CN108132027A - Alignment measurement instrument integration school zero and alignment device - Google Patents

Alignment measurement instrument integration school zero and alignment device Download PDF

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Publication number
CN108132027A
CN108132027A CN201611090022.7A CN201611090022A CN108132027A CN 108132027 A CN108132027 A CN 108132027A CN 201611090022 A CN201611090022 A CN 201611090022A CN 108132027 A CN108132027 A CN 108132027A
Authority
CN
China
Prior art keywords
liquid level
reflective liquid
alignment
linear guide
measurement instrument
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201611090022.7A
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Chinese (zh)
Inventor
赵天承
刘凯
王锴磊
王占涛
汪涛
姜云翔
高秋娟
王强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Academy of Launch Vehicle Technology CALT
Beijing Aerospace Institute for Metrology and Measurement Technology
Original Assignee
China Academy of Launch Vehicle Technology CALT
Beijing Aerospace Institute for Metrology and Measurement Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by China Academy of Launch Vehicle Technology CALT, Beijing Aerospace Institute for Metrology and Measurement Technology filed Critical China Academy of Launch Vehicle Technology CALT
Priority to CN201611090022.7A priority Critical patent/CN108132027A/en
Publication of CN108132027A publication Critical patent/CN108132027A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/26Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B11/27Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/02Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring length, width, or thickness
    • G01B21/04Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring length, width, or thickness by measuring coordinates of points
    • G01B21/042Calibration or calibration artifacts

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Length Measuring Devices By Optical Means (AREA)

Abstract

Alignment measurement instrument integration school zero and alignment device, including autocollimator 1, enocscope 2, reflective liquid level 3, position sensor 4, control box 5, laser 6, the linear guide 8, motor 9, double-deck steelframe 10.Wherein autocollimator 1 is located at the upper strata of double-deck steelframe 10 with enocscope 2, the linear guide 8 is installed in the lower floor of double-deck steelframe 10, it is motor 9 in the left end of the linear guide 8, the right end of the linear guide 8 is reflective liquid level 3, the lower section of reflective liquid level 3 is laser 6, and position sensor 4 is also equipped on reflective liquid level 3.

Description

Alignment measurement instrument integration school zero and alignment device
Technical field
The technology belongs to school zero and alignment field, and in particular to a kind of alignment measurement instrument integration school zero and alignment dress It puts.
Background technology
On many spacecrafts, the foundation of carrier initial coordinate system is using reference mirror as observed object, thus to base The detection of quasi- mirror leveling precision is critically important test index.Original test process is mainly completed by manual operation, and process is numerous Trivial, man's activity is big, not intelligence, poor operability.
Therefore a kind of alignment measurement instrument integration school zero and alignment device is needed to solve problem above.In this process The alignment of the benchmark acquisition of zero-bit and test equipment optical axis and reference mirror measurement plane, which is one, needs the importance solved.
Invention content
It is an object of the invention to:A kind of alignment measurement instrument integration school zero and alignment device are provided, solved artificial The problem of cumbersome, complicated.
Technical scheme is as follows:A kind of alignment measurement instrument integration school zero and alignment device, including auto-collimation Instrument, enocscope, reflective liquid level, position sensor, control box, laser, the linear guide, motor, double-deck steelframe;Wherein auto-collimation Instrument is located at the upper strata of double-deck steelframe with enocscope, the linear guide is equipped in the lower floor of double-deck steelframe, in the left end of the linear guide For motor, the right end of the linear guide is reflective liquid level, and the lower section of reflective liquid level is laser, and position is also equipped on reflective liquid level Put sensor.
Further include control box, control box control motor.
Tested reference mirror is further included, device in use, reflective liquid level to be moved to the trigger point of position sensor, move by entirety The dynamic present apparatus makes laser beam beat in tested reference mirror.
The remarkable result of the present invention is:Operating process is simple, structure novel, and integrated solves existing reference mirror tune The alignment of flat accuracy test process lieutenant colonel zero-sum it is cumbersome, complicated, inconvenient for operation the problem of.The acquisition of benchmark and small prism are surveyed The alignment in amount face is accurately and reliably, while easy to maintenance.
Description of the drawings
Fig. 1 is alignment measurement instrument integration school zero of the present invention and alignment device schematic diagram
In figure:1 autocollimator, 2 enocscopes, 3 reflective liquid levels, 4 position sensors, 5 control box, 6 lasers, 7 tested bases Quasi- mirror, 8 the linear guides, 9 motors, 10 double-deck steelframes.
Specific embodiment
Below in conjunction with the accompanying drawings and specific embodiment is described in further detail the present invention.
Alignment measurement instrument integration school zero and alignment device, including autocollimator 1, enocscope 2, reflective liquid level 3, position Sensor 4, control box 5, laser 6, the linear guide 8, motor 9, double-deck steelframe 10.
Wherein autocollimator 1 is located at the upper strata of double-deck steelframe 10 with enocscope 2, is equipped with directly in the lower floor of double-deck steelframe 10 Line guide rail 8 is motor 9 in the left end of the linear guide 8, and the right end of the linear guide 8 is reflective liquid level 3, and the lower section of reflective liquid level 3 is Laser 6 is also equipped with position sensor 4 on reflective liquid level 3.
Control box 5 controls motor 9.
In use, reflective liquid level 3 to be moved to the trigger point of position sensor 4 first, the overall movement present apparatus makes device 6 light beam of laser is beaten in tested reference mirror 7, then acquires benchmark zero-bit, it is reflective that receipts are removed in school zero under the driving of motor 9 after the completion Liquid level 3 leaves the field range of autocollimator 1,
6 optical axis of laser is located at the lower section of reflective liquid level 3, can represent measurement optical axis position.Looked for when reducing measurement as Difficulty.
Reflective liquid level 3 is automatically parallel with the earth horizontal plane under gravity, can represent the detection zero of leveling precision Position.Laser 6 is located at the lower section of reflective liquid level 3, its displacement of the lines is accurately limited by position sensor 4.Whole device is being transported in this way After moving in place, the numerical value of reflective liquid level 3 can be acquired by autocollimator 1, carries out zero correction;Laser 6 is sent out visible simultaneously , laser beam coaxial with autocollimator 1, progress is aligned with tested reference mirror 7, this completes integrated school zero with it is right It is accurate.

Claims (3)

1. a kind of alignment measurement instrument integration school zero and alignment device, it is characterised in that:Including autocollimator (1), enocscope (2), reflective liquid level (3), position sensor (4), control box (5), laser (6), the linear guide (8), motor (9), clad steel Frame (10);Wherein autocollimator (1) and enocscope (2) is positioned at the upper strata of double-deck steelframe (10), the lower floor in double-deck steelframe (10) The linear guide (8) is installed, is motor (9) in the left end of the linear guide (8), the right end of the linear guide (8) is reflective liquid level (3), the lower section of reflective liquid level (3) is laser (6), and position sensor (4) is also equipped on reflective liquid level (3).
2. a kind of alignment measurement instrument integration school zero according to claim 1 and alignment device, it is characterised in that:Also wrap Include control box (5), control box (5) control motor (9).
3. a kind of alignment measurement instrument integration school zero according to claim 1 and alignment device, it is characterised in that:Also wrap Tested reference mirror (7) is included, device is moved integrally in use, reflective liquid level (3) to be moved to the trigger point of position sensor (4) The present apparatus makes laser (6) light beam beat on tested reference mirror (7).
CN201611090022.7A 2016-11-30 2016-11-30 Alignment measurement instrument integration school zero and alignment device Pending CN108132027A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611090022.7A CN108132027A (en) 2016-11-30 2016-11-30 Alignment measurement instrument integration school zero and alignment device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611090022.7A CN108132027A (en) 2016-11-30 2016-11-30 Alignment measurement instrument integration school zero and alignment device

Publications (1)

Publication Number Publication Date
CN108132027A true CN108132027A (en) 2018-06-08

Family

ID=62387503

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611090022.7A Pending CN108132027A (en) 2016-11-30 2016-11-30 Alignment measurement instrument integration school zero and alignment device

Country Status (1)

Country Link
CN (1) CN108132027A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101699222A (en) * 2009-11-02 2010-04-28 中国人民解放军国防科学技术大学 Star sensor calibrator and method for calibrating high-precision star sensor
CN103486998A (en) * 2013-09-18 2014-01-01 中国科学院西安光学精密机械研究所 Autocollimator indication error calibration device and calibration method
CN203479294U (en) * 2013-09-09 2014-03-12 中国科学院西安光学精密机械研究所 High-precision vertical axis inclination angle measuring system
CN103925891A (en) * 2014-04-01 2014-07-16 中国人民解放军63863部队 Auxiliary collimation device of autocollimator
CN104819899A (en) * 2015-04-16 2015-08-05 吴江市天龙机械有限公司 Rigidity detector
CN105318891A (en) * 2014-07-25 2016-02-10 北京航天计量测试技术研究所 Star sensor reference cube-prism installation error calibration apparatus
CN105547344A (en) * 2015-12-08 2016-05-04 武昌船舶重工集团有限公司 Test equipment calibration device and calibration method thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101699222A (en) * 2009-11-02 2010-04-28 中国人民解放军国防科学技术大学 Star sensor calibrator and method for calibrating high-precision star sensor
CN203479294U (en) * 2013-09-09 2014-03-12 中国科学院西安光学精密机械研究所 High-precision vertical axis inclination angle measuring system
CN103486998A (en) * 2013-09-18 2014-01-01 中国科学院西安光学精密机械研究所 Autocollimator indication error calibration device and calibration method
CN103925891A (en) * 2014-04-01 2014-07-16 中国人民解放军63863部队 Auxiliary collimation device of autocollimator
CN105318891A (en) * 2014-07-25 2016-02-10 北京航天计量测试技术研究所 Star sensor reference cube-prism installation error calibration apparatus
CN104819899A (en) * 2015-04-16 2015-08-05 吴江市天龙机械有限公司 Rigidity detector
CN105547344A (en) * 2015-12-08 2016-05-04 武昌船舶重工集团有限公司 Test equipment calibration device and calibration method thereof

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Application publication date: 20180608

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