuit with a pulse width modulated control signal to direct the switching circuit to apply the modulated test signal from the power rail to the motor winding involved in steering the guidable projectile.

7. A device as in claim 6 wherein the controller of the test circuitry includes a pulse width modulator which is constructed and arranged to provide the pulse width modulated control signal with a predefined duty cycle and a predefined modulating frequency.

8. A device as in claim 7, further comprising

a capacitor which is constructed and arranged to stabilize a rail voltage between the power rail and a ground reference during application of the modulated test signal from the power rail to the motor winding involved in steering the guidable projectile.

9. A device as in claim 7 wherein the controller of the test circuitry further includes an analog-to-digital converter having (i) an input which is constructed and arranged to obtain the result signal by inputting an analog signal from the power rail, and (ii) an output which is constructed and arranged to provide the output signal by outputting a digital value indicating which state the inductive load is in.

10. A device as in claim 9, further comprising:

steering circuitry which is constructed and arranged to steer the guidable projectile housing while the guidable projectile housing is in flight; and

wherein the test circuitry further includes switching circuitry which is constructed and arranged to isolate the motor winding from the steering circuitry while the analog-to-digital converter outputs the digital value indicating which state the inductive load is in.

11. A device as in claim 5 wherein the device is a guidable projectile;

and

wherein the test circuitry is further constructed and arranged to enable launch of the guidable projectile when the output signal indicates that the inductive load is in the normal inductive load state, and disable launch of the guidable projectile when the output indicates that the inductive load is in either of (i) the shorted inductive load state, and (ii) the abnormally high inductive load state.

12. A device as in claim 5 wherein the test circuitry, when obtaining the result signal, is constructed and arranged to acquire, as the result signal, (i) a first voltage when the inductive load is in the shorted inductive load state, (ii) a second voltage when the inductive load is in the normal inductive load state, and (iii) a third voltage when the inductive load is the abnormally high inductive load state;

wherein the absolute value of the second voltage is greater than the absolute value of the first voltage; and

wherein the absolute value of the third voltage is greater than the absolute value of the second voltage.

13. A guidable projectile deployment system, comprising:

a support platform;

a command interface supported by the support platform; and

a guidable projectile supported by the support platform, the guidable projectile having a housing, an inductive load disposed within the housing, and test circuitry disposed within the housing, the test circuitry being constructed and arranged to;

effectuate application of a modulated test signal to the inductive load in response to a command from the command interface,

obtain a result signal in response to the application of the modulated test signal to the inductive load, and

generate an output signal and provide the output signal to the command interface, the output signal indicating that the inductive load is in one of (i) a shorted inductive load state, (ii) a normal inductive load state, and (iii) an abnormally high inductive load state, based on the result signal.

14. A guidable projectile deployment system as in claim 13 wherein the inductive load is a motor winding involved in steering the guidable projectile while the guidable projectile is in flight;

and

wherein the test circuitry includes a switching circuit and a controller, the switching circuit being disposed between the motor winding and a power rail, the controller being constructed and arranged to drive the switching circuit with a pulse width modulated control signal to direct the switching circuit to apply the modulated test signal from the power rail to the motor winding involved in steering the guidable projectile.

15. A guidable projectile deployment system as in claim 14 wherein the controller of the test circuitry includes a pulse width modulator which is constructed and arranged to provide the pulse width modulated control signal with a predefined duty cycle and a predefined modulating frequency.

16. A guidable projectile deployment system as in claim 15, further comprising:

a capacitor which is constructed and arranged to stabilize a rail voltage between the power rail and a ground reference during application of the modulated test signal from the power rail to the motor winding involved in steering the guidable projectile.

17. A guidable projectile deployment system as in claim 15 wherein the controller of the test circuitry further includes an analog-to-digital converter having (i) an input which is constructed and arranged to obtain the result signal by measuring a voltage from the power rail, and (ii) an output which is constructed and arranged to provide the output signal by outputting a digital value indicating which state the inductive load is in.

18. A guidable projectile deployment system as in claim 17, further comprising:

steering circuitry which is constructed and arranged to steer the guidable projectile housing while the guidable projectile housing is in flight; and

wherein the test circuitry further includes switching circuitry which is constructed and arranged to isolate the motor winding from the steering circuitry while the analog-to-digital converter outputs the digital value indicating which state the inductive load is in.

19. A guidable projectile deployment system as in claim 13 wherein the test circuitry is further constructed and arranged to enable launch of the guidable projectile when the output signal indicates that the inductive load is in the normal inductive load state, and disable launch of the guidable projectile when the output indicates that the inductive load is in either of (i) the shorted inductive load state, and (ii) the abnormally high inductive load state.

20. A guidable projectile deployment system as in claim 13 wherein the test circuitry, when obtaining the result signal, is constructed and arranged to acquire, as the result signal, (i) a first voltage when the inductive load is in the shorted inductive load state, (ii) a second voltage when the inductive load is in the normal inductive load state, and (iii) a third voltage when the inductive load is the abnormally high inductive load state;

wherein the absolute value of the second voltage is greater than the absolute value of the first voltage; and

wherein the absolute value of the third voltage is greater than the absolute value of the second