Wide-range linear displacement sensor winding structure

By designing a new linear displacement sensor winding structure, including uniformly segmented output winding, the problem of product volume and weight increase in the prior art is solved, and the effect of improving sensitivity and output linearity is achieved, while improving production efficiency and reliability.

CN119803254APending Publication Date: 2025-04-11BEIJING SHUGUANG AERO ELECTRICAL
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Patent Information

Application Number
CN202411897787.6
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-12-23
Publication Date
2025-04-11

AI Technical Summary

Technical Problem

While existing large number of range line displacement sensor windings increase sensitivity and output linearity, the product volume and weight increase, and the production efficiency and reliability are low.

Method used

A new type of winding structure is designed, including one layer of excitation winding and two layers of output windings A and B. The output winding is evenly segmented from the center to both ends, and the density of the winding turns on each section is controlled to increase in equal amounts.

Benefits of technology

The winding structure improves sensitivity and output linearity, reduces the number of winding layers and winding space requirements, reduces product volume and weight, and improves production efficiency and reliability.

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Abstract

The invention discloses a wide-range linear displacement sensor winding structure, and belongs to the technical field of linear displacement sensors. Comprising a winding framework (1), an exciting winding (2), an output winding A (3) and an output winding B (4), the output windings are divided into an output winding A3 and an output winding B4, the two output windings are uniformly segmented from the center to the two ends, and the density of the number of turns of the windings on each segment is controlled to be equivalently and progressively increased. Through the winding structure, the sensitivity (slope) can be improved, the output linearity can be improved, and the winding efficiency of the winding can be improved. The number of winding layers is reduced, the winding space requirement is reduced, the volume and the weight of the product can be further compressed, the reliability is high, and the structure is more suitable for aviation equipment products.
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Description

Technical Field

[0001] The invention discloses a large-range linear displacement sensor winding structure, belonging to the technical field of linear displacement sensors. Background Art

[0002] The winding of the linear displacement sensor includes an excitation winding and two output windings. In order to improve the sensitivity (slope) requirements of the large-range linear displacement sensor, it is necessary to significantly increase the number of output winding layers, which correspondingly requires more winding space, increases the volume and weight of the product, and has low production efficiency and reliability. Summary of the invention

[0003] The purpose of the present invention is to design a new type of large-range linear displacement sensor winding structure, a layer of excitation winding, a layer of output winding, the output winding is divided into output winding A3 and output winding B4, the two output windings are evenly segmented from the center to the two ends, and the density of the number of winding turns on each segment is controlled to increase by an equal amount. The winding structure can improve the sensitivity (slope), improve the output linearity, and enhance the winding efficiency.

[0004] The technical solution of the present invention is: a winding structure of a large-range linear displacement sensor, comprising a winding skeleton 1, an excitation winding 2, an output winding A3 and an output winding B4; a layer of the excitation winding 2 is evenly and densely wound in the winding space of the winding skeleton 1, and the winding space of the winding skeleton 1 is divided into two sections, one section is the output winding A3, and the other section is the output winding B4, the output winding A3 and the output winding B4 are on the surface of the excitation winding 2, wherein the output winding A3 and the output winding B4 are evenly segmented from the middle to the two ends, and the density of the number of winding turns on each section is controlled to increase by an equal amount.

[0005] The winding frame 1 is a hollow cylindrical structure with baffles at both ends to provide winding space.

[0006] The material used for the winding frame 1 is non-magnetic stainless steel.

[0007] The enameled wires used for the excitation winding 2, the output winding A3 and the output winding B4 are self-adhesive wires.

[0008] The winding spaces of the output winding A3 and the output winding B4 are divided into N sections of equal length, where N≥3.

[0009] Each winding section of the output winding A3 and the output winding B4 is evenly arranged, and the number of turns of each winding section increases exponentially.

[0010] The density of the number of turns of the output winding A3 and the output winding B4 increases by an equal amount from the center to the two ends, and the density change is set by programming the automatic winding machine.

[0011] The density of the number of turns of the output winding A3 and the output winding B4 increases equally from the center to the two ends, and this is achieved by controlling the density change of the windings using a semi-automatic winding machine using a multi-wire parallel winding method.

[0012] The beneficial effects of the present invention are as follows: the two output windings are evenly segmented from the center to the two ends, and the density of the winding turns on each segment is controlled to increase by an equal amount. When the mover core moves from the center to the two ends, the difference in the number of induced turns increases stepwise, thereby achieving the purpose of improving sensitivity (slope) and improving output linearity. In addition, the number of winding layers is reduced, the winding space requirement is reduced, the product volume and weight can be further compressed, the reliability is high, and it is more suitable for aviation equipment products. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the winding structure of the large-range linear displacement sensor of the present invention;

[0014] Among them: 1-winding frame, 2-excitation winding, 3-output winding A, 4-output winding B DETAILED DESCRIPTION

[0015] The present invention is further described in detail below. In the following detailed description, many specific details are provided to provide a comprehensive understanding of the present invention. However, it is obvious to those skilled in the art that the present invention can also be implemented without these specific details. The following description of the embodiments is only for the purpose of providing a better understanding by illustrating examples of the present invention. The present invention is not limited to any specific settings and methods provided below, but covers all product structures, any improvements, replacements, etc. of methods covered without departing from the spirit of the present invention.

[0016] A large-range linear displacement sensor winding structure comprises: a winding frame 1, an excitation winding 2, an output winding A3 and an output winding B4; a layer of the excitation winding 2 is evenly and densely wound in the winding space of the winding frame 1, and the winding space of the winding frame 1 is divided into two sections, one section is the output winding A3, and the other section is the output winding B4, and the output winding A3 and the output winding B4 are on the surface of the excitation winding 2, wherein the output winding A3 and the output winding B4 are evenly divided into sections from the middle to the two ends, and the density of the number of winding turns on each section is controlled to increase by an equal amount.

[0017] The winding frame 1 is a hollow cylindrical structure with baffles at both ends to provide winding space.

[0018] The material used for the winding frame 1 is non-magnetic stainless steel.

[0019] The enameled wires used for the excitation winding 2, the output winding A3 and the output winding B4 are self-adhesive wires.

[0020] The winding spaces of the output winding A3 and the output winding B4 are divided into N sections of equal length, where N≥3.

[0021] Each section of the output winding A3 and the output winding B4 is evenly arranged, and the number of turns of each section increases exponentially. The density of the number of turns of each section of the output winding A3 and the output winding B4 increases by an equal amount from the center to the two ends, which is achieved by programming the density change of the automatic winding machine.

[0022] The density of the number of turns of the output winding A3 and the output winding B4 increases from the center to the two ends in an equal amount, and the semi-automatic winding machine uses a multi-wire parallel winding method to control the change in the density of the winding. Figure 1 The schematic diagram of the winding structure of the large-range linear displacement sensor of the present invention is shown in Figure 1. Taking a certain type of linear displacement sensor as an example, a layer of excitation winding 108mm is evenly and densely wound on the winding frame, with a total of 984 turns. Output winding 3 and output winding 4 are symmetrically wound above the excitation winding. Output winding 3 and output winding 4 are each divided into 3 sections, where a1=a2=a3=b1=b2=b3=18mm, a1 and b1 sections have 41 turns, a2 and b2 sections have 82 turns, and a3 and b3 sections have 164 turns.

Claims

1. A large-range linear displacement sensor winding structure, characterized in that: The invention comprises a winding frame (1), an exciting winding (2), an output winding A (3) and an output winding B (4); a layer of the exciting winding (2) is evenly and densely wound in the winding space of the winding frame (1); the winding space of the winding frame (1) is divided into two sections, one section is the output winding A (3), and the other section is the output winding B (4); the output winding A (3) and the output winding B (4) are on the surface of the exciting winding (2); the output winding A (3) and the output winding B (4) are evenly divided into sections from the middle to the two ends, and the density of the number of turns of the winding on each section is controlled to increase by an equal amount.

2. The large-range linear displacement sensor winding structure according to claim 1 is characterized in that: The winding frame (1) is a hollow cylindrical structure with baffles at both ends to provide winding space.

3. The winding structure of the large-range linear displacement sensor according to claim 1 is characterized in that: The material used for the winding frame (1) is non-magnetic stainless steel.

4. The large-range linear displacement sensor winding structure according to claim 1 is characterized in that: The enameled wires used for the excitation winding (2), the output winding A (3) and the output winding B (4) are self-adhesive wires.

5. The large-range linear displacement sensor winding structure according to claim 1 is characterized in that: The winding spaces of the output winding A (3) and the output winding B (4) are divided into N sections of equal length, where N ≥ 3.

6. The large-range linear displacement sensor winding structure according to claim 5 is characterized in that: Each winding section of the output winding A (3) and the output winding B (4) is evenly arranged, and the number of turns of each winding section increases exponentially.

7. The large-range linear displacement sensor winding structure according to claim 6 is characterized in that: The density of the number of turns of the output winding A (3) and the output winding B (4) increases uniformly from the center to the two ends in each section by programming the density change of the automatic winding machine.

8. The large-range linear displacement sensor winding structure according to claim 6, characterized in that: The density of the number of turns of the output winding A (3) and the output winding B (4) increases uniformly from the center to the two ends in each section by controlling the density change of the winding by a semi-automatic winding machine using a multi-wire parallel winding method.

Citation Information

Patent Citations

  • Linear variable displacement transformer (LVDT) with improved linearity using extreme end booster winding

    US20170352464A1

  • Displacement sensor

    WO2008087880A1