Linear position sensing system and coil switching methods for closed-loop control of large linear induction motor systems

• US 6,952,086 B1
• Filed: 10/10/2003
• Issued: 10/04/2005
• Est. Priority Date: 10/10/2003
• Status: Active Grant

• Current Assignee: Curtiss-Wright Electro-Mechanical Corporation (Curtiss-Wright Corporation)
• Original Assignee: Curtiss-Wright Electro-Mechanical Corporation (Curtiss-Wright Corporation)
• Inventors: Eichler, Kenneth Martin, Brennen, Michael Barnaby, Wu, Jiing-Liang, Strickler, Robert E., Hall, David Jonathan, Krefta, Mark Peter
• Primary Examiner(s): Schuberg, Darren
• Assistant Examiner(s): JONES, JUDSON
• Application Number:
  US10/683,964
• Time in Patent Office: 725 Days
• Field of Search: 310 12- 14
• US Class Current: 318/135
• CPC Class Codes: H02K 17/30 Structural association of asynchronous induction motors with auxiliary electric devices influencing the characteristics of the motor or controlling the motor, e.g. with impedances or switches
• CPC Class Codes: H02K 41/025 Asynchronous motors
• CPC Class Codes: H02P 25/06 Linear motors
• CPC Class Codes: H02P 25/062 of the induction type

Abstract

A control system for a linear motor adapted to accurately supply a moving window of power to the stator coils. A plurality of individually switched stator coils run the length of a linear motor to move a rotor down the long axis of the stator. Accurate inductive-based position sensors continuously provide position data for the moving rotor. A processing unit calculates a proper time delay from a source voltage peak in order to apply power to the next stator coil in the moving direction of the rotor such that no DC offshoot/undershoot occurs. The linear motor control system optionally includes a failure prevention switching scheme in which pairs of individual stator coils on opposite sides of a double-sided stator are switched together.

Claims

1. A linear motor control system, comprising:

a stator including a plurality of individually switched stator coils;

a moving rotor adapted to move down a long axis of the stator;

an inductive-based position sensing system with first components attached to said rotor and second components attached to said stator;

calculation means for determining, based on sensed position data, a proper voltage time delay angle with respect to a voltage source peak voltage for applying current to a next leading coil of said stator coils such that the current in said next coil is at its steady state value immediately after switching.

2. The linear motor control system of claim 1, wherein said first components include a one-phase tape scale.

3. The linear motor control system of claim 2, wherein said second components include a two-phase bar scale.

4. The linear motor control system of claim 3, wherein said one-phase tape scale is loosely coupled to said moving rotor.

5. The linear motor control system of claim 4, wherein the position sensing system maintains no more than a 15% distance tolerance between the one-phase tape scale coupled to the moving rotor and the two-phase bar scale coupled to the stator as the one-phase tape scale moves past the two-phase bar scale down the long axis of the stator.

6. The linear motor control system of claim 1, wherein said position sensing system further includes a plurality of Hall-effect sensors for absolute positioning.

7. The linear motor control system of claim 1, further comprising:

a plurality of temperature sensors located down the long axis of the stator to sense local operating temperatures.

8. The linear motor control system of claim 1, wherein the stator is double-sided, with independently switched stator coils on each side.

9. The linear motor control system of claim 8, wherein individually switched stator coils are turned on and off in pairs, with a single switch turning on a pair of coils, one on each side of the double-sided stator.

10. The linear motor control system of claim 1, wherein said calculation means determines the voltage time delay angle with respect to the voltage source peak voltage based on the flux linkage of said next leading coil before said switching.

11. The linear motor control system of claim 1, wherein said calculation means includes a processing unit with a digital signal processor to calculate the voltage time delay angle with respect to the voltage source peak voltage.

12. The linear motor control system of claim 11, wherein said calculation means includes a coil switch controller for providing commands for the individually switched coils to turn on and off.

13. A method for controlling the application of power to a series of stator coils in a linear motor, comprising the steps of:

sensing the instantaneous position of a moving rotor with respect to the stationary stator coils using an inductive sensor;

calculating, based on the sensed rotor position, a source voltage phase shift for a next one of said stator coils in the moving direction of the rotor that results in a current in the next one of said stator coils moving immediately to a steady state value;

applying source voltage to said next stator coil at said calculated phase shift.

14. The method of claim 13, further comprising the step of:

removing an applied source voltage from a previous stator coil that is located behind the moving direction of the rotor.

15. The method of claim 13, wherein said inductive sensor is a two-piece inductive-type sensor and a series of Hall-effect sensors.

16. The method of claim 15, wherein said inductive-type sensor includes a one-phase tape scale loosely coupled to said rotor.

17. The method of claim 16, wherein said inductive-type sensor includes a two-phase bar scale attached to said stator.

18. The method of claim 13, wherein said stator is a double-sided stator, and in said applying step, the voltage is applied to a pair of individual stator coils, one on each side of the double-sided stator at the same time.

19. The method of claim 13, wherein said calculation step is based on the flux linkage of said next coil before said applying step.

20. An electromagnetic aircraft launching system, comprising:

a double-sided stator assembly including a plurality of individually switched stator coils;

a moving rotor assembly adapted to move down a long axis of the stator and further adapted to engage an aircraft;

an inductive-based position sensing system with first components loosely coupled to said rotor assembly and second components attached to said stator assembly;

a processing unit including a digital signal processor for determining, based on sensed position data, a proper voltage time delay angle with respect to a voltage source peak voltage for applying current to a next leading coil of said stator coils such that a DC offset component of the current supplied to said next leading coil is removed.