Linear variable differential transformer with multi-range secondary windings for high precision

Patent metadata

Field	Value
Publication number	US-9863787-B2
Application number	US-201514814972-A
Country	US
Kind code	B2
Filing date	Jul 31, 2015
Priority date	Jul 31, 2014
Publication date	Jan 9, 2018
Grant date	Jan 9, 2018

Abstract

A linear variable differential transformer (LVDT) having an electrical stroke includes a probe axially movable along a length of the LVDT electrical stroke, a primary winding extending axially over the length of the LVDT electrical stroke, and a secondary winding extending axially over the length of the LVDT electrical stroke. The LVDT further includes a tertiary winding extending axially over less than the length of the LVDT electrical stroke, the tertiary winding at least partially overlapping with the secondary winding. An advantage of the LVDT in accordance with the present disclosure is that the accuracy of the position calculated from the tertiary winding is greater relative to the total stroke of the LVDT than that calculated from the secondary winding. This is accomplished while still fitting within the envelope of a standard single output LVDT.

First claim

What is claimed is:

1. A linear variable differential transformer (LVDT) having an electrical stroke, comprising:
a probe axially movable along a length of the LVDT electrical stroke;
a primary winding extending axially over the length of the LVDT electrical stroke;
a secondary winding extending axially over the length of the LVDT electrical stroke; and
a tertiary winding extending axially over less than the length of the LVDT electrical stroke, the tertiary winding at least partially overlapping with the secondary winding.

2. The LVDT according to claim 1 , wherein the primary winding, secondary winding, and tertiary winding are concentric.

3. The LVDT according to claim 1 , wherein the primary winding comprises a first number of turns per unit length, the secondary winding comprises a second number of turns per unit length, and the tertiary winding comprises a third number of turns per unit length, the third number of turns per unit length greater than the second number of turns per unit length.

4. The LVDT according to claim 1 , wherein the primary winding comprises a first winding pitch, the secondary winding comprises a second winding pitch, and the tertiary winding comprises a third winding pitch, the third winding pitch being narrower than the second winding pitch.

5. The LVDT according to claim 1 , wherein the secondary winding is a standard-accuracy winding that provides a ratio output over the length of the LVDT, and the tertiary winding is a high-accuracy winding that provides a ratio output for a lesser portion than the length of the LVDT.

6. The LVDT according to claim 1 , wherein the secondary winding is a standard-accuracy winding that provides a ratio output through the full LVDT electrical stroke, and the tertiary winding is a high-accuracy winding that provides a ratio output for a lesser portion of the full LVDT electrical stroke.

7. The LVDT according to claim 6 , wherein when the probe is within the portion of the LVDT electrical stroke where the high-accuracy tertiary winding is disposed, the tertiary winding produces position output function that is subject to less error relative to the stroke of the LVDT than the standard-accuracy secondary winding.

8. The LVDT according to claim 1 , wherein the windings are arranged such that the secondary winding and tertiary winding receive magnetic coupling from the primary winding depending on a position of the probe along the LVDT electrical stroke.

9. The LVDT according to claim 1 , wherein the primary winding surrounds the tertiary winding and the secondary winding surrounds the primary and tertiary windings.

10. The LVDT according to claim 1 , wherein the primary winding surrounds the secondary winding and the tertiary winding surrounds the primary and secondary windings.

11. The LVDT according to claim 1 , wherein the probe is a single probe comprising a single magnetic core.

12. The LVDT according to claim 1 , wherein the probe is a single probe comprising an iron core.

13. The LVDT according to claim 1 , further comprising a spacer arranged adjacent to the tertiary winding.

14. The LVDT according to claim 1 , wherein the secondary winding and the tertiary winding each comprise a tapered winding configuration.

15. The LVDT according to claim 1 , wherein the secondary winding and the tertiary winding each comprise multiple discrete coils.

16. The LVDT according to claim 1 , wherein the secondary winding comprises a first coil part and a second coil part, the first and second coil parts electrically in series.

17. The LVDT according to claim 16 , further including a first terminal connected to one end of the first coil part, a second terminal connected to one end of the second coil part, and a common terminal connected to a second end of each of the first coil part and the second winding part.

18. The LVDT according to claim 1 , wherein the tertiary winding comprises a first coil part and a second coil part, the first and second coil parts electrically in series.

19. The LVDT according to claim 1 , wherein the secondary winding comprises a first secondary output, and the tertiary winding comprises a second secondary output.

20. The LVDT according to claim 1 , wherein the position output of at least one of the secondary winding or the tertiary winding is computed by the ratio A−B/(A+B), where A represents the signal output from a first coil part of the respective winding and B represents the signal output of a second coil part of the respective winding.

21. The LVDT according to claim 1 , wherein an overall position of the LVDT is calculated as a blending of the outputs of the secondary and tertiary winding over a small fraction of the LVDT electrical stroke as the probe transitions from a region where only the secondary winding is disposed to a region where both the secondary and tertiary winding are disposed.

22. An aircraft, comprising:
a flight control surface arranged on the aircraft; and
the LVDT according to claim 1 operatively coupled to the flight control surface.

23. The aircraft according to claim 22 , further comprising a flight controller for controlling a position of the flight control surface, the flight controller including a first output for controlling a position of the flight control surface, first input operatively coupled to the secondary winding, and a second input operatively coupled to the tertiary winding, the controller configured to control the position of the flight control surface based on a position feedback signal provided by the secondary and tertiary windings.

24. The LVDT according to claim 1 , wherein the electrical stroke is defined by a longitudinal span of the primary winding and the secondary winding over which the probe travels, and wherein the primary and secondary windings extend axially over the entire longitudinal span.

Assignees

• Parker Hannifin Corp
• Parker Hannifin Corp

Inventors

• Hubbell Lawrence Alden

Classifications

• G01D5/2291 Primary

  Linear or rotary variable differential transformers (LVDTs/RVDTs) having a single primary coil and two secondary coils · CPC title