CN202126242U - Circular induction synchronizer - Google Patents

Circular induction synchronizer Download PDF

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Publication number
CN202126242U
CN202126242U CN2010206796233U CN201020679623U CN202126242U CN 202126242 U CN202126242 U CN 202126242U CN 2010206796233 U CN2010206796233 U CN 2010206796233U CN 201020679623 U CN201020679623 U CN 201020679623U CN 202126242 U CN202126242 U CN 202126242U
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China
Prior art keywords
rotor
conductor
stator
winding
metallic conductor
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Expired - Fee Related
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CN2010206796233U
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Chinese (zh)
Inventor
汤文军
娄敏
王智勇
郑宇�
林兴颜
李丰
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Jiujiang Precision Measuring Technology Research Institute
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Jiujiang Precision Measuring Technology Research Institute
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Abstract

The utility model relates to a circular induction synchronizer, which comprises a stator base plate and a rotor base plate. The stator base plate is provided with a stator metallic conductor area, and the stator metallic conductor area is provided with a winding. The rotor base plate is provided with a rotor metallic conductor area, and the rotor metallic conductor area is provided with a winding. The rotor conductor winding is provided with a shielding layer, and an insulation layer is added between winding of the rotor metallic conductor area and the shielding layer. Therefore, coupling capacitance of the circular induction synchronizer is eliminated, and the effect of improving accuracy of products is achieved. The circular induction synchronizer has the advantages of being high in accuracy and reliability and especially suitable to work in vacuum environment.

Description

A kind of round induction synchrometer
Technical field
The utility model relates to a kind of round induction synchrometer, particularly a kind of space circle inductosyn that can be applicable to vacuum environment.
Background technology
Round induction synchrometer is a kind of electromagnetic induction position detecting element; It has adverse environment resistant; Measuring accuracy is high, the life-span is long, cost is low, easy for installation, travelling speed is fast, series of advantages such as reliable and stable, be usually used in the equipment such as turntable, gyropanel, cannon control, navigational guidance, radar antenna, transit.Round induction synchrometer is divided into stator and rotor two parts; Wherein stator is installed on the fixed body, and rotor is installed in the rotating shaft, and rotor is applied pumping signal; Stator will induce two phases just, cosine signal; Course of work shaft drives rotor makes itself and stator produce relative rotary motion, stator induce two mutually just, cosine signal also can take place along with the rotation of rotor clocklike to change, through monitoring, resolve the purpose that this two paths of signals is realized measurement of angle.
Cover a mylar on the conductor group of the rotor surface of traditional round induction synchrometer as insulation course; On this insulation course, cover an aluminium foil subsequently again as screen layer; This screen layer is connected with the metallic matrix of rotor; This technological measure can play the elimination coupling capacitance, improves the effect of synchronizer precision.
High precision, high reliability in view of round induction synchrometer; Each military and civilian field is widely-used at home for this product; But formally use as yet in the space field of China's most significant end, it has air in twos between interlayer when covering successively to study carefully its main cause and be mylar and aluminium foil on the rotor surface conductor group, and this makes under space environment; Air between interlayer can make mylar and aluminium foil outwards bloat; And the spacing of stator and rotor is very little (about 0.15mm) in the synchronizer installation process, thereby makes stator and rotor touch each other owing to mylar and aluminium foil outwards bloat, and causes product to work.
The utility model content
Its purpose of the utility model just is a kind of round induction synchrometer is provided, and has the characteristics of high precision, high reliability, is particularly suitable under vacuum environment, working.
The technical scheme that realizes above-mentioned purpose and take comprises stator substrate, rotor substrate, and described stator substrate is provided with stator metallic conductor zone, and stator metallic conductor zone is provided with winding; Described rotor substrate is provided with rotor metallic conductor zone, and rotor metallic conductor zone is provided with winding, and described rotor conductor winding is provided with screen layer, and is increasing insulation course between winding and the screen layer on the rotor metallic conductor zone.
Compared with prior art; The beneficial effect of the utility model is that the utility model has adopted the structural design of winding layers, insulation course and the screen layer seamless link of rotor surface, and there is not air in its layer with interlayer; Thereby make rotor the phenomenon of top layer bubbling under vacuum environment, can not occur; Thereby can operate as normal, have the characteristics of high precision, high reliability, be particularly suitable under vacuum environment, working.
Description of drawings
Below in conjunction with accompanying drawing the utility model is done further to detail.
Fig. 1 is a synchronizer side-looking structural representation.
Fig. 2 be among Fig. 1 A to the structure for amplifying synoptic diagram.
Fig. 3 is a rotor winding synoptic diagram.
Fig. 4 is the stator winding synoptic diagram.
Fig. 5 is stator and rotor active conductor relative position figure.
Fig. 6 is stator and rotor active conductor relative position figure.
Fig. 7 is stator and rotor active conductor relative position figure.
Fig. 8 is stator and rotor active conductor relative position figure.
Fig. 9 turns over a Machine cycle for the rotor relative stator, and stator voltage output signal amplitude changes synoptic diagram.
Embodiment
Embodiment comprises stator substrate 1, rotor substrate 2, and is as shown in Figure 1, and described substrate 1 is provided with stator metallic conductor zone 3, and stator metallic conductor zone 3 is provided with winding; Described rotor substrate 2 is provided with rotor metallic conductor zone 4, and rotor metallic conductor zone 4 is provided with winding, and described rotor conductor winding 4 is provided with screen layer 6, and is increasing insulation course 5 between winding and the screen layer 6 on the rotor metallic conductor zone 4.
Described insulation course 5 is an epoxide resin material, and insulation course 5 flatnesses are less than 0.01mm.
Described insulation course 6 plated films, Coating Materials is a conductive material, like, aluminium, copper, silver or its alloy material.
Winding on the described rotor metallic conductor zone 4 is a continous way, comprises many active conductors 7 being formed by connecting through conductor inner end 8 and conductor outer end 9 that the radical of conductor is identical with the number of poles of synchronizer.
Winding on the described stator metallic conductor zone 3 is a sectional type, is called the segmentation winding, comprises 2K conductor group; The conductor group belong to respectively A mutually with B mutually; Every all have K conductor group mutually, and every group is formed by connecting through conductor inner end 11 and conductor outer end 12 M root active conductor 10, and wherein K, M are positive integer; Belong to each group of homophase, connect with the lead differential concatenation.The stator and rotor active conductor all radially.
Described stator active conductor 13, rotor active conductor 14 are radially.
Below in conjunction with accompanying drawing the embodiment of the utility model is described.
The round induction synchrometer that constitutes by aluminium base, metallic conductor winding etc.; Traditional handicraft all needs on the conductor group of the rotor surface of round induction synchrometer, to cover a mylar as insulation course; On this insulation course, cover an aluminium foil subsequently again as screen layer; This technology can be eliminated the coupling capacitance of round induction synchrometer, plays the effect that improves the product precision.But mylar and aluminium foil on this technology lower rotor part surface conductor group have air in twos at it between interlayer, this makes that under vacuum environment the air between interlayer can make mylar and aluminium foil outwards bloat, thereby makes product to use.This paper proposes a kind of brand-new process means; Through applying colloidal state epoxy resin as insulation course at rotor surface; Eliminate the air between interlayer in twos in the mode of plating conducting film on the insulation course more subsequently, make that round induction synchrometer can be in normal use under the vacuum environment.
As shown in Figure 1, the utility model is a kind of round induction synchrometer, comprises stator substrate 1, rotor substrate 2, stator metallic conductor zone 3, rotor metallic conductor zone 4, insulation course 5, screen layer 6.
As shown in Figure 3, the rotor winding on the rotor metallic conductor zone 4 is made continous way, and it is formed by connecting through conductor inner end 8 and conductor outer end 9 many active conductors 7, and the number of definition active conductor is the number of poles of round induction synchrometer.
After the rotor winding machined, the insulating epoxy glue that debugging is good was coated on the winding surface, places it in vacuum tank, and the vacuum tightness of its vacuum tank is adjusted to and is not higher than 1X10 -2Handkerchief vacuumized 20 minutes.Subsequently rotor is placed in the temperature control box its 60 degrees centigrade were solidified 2 hours.The surface of the rotor after epoxy glue solidified is handled smooth with the mode of turning or polishing, the solid-state epoxy layer thickness after the processing is not more than 0.05mm, and flatness is not less than 0.01mm, and this epoxy layer is the insulation course of rotor.Rotor is taken under the coating machine subsequently again plated film is carried out on its surface, the material of plated film needs conductive materials such as aluminium, silver, copper, and this coatings is the screen layer of rotor.
As shown in Figure 4, winding on the stator metallic conductor zone 3 is made sectional type, is called the segmentation winding.It is made up of 2K conductor group, the conductor group belong to respectively A mutually with B mutually, every all have K conductor group mutually.Every group is formed by connecting through conductor inner end 11 and conductor outer end 12 M root active conductor 10.Wherein K, M are positive integer.Belong to each group of homophase, connect with the lead differential concatenation.The stator and rotor active conductor all radially.
Fig. 5 has described in the rotor rotation process, the change procedure of stator active conductor 13 and rotor active conductor 14 relative positions.Distance between wherein per two active conductor center lines is called a pole span.
As shown in Figure 5, the effective separately conductor position of stator and rotor winding overlaps, and remembers that it is an initial position, and this phase output voltage amplitude of stator has maximal value this moment; When stator and rotor relative position during like Fig. 6,7, shown in 8, this phase output voltage amplitude of stator is respectively 0, maximum negative value, 0; In position shown in Figure 8, rotor turns over pole span again half, and this phase output voltage amplitude of stator reaches maximal value once more.
Therefore, can know that the magnitude one-period of the induced voltage of stator output shows that promptly the rotor relative stator has turned over two pole spans by above analysis.To number of poles is that the corresponding mechanical angle value of inductosyn its each pole span of N is 360/N, also be stator induction output voltage amplitude change one-period corresponding mechanical angle be 720/N.Because the distance between stator A, B two phase windings has differed (n+1/2) individual pole span, n is an integer.Therefore the output voltage signal magnitude of two phase windings also differs 1/4 cycle all the time.
According to shown in Figure 9, introduce the course of work of a kind of round induction synchrometer of the utility model.
Rotor is all applied excited signal; This moment stator A, the voltage signal that B all can induce same frequency mutually; Note
Figure DEST_PATH_723705DEST_PATH_IMAGE001
= ,
Figure DEST_PATH_DEST_PATH_IMAGE003
=
Figure DEST_PATH_DEST_PATH_IMAGE004
; Wherein
Figure DEST_PATH_DEST_PATH_IMAGE005
is the frequency of rotor excited signal,
Figure DEST_PATH_DEST_PATH_IMAGE006
,
Figure DEST_PATH_DEST_PATH_IMAGE007
be the range value of A, B phase output voltage signal. =
Figure DEST_PATH_DEST_PATH_IMAGE008
,
Figure DEST_PATH_171315DEST_PATH_IMAGE007
=
Figure DEST_PATH_DEST_PATH_IMAGE009
;
Figure DEST_PATH_DEST_PATH_IMAGE010
is the current electrical angle of this passage,
Figure DEST_PATH_DEST_PATH_IMAGE011
be , the maximal value of
Figure DEST_PATH_66383DEST_PATH_IMAGE007
.Can know that according to aforementioned analysis to the passage of a N utmost point (or N/2 is concerning utmost point), mechanically turn over one-period, stator output voltage signal amplitude will change N/2 cycle.Therefore ought mechanically turn over angle
Figure DEST_PATH_DEST_PATH_IMAGE012
, on electricity with the angle that turns over
Figure DEST_PATH_951162DEST_PATH_IMAGE010
=(N/2) * .Shown in Figure 9 is that the rotor relative stator is rotated a Machine cycle, and
Figure DEST_PATH_417096DEST_PATH_IMAGE006
,
Figure DEST_PATH_899024DEST_PATH_IMAGE007
change synoptic diagram.
Can know by Fig. 9; Spend when rotor turns over 360, stator output voltage signal amplitude
Figure DEST_PATH_892388DEST_PATH_IMAGE006
, all change a plurality of cycles.
Obtain current electrical angle for
Figure DEST_PATH_446046DEST_PATH_IMAGE010
, as long as record current A, B phase output voltage
Figure DEST_PATH_969431DEST_PATH_IMAGE001
,
Figure DEST_PATH_212325DEST_PATH_IMAGE003
.
Basis again:
Figure DEST_PATH_DEST_PATH_IMAGE013
Obtain:
Figure DEST_PATH_DEST_PATH_IMAGE014
.

Claims (4)

1. a round induction synchrometer comprises stator substrate (1), rotor substrate (2), it is characterized in that, described stator substrate (1) is provided with stator metallic conductor zone (3), and stator metallic conductor zone (3) is provided with winding; Described rotor substrate (2) is provided with rotor metallic conductor zone (4); Rotor metallic conductor zone (4) is provided with winding; Described rotor conductor winding (4) is provided with screen layer (6), and between last winding in rotor metallic conductor zone (4) and screen layer (6), increases insulation course (5).
2. a kind of round induction synchrometer according to claim 1 is characterized in that, described insulation course (5) is an epoxide resin material, and insulation course (5) flatness is less than 0.01mm.
3. a kind of round induction synchrometer according to claim 1; It is characterized in that; Winding on the described rotor metallic conductor zone (4) is a continous way; Comprise many active conductors (7) being formed by connecting that the radical of conductor is identical with the number of poles of synchronizer through conductor inner end (8) and conductor outer end (9).
4. a kind of round induction synchrometer according to claim 1 is characterized in that, winding on the described stator metallic conductor zone (3) is a sectional type; Be called the segmentation winding, comprise 2K conductor group, the conductor group belong to respectively A mutually with B mutually; Every all have K conductor group mutually; Every group is formed by connecting through conductor inner end (11) and conductor outer end (12) M root active conductor (10), and wherein K, M are positive integer, belong to each group of homophase; Connect with the lead differential concatenation, the stator and rotor active conductor all radially.
CN2010206796233U 2010-12-25 2010-12-25 Circular induction synchronizer Expired - Fee Related CN202126242U (en)

Priority Applications (1)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104677267A (en) * 2015-02-02 2015-06-03 九江精达检测技术有限公司 Rotary inductosyn with strong electromagnetic interference resisting capability and preparation method thereof
CN107727057A (en) * 2017-08-30 2018-02-23 中国科学院上海技术物理研究所 A kind of Method of Adjustment of round induction synchrometer
CN109459069A (en) * 2018-12-17 2019-03-12 焦明 Difference absolute type round induction synchrometer and its angle-measuring method
CN109974575A (en) * 2017-12-27 2019-07-05 海智芯株式会社 For using the method and its equipment of automatic gain adjustment algorithm detection rotation angle
CN110726428A (en) * 2019-10-12 2020-01-24 中船九江精达科技股份有限公司 Detection system and detection method for precision of circular induction synchronizer
CN112212885A (en) * 2019-07-10 2021-01-12 九江精密测试技术研究所 Vertical angle calibrating installation of theodolite

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104677267A (en) * 2015-02-02 2015-06-03 九江精达检测技术有限公司 Rotary inductosyn with strong electromagnetic interference resisting capability and preparation method thereof
CN107727057A (en) * 2017-08-30 2018-02-23 中国科学院上海技术物理研究所 A kind of Method of Adjustment of round induction synchrometer
CN109974575A (en) * 2017-12-27 2019-07-05 海智芯株式会社 For using the method and its equipment of automatic gain adjustment algorithm detection rotation angle
CN109459069A (en) * 2018-12-17 2019-03-12 焦明 Difference absolute type round induction synchrometer and its angle-measuring method
CN109459069B (en) * 2018-12-17 2023-11-07 焦明 Differential absolute type circular induction synchronizer and angle measurement method thereof
CN112212885A (en) * 2019-07-10 2021-01-12 九江精密测试技术研究所 Vertical angle calibrating installation of theodolite
CN110726428A (en) * 2019-10-12 2020-01-24 中船九江精达科技股份有限公司 Detection system and detection method for precision of circular induction synchronizer

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Granted publication date: 20120125

Termination date: 20141225

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