CN1069570A - Multi-hole coaxial error measuring method and device - Google Patents
Multi-hole coaxial error measuring method and device Download PDFInfo
- Publication number
- CN1069570A CN1069570A CN91107268A CN91107268A CN1069570A CN 1069570 A CN1069570 A CN 1069570A CN 91107268 A CN91107268 A CN 91107268A CN 91107268 A CN91107268 A CN 91107268A CN 1069570 A CN1069570 A CN 1069570A
- Authority
- CN
- China
- Prior art keywords
- hole
- rotating shaft
- measured
- sensor
- measured hole
- 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.)
- Granted
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/003—Measuring of motor parts
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
- G01B21/20—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring contours or curvatures, e.g. determining profile
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
- G01B21/22—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes
- G01B21/24—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes for testing alignment of axes
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
Abstract
The present invention is method and a device of measuring multi-hole coaxial error.Measurement is carried out under computer control, each measured hole is measured by corresponding sensor, the all the sensors of measuring same coaxiality error is installed in the same shaft section of rotating shaft, rotating shaft rotates a circle, sensor carries out scanning survey to the measured hole real profile, the data that computing machine obtains according to sensor, calculate the measured hole least square center, reach the distance of each hole, thereby try to achieve the coaxiality error in measured hole relative datum hole about benchmark.The present invention has that automaticity height, measuring accuracy height, detection speed are fast, reliable, easy to operate, the characteristics of advanced technology.
Description
The present invention relates to a kind of measuring technique of multi-hole coaxial error, particularly relate to method and the device of measuring multi-hole coaxial error by computer controlled automatic.
The measurement of multi-hole coaxial error is the important step in the machine industry normally, as in the explosive motor manufacturing, crankshaft hole on the cylinder body, camshaft hole coaxial accuracy are the important technology indexs that guarantees the cylinder body quality, it has bigger influence to the performance of engine, and therefore convenient its coaxiality error of measuring exactly is a gordian technique in the explosive motor manufacturing.Detection for cylinder body crankshaft hole, camshaft hole coaxiality error, always each producer all adopts receiver ga(u)ge method (axle method) to carry out the qualitative detection of qualified (gauge by) and defective (gauge can't pass), for underproof cylinder body, can not determine because that measured hole causes the defective of cylinder body, error size and the direction of measured hole with respect to benchmark can not be provided again, and measuring error is big and can not be provided as adjustment lathe and the required data of quality management in the processing.
The objective of the invention is to avoid the weak point of prior art, and provide a kind of by the computer controlled automatic measuring process, can determine underproof measured hole rapidly, the error size of measured hole with respect to benchmark and the measuring method and the device of the high multi-hole coaxial error of direction, measuring accuracy and efficient can be provided rapidly again.
The objective of the invention is to realize by following method and apparatus.
Disclosed multi-hole coaxial error measuring method is that its measuring process is as follows by the whole measuring process of computer controlled automatic:
With measured workpiece in accordance with regulations direction be placed in movably on the worktable, be transplanted on the measuring position and be locked;
2. the rotating shaft that survey sensor is housed is inserted in the measured hole of measured workpiece and the location automatically;
3. rotating shaft is rotated, and the sensor equiangular sampling in each hole of computer controlled measurement shows the each measured value of sampling of each hole profile simultaneously respectively successively on screen;
4. computing machine calculates the cross section least square center of each sensor scan by minimum two-multiply law;
With the least square center line of the above-mentioned 4 two ends measured holes that calculated as the benchmark of measuring other each measured hole, calculate the distance of the least square center of each measured hole, 2 times of coaxiality errors that are measured hole of this distance to benchmark;
6. measure and finish, screen display measured hole least square center is with respect to the eccentric direction synoptic diagram of benchmark, and X, Y coordinate figure and coaxiality error value are printed measurement result.
Purpose of the present invention can obtain better realization by taking following technical measures:
1. the error of the center of circle of least square circle and right alignment is calculated by following formula:
(1) calculate the round formula of least square:
a
K= 2/(N) X
KR(1) b
K= 2/(N) X
KI(1)
K=1,2 ..., m, m are the numbers of measured hole.a
KBe sad conversion in the richness a component of degree n n real part 2/N doubly, b
KBe a component of degree n n imaginary part of sad conversion in the richness 2/N doubly;
(2) straight-line equation of measured hole benchmark is:
(x-a
1)/(a
m-a
1) = (y-b
1)/(b
m-b
1) = (z-z
1)/(z
m-z
1)
The direction number of this straight line is:
(3) least square center of measured hole profile to the distance of reference line is:
(4) coaxiality error is:
Φfi=2h
i
I=2 in the formula, 3,4 ..., m-1.
2. when the length-diameter ratio of measured hole≤0.5, measure the least square center that calculates a cross section of measured hole, estimate coaxiality error to the distance of benchmark with this center of circle; When the length-diameter ratio of measured hole>0.5, measure the least square center that calculates two cross sections of measured hole and the center of circle distance to benchmark, estimate coaxiality error with big one of error in two cross sections.
3. measure the per 10 ° of once sampling of sensor in each hole, the profile in each hole 36 points of sampling altogether.
Realize a kind of device of above-mentioned measuring method, it comprises the computing machine, display device, printing equipment of automatic control survey process, as the rotating shaft that sensor is housed of measurement component, drive the axially movable drive unit of rotating shaft, drive motor that rotating shaft rotates, movably worktable and the angle sender set and the photoelectric sensor that take measurement of an angle, measured workpiece is placed in movably on the worktable, measured hole is to facing toward rotating shaft, each measured hole is measured by the respective sensor that is installed in the rotating shaft, motor is by x, and y bidirectional elastic shaft coupling drives rotating shaft and rotates.The angle sender set is installed in the position of rotating synchronously with rotating shaft, and photoelectric sensor is placed on the static housing of phase countershaft, and rotating shaft, motor and housing are coupled to one, and guide rail moves in the driving lower edge of drive unit.
Realize the device of the inventive method, better realized, also taked following technical measures in order to make goal of the invention:
Each measured hole of measured workpiece is measured by one or two sensor scan, all sensors are arranged in the same shaft section of rotating shaft, support and rotating shaft that computer CPU plate and sensor circuit board are installed are fixedly installed togather, between rotating shaft and motor;
Measurement mechanism is a vertical structure, and assembling connects all-in-one-piece motor, support and rotating shaft, and being suspended on by the end face floating bearing can be along on the balladeur train of guide rail slip, the balance weight balance that the chain other end that the weight of suspension body by sprocket bearing is hung;
The rotating shaft lower end is a cone structure, rotating shaft is a two supports, the outer conical surface positioning support of bearing holder (housing, cover) is passed through at measured workpiece nose end topmost in the upper end, the lower end is by having the bearing radial location of special construction, and the structure of bearing is to drive locking ball by sliding sleeve to move that to make cylindrical be that the lower bearing sleeve swelling of the conical surface is in the measured hole of lower end;
It is cylinder piston structure that axially movable drive unit is made in the driving rotating shaft, and the sensor that is installed in the rotating shaft is the eddy current sensor of band contact.
Accompanying drawing 1 is the integral layout synoptic diagram of measurement mechanism of the present invention.
Accompanying drawing 2 is location survey schematic diagrams of the present invention.
Accompanying drawing 3 is coaxiality error schematic diagram calculations of the present invention.
The present invention is described in further detail by embodiment below in conjunction with description of drawings.Embodiment is that the present invention is applied to EQ153 diesel motor cylinder crankshaft hole, the camshaft hole measuring for the coaxiality error device that No. 2 Automobile Factory introduces the technology processing of U.S. Cummins company.Measured workpiece is 6 Cylinder engine cylinder bodies, and tested crankshaft hole, camshaft hole respectively are 7.Measurement mechanism is a vertical structure.Tested cylinder body (12) is lifted on the dolly worktable (13), and the dolly worktable can and be measured station with lifting station and be locked on the track support.(11) be the rotating shaft of measuring the camshaft hole coaxiality error, (10) are the rotating shafts of measuring the crankshaft hole coaxiality error.The eddy current sensor (20) of 7 band contacts all is equipped with in each rotating shaft respectively, and all the sensors in each rotating shaft is positioned at same shaft section, and during measurement, each sensor scan is measured corresponding crankshaft hole or camshaft hole.Each rotating shaft is integral with support (17) fixed connection that computer CPU plate, sensor circuit board (16) are housed separately respectively, pass through x more respectively, y bidirectional elastic shaft coupling (15) and drive motor (14) separately connect, motor is placed in the housing (9), constitutes the measurement component of measuring crankshaft hole and camshaft hole coaxiality error respectively.Photoelectric sensor that takes measurement of an angle (18) and angle sender set (19) are separately fixed on housing (9) and the support (17).The measurement component of the measurement component of measurement crankshaft hole and measurement camshaft hole is respectively by being suspended on the same sliding support (6) chain (4) that the weight of two measurement components is being supported by sprocket wheel (5) balance weight (2) balance that the other end hung at hinge and the end face floating bearing (7) that both direction rotates.Cylinder piston (3) as driving mechanism moves axially up and down by balladeur train (6) drive measurement component, makes the rotating shaft that sensor is housed enter or withdraw from tested crankshaft hole or camshaft hole.(1) is the frame of measurement mechanism.
During measurement, elder generation vertically upward is placed on the dolly worktable its crankshaft hole, camshaft hole tested cylinder body, tested cylinder body is delivered to make its measured hole to measuring position and locking facing to rotating shaft again.Cylinder piston (3) is under the control of computing machine, the driving measurement component moves down, since the end of rotating shaft be the conical surface and whole measurement component by being suspended on the balladeur train at hinge and the end face floating bearing that both direction rotates, the rotating shaft that sensor is housed automatically enters tested crankshaft hole and camshaft hole.Rotating shaft is inserted when putting in place, the conical surface (21) that housing (9) lower end is 90 ° contacts the location with tested cylinder body crankshaft hole (camshaft hole) topmost, simultaneously rotating shaft bottom end bearing (22) is in swelling is positioned cylinder body crankshaft hole (camshaft hole) bottom, and the structure of bearing (22) is to drive locking ball by sliding sleeve to move that to make cylindrical be that the lower bearing sleeve swelling of the conical surface is in measured hole.Motor starts under the control of computing machine, the drive rotating shaft is returned and is circled, put in place and stop automatically, each sensor scans the profile in a cross section of 1,2,3,4,5,6,7 crankshaft holes of cylinder body, camshaft hole in the rotation, computing machine according to angle sender set and the per 10 ° of signals that send of photoelectric sensor, respectively 36 measurement data of each sensor of acquisition and recording, calculate least square center, calculate 2,3,4,5,6 each hole circle heart 2 times again, be the coaxiality error of measured hole relative datum to the distance of 1.7 hole circle heart lines.Measure in the scanning process, the measured value that shows each each sampled point of hole in crankshaft hole, the camshaft hole on the screen respectively successively, measure the coordinate figure, coordinate signal figure and the coaxiality error value that finish promptly to show each measured hole center of circle relative datum, the data of the measurement result that printer prints is shown and synoptic diagram.
The calculating principle of coaxiality error of the present invention as shown in Figure 3 and Figure 4.If the sampled value of the i hole measured circle of crankshaft hole (or camshaft hole) is △ r
Ij, i=1,2 ... 7, j=0,1 ... N-1, N are sampling number, △ r
IjBe j change in radius amount of i hole measured circle.0(0 among the figure, 0) for measuring the centre of gyration, O
1 i(a
i, b
i) be the round center of least square, e
iBe offset.According to traditional recommended formula
Can obtain least square center O
1 i(a
i, b
i).Measuring basis is the common axis in 1,7 hole as requested, i.e. the round heart O of 1,7 crankshaft hole (or camshaft hole) measured circle least square
1' (a, b, Z), O
7' (a
7, b
7, Z
7) line L.
The coaxiality error of each measured hole is each least square center O '
i(a
i, b
i, Z
i) to the distance of space line L every twice.
φfi=2h
i
i=2,3,4,5,6
Calculate the least square center of each measured circle according to this traditional recommended formula, need to calculate 2N COS, sin; 2N time real number multiplies each other; 2(N-1) inferior real number addition.If the cross section number is more, sampled data is many, and then speed is slower, and the present invention has adopted sad transform method in a kind of quick recurrence richness, and it can calculate a certain component of degree n n separately, makes computing velocity improve 2/3, is applied to ask the derivation of equation of least square center as follows:
a
K= 2/(N) X
KR(1) b
K= 2/(N) X
KI(1)
K=1,2,3,4,5,6,7
By following formula as can be known, a of least square center
KBe exactly a component of degree n n real part of sad conversion in the richness 2/N doubly, b
KBe exactly a component of degree n n imaginary part of sad conversion in the richness 2/N doubly.
After having determined least square center, the formula that calculates coaxiality error is as follows:
O
1' (a
1, b
1, Z
1), O
7' (a
7, b
7, Z
7) straight-line equation of line is:
(x-a
1)/(a
m-a
1) = (y-b
1)/(b
m-b
1) = (z-z
1)/(z
m-z
1)
The direction number of straight line is
So spatial point to the distance of straight line is:
Coaxiality error is:
φfi=2h
i
I=2 in the formula, 3,4,5,6.
In the present invention owing to adopted the method for determining measured hole least square center coordinate with the resulting formula of sad conversion in the quick recurrence richness; Each measured hole is self-corresponding with each, has the electric vortex sensor measuring of average effect; The all the sensors of measuring crankshaft hole is installed in respectively in the same shaft section of each axis of rotation with all the sensors of measuring camshaft hole; The rotating shaft positioning support is in tested crankshaft hole, camshaft hole up and down in two stomidiums; The rotating shaft band sensor rotation and each hole real profile is carried out putting in place in one week of scanning survey is stopped automatically; Whole measuring process is by computer-implemented control, data acquisition, calculate the least square center in each hole and the advanced technology measures such as coaxiality error in measured hole relative datum hole, guaranteed high-level efficiency of the present invention, high-acruracy survey, make the present invention just can measure crankshaft hole by the one-step installation cylinder body at 3 minutes, the coaxiality error of camshaft hole, uncertainty of measurement reaches≤level of 2 μ m, display device and printer are along with the carrying out of measuring process, demonstration and printing measured hole center are with respect to the coordinate figure of benchmark, coordinate signal figure and coaxiality error value are for adjustment lathe and factory's quality management in the processing provide reliable foundation.
The present invention also has tested cylinder body installation accuracy and requires low advantage except that having above-mentioned advantage.Because device of the present invention is a vertical structure, the bottom of rotating shaft is a circular conical surface, but whole measurement component is suspended on the sliding support by hinge and the end face floating bearing that both direction rotates, therefore as long as the roller end cone enters measured hole, whole rotating shaft just can be inserted in the measured hole, carries out high-precision measurement.
It is fast that the present invention has automaticity height, measuring accuracy height, detection speed, easy to operate, reliable, the characteristics of advanced technology, it is the satisfactory technology of measuring multi-hole coaxial error, solved the explosive motor manufacturing and thirsted for for a long time solving and open question, the powerful measure that detects cylinder body crankshaft hole, cam hole coaxiality error is provided for them.
Measuring method of the present invention is not limited to only be suitable for measurement mechanism of the present invention, also can be used for other similar device, measures the coaxiality error of porous.
Measurement mechanism of the present invention also is not limited to the described embodiment of accompanying drawing.
Claims (10)
1, a kind of measuring method of multi-hole coaxial error, measuring process is characterized in that by computer controlled automatic measuring process is as follows:
(1) with measured workpiece in accordance with regulations direction be placed in movably on the worktable, be transplanted on the measuring position and be locked;
(2) rotating shaft that survey sensor is housed is inserted in the measured hole of measured workpiece and the location automatically;
(3) rotating shaft is rotated, the sensor equiangular sampling in each hole of computer controlled measurement shows the each measured value of sampling of each hole profile simultaneously respectively successively on screen;
(4) computing machine calculates the cross section least square center of each sensor scan by minimum two-multiply law;
(5) the least square center line of the two ends measured hole that is calculated with above-mentioned (4) calculates the distance of the least square center of each measured hole to benchmark, 2 times of coaxiality errors that are measured hole of this distance as the benchmark of measuring other each measured hole;
(6) measure end.Screen display measured hole least square center is with respect to the eccentric direction synoptic diagram of benchmark, X, and y coordinate figure and coaxiality error value are printed measurement result.
2, the measuring method of multi-hole coaxial error according to claim 1 is characterized in that:
(1) center of circle of least square circle is calculated by following formula and is determined:
a
K= 2/(N) X
KR(1) b
K= 2/(N) X
KI(1)
K=1,2 ..., m, m are the numbers of measured hole.a
kBe a component of degree n n real part of conversion in the richness 2/N doubly, b
kBe a component of degree n n imaginary part of sad conversion in the richness 2/N doubly;
(2) straight-line equation as the measured hole benchmark is:
(x-a
1)/(a
m-a
1) = (y-b
1)/(b
m-b
1) = (z-z
1)/(z
m-z
1)
The direction number of this straight line is:
(3) formula of the least square center of measured hole profile below the distance of reference line is pressed calculates:
(4) coaxiality error calculates by following formula:
Φfi=2hi
I=2 in the formula, 3,4 ..., m-1.
3, multi-hole coaxial error measuring method according to claim 1 and 2 is characterized in that, when the length-diameter ratio of measured hole≤0.5, measures the least square center that calculates a cross section of measured hole, estimates coaxiality error with this center of circle to the distance of benchmark; When the length-diameter ratio of measured hole>0.5, measure the least square center that calculates two cross sections of measured hole and the center of circle distance to benchmark, estimate coaxiality error with big one of error in two cross sections.
4, the measuring method of multi-hole coaxial error according to claim 3 is characterized in that measuring the per 10 ° of once sampling of sensor in each hole, the profile in each hole 36 points of sampling altogether.
5, a kind of multi-hole coaxial error measurement mechanism that designs according to the described multi-hole coaxial error measuring method of claim 1, the computing machine that comprises the automatic control survey process, display device, printing equipment, it is characterized in that also comprising the rotating shaft (10) (11) that sensor (20) are housed, drive the axially movable drive unit of rotating shaft (3), drive the motor (14) that rotating shaft is rotated, movably worktable (13) and angle sender set (19) that takes measurement of an angle and photoelectric sensor (18), measured workpiece (12) is placed in movably on the worktable (13), measured hole is to facing toward rotating shaft (10) (11), each measured hole is measured by the respective sensor (20) that is installed in the rotating shaft, motor passes through x, y bidirectional elastic shaft coupling (15) drives rotating shaft and rotates, the angle sender set is placed in the position of rotating synchronously with rotating shaft, photoelectric sensor is placed on the static housing of phase countershaft (9), rotating shaft, motor and housing are coupled to one, move at the driving lower edge of drive unit (3) guide rail (8).
6, measurement mechanism according to claim 4, each measured hole that it is characterized in that measured workpiece is measured by one or two sensor scan, all sensors is arranged in the same shaft section of rotating shaft, the support (17) that computer CPU plate and sensor circuit board (16) are installed is fixedly installed togather with rotating shaft, between rotating shaft and motor.
7, according to claim 5 or 6 described measurement mechanisms, it is characterized in that measurement mechanism is a vertical structure, assembling connects all-in-one-piece motor (14), support (17) and rotating shaft (10), (11), be suspended on along guide rail (8) slidably on the balladeur train (6) balance weight (2) balance that the chain (4) that the weight of suspension body is being supported by sprocket wheel (5) hangs by end face floating bearing (7).
8, measurement mechanism according to claim 7, it is characterized in that the rotating shaft lower end is the conical surface, rotating shaft is a two supports, outer conical surface (21) positioning support of upper end by bearing holder (housing, cover) is at the measured workpiece nose end in hole topmost, the lower end is by bearing (22) radial location, and its structure is to drive locking ball by sliding sleeve to move that to make cylindrical be that the lower bearing sleeve swelling of the conical surface is in the measured hole of lower end.
9, measurement mechanism according to claim 7, it is characterized in that driving rotating shaft, to make axially movable drive unit be cylinder piston structure, the sensor that is installed in the rotating shaft is the eddy current sensor of band contact.
10, measurement mechanism according to claim 8, it is characterized in that driving rotating shaft, to make axially movable drive unit be cylinder piston structure, the sensor that is installed in the rotating shaft is the eddy current sensor of band contact.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN91107268A CN1034692C (en) | 1991-08-13 | 1991-08-13 | Method and apparatus for multi-hole coaxial error measuring |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN91107268A CN1034692C (en) | 1991-08-13 | 1991-08-13 | Method and apparatus for multi-hole coaxial error measuring |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1069570A true CN1069570A (en) | 1993-03-03 |
CN1034692C CN1034692C (en) | 1997-04-23 |
Family
ID=4908623
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN91107268A Expired - Fee Related CN1034692C (en) | 1991-08-13 | 1991-08-13 | Method and apparatus for multi-hole coaxial error measuring |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1034692C (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100455980C (en) * | 2005-01-24 | 2009-01-28 | 青岛科技大学 | Coaxiality measuring instrument |
CN101915538A (en) * | 2010-07-16 | 2010-12-15 | 沈阳飞机工业(集团)有限公司 | Method for measuring coaxiality of porous part |
CN101694374B (en) * | 2009-10-20 | 2012-07-04 | 西安交通大学 | Rapid detecting device and detecting method of precision of blades of gas turbine |
CN103604395A (en) * | 2013-11-05 | 2014-02-26 | 西安航空动力控制科技有限公司 | Geometric element measurement method with short hole as reference |
CN103868479A (en) * | 2014-03-18 | 2014-06-18 | 同济大学 | Automatic nozzle hole structure parameter measuring method |
CN104390542A (en) * | 2014-11-12 | 2015-03-04 | 郑州磨料磨具磨削研究所有限公司 | Limit gauge detecting device and limit gauge detecting method using same |
CN104675385A (en) * | 2014-09-12 | 2015-06-03 | 北京精密机电控制设备研究所 | Mounting error correcting method and system |
CN106168468A (en) * | 2016-08-31 | 2016-11-30 | 徐工集团工程机械有限公司 | Hole detecting system and method |
CN106556359A (en) * | 2016-11-25 | 2017-04-05 | 中车戚墅堰机车有限公司 | The method that body axiality is detected using body coaxality measuring mechanism |
CN106643443A (en) * | 2017-03-03 | 2017-05-10 | 许昌德通振动搅拌技术有限公司 | Coaxiality detection device and method for mixing cylinders of concrete mixer |
CN106969740A (en) * | 2017-04-14 | 2017-07-21 | 微微百检测技术(北京)有限公司 | Hole perpendicularity measurement apparatus and system |
CN108981642A (en) * | 2018-09-19 | 2018-12-11 | 北京铂阳顶荣光伏科技有限公司 | Axiality detection device and concentricity detection system |
CN111521144A (en) * | 2020-05-13 | 2020-08-11 | 山西汾西重工有限责任公司 | Concentricity processing method and system |
CN113624192A (en) * | 2021-08-18 | 2021-11-09 | 江苏科技大学 | Large diesel engine hole coaxiality measuring method based on multiple optimization |
CN114111690A (en) * | 2021-10-29 | 2022-03-01 | 江苏上汽汽车变速器有限公司 | Method and system for measuring coaxiality and roundness of differential shell |
CN117592313A (en) * | 2024-01-18 | 2024-02-23 | 成都飞机工业(集团)有限责任公司 | Simulation optimization method for uncertainty of shape and position error measurement |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1285887C (en) * | 2004-06-23 | 2006-11-22 | 潘汉军 | Method for measuring and adjusting alignment error for coupling members of rotating shaft and instrument system therefor |
CN100582659C (en) * | 2004-11-13 | 2010-01-20 | 鸿富锦精密工业(深圳)有限公司 | Complex position degree computing system and method |
CN106863014B (en) * | 2017-02-24 | 2018-09-04 | 大连理工大学 | A kind of five-axle number control machine tool linear axis geometric error detection method |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4064633A (en) * | 1976-03-10 | 1977-12-27 | Wertepny Alexander W | Gauging instrument |
CN86200163U (en) * | 1986-01-20 | 1986-09-03 | 北京工业学院 | Large-sized part axiality meter |
CN86205007U (en) * | 1986-07-29 | 1987-09-02 | 沈阳第一机床厂 | Hole concentricity inspection instrument |
-
1991
- 1991-08-13 CN CN91107268A patent/CN1034692C/en not_active Expired - Fee Related
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100455980C (en) * | 2005-01-24 | 2009-01-28 | 青岛科技大学 | Coaxiality measuring instrument |
CN101694374B (en) * | 2009-10-20 | 2012-07-04 | 西安交通大学 | Rapid detecting device and detecting method of precision of blades of gas turbine |
CN101915538A (en) * | 2010-07-16 | 2010-12-15 | 沈阳飞机工业(集团)有限公司 | Method for measuring coaxiality of porous part |
CN103604395A (en) * | 2013-11-05 | 2014-02-26 | 西安航空动力控制科技有限公司 | Geometric element measurement method with short hole as reference |
CN103868479A (en) * | 2014-03-18 | 2014-06-18 | 同济大学 | Automatic nozzle hole structure parameter measuring method |
CN103868479B (en) * | 2014-03-18 | 2017-07-28 | 同济大学 | A kind of hole structural parameter method for automatic measurement |
CN104675385A (en) * | 2014-09-12 | 2015-06-03 | 北京精密机电控制设备研究所 | Mounting error correcting method and system |
CN104675385B (en) * | 2014-09-12 | 2018-03-09 | 北京精密机电控制设备研究所 | Alignment error bearing calibration and system |
CN104390542A (en) * | 2014-11-12 | 2015-03-04 | 郑州磨料磨具磨削研究所有限公司 | Limit gauge detecting device and limit gauge detecting method using same |
CN104390542B (en) * | 2014-11-12 | 2017-08-25 | 郑州磨料磨具磨削研究所有限公司 | Difference gauge detection means and the difference gauge detection method using the device |
CN106168468A (en) * | 2016-08-31 | 2016-11-30 | 徐工集团工程机械有限公司 | Hole detecting system and method |
CN106556359A (en) * | 2016-11-25 | 2017-04-05 | 中车戚墅堰机车有限公司 | The method that body axiality is detected using body coaxality measuring mechanism |
CN106643443A (en) * | 2017-03-03 | 2017-05-10 | 许昌德通振动搅拌技术有限公司 | Coaxiality detection device and method for mixing cylinders of concrete mixer |
CN106643443B (en) * | 2017-03-03 | 2022-09-13 | 德通智能科技股份有限公司 | Device and method for detecting coaxiality of mixing cylinder of concrete mixer |
CN106969740A (en) * | 2017-04-14 | 2017-07-21 | 微微百检测技术(北京)有限公司 | Hole perpendicularity measurement apparatus and system |
CN106969740B (en) * | 2017-04-14 | 2023-07-14 | 微微一百检测技术(北京)有限公司 | Hole verticality measuring device and system |
CN108981642A (en) * | 2018-09-19 | 2018-12-11 | 北京铂阳顶荣光伏科技有限公司 | Axiality detection device and concentricity detection system |
CN111521144A (en) * | 2020-05-13 | 2020-08-11 | 山西汾西重工有限责任公司 | Concentricity processing method and system |
CN113624192A (en) * | 2021-08-18 | 2021-11-09 | 江苏科技大学 | Large diesel engine hole coaxiality measuring method based on multiple optimization |
CN114111690A (en) * | 2021-10-29 | 2022-03-01 | 江苏上汽汽车变速器有限公司 | Method and system for measuring coaxiality and roundness of differential shell |
CN114111690B (en) * | 2021-10-29 | 2024-05-03 | 江苏上汽汽车变速器有限公司 | Method and system for measuring coaxiality and roundness of inferior shell |
CN117592313A (en) * | 2024-01-18 | 2024-02-23 | 成都飞机工业(集团)有限责任公司 | Simulation optimization method for uncertainty of shape and position error measurement |
CN117592313B (en) * | 2024-01-18 | 2024-05-14 | 成都飞机工业(集团)有限责任公司 | Simulation optimization method for uncertainty of shape and position error measurement |
Also Published As
Publication number | Publication date |
---|---|
CN1034692C (en) | 1997-04-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1069570A (en) | Multi-hole coaxial error measuring method and device | |
CN102313747B (en) | Image acquisition system for sawn timber surface defects and detection method | |
CN108775887B (en) | A kind of detection method of lithium battery | |
CN101769727B (en) | Online automatic detection system of local straight degree of circular-section workpiece | |
CN101975819A (en) | Automatic eddy current/ magnetic memory device for detecting defect on surface layer of inner wall of old cylinder barrel | |
CN116223527B (en) | Corrosion detection device and detection method for hydraulic hoist piston rod | |
CN220040286U (en) | Adjustable climbing mechanism of hydraulic hoist piston rod rust detection device | |
CN1527022A (en) | Self-separation method and device for spatial error of superprecise revolution reference | |
CN116678297A (en) | Aluminum profile flatness detection device | |
CN209877932U (en) | Nuclear reaction column assembly installation and measurement tool | |
CN107339967B (en) | Roundness measuring instrument | |
CN109188027A (en) | A kind of six-dimension acceleration sensor experimental rig and its test method | |
CN109489613A (en) | A kind of high-acruracy survey mechanism for measuring for verticality | |
CN117968946A (en) | Dynamic balance testing device for counterweight eccentric sleeve | |
CN1580687A (en) | Detector for measuring the thickness of an medium | |
CN210625623U (en) | Novel parallelism detector | |
CN109341552A (en) | A kind of tubular element bidimensional automatic laser measuring thickness device, system and method | |
CN103852473B (en) | Detection device for detector and detection method | |
CN209512819U (en) | A kind of high-acruracy survey mechanism for measuring for verticality | |
CN209455630U (en) | Cylindrical glass stick lifting translational transport device | |
CN111380483A (en) | Internal combustion engine camshaft outline detector and detection method | |
CN111397469A (en) | System and method for detecting errors and dynamics of profile of cylindrical intermittent cam | |
CN109974650A (en) | Plain thrust bearing retainer clearance detector and method | |
CN2107008U (en) | Multihole axiality error measuring system | |
CN210036625U (en) | Crankshaft part crank phase detection device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |