CN102128586B - Angular displacement sensor - Google Patents

Angular displacement sensor Download PDF

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Publication number
CN102128586B
CN102128586B CN 201010590893 CN201010590893A CN102128586B CN 102128586 B CN102128586 B CN 102128586B CN 201010590893 CN201010590893 CN 201010590893 CN 201010590893 A CN201010590893 A CN 201010590893A CN 102128586 B CN102128586 B CN 102128586B
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China
Prior art keywords
angular displacement
magnetic core
stator
input
displacement sensor
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CN102128586A (en
Inventor
雷体高
肖息
黄辉
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AVIC Jincheng Nanjing Engineering Institute of Aircraft Systems
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AVIC Jincheng Nanjing Engineering Institute of Aircraft Systems
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Abstract

The invention relates to an angular displacement sensor belonging to the field of rotary transformers. The angular displacement sensor inputs excitation by arranging an exciting winding to generate a changed magnetic field and the changed magnetic field is input to an input stator. The changed magnetic field is input to a magnetic core of a rotor by the input stator, and then, the rotation angle of the magnetic core of the rotor is output to an output stator armature by the magnetic field change of the magnetic core of the rotor to be transformed into electrical signals to be output, thus the measurement to the angular displacement of the magnetic core of the rotor can be realized. The angular displacement sensor can measure the rotation angle of +/-90 DEG of the magnetic core of the rotor by installing a magnetic circuit. The angular displacement sensor is novel in structure and convenient to process, and can not only realize functions of the angular displacement sensor, but also avoid disadvantages of the traditional structure, such as poor additional technology, low output precision, high installation difficulty, low product passing rate and the like.

Description

A kind of angular displacement sensor
Technical field
The invention belongs to the rotary transformer field, relate to a kind of angular displacement sensor.
Background technology
Existing angular displacement sensor generally can only be suitable for ± and 45 ° with interior occasion, and surpass the angular displacement sensor that ± 45 ° of occasions use and mainly have following deficiency: 1) rotor winding trouble needs input rotor winding and output rotor coil; 2) manufacturability is poor, and rotor winding needs artificial coiling in winding process, phenomenons such as tangent line, short circuit take place easily, and reliability is not high, and qualification rate is also lower; 3) in order to satisfy the properties of product requirement, have only the size that increases product, increase the increase that product size can be brought product weight.
Summary of the invention
The object of the invention: provide a kind of wheel measuring scope to surpass ± 45 ° angular displacement sensor, can realize the feedback of big corner.
Technical scheme of the present invention: a kind of angular displacement sensor; Comprise input stator, field copper, output stator armature, rotor magnetic core, it is characterized in that said rotor magnetic core is the circle ring column with some convex shoulders; It is the full circle ring that circle ring column wherein has a convex shoulder; Other has a convex shoulder band breach, and said field copper is between input stator and output stator armature, near the input stator; Said rotor magnetic core is packed in input stator, field copper, the output stator armature; Coaxial with input stator, field copper, output stator armature, said input stator is positioned at rotor magnetic core full circle ring convex shoulder one end, and said output stator armature is positioned at rotor magnetic core band breach convex shoulder one end.
Said rotor magnetic core band breach one end convex shoulder is a semicircular ring.
Said input stator is the sheet overlaying structure.
Said field copper is the enameled wire coiling.
Said output stator armature is the sheet overlaying structure, and the coiling enameled wire.
Field copper is because the magnetic field that input stimulus changes; The magnetic field that changes is input to the input stator; The input stator is input to rotor magnetic core with the magnetic field that changes; And then the anglec of rotation of rotor magnetic core is outputed to the output stator armature through the rotor magnetic core changes of magnetic field be converted into electric signal output, thereby realize measurement to the rotor magnetic core angular displacement.
Beneficial effect of the present invention: this angular displacement sensor, through a magnetic loop, realized measurement to the rotor magnetic core anglec of rotation, realized the measurement of right ± 90 ° angular displacement.Novel, the easy making process of this angular displacement sensor structure not only can realize the function of existing state-of-the-art technology, and broken through that the additional process property that traditional structure brings is poor, output accuracy is low, installation difficulty is big and shortcoming such as product percent of pass is low.
Description of drawings
Fig. 1 is the principle assumption diagram of this angular displacement sensor, wherein 1 imports stator, 2 field copper, 3 output stator armatures, 4 rotor magnetic cores;
Fig. 2 is the rotor magnetic core structure cut-open view of this angular displacement sensor one preferred embodiments;
Fig. 3 is the rotor magnetic core structure three-dimensional figure of this angular displacement sensor one preferred embodiments.
Embodiment
For better explanation the present invention, specify below in conjunction with accompanying drawing.
See also accompanying drawing 1, a kind of angular displacement sensor comprises input stator 1, field copper 2, output stator armature 3, rotor magnetic core 4.Rotor magnetic core 4 is important component parts of this angular displacement sensor, and it is by magnetic conductive material machine-shaping, and said rotor magnetic core 4 is the circle ring columns with some convex shoulders, and it is the full circle ring that circle ring column wherein has a convex shoulder, and other has a convex shoulder band breach.Said field copper 2 is between input stator 1 and output stator armature 3, and near input stator 1, thereby the magnetic field transmission that realizes field copper 2 is produced is in input stator 1.Said rotor magnetic core 4 is packed in input stator 1, field copper 2, the output stator armature 3; Coaxial with input stator 1, field copper 2, output stator armature 3; Said input stator 1 is positioned at rotor magnetic core 4 full circle ring convex shoulders one end, and said output stator armature 3 is positioned at rotor magnetic core 4 band breach convex shoulders one end.
Said rotor magnetic core 4 band breach one end convex shoulder is a semicircular ring.
Said input stator 1 can be the sheet overlaying structure.
Said field copper 2 can be the enameled wire coiling.
Said output stator armature 3 can be the sheet overlaying structure, and the coiling enameled wire.
Consult Fig. 2~Fig. 3, the annulus that said rotor magnetic core 4 has breach can be semicircular ring.
Field copper 2 is because the magnetic field that input stimulus changes; The magnetic field that changes is input to input stator 1; Input stator 1 is input to rotor magnetic core 4 with the magnetic field that changes; And then the anglec of rotation of rotor magnetic core 4 is outputed to output stator armature 3 through rotor magnetic core 4 changes of magnetic field be converted into electric signal output, thereby realize measurement to the rotor magnetic core angular displacement.

Claims (5)

1. an angular displacement sensor comprises input stator, field copper, output stator armature, rotor magnetic core, it is characterized in that; Said rotor magnetic core is the circle ring column with some convex shoulders, and it is the full circle ring that circle ring column wherein has a convex shoulder, and other has a convex shoulder band breach; Said field copper is between input stator and output stator armature; Near the input stator, said rotor magnetic core is packed in input stator, field copper, the output stator armature, and is coaxial with input stator, field copper, output stator armature; Said input stator is positioned at rotor magnetic core full circle ring convex shoulder one end, and said output stator armature is positioned at rotor magnetic core band breach convex shoulder one end.
2. according to the said angular displacement sensor of claim 1, it is characterized in that said rotor magnetic core band breach one end convex shoulder is a semicircular ring.
3. according to claim 1 or 2 said angular displacement sensors, it is characterized in that said input stator is the sheet overlaying structure.
4. according to claim 1 or 2 said angular displacement sensors, it is characterized in that said field copper is the enameled wire coiling.
5. according to claim 1 or 2 said angular displacement sensors, it is characterized in that said output stator armature is the sheet overlaying structure, and the coiling enameled wire.
CN 201010590893 2010-12-16 2010-12-16 Angular displacement sensor Active CN102128586B (en)

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Application Number Priority Date Filing Date Title
CN 201010590893 CN102128586B (en) 2010-12-16 2010-12-16 Angular displacement sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201010590893 CN102128586B (en) 2010-12-16 2010-12-16 Angular displacement sensor

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CN102128586A CN102128586A (en) 2011-07-20
CN102128586B true CN102128586B (en) 2012-12-26

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2580153C1 (en) * 2014-11-25 2016-04-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method for measurement of turning angle of shaft drive and device therefor

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102588649B (en) * 2011-12-27 2014-09-17 中国航空工业集团公司金城南京机电液压工程研究中心 Servo valve and zero compensation method for same
CN102930966B (en) * 2012-09-21 2015-02-04 谭成忠 Brushless linear rotary transformer
CN104697434A (en) * 2013-12-10 2015-06-10 中国航空工业第六一八研究所 Rotor zero-adjustment structure of double-redundancy angular displacement sensor and adjustment method of rotor zero-adjustment structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5030867A (en) * 1989-08-02 1991-07-09 Technical Associate Co., Ltd. Same polarity induction generator
CN1073555A (en) * 1991-12-18 1993-06-23 株式会社山崎剪切 Magneto-controlled like poles induction generator
CN2567543Y (en) * 2002-09-24 2003-08-20 上海云飞机电自动化研究所 Straight-line/angle displacement sensor
EP1500909A2 (en) * 2003-07-25 2005-01-26 Minebea Co., Ltd. Rotation angle sensor with housing and several resolvers
CN101299048A (en) * 2008-07-04 2008-11-05 嘉兴学院 Rotating angular acceleration sensor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5030867A (en) * 1989-08-02 1991-07-09 Technical Associate Co., Ltd. Same polarity induction generator
CN1073555A (en) * 1991-12-18 1993-06-23 株式会社山崎剪切 Magneto-controlled like poles induction generator
CN2567543Y (en) * 2002-09-24 2003-08-20 上海云飞机电自动化研究所 Straight-line/angle displacement sensor
EP1500909A2 (en) * 2003-07-25 2005-01-26 Minebea Co., Ltd. Rotation angle sensor with housing and several resolvers
CN101299048A (en) * 2008-07-04 2008-11-05 嘉兴学院 Rotating angular acceleration sensor

Non-Patent Citations (1)

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Title
柏受军等.差动变压器式大量程精密角位移传感器的设计.《传感器与微系统》.2006,第25卷(第11期),63-65. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2580153C1 (en) * 2014-11-25 2016-04-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method for measurement of turning angle of shaft drive and device therefor

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