CN104330065A - Spiral bevel gear tooth surface curvature interference detection method - Google Patents

Spiral bevel gear tooth surface curvature interference detection method Download PDF

Info

Publication number
CN104330065A
CN104330065A CN201410362434.6A CN201410362434A CN104330065A CN 104330065 A CN104330065 A CN 104330065A CN 201410362434 A CN201410362434 A CN 201410362434A CN 104330065 A CN104330065 A CN 104330065A
Authority
CN
China
Prior art keywords
tooth
flank
steamboat
actual measurement
interference
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
Application number
CN201410362434.6A
Other languages
Chinese (zh)
Other versions
CN104330065B (en
Inventor
曹雪梅
孙宁
刘数
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.)
Henan University of Science and Technology
Original Assignee
Henan University of Science and 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 Henan University of Science and Technology filed Critical Henan University of Science and Technology
Priority to CN201410362434.6A priority Critical patent/CN104330065B/en
Publication of CN104330065A publication Critical patent/CN104330065A/en
Application granted granted Critical
Publication of CN104330065B publication Critical patent/CN104330065B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • G01B21/20Measuring 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

The invention discloses a spiral bevel gear tooth surface curvature interference detection method. Only by providing coordinate values of a plurality of discrete points of two tooth surfaces, tooth surface interference position can be accurately judged and actually-measured engagement position can be prejudged, and efficient and convenient and fast tooth surface curvature interference detection is provided for a gear pair, so that the technical problem that the gear pair can only carry out pairing rolling inspection on a rolling inspection machine to detect the tooth surface curvature interference is solved; not only the position of tooth surface interference can be accurately judged, but also the actually-measured engagement position can be prejudged. The detection method helps to expand the detection function of a gear measurement center without carrying out rolling inspection on the gear rolling inspection machine; whether the two tooth surfaces have tooth surface curvature interference can be judged directly according to the position vector and normal vector of the tooth surface points measured by the gear measurement center; and if interference occurs, the position of the interference can be judged.

Description

A kind of spiral bevel gear flank of tooth curvature interference method of inspection
Technical field
The invention belongs to gears meshing analysis and testing technology field, be specifically related to a kind of spiral bevel gear flank of tooth curvature interference method of inspection.
Background technology
The necessary condition realizing correct engagement without curvature interference at contact point place during two flank engagement.When Gear Processing because the factors such as machine tool error, alignment error, heat treatment deformation cause larger tooth surface error, during two mating gears engagements, there is flank of tooth curvature interference and cannot correct engagement.
The inspection of flank of tooth curvature interference only calculates in tooth surface design phase analysis at present, and judged with relative Geodesic torsion by the Relative normal curvature calculating two tooth face meshing point, the method is the determination methods based on local topology.As Shen Yunbo, in the paper " method of face gear drive engagement process Relative normal curvature interference detection " of the people such as Fang Zongde, propose the method for the Relative normal curvature extremal curvature interference inspection of a kind of the whole engagement process of gear drive, namely the method is a kind of determination methods based on local topology, finished gear pair needs inspection machine carries out pairing to roll inspection rolling, by particular location and the degree of rolling tested stamp trace and rule of thumb judge flank of tooth curvature interference.
In addition, carry out at gear measuring center the important means that the detection of flank of tooth three-dimensional has become flank of tooth detection, but this flank of tooth detects just for measurement and the analysis of the tooth accuracy of single gear, cannot analyze two flank engagement performances.
Summary of the invention
The object of this invention is to provide a kind of spiral bevel gear flank of tooth curvature interference method of inspection, only need the coordinate figure of some discrete points that two flank of tooth are provided, the position of flank interference can be judged accurately and the position of engagement can be surveyed to it and carry out anticipation.
In order to realize above object, the technical solution adopted in the present invention is: a kind of spiral bevel gear flank of tooth curvature interference method of inspection, comprises the steps:
(1) theoretical tooth surface equation and the steamboat benchmark flank of tooth of spiral bevel gear bull wheel is set up;
(2) three-dimensional detection is carried out to the large and small actual measurement processing flank of tooth of taking turns, obtain large and small position vector and method arrow of taking turns actual measurement processing flank of tooth check point;
(3) based on mesh equation, to vow according to the position vector of bull wheel actual measurement processing flank of tooth check point, method and large steamboat ratio of gear is set up and surveyed with bull wheel the steamboat subsidiary face processing flank of tooth total conjugated;
(4) digital tooth that steamboat subsidiary face is set up in the matching of bicubic nurbs surface is carried out to the discrete point on steamboat subsidiary face;
(5) net point calculated respectively by position equation in the digital tooth in the steamboat benchmark flank of tooth and steamboat subsidiary face is vowed according to the position vector of steamboat actual measurement processing flank of tooth check point and method;
(6) flank of tooth topological variation value of the steamboat actual measurement processing flank of tooth, steamboat subsidiary face and steamboat reference field is calculated respectively with thus calculate steamboat subsidiary face and the flank of tooth topological variation value δ processing the flank of tooth surveyed by steamboat ij, according to δ ijjudge whether the large and small flank of tooth of taking turns of surveying processing flank of tooth curvature interference occurs.
The steamboat benchmark flank of tooth in described step (1) is that theoretical tooth surface equation, mesh equation and the large steamboat ratio of gear relation according to bull wheel is set up, this steamboat benchmark flank of tooth and the theoretical flank of tooth total conjugated of bull wheel.
The flank of tooth topological variation value of the steamboat actual measurement processing flank of tooth and steamboat reference field computation process as follows:
δ 1 ij = ( x 1 ij - x 0 ij ) 2 + ( y 1 ij - y 0 ij ) 2 + ( z 1 ij - z 0 ij ) 2 cos γ 1
Wherein, γ 1it is steamboat actual measurement processing flank of tooth check point measuring point to steamboat reference field line and steamboat reference field on the angle of measuring point normal.
The computing formula of the flank of tooth topological variation value of steamboat subsidiary face and steamboat reference field is as follows:
δ 3 ij = ( x 3 ij - x 0 ij ) 2 + ( y 3 ij - y 0 ij ) 2 + ( z 3 ij - z 0 ij ) 2 cos γ 3
Wherein, γ 3for steamboat subsidiary face check point measuring point to steamboat reference field line and steamboat reference field on the angle of measuring point normal.
The flank of tooth topological variation value δ of the flank of tooth surveyed by steamboat subsidiary face and steamboat ijcomputing formula:
δ ij = δ 1 ij - δ 3 ij .
According to δ ijwhat judge to survey processing large and smallly takes turns the flank of tooth that whether the principle of flank of tooth curvature interference occurs is as follows: if δ ijbe less than 0, illustrate this steamboat actual measurement the flank of tooth and steamboat subsidiary face have gap, this point is without curvature interference; If δ ijbe greater than 0, illustrate that in this point two flank of tooth gap be negative, then this some generation curvature interference, can not correct engagement; δ ijlarger, interfere more serious, the actual measurement position of engagement appears in the maximum position of interference degrees.
The spiral bevel gear flank of tooth curvature interference method of inspection of the present invention only needs the coordinate figure of the some discrete points providing two flank of tooth, the position of flank interference can be judged accurately and the position of engagement can be surveyed to it and carry out anticipation, for gear pair provide efficiently, the flank of tooth curvature interference method of inspection easily, solve gear pair and can only roll technical barrier inspection machine carrying out matching and rolls inspection inspection flank of tooth curvature interference, not only can judge the position of flank interference accurately but also the position of engagement can be surveyed to it and carry out anticipation.This method of inspection has expanded the measuring ability of gear measuring center, inspection is rolled without the need to rolling at gear on inspection machine, the position vector of the flank of tooth point that can directly detect according to gear measuring center and method are vowed and are judged whether two flank of tooth flank of tooth curvature interference occurs, if interfered, can judge the position of interfering.
Accompanying drawing explanation
Fig. 1 is the process flow diagram of the spiral bevel gear flank of tooth curvature interference method of inspection of the present invention;
Fig. 2 is the perspective view of net point in rotating and projection plane;
Fig. 3 is without curvature interference surface deviation topological diagram;
Fig. 4 curvature interference surface deviation topological diagram.
Embodiment
Below in conjunction with accompanying drawing and specific embodiment, the present invention is described further.
Be illustrated in figure 1 the process flow diagram of the spiral bevel gear flank of tooth curvature interference method of inspection of the present invention, as seen from the figure, this method of inspection comprises the steps:
(1) theoretical tooth surface equation and the steamboat benchmark flank of tooth of spiral bevel gear bull wheel is set up: set up the theoretical tooth surface equation of bull wheel according to the basic parameter of spiral bevel gear and machined parameters, wheel blank parameter and machined parameters, as shown in table one and table two, are set up by coordinate transform and mesh equation and are set up bull wheel tooth surface equation respectively:
r 2=r 2gg)
In formula, θ g, φ git is bull wheel tooth surface parameters.
Steamboat benchmark flank of tooth Σ 0be defined as the steamboat flank of tooth with bull wheel flank of tooth total conjugated---be linear contact lay during bull wheel flank engagement, and ratio of gear is gear ratio, and known bull wheel tooth surface equation is r 2g, φ g), according to mesh equation
And bull wheel engagement corner with steamboat engagement corner relation:
Steamboat reference field Σ can be obtained 0tooth surface equation r 0g, φ g).
Table 1 wheel blank parameter
Table 2 machined parameters
Parameter Bull wheel machined parameters Steamboat machined parameters
Cutter diameter D C2/mm 228.6 152.4
Point width p w2/mm 2.5511 2.5511
Cutter number 12 7.5
Radial S r/mm 97.82527 80.099557
Angle cutter spacing q/mm 73.157580 51.194019
Roll and compare m p 1.268996 1.624315
Workhead offset E m/mm -0.1 0.1
Axial position of wheel X G/mm -0.8 -0.8
Berth X B/mm 0.378493 -0.554708
Wheel blank established angle r/ (°) 48.2833 35.8675
(2) respectively three-dimensional detection is carried out to the large and small actual measurement processing flank of tooth of taking turns at gear measuring center, obtain large and small position vector and method arrow (position vector and the method that obtain flank of tooth discrete point are vowed) of taking turns actual measurement processing flank of tooth check point: bull wheel actual measurement processing flank of tooth check point position vector and method are vowed and are expressed as steamboat actual measurement processing flank of tooth check point position vector and method are vowed and are expressed as subscript ij represents the numbering of check point, as shown in Figure 2.
(3) structure steamboat subsidiary face: based on mesh equation, surveys position vector, the method arrow of processing flank of tooth check point according to bull wheel and the steamboat subsidiary face processing flank of tooth total conjugated surveyed by the foundation of steamboat ratio of gear and bull wheel greatly.
Bull wheel is surveyed flank of tooth check point be transformed in steamboat coordinate system through coordinate transform, corresponding position vector and method are vowed and are solve mesh equation
Bull wheel actual measurement flank of tooth check point can be obtained be transformed into engagement corner during steamboat coordinate system thus obtain the corresponding check point detected with bull wheel on the steamboat subsidiary face of flank of tooth total conjugated the position vector of this point can be expressed as r' ij.
(4) the digital tooth Σ that steamboat subsidiary face is set up in the matching of bicubic nurbs surface is carried out to the discrete point on steamboat subsidiary face 3.
The digital tooth Σ in steamboat subsidiary face 3equation is: r 3=r 3(u, v).
(5) according to the check point on the steamboat actual measurement flank of tooth position vector and method vow and find corresponding point on steamboat reference field the net point calculated respectively by position equation in the digital tooth in the steamboat benchmark flank of tooth and steamboat subsidiary face is vowed according to the position vector of steamboat actual measurement processing flank of tooth check point and method:
1. coordinate figure (the L of check point on steamboat rotating and projection face on the steamboat actual measurement flank of tooth is calculated ij, R ij), as shown in Figure 2,
L ij = x 1 ij
R ij = ( y 1 ij ) 2 + ( z 1 ij ) 2
2. according to the check point on the steamboat actual measurement flank of tooth coordinate (L on rotating and projection face ij, R ij) set up corresponding point on steamboat reference field position equation
x 0 ( θ g ij , φ g ij ) = L ij
y 0 ( θ g ij , φ g ij ) 2 + z 0 ( θ g ij , φ g ij ) 2 = R ij
Solving equation group, can obtain on steamboat reference field with check point corresponding point position vector and method is vowed
3. in like manner, according to the check point on the steamboat flank of tooth position vector and method vow, calculate steamboat digitizing subsidiary face Σ by position equation 3on corresponding point position vector can be expressed as method is vowed
(6) flank of tooth topological variation value of the steamboat actual measurement processing flank of tooth, steamboat subsidiary face and steamboat reference field is calculated respectively with thus calculate steamboat subsidiary face and the flank of tooth topological variation value δ processing the flank of tooth surveyed by steamboat ij, according to δ ijjudge whether the large and small flank of tooth of taking turns of surveying processing flank of tooth curvature interference occurs.
1. steamboat actual measurement flank of tooth Σ is calculated 1with steamboat reference field Σ 0flank of tooth topological variation value, the surface deviation of each measuring point is:
δ 1 ij = ( x 1 ij - x 0 ij ) 2 + ( y 1 ij - y 0 ij ) 2 + ( z 1 ij - z 0 ij ) 2 cos γ 1
γ 1for steamboat actual measurement flank of tooth check point measuring point to steamboat reference field line and steamboat reference field on the angle of measuring point normal.
2. steamboat subsidiary face Σ is calculated 3with steamboat reference field Σ 0flank of tooth topological variation, according to surface deviation definition, determine that the surface deviation of measuring point is:
δ 3 ij = ( x 3 ij - x 0 ij ) 2 + ( y 3 ij - y 0 ij ) 2 + ( z 3 ij - z 0 ij ) 2 cos γ 3
γ 3for steamboat subsidiary face check point measuring point to steamboat reference field line and steamboat reference field on the angle of measuring point normal.
The measuring point obtained on all steamboat subsidiary faces can obtain the flank of tooth topological variation of steamboat subsidiary face and steamboat reference field to the steamboat reference field upper deviation.
3. the flank of tooth topological variation value in the COMPREHENSIVE CALCULATING steamboat actual measurement flank of tooth and steamboat subsidiary face:
δ ij = δ 1 ij - δ 3 ij .
According to the topological variation δ of the flank of tooth ijjudge whether the size wheel flank of tooth of surveying processing flank of tooth curvature interference occurs: if δ ijbe less than 0, illustrate this steamboat actual measurement the flank of tooth and steamboat subsidiary face have gap, this point without curvature interference, as shown in Figure 3; If δ ijbe greater than 0, illustrate that in this point two flank of tooth gap be negative, then this some generation curvature interference, can not correct engagement, as shown in Figure 4; δ ijlarger, interfere more serious, the actual measurement position of engagement appears in the maximum position of interference degrees.
Above embodiment only understands core concept of the present invention for helping; the present invention can not be limited with this; for those skilled in the art; every according to thought of the present invention; the present invention is modified or equivalent replacement; any change done in specific embodiments and applications, all should be included within protection scope of the present invention.

Claims (6)

1. a spiral bevel gear flank of tooth curvature interference method of inspection, is characterized in that, comprise the steps:
(1) theoretical tooth surface equation and the steamboat benchmark flank of tooth of spiral bevel gear bull wheel is set up;
(2) three-dimensional detection is carried out to the large and small actual measurement processing flank of tooth of taking turns, obtain large and small position vector and method arrow of taking turns actual measurement processing flank of tooth check point;
(3) based on mesh equation, to vow according to the position vector of bull wheel actual measurement processing flank of tooth check point, method and large steamboat ratio of gear is set up and surveyed with bull wheel the steamboat subsidiary face processing flank of tooth total conjugated;
(4) digital tooth that steamboat subsidiary face is set up in the matching of bicubic nurbs surface is carried out to the discrete point on steamboat subsidiary face;
(5) net point calculated respectively by position equation in the digital tooth in the steamboat benchmark flank of tooth and steamboat subsidiary face is vowed according to the position vector of steamboat actual measurement processing flank of tooth check point and method;
(6) flank of tooth topological variation value of the steamboat actual measurement processing flank of tooth, steamboat subsidiary face and steamboat reference field is calculated respectively with thus calculate steamboat subsidiary face and the flank of tooth topological variation value δ processing the flank of tooth surveyed by steamboat ij, according to δ ijjudge whether the large and small flank of tooth of taking turns of surveying processing flank of tooth curvature interference occurs.
2. the spiral bevel gear flank of tooth curvature interference method of inspection according to claim 1, it is characterized in that: the steamboat benchmark flank of tooth in described step (1) is that theoretical tooth surface equation, mesh equation and the large steamboat ratio of gear relation according to bull wheel is set up, this steamboat benchmark flank of tooth and the theoretical flank of tooth total conjugated of bull wheel.
3. the spiral bevel gear flank of tooth curvature interference method of inspection according to claim 1, is characterized in that: the flank of tooth topological variation value of the steamboat actual measurement processing flank of tooth and steamboat reference field computation process as follows:
δ 1 ij = ( x 1 ij - x 0 ij ) 2 + ( y 1 ij - y 0 ij ) 2 + ( z 1 ij - z 0 ij ) 2 cos γ 1
Wherein, γ 1it is steamboat actual measurement processing flank of tooth check point measuring point to steamboat reference field line and steamboat reference field on the angle of measuring point normal.
4. the spiral bevel gear flank of tooth curvature interference method of inspection according to claim 1, is characterized in that: the computing formula of the flank of tooth topological variation value of steamboat subsidiary face and steamboat reference field is as follows:
δ 3 ij = ( x 3 ij - x 0 ij ) 2 + ( y 3 ij - y 0 ij ) 2 + ( z 3 ij - z 0 ij ) 2 cos γ 3
Wherein, γ 3for steamboat subsidiary face check point measuring point to steamboat reference field line and steamboat reference field on the angle of measuring point normal.
5. the spiral bevel gear flank of tooth curvature interference method of inspection according to claim 1, is characterized in that, the flank of tooth topological variation value δ of the flank of tooth surveyed by steamboat subsidiary face and steamboat ijcomputing formula:
δ ij = δ 1 ij - δ 3 ij .
6. the spiral bevel gear flank of tooth curvature interference method of inspection according to claim 1, is characterized in that, according to δ ijwhat judge to survey processing large and smallly takes turns the flank of tooth that whether the principle of flank of tooth curvature interference occurs is as follows: if δ ijbe less than 0, illustrate this steamboat actual measurement the flank of tooth and steamboat subsidiary face have gap, this point is without curvature interference; If δ ijbe greater than 0, illustrate that in this point two flank of tooth gap be negative, then this some generation curvature interference, can not correct engagement; δ ijlarger, interfere more serious, the actual measurement position of engagement appears in the maximum position of interference degrees.
CN201410362434.6A 2014-07-28 2014-07-28 A kind of spiral bevel gear flank of tooth curvature interference method of inspection Expired - Fee Related CN104330065B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410362434.6A CN104330065B (en) 2014-07-28 2014-07-28 A kind of spiral bevel gear flank of tooth curvature interference method of inspection

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410362434.6A CN104330065B (en) 2014-07-28 2014-07-28 A kind of spiral bevel gear flank of tooth curvature interference method of inspection

Publications (2)

Publication Number Publication Date
CN104330065A true CN104330065A (en) 2015-02-04
CN104330065B CN104330065B (en) 2017-03-29

Family

ID=52404835

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410362434.6A Expired - Fee Related CN104330065B (en) 2014-07-28 2014-07-28 A kind of spiral bevel gear flank of tooth curvature interference method of inspection

Country Status (1)

Country Link
CN (1) CN104330065B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108120596A (en) * 2017-12-13 2018-06-05 长安大学 A kind of spiral bevel gear root interference method of inspection
CN108917687A (en) * 2018-04-26 2018-11-30 太原理工大学 A kind of blade of aviation engine front and rear edge slight camber detection method
CN113175903A (en) * 2021-04-07 2021-07-27 湖北文理学院 Face gear error detection and machining control method, device and system
CN114754698A (en) * 2022-04-11 2022-07-15 重庆大学 Surface gear tooth surface measuring point planning and on-machine measuring method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002005654A (en) * 2000-06-20 2002-01-09 Akira Yoshida Measuring method for error in tooth plane of bevel bear
JP2004101247A (en) * 2002-09-05 2004-04-02 Osaka Seimitsu Kikai Kk Testing method for tooth profile measuring device
CN101294868A (en) * 2008-06-27 2008-10-29 北京工业大学 Single tooth type gear global error measuring apparatus and method
CN102636097A (en) * 2012-04-26 2012-08-15 北京工业大学 Method for measuring tooth profile deviation of gear based on double-side meshing
CN203053405U (en) * 2013-01-22 2013-07-10 北京工业大学 Rapid gear single error field measuring device based on double-face engagement
CN103344210A (en) * 2013-07-22 2013-10-09 北京工业大学 Gear error multi-degree of freedom assessing method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002005654A (en) * 2000-06-20 2002-01-09 Akira Yoshida Measuring method for error in tooth plane of bevel bear
JP2004101247A (en) * 2002-09-05 2004-04-02 Osaka Seimitsu Kikai Kk Testing method for tooth profile measuring device
CN101294868A (en) * 2008-06-27 2008-10-29 北京工业大学 Single tooth type gear global error measuring apparatus and method
CN102636097A (en) * 2012-04-26 2012-08-15 北京工业大学 Method for measuring tooth profile deviation of gear based on double-side meshing
CN203053405U (en) * 2013-01-22 2013-07-10 北京工业大学 Rapid gear single error field measuring device based on double-face engagement
CN103344210A (en) * 2013-07-22 2013-10-09 北京工业大学 Gear error multi-degree of freedom assessing method

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
刘东超: "弧齿锥齿轮真实齿面的测量重构及啮合性能分析", 《中国优秀硕士学位论文全文数据库 工程科技II辑》 *
吕罕聪: "螺旋锥齿轮测量方法研究", 《中国优秀硕士学位论文全文数据库 工程科技I辑》 *
张军辉等: "基于NURBS的弧齿锥齿轮真实齿面的数字化仿真", 《航空动力学报》 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108120596A (en) * 2017-12-13 2018-06-05 长安大学 A kind of spiral bevel gear root interference method of inspection
CN108120596B (en) * 2017-12-13 2019-07-30 长安大学 A kind of spiral bevel gear root interference method of inspection
CN108917687A (en) * 2018-04-26 2018-11-30 太原理工大学 A kind of blade of aviation engine front and rear edge slight camber detection method
CN113175903A (en) * 2021-04-07 2021-07-27 湖北文理学院 Face gear error detection and machining control method, device and system
CN114754698A (en) * 2022-04-11 2022-07-15 重庆大学 Surface gear tooth surface measuring point planning and on-machine measuring method
CN114754698B (en) * 2022-04-11 2023-08-04 重庆大学 Face gear tooth surface measuring point planning and on-machine measuring method

Also Published As

Publication number Publication date
CN104330065B (en) 2017-03-29

Similar Documents

Publication Publication Date Title
CN104330065A (en) Spiral bevel gear tooth surface curvature interference detection method
CN103256916B (en) Evaluation method of part flatness error based on minimum area
CN105159228B (en) 5-shaft linkage numerical control lathe realizes five axle scaling methods of RTCP functions
CN102636097B (en) Method for measuring tooth profile deviation of gear based on double-side meshing
CN107330142B (en) On-machine detection measuring point normal vector estimation method based on STL model
CN103925902A (en) Profile tolerance error measurement device and method based on arc surfaced cam isometric model
CN102554705B (en) Compensation machining method for optical free-form surfaces
CN104392476A (en) Method of extracting three-dimensional axis of tunnel based on minimum bounding box algorithm
CN103926563B (en) Ultra-short basic line five-element receiving array and water sound locating method thereof
CN103673976A (en) Method and system for converting and unifying composite type precision measuring coordinate system
CN103471572A (en) Total station networking measurement method of large-scale structural component
CN107617794B (en) A kind of double helical tooth annular gear processing method
CN104123725B (en) A kind of computational methods of single line array camera homography matrix H
CN104268837B (en) Electronic speckle interference fringe pattern phase information extracting method
CN105651311B (en) The test method of agricultural machinery working satellite navigation automatic Pilot precision
CN103994726A (en) Method for detecting fitting clearance between sheet metal part and mould
CN102862018A (en) Bacterial type blade simulation assembling method
CN106326575B (en) A kind of non-circular gear detection method based on coordinate method
CN102607386B (en) Method for measuring local geometric initial defects of steel member with box-shaped section
CN104750977B (en) A kind of method and device of complex position degree error evaluation
CN102768025B (en) Multi-step variable frequency projected fringe measurement method for measuring each point on object independently
CN104864800A (en) Hobbing cutter front angle detector and usage method
CN105604541A (en) Production logging multi-arm caliper inclined shaft correction processing method
CN104608876A (en) Digitized dock building method
CN103729559B (en) A kind of Workpiece's Tack Error analysis based on tolerance parameter and method of adjustment

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170329

Termination date: 20170728