CN107727057A - A kind of Method of Adjustment of round induction synchrometer - Google Patents

A kind of Method of Adjustment of round induction synchrometer Download PDF

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Publication number
CN107727057A
CN107727057A CN201710760245.8A CN201710760245A CN107727057A CN 107727057 A CN107727057 A CN 107727057A CN 201710760245 A CN201710760245 A CN 201710760245A CN 107727057 A CN107727057 A CN 107727057A
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CN
China
Prior art keywords
round induction
induction synchrometer
stator
adjustment
rotor
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CN201710760245.8A
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Chinese (zh)
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CN107727057B (en
Inventor
邓容
张勇
王伟成
王飞
袁海涛
胡亭亮
孙小进
孙胜利
陈凡胜
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Shanghai Institute of Technical Physics of CAS
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Shanghai Institute of Technical Physics of CAS
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C1/00Measuring angles

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Transmission And Conversion Of Sensor Element Output (AREA)

Abstract

The invention discloses a kind of Method of Adjustment of round induction synchrometer, method and step are as follows:1) control of the axiality of round induction synchrometer stator and axle is less than or equal to 0.020mm;2) working clearance of round induction synchrometer stator and round induction synchrometer rotor is controlled in 0.2 ± 0.05mm;3) end face of round induction synchrometer rotor and the depth of parallelism of the mounting surface of round induction synchrometer stator are controlled less than or equal to 0.015mm;4) the cylindrical and outer circles of round induction synchrometer stator of round induction synchrometer rotor are controlled less than or equal to 0.020mm.The present invention solves the problems, such as that the adjustment quality of round induction synchrometer is inconsistent and needs adjustment repeatedly, and Method of Adjustment of the invention makes round induction synchrometer adjustment uniform quality, it is not necessary to does over again, saves the adjustment time, while improves adjustment quality and efficiency.

Description

A kind of Method of Adjustment of round induction synchrometer
Technical field
The present invention relates to a kind of Method of Adjustment of round induction synchrometer, more particularly to a kind of application of aerospace field The Method of Adjustment of round induction synchrometer.
Background technology
Round induction synchrometer is angle measurement element, and its adjustment is bad, can not play the high-precision performance of round induction synchrometer, And adjustment quality directly affects the running accuracy of rotating mechanism, the adjustment of traditional round induction synchrometer is according to assembling master worker Experience adjustment, by with after control system integration joint debugging, its adjustment quality being examined by control system, when shortcoming is after adjustment Between the cycle it is long and risk of doing over again be present.
The content of the invention
In order to overcome the above-mentioned deficiencies of the prior art, the invention provides a kind of Method of Adjustment of round induction synchrometer.Solution The problem of round induction synchrometer adjustment quality of having determined is inconsistent and needs adjustment repeatedly, saves the adjustment time.
Required precision more and more higher of certain aerospace system to round induction synchrometer, in order to meet aerospace system to high-precision It is required that the adjustment to round induction synchrometer has carried out substantial amounts of experiment and validation test.Test result shows, by the dress of the present invention The round induction synchrometer of tune method adjustment, the running accuracy of rotating mechanism have reached the precision of dispatching from the factory of round induction synchrometer.
A kind of Method of Adjustment of round induction synchrometer, the round induction synchrometer are felt by round induction synchrometer stator 4 and circle Synchronizer rotor 5 is answered to form, wherein round induction synchrometer stator 4 is arranged on hold-down support 2, and round induction synchrometer rotor 5 is pacified On axle 1, wherein:
The axiality of described round induction synchrometer stator 4 and axle 1 is less than or equal to 0.020mm.
The working clearance control of described round induction synchrometer stator 4 and round induction synchrometer rotor 5 0.2 ± 0.05mm。
The end face of described round induction synchrometer rotor 5 and the depth of parallelism of the mounting surface of round induction synchrometer stator 4 are less than etc. In 0.015mm.
The cylindrical outer circles with round induction synchrometer stator 4 of described round induction synchrometer rotor 5 are less than or equal to 0.020mm。
Method of Adjustment of the present invention is as follows:
1) round induction synchrometer stator 4 is installed, round induction synchrometer stator 4 is installed to fixed branch with standard component screw A3 Seat 2, standard component screw A3 need not be tightened;
2) outer ring of round induction synchrometer stator 4 and the axiality of axle 1 are adjusted, axiality is controlled less than or equal to 0.020mm;
3) round induction synchrometer stator 4 adjust it is qualified after, standard component screw A3 is tightened;
4) spacer thickness calculating and repair pad, by repair pad, adjustment round induction synchrometer stator 4 senses together with circle The working clearance between device rotor 5 is walked, the working clearance should be controlled in 0.2 ± 0.05mm;Working clearance measuring process is as follows:
4-1) measure its winding sensitive surface of round induction synchrometer stator 4 and end face difference in height h1 is installed to the rotor of axle 1;
The installation end face for 4-2) measuring its winding sensitive surface of round induction synchrometer rotor 5 to round induction synchrometer rotor 5 is high Spend poor h2;
4-3) spacer thickness X is:X=0.2+h2-h1, tolerance are ± 0.05mm;
4-4) according to result of calculation repair pad, the good spacer thickness X1 of repair is surveyed, then working clearance H is:H=h1+ X1-h2;
5) round induction synchrometer rotor (5), first mounting and adjusting pad are installed, then sensed circle synchronously with standard component screw B6 Device rotor 5 is installed on axle 1, and standard component screw B6 need not be tightened;
6) end face and the depth of parallelism of the mounting surface of round induction synchrometer stator 4 of round induction synchrometer rotor 5, adjustment are adjusted And repair pad, the depth of parallelism are controlled less than or equal to 0.015mm;
7) the cylindrical and outer circles of round induction synchrometer stator 4 of round induction synchrometer rotor 5, axiality control are adjusted System is less than or equal to 0.020mm;
8) round induction synchrometer rotor 5 adjust it is qualified after, standard component screw B (6) is tightened.
Compared with prior art, it is simple the beneficial effects of the invention are as follows adjustment, it is ensured that adjustment quality conformance, to avoid Do over again, save the adjustment time, while improve adjustment quality and efficiency.
Brief description of the drawings
Fig. 1 is round induction synchrometer adjustment schematic diagram;
In figure, 1 is axle, and 2 be hold-down support, and 3 be standard component mounting screw A, and 4 be round induction synchrometer stator, and 5 be round sense Synchronizer rotor is answered, 6 be standard component mounting screw B.
Embodiment
By substantial amounts of adjustment, test and experiment, finally it is determined that the Method of Adjustment of round induction synchrometer is as follows:
1) round induction synchrometer stator 4 is installed, round induction synchrometer stator 4 is installed to fixed branch with standard component screw A3 Seat 2, standard component screw A3 need not be tightened;
2) adjust the outer ring of round induction synchrometer stator 4 and the axiality of axle (1), axiality control less than or equal to 0.020mm;
3) round induction synchrometer stator 4 adjust it is qualified after, standard component screw A3 is tightened;
4) spacer thickness calculating and repair pad, by repair pad, adjustment round induction synchrometer stator 4 senses together with circle The working clearance between device rotor 5 is walked, the working clearance should be controlled in 0.2 ± 0.05mm;
4-1) measure its winding sensitive surface of round induction synchrometer stator 4 and end face difference in height h1 is installed to the rotor of axle 1;
The installation end face for 4-2) measuring its winding sensitive surface of round induction synchrometer rotor 5 to round induction synchrometer rotor 5 is high Spend poor h2;
4-3) spacer thickness X is:X=0.2+h2-h1, tolerance are ± 0.05mm;
4-4) according to result of calculation repair pad, the good spacer thickness X1 of repair is surveyed, then real work gap H is:H= h1+X1-h2;
5) round induction synchrometer rotor 5 is installed, first mounting and adjusting pad, then with standard component screw B6 by round induction synchrometer Rotor 5 is installed on axle 1, and standard component screw B6 need not be tightened;
6) end face and the depth of parallelism of the mounting surface of round induction synchrometer stator 4 of round induction synchrometer rotor 5, adjustment are adjusted And repair pad, the depth of parallelism are controlled less than or equal to 0.015mm;
7) the cylindrical and outer circles of round induction synchrometer stator 4 of round induction synchrometer rotor 5, axiality control are adjusted System is less than or equal to 0.020mm;
8) round induction synchrometer rotor 5 adjust it is qualified after, standard component screw B6 is tightened.
Round induction synchrometer adjustment is completed, and after control system integration and joint debugging, the scanning accuracy of rotating mechanism reaches Round induction synchrometer dispatches from the factory precision, and it is correct to demonstrate Method of Adjustment.

Claims (1)

1. a kind of Method of Adjustment of round induction synchrometer, the round induction synchrometer is felt by round induction synchrometer stator (4) and circle Synchronizer rotor (5) is answered to form, wherein round induction synchrometer stator (4) is arranged on hold-down support (2), and round induction synchrometer turns Sub (5) are arranged on axle (1), it is characterised in that Method of Adjustment comprises the following steps:
1) round induction synchrometer stator (4) is installed, round induction synchrometer stator (4) is installed to fixation with standard component screw A (3) Bearing (2), standard component screw A (3) need not be tightened;
2) round induction synchrometer stator (4) outer ring and the axiality of axle (1) are adjusted, axiality is controlled less than or equal to 0.020mm;
3) after round induction synchrometer stator (4) adjustment is qualified, standard component screw A (3) is tightened;
4) spacer thickness calculating and repair pad, by repair pad, adjustment round induction synchrometer stator (4) is synchronous with circle sensing Working clearance between device rotor (5), working clearance should be controlled in 0.2 ± 0.05mm;Working clearance measuring process is as follows:
4-1) measure round induction synchrometer stator (4) its winding sensitive surface and end face difference in height h1 is installed to the rotor of axle (1);
The installation end face for 4-2) measuring round induction synchrometer rotor (5) its winding sensitive surface to round induction synchrometer rotor (5) is high Spend poor h2;
4-3) spacer thickness X is:X=0.2+h2-h1, tolerance are ± 0.05mm;
4-4) according to result of calculation repair pad, the good spacer thickness X1 of repair is surveyed, then working clearance H is:H=h1+X1- h2;
5) round induction synchrometer rotor (5) is installed, first mounting and adjusting pad, then with standard component screw B (6) by round induction synchrometer Rotor (5) is installed on axle (1), and standard component screw B (6) need not be tightened;
6) end face and the depth of parallelism of the mounting surface of round induction synchrometer stator (4) of round induction synchrometer rotor (5), adjustment are adjusted And repair pad, the depth of parallelism are controlled less than or equal to 0.015mm;
7) the cylindrical and outer circles of round induction synchrometer stator (4) of round induction synchrometer rotor (5), axiality control are adjusted System is less than or equal to 0.020mm;
8) after round induction synchrometer rotor (5) adjustment is qualified, standard component screw B (6) is tightened.
CN201710760245.8A 2017-08-30 2017-08-30 Method for assembling and adjusting circular induction synchronizer Active CN107727057B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710760245.8A CN107727057B (en) 2017-08-30 2017-08-30 Method for assembling and adjusting circular induction synchronizer

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Application Number Priority Date Filing Date Title
CN201710760245.8A CN107727057B (en) 2017-08-30 2017-08-30 Method for assembling and adjusting circular induction synchronizer

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CN107727057A true CN107727057A (en) 2018-02-23
CN107727057B CN107727057B (en) 2020-06-26

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110146009A (en) * 2019-05-17 2019-08-20 中国科学院上海技术物理研究所 A kind of sandwich inductosyn structure

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1411356A1 (en) * 1986-07-09 1988-07-23 А. П. Андрейцев и Д. П. Пономарев Installation for checking thickness of electroplating in depositing process
CN101106322A (en) * 2006-05-30 2008-01-16 党程科 Super sensing motion exploration
CN201083498Y (en) * 2007-08-03 2008-07-09 金少舫 Cylinder type inductosyn
CN201244731Y (en) * 2008-09-01 2009-05-27 陈耀忠 Horizontal borer digital display indexing worktable
US20110015021A1 (en) * 2009-07-16 2011-01-20 Gm Global Technology Operations, Inc. Clutch arrangements for an electrically-variable transmission
CN202126242U (en) * 2010-12-25 2012-01-25 九江精密测试技术研究所 Circular induction synchronizer
CN202781993U (en) * 2012-06-28 2013-03-13 中国科学院上海技术物理研究所 Shielding layer structure of round inductosyn
CN203405173U (en) * 2013-08-29 2014-01-22 九江精达检测技术有限公司 Circle inductosyn having high precision aligning function in winding corrosion technology
CN205825940U (en) * 2016-06-20 2016-12-21 南京淳泰控制设备有限公司 A kind of index precision detecting device positioning dish indexing trough

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1411356A1 (en) * 1986-07-09 1988-07-23 А. П. Андрейцев и Д. П. Пономарев Installation for checking thickness of electroplating in depositing process
CN101106322A (en) * 2006-05-30 2008-01-16 党程科 Super sensing motion exploration
CN201083498Y (en) * 2007-08-03 2008-07-09 金少舫 Cylinder type inductosyn
CN201244731Y (en) * 2008-09-01 2009-05-27 陈耀忠 Horizontal borer digital display indexing worktable
US20110015021A1 (en) * 2009-07-16 2011-01-20 Gm Global Technology Operations, Inc. Clutch arrangements for an electrically-variable transmission
CN202126242U (en) * 2010-12-25 2012-01-25 九江精密测试技术研究所 Circular induction synchronizer
CN202781993U (en) * 2012-06-28 2013-03-13 中国科学院上海技术物理研究所 Shielding layer structure of round inductosyn
CN203405173U (en) * 2013-08-29 2014-01-22 九江精达检测技术有限公司 Circle inductosyn having high precision aligning function in winding corrosion technology
CN205825940U (en) * 2016-06-20 2016-12-21 南京淳泰控制设备有限公司 A kind of index precision detecting device positioning dish indexing trough

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Title
ZOU AN: "Analysis Calculation and Testing of Rotary Inductosyn Angle Measuring Errors", 《PROCEEDINGS OF THE 33RD CHINESE CONTROL CONFERENCE》 *
王鹰: ""组装式圆感应同步器安装"", 《机械工人.冷加工》 *
齐凤梅: ""圆感应同步器安装误差修正方法研究"", 《光学技术》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110146009A (en) * 2019-05-17 2019-08-20 中国科学院上海技术物理研究所 A kind of sandwich inductosyn structure

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