CN110360962B - Method for rapidly identifying plane flatness - Google Patents

Method for rapidly identifying plane flatness Download PDF

Info

Publication number
CN110360962B
CN110360962B CN201910657320.7A CN201910657320A CN110360962B CN 110360962 B CN110360962 B CN 110360962B CN 201910657320 A CN201910657320 A CN 201910657320A CN 110360962 B CN110360962 B CN 110360962B
Authority
CN
China
Prior art keywords
plane
laser
flatness
defect position
identification line
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.)
Active
Application number
CN201910657320.7A
Other languages
Chinese (zh)
Other versions
CN110360962A (en
Inventor
胡志刚
王长军
唐葆华
李勇会
王保平
赵昆鹏
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.)
Beijing No6 Construction Engineering Quality Test Department Co ltd
China Construction First Group Corp Ltd
Beijing Building Research Institute Corp Ltd of CSCEC
Original Assignee
Beijing No6 Construction Engineering Quality Test Department Co ltd
China Construction First Group Corp Ltd
Beijing Building Research Institute Corp Ltd of CSCEC
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 Beijing No6 Construction Engineering Quality Test Department Co ltd, China Construction First Group Corp Ltd, Beijing Building Research Institute Corp Ltd of CSCEC filed Critical Beijing No6 Construction Engineering Quality Test Department Co ltd
Priority to CN201910657320.7A priority Critical patent/CN110360962B/en
Publication of CN110360962A publication Critical patent/CN110360962A/en
Application granted granted Critical
Publication of CN110360962B publication Critical patent/CN110360962B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • G01B11/30Measuring arrangements characterised by the use of optical techniques for measuring roughness or irregularity of surfaces

Abstract

The invention relates to a method for rapidly identifying the flatness of a plane, wherein the plane comprises a flat part, a concave part and a convex part and comprises a laser generator, laser emitted by the laser generator is a laser plane, the laser plane irradiates on the plane at a certain angle with the plane, and identification lines are formed on the flat part, the concave part and the convex part. According to the principle that the laser oblique projection length is far larger than the height of the barrier, the flatness of the barrier is accurately and quickly identified according to the relation between the defect height and the reverse projection length, the purpose of judging whether the flatness of the plane is qualified or not in the construction process, quality acceptance and maintenance monitoring is achieved, the testing, acceptance and monitoring speed is increased, and the barrier height detection method has the advantages of being high in speed, high in efficiency, stable in performance, high in precision and low in cost.

Description

Method for rapidly identifying plane flatness
Technical Field
The invention relates to a method for rapidly identifying plane flatness, which is used for detecting, checking and monitoring the quality of constructional engineering.
Background
The plane is the main expression form of buildings and roads. In current road traffic, the quality of road surface evenness is directly related to the conditions of vehicles in the aspects of driving safety, oil consumption, speed, mechanical wear, comfort and the like, and the building wall surface evenness is more related to the visual perception of each user, so that the attention and the control on the plane evenness are required to be strengthened. At present, the flatness is controlled and measured by a 2m guiding rule.
Meanwhile, the amount of the engineering is huge, the measurement work is heavy, and technicians are in trouble and labor. For years, the measurement of flatness can be said to be 'measuring the ruler to the end', and a reliable rapid test technology does not exist at present.
Disclosure of Invention
The invention aims to solve the technical problem of providing a method for quickly identifying plane flatness, and overcoming the huge defects of the prior art that a guiding rule is adopted for controlling and checking engineering.
The technical scheme for solving the technical problems is as follows: the plane comprises a leveling part, a concave part and a convex part, and comprises a laser generator, wherein laser emitted by the laser generator is a laser plane, the laser plane irradiates on the plane at a certain angle with the plane, and identification lines are formed on the leveling part, the concave part and the convex part.
The invention has the beneficial effects that: adopt the laser of laser generator transmission to be the laser plane, the laser plane is in order to become certain angle with the plane and shine on the plane level position, sunken position and protrusion position are gone up and are formed the identification line, are greater than the principle of barrier height according to laser oblique projection length, according to the relation of defect height rather than reverse projection length, come accurate quick identification its roughness size, reach and judge in the work progress, when quality is examined, whether qualified purpose of planar roughness when dimension guarantor monitors for test, acceptance, monitoring speed, it is fast to have test speed, high efficiency, stable performance, high accuracy, low cost.
On the basis of the technical scheme, the invention can be further improved as follows.
The invention relates to a method for rapidly identifying plane flatness, and further, a laser plane is arranged in a horizontal direction or a vertical direction.
The invention relates to a method for rapidly identifying plane flatness, which further comprises the following steps of calibrating test equipment to draw a standard curve:
step (1), setting an angle between a laser plane and a test position as alpha, projecting the laser plane on the test plane, and presenting an identification line;
setting the central axis of the identification line relative to the concave area defect position and the convex area defect position, and measuring the vertical distance between the concave area defect position and/or the convex area defect position and the central axis by using a ruler to be the laser measurement defect distance L;
step (3), measuring the actual defect distance L' by using a feeler gauge, and repeating the steps (2) and (3);
a full 10 log number is uniformly collected from 0 to 10cm (wherein a pair of quantitative numbers must be present, i.e., at least one set of actual defect distances L 'corresponding to the laser measured defect distances L, such as 2mm for the actual defect distance L' and 2cm for the laser measured defect distance L to be determined, so that accurate determination is facilitated),
and (4) taking the reading L of the ruler as a horizontal coordinate and taking the reading L' of the feeler gauge as a vertical coordinate to draw a standard curve.
The invention relates to a method for rapidly identifying plane flatness, and further, calculating the flatness x at a defect position according to the following formula, wherein the flatness x is kL, and k is tg alpha, L'/L.
The invention relates to a method for rapidly identifying plane flatness, and further relates to a ruler for measuring a laser measurement defect distance L, which is accurate to 0.5 mm.
The invention relates to a method for rapidly identifying plane flatness, which further comprises the step (2) of setting the central axis of an identification line relative to a concave area defect position and a convex area defect position, and aligning the central axis of the identification line by using a running rule.
The invention relates to a method for rapidly identifying plane flatness, which further comprises a field test step (A), wherein a laser generator is started, and an identification line displayed on a plane by a laser plane is stable;
step (B), starting measurement and observing the shape of the identification line; and selecting an abnormal defect position to measure a relative defect distance L, and converting L' according to a standard curve to obtain the flatness x.
The invention relates to a method for rapidly identifying plane flatness, which is characterized in that two laser generators are symmetrically arranged for field test, identification lines are respectively provided, and the central axis of the identification lines is accurately positioned.
The beneficial effect of adopting the further scheme is that: two laser generators are adopted to emit two laser planes to position a positioning identification line, so that the central axis of the identification line with the concave area defect position and the convex area defect position can be accurately positioned.
Drawings
FIG. 1 is a schematic structural diagram of an identification line formed by a laser plane emitted by a laser emitter and a plane to be detected in the method for rapidly identifying plane flatness according to the present invention;
FIG. 2 is a schematic structural diagram of the principle of measurement of the method for rapidly identifying plane flatness of the invention;
FIG. 3 is a schematic diagram of a standard defect produced in the measurement process by the method for rapidly identifying plane flatness according to the present invention;
in the drawings, the components represented by the respective reference numerals are listed below:
1. the identification line comprises a flat part, 2, a concave part, 3, a convex part, 4, a plane, 11, a laser generator, 12, laser, 13 and an identification line.
Detailed Description
The principles and features of this invention are described below in conjunction with the following drawings, which are set forth by way of illustration only and are not intended to limit the scope of the invention.
Referring to fig. 1, according to the embodiment of the invention, a plane 4 comprises a flat part 1, a concave part 2 and a convex part 3, and comprises a laser generator 11, the laser generator 11 emits laser 12, the laser 12 is irradiated on the plane at a certain angle with the plane, and an identification line 13 is formed on the flat part 1, the concave part 2 and the convex part 3. Specifically, the laser plane may be disposed in a horizontal direction or a vertical direction.
As shown in fig. 2 and 3, the method for rapidly identifying plane flatness according to the present invention includes calibrating a testing device to draw a standard curve: step (1), setting a laser plane to form an angle alpha with the plane; alpha is greater than 0 degree and less than 90 degrees; preferably 15-60 degrees.
Setting the central axis of the identification line relative to the concave area defect position and the convex area defect position, and measuring the vertical distance between the concave area defect position and/or the convex area defect position and the central axis by using a ruler to be the laser measurement defect distance L; the ruler is required to be accurate to 0.5 mm;
the central axis of the identification line relative to the concave area defect position and the convex area defect position is set in the step, the central axis of the identification line can be aligned by using a guiding ruler, and then the perpendicular distance between the concave area defect position and the central axis is measured by a ruler to be the laser measurement defect distance L.
Step (3), measuring the actual defect distance L' by using a feeler gauge, and repeating the steps (2) and (3);
and (4) taking the reading L of the ruler as a horizontal coordinate and taking the reading L' of the feeler gauge as a vertical coordinate to draw a standard curve. The flatness x of a specific test plane can be calculated by the following formula, where k tg α L '/L, L is the perpendicular distance between the position of the laser projection and the central axis of the identification line, and L' is the actual flatness.
The method for rapidly identifying the plane flatness carries out field test, step (A), a laser generator is started, and an identification line displayed on a plane to be detected by a laser plane is stable;
step (B), starting measurement and observing the shape of the identification line; and selecting an abnormal defect position to measure a relative defect distance L, and converting L' according to a standard curve to obtain the flatness x.
Specifically, when the device is used for field test, two laser generators can be symmetrically arranged to respectively provide identification lines and accurately position the central axis of the identification lines. Therefore, the two laser generators are adopted to emit two laser planes to position the positioning identification line, and the central axis of the positioning identification line can be accurately determined.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.

Claims (4)

1. A method for rapidly identifying the flatness of a plane, wherein the plane comprises a flat part, a concave part and a convex part, and is characterized by comprising a laser generator, wherein laser emitted by the laser generator is a laser plane, the laser plane irradiates on the plane at a certain angle with the plane, and identification lines are formed on the flat part, the concave part and the convex part;
the method comprises the following steps of calibrating test equipment to draw a standard curve:
step (1), setting an angle between a laser plane and a test position as alpha, projecting the laser plane on the test plane, and presenting an identification line;
setting the central axis of the identification line relative to the concave area defect position and the convex area defect position, and measuring the vertical distance between the concave area defect position and/or the convex area defect position and the central axis by using a ruler to be the laser measurement defect distance L;
step (3), measuring the actual defect distance L' by using a feeler gauge, and repeating the steps (2) and (3);
step (4), drawing a standard curve by taking the reading L of the ruler as a horizontal coordinate and the reading L' of the feeler gauge as a vertical coordinate;
calculating the flatness x at the defect position by the following formula, wherein the flatness x is k.L, and k is tg alpha is L'/L;
setting the central axis of the identification line relative to the concave area defect position and the convex area defect position, aligning the central axis of the identification line by using a guiding rule, and further measuring L' by using a feeler gauge;
the method comprises the following steps of (A) carrying out field test, starting a laser generator, and stabilizing an identification line to be displayed on a plane by a laser plane;
step (B), starting measurement and observing the shape of the identification line; and selecting an abnormal defect position to measure a relative defect distance L, and converting L' according to a standard curve to obtain the flatness x.
2. The method for rapidly identifying the plane flatness of the steel plate as claimed in claim 1, wherein the laser plane is arranged in a horizontal direction or a vertical direction.
3. The method for rapidly identifying plane flatness of claim 1, wherein the ruler for measuring the laser measurement defect distance L is accurate to 0.5 mm.
4. The method for rapidly identifying the plane flatness of claim 1, wherein the field test uses two laser generators which are symmetrically arranged to respectively provide identification lines and accurately position the central axes of the identification lines.
CN201910657320.7A 2019-07-19 2019-07-19 Method for rapidly identifying plane flatness Active CN110360962B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910657320.7A CN110360962B (en) 2019-07-19 2019-07-19 Method for rapidly identifying plane flatness

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910657320.7A CN110360962B (en) 2019-07-19 2019-07-19 Method for rapidly identifying plane flatness

Publications (2)

Publication Number Publication Date
CN110360962A CN110360962A (en) 2019-10-22
CN110360962B true CN110360962B (en) 2021-07-02

Family

ID=68221333

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910657320.7A Active CN110360962B (en) 2019-07-19 2019-07-19 Method for rapidly identifying plane flatness

Country Status (1)

Country Link
CN (1) CN110360962B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111044003A (en) * 2019-12-04 2020-04-21 常州三立精图光电有限公司 Method for improving flatness of screen printing plate

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1040265A (en) * 1988-08-10 1990-03-07 北京科技大学 The method and the measuring instrument of roughness surveyed in laser scanning
CN101576376A (en) * 2008-12-24 2009-11-11 北京神网创新科技有限公司 Method and system for laser detection of shape of charge level

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58115314A (en) * 1981-12-28 1983-07-09 Matsushita Electric Works Ltd Measuring device of flatness
DE3728210A1 (en) * 1987-08-24 1989-03-16 Sick Optik Elektronik Erwin OPTICAL SCANNER FOR TRANSPARENT RAILWAY MATERIAL
CN2938028Y (en) * 2006-06-13 2007-08-22 武汉武大卓越科技有限责任公司 Device for measuring road surface planeness
CN100561121C (en) * 2007-02-02 2009-11-18 西安交通大学 Measurement method of planeness based on Flame Image Process and image recognition
CN100573043C (en) * 2008-03-21 2009-12-23 哈尔滨工业大学 The surface evenness automatic testing method
CN101644023B (en) * 2009-08-21 2011-01-26 赵怀志 Detection method of road-surface evenness
CN106248005A (en) * 2016-10-16 2016-12-21 欧阳平 A kind of optical measurement flatness and the method for gradient

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1040265A (en) * 1988-08-10 1990-03-07 北京科技大学 The method and the measuring instrument of roughness surveyed in laser scanning
CN101576376A (en) * 2008-12-24 2009-11-11 北京神网创新科技有限公司 Method and system for laser detection of shape of charge level

Also Published As

Publication number Publication date
CN110360962A (en) 2019-10-22

Similar Documents

Publication Publication Date Title
CN105423946B (en) Axle journal axle center measuring device based on laser displacement sensor and measurement scaling method
CN101464163B (en) Straightness detecting method for platform normal point used for total station instrument check
CN106813600B (en) Non-contact discontinuous plane flatness measuring system
CN103363923A (en) Non-contact type gear tooth direction measuring method of laser vision distance measurement
CN104990478A (en) Calibration method for textile spinning machine roller entry and exit fixing gauge
CN110360962B (en) Method for rapidly identifying plane flatness
CN216925477U (en) Wafer rod detection device
CN103673998B (en) Tool pedestal for detecting reference point through laser tracker
CN105466381A (en) Concave arc radius detection and arc degree determination apparatus and method
CN112620139A (en) Concrete test piece size detection device and method
CN112033412A (en) Method and device for improving positioning precision of inspection robot
CN106959449B (en) High-speed roller machine repetitive positioning accuracy detection method
CN106181027A (en) Laser welding system verticality adjusting method and laser welding head unit
CN106643443B (en) Device and method for detecting coaxiality of mixing cylinder of concrete mixer
CN107314733B (en) Rolling mill roller system parallelism measuring device and application method thereof
CN216283307U (en) Warping degree detection device
CN107010513B (en) Simple and convenient calibration tool for elevator guide rail and guide rail calibration method
CN206291832U (en) A kind of tapped blind hole depth fast detecting tool
CN211954057U (en) Straightness laser detection device
CN205027339U (en) Deep hole straightness accuracy detection device based on ultrasonic thickness measurement appearance
CN213238811U (en) Detector for automatically and rapidly detecting flatness
CN108637037A (en) A kind of method of steel cold straightener verification straightening roll levelness
CN203785677U (en) Tooling base for reference point detection of laser tracker
CN206891361U (en) A kind of cylinder linearity testing apparatus
CN219869732U (en) Elevator guide rail perpendicularity detector

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant