CN108168887A - A kind of test method investigated fabrication process parameters and influenced on gear engagement fatigue life - Google Patents

A kind of test method investigated fabrication process parameters and influenced on gear engagement fatigue life Download PDF

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Publication number
CN108168887A
CN108168887A CN201711455570.XA CN201711455570A CN108168887A CN 108168887 A CN108168887 A CN 108168887A CN 201711455570 A CN201711455570 A CN 201711455570A CN 108168887 A CN108168887 A CN 108168887A
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gear
parameters
fatigue life
engagement
experiment
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CN108168887B (en
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王延忠
陈燕燕
刘旸
刘鹏
杨凯
齐荣华
李菲
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Liu Xiaoyan
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Beihang University
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • G01M13/04Bearings
    • G01M13/045Acoustic or vibration analysis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H55/00Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
    • F16H55/02Toothed members; Worms
    • F16H55/17Toothed wheels

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Acoustics & Sound (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

The present invention is a kind of test method investigated fabrication process parameters and fatigue life is engaged on gear and is influenced, including:1. design experiment Basic parameters of gear;2. the combination of process parameters of large and small wheel processing is determined respectively;3. respectively to large and small wheel gear teeth grouping, and being processed according to fixed machined parameters, a pair of of gear exemplar is obtained;4. adjustment machines on test-bed a pair of of gear simultaneously carries out the engagement experiment of gear fatigue, tooth failure evolution is recorded every one section of set time;5. analyzing tooth failure data, the mean value in each group gear teeth service life is calculated, judges influence direction and size of each group machined parameters combination to gear engagement fatigue life, and filters out several group machined parameters optimal to extension gear engagement fatigue life and combines.The present invention can greatly reduce the quantity of tests exemplar, shorten the test period, reduce financial cost and time cost, avoid the error that respectively adjustment introduces during multipair Gear Processing and experiment, be conducive to improve test accuracy.

Description

A kind of test method investigated fabrication process parameters and influenced on gear engagement fatigue life
Technical field
The invention belongs to high performance and long service life gear drive fields, and in particular to a kind of investigation fabrication process parameters are to engagement The test method that fatigue life influences.
Background technology
Gear is actuated element indispensable in aviation, ship, precision machinery.Current manufacturing industry upgrading, equipment carry The overall situation of effect proposes various mechanical structure systems higher requirement, gear transmission structure bearing capacity therein, fatigue Reliability just seems even more important.And in today of gear geometry designs and analytical technology maturation, gear working method and technique Parameter optimization just becomes and extends gear fatigue life, improves the effective means of its fatigue reliability.
In order to really assess influence of the different process combination to the gear engagement service life, most effective believable method is to carry out not Same parameter processes the engagement fatigue test of gear.Existing general gear engagement fatigue test method is in the preparation of experiment gear In, whole gear teeth of single test gear are all processed using same set of machined parameters.Only by taking grinding process as an example, it is assumed that The combination of p group bull wheels grinding parameter and the combination of q group steamboats grinding parameter are investigated, corresponding every group of grinding parameter processes a full teeth Wheel need to process p × q to gear to complete the big steamboat engagement pairing loading fatigue test of different grinding parameter groupings.This scheme Although the steamboat that can more accurately obtain specific grinding parameter processing and the influence after bull wheel mating engagement, sample size is excessive, Test period is long.
Invention content
It is an object of the invention to:Under the premise of result of the test information content and test accuracy target is met, the present invention carries A kind of test method for simplifying quick investigation fabrication process parameters and being influenced on gear engagement fatigue life is gone out, for multigroup manufacture Technological parameter carries out gear engagement comparative test for fatigue life.
The present invention proposes a kind of test method investigated fabrication process parameters and influenced on gear engagement fatigue life, packet It includes:
Step S1:Design experiment Basic parameters of gear, including big tooth number z2, small tooth number z1, modulus m, pressure angle α, Helixangleβ etc.;
Step S2:The combination of process parameters of large and small wheel processing is determined respectively, and clearly needs the bull wheel machined parameters investigated Number of combinations p and steamboat machined parameters number of combinations q;
Step S3:The gear teeth on bull wheel and steamboat are divided into p groups and q groups respectively, are joined according to the processing determined in step S2 Number is processed so that machined parameters different from according to different gear teeth groupings.A pair of of gear exemplar is finally obtained, they The gear teeth there is same macroscopical geometry and different microscopic appearances by group differentiation;
Step S4:A pair of of the gear machined in step S3 is subjected to adjustment, gear fatigue is carried out on test-bed Engagement experiment.It is shut down every one section of set time and observation of taking pictures is carried out to whole flank of tooth, to find flank engagement failure in time simultaneously Record failure evolution;The gear teeth number of record failure, the gear teeth grouping where it and out-of-service time.Until each group occurs Fail the gear teeth, stops experiment;
Step S5:Tooth failure data are analyzed, calculate the mean value in each group gear teeth service life, it can be determined that each group machined parameters group The influence direction to gear engagement fatigue life and size are closed, and filters out and engages fatigue life optimal several groups to extending gear Machined parameters combine.
Further, in above-mentioned steps S3, every group of gear teeth number is no less than 2 teeth when being grouped to the gear teeth, to protect Confirmatory test data acquire enough information content.
Further, during the experiment of above-mentioned steps S4, can the big steamboat of subsidiary nearby vibration signal, monitor gear Tired state of development in engagement.
Beneficial effects of the present invention:
(1) the present invention provides a kind of method, and multigroup machined parameters are applied in multigroup gear teeth processing of same gear, And fatigue engagement experiment is carried out to single pair gear, for investigating influence of the different machining parameters to gear engagement fatigue behaviour.With Conventional gears engagement experiment process is compared, and method provided by the invention can greatly reduce the quantity of tests exemplar, and can be significantly Shorten the test period, reduce financial cost and time cost.
(2) method provided by the invention causes a pair of of gear of a needs during processing and testing.For each on gear For the gear teeth of the group using different machining parameters processing, trueness error caused by adjustment is consistent during processing and experiment, avoids The error that respectively adjustment introduces during multipair Gear Processing and experiment is conducive to improve test accuracy.
Description of the drawings
Fig. 1 is the test method flow chart of the present invention;
Fig. 2 is grinding test parameter grouping Processing scheme.
Specific embodiment
It elaborates below in conjunction with the accompanying drawings to the embodiment of the method for the present invention.Although the disclosure is shown in attached drawing Exemplary embodiment, it being understood, however, that may be realized in various forms the disclosure without should be by embodiments set forth here institute Limitation.It is to be able to be best understood from the disclosure, and can be complete by the scope of the present disclosure on the contrary, providing embodiment It is communicated to those skilled in the art.It should be noted that in the absence of conflict, embodiment and embodiment in the present invention In feature can be combined with each other.The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
The embodiment of the present invention investigates different technological parameter groups using the grinding process parameters of a pair of of spiral bevel gear as object Close the influence that fatigue life is engaged to it.The grinding process parameters of investigation include grinding linear velocity, transform into two factors of speed.It is real Example is applied to include the following steps:
Step (1):Design gear basic parameter, such as table 1.
1 embodiment gear parameter of table
Step (2):In view of the number of teeth of bull wheel and steamboat, steamboat is ground linear velocity, speed is transformed into and is set to two water respectively It is flat, such as table 2;By the grinding linear velocity of bull wheel, transform into speed be set to respectively three level, such as table 3.The steamboat then to be investigated processing ginseng Array conjunction has 4 groups, and the combination of bull wheel machined parameters has 9 groups.
2 steamboat cutting parameter testing program of table
3 bull wheel cutting parameter of table is grouped scheme
Step (3):The gear teeth on steamboat and bull wheel are divided into 4 groups and 9 groups, and respectively according to gear teeth group number in table 2 and table 3 The grinding process parameters combination of distribution, is processed on a pair of of gear blank, such as Fig. 2.
Step (4):It will process in obtained a pair of of gear normal mounting to engagement testing stand and carry out fatigue test.Every 2 is small When shut down the observation flank of tooth and tooth root situation and photograph to record, while gear revolution when recording shutdown.
Step (5):Due in this example steamboat failure occur earlier, to steamboat flank engagement failure logging (record) data into It goes and handles, calculate the average burn-out life of each group gear teeth, difference is ground linear velocities, transforms into velocity composition pair during contrast process Steamboat engages the influence of fatigue failure life, such as table 4.
Each tooth burn-out life statistical data of 4 steamboat of table
By statistical result it can be seen that:For each group gear teeth being processed using the combination of different grinding parameters, service life It is descending to be arranged as L1>L4>L2>L3.It can be found that transform into smaller two groups of gear teeth (the L1 and L4) longest-lived of speed;Grinding One group of (L3) service life that linear velocity is relatively low, to transform into speed larger is minimum.Conclusion obtains higher grinding linear velocity, relatively low transforms into Speed can play gear teeth meshing fatigue behaviour facilitation, the conclusion that the 1st group of machined parameters is selected to be processed as far as possible.
To sum up, by more than flow, multigroup machined parameters combination can be realized in the engagement fatigue test of a pair of of gear The assessment influenced on gear engagement fatigue life.The present invention is investigates gear multi-processing technological parameter to gear teeth meshing fatigue life Influence provide it is a kind of quick, save, high-precision test method.
Non-elaborated part of the present invention belongs to techniques well known.All shapes using equivalent transformation or equivalent replacement Into technical solution, all fall within rights protection scope of the present invention.

Claims (3)

1. a kind of test method investigated fabrication process parameters and influenced on gear engagement fatigue life, it is characterised in that:This method Include the following steps:
Step S1:Design experiment Basic parameters of gear, including big tooth number z2, small tooth number z1, modulus m, pressure angle α, spiral Angle beta;
Step S2:The combination of process parameters of large and small wheel processing is determined respectively, and clearly needs the bull wheel machined parameters combination investigated Number p and steamboat machined parameters number of combinations q;
Step S3:The gear teeth on bull wheel and steamboat are divided into p groups and q groups respectively, according in step S2 determine machined parameters into Row processing so that machined parameters different from according to different gear teeth groupings finally obtains a pair of of gear exemplar, their wheel Tooth has same macroscopical geometry and different microscopic appearances by group differentiation;
Step S4:A pair of of the gear machined in step S3 is subjected to adjustment, gear fatigue engagement is carried out on test-bed Experiment shuts down every one section of set time and carries out observation of taking pictures to whole flank of tooth, to find that flank engagement fails and records in time Failure evolution records the gear teeth number of failure, the gear teeth grouping where it and out-of-service time, until each group fails The gear teeth stop experiment;
Step S5:Tooth failure data are analyzed, calculate the mean value in each group gear teeth service life, it can be determined that the combination pair of each group machined parameters The influence direction of gear engagement fatigue life and size, and filter out and engage several groups of optimal processing of fatigue life to extending gear Parameter combination.
2. a kind of experiment side for investigating fabrication process parameters and being influenced on gear engagement fatigue life according to claim 1 Method, it is characterised in that:In the step S3, every group of gear teeth number is no less than 2 teeth when being grouped to the gear teeth, to ensure to try It tests data and acquires enough information content.
3. a kind of experiment side for investigating fabrication process parameters and being influenced on gear engagement fatigue life according to claim 1 Method, it is characterised in that:During the experiment of the step S4, can the big steamboat of subsidiary nearby vibration signal, monitoring gear nibble Tired state of development in conjunction.
CN201711455570.XA 2017-12-28 2017-12-28 A kind of test method investigated grinding process parameters and gear engagement fatigue life is influenced Active CN108168887B (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108533717A (en) * 2018-06-29 2018-09-14 重庆齿轮箱有限责任公司 A method of making double set gear teeth on Same Part
CN114216674A (en) * 2021-09-29 2022-03-22 中国航发湖南动力机械研究所 Gear fatigue test piece and manufacturing method thereof

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US20070058854A1 (en) * 2005-09-14 2007-03-15 Caskey Gregory T Gear pattern inspection system
CN103616303A (en) * 2013-12-02 2014-03-05 北京乐冶液压气动设备技术有限公司 Tension-compression and torsion vibration fatigue test device
CN104048825A (en) * 2014-05-28 2014-09-17 北京航空航天大学 Multi-sensor fusion type fault locating method for gearbox of wind turbine generator
CN104081173A (en) * 2012-01-30 2014-10-01 S.P.M.仪器公司 Apparatus and method for analysing the condition of a machine having a rotating part
CN106124198A (en) * 2016-06-17 2016-11-16 广西汽车集团有限公司 The main detection method by gear quality and system in a kind of main speed reducer of rear axle
CN106959211A (en) * 2017-03-15 2017-07-18 清华大学 The fatigue test device and its method of testing of a kind of gear engagement
CN107003207A (en) * 2015-03-13 2017-08-01 宝马股份公司 Method and apparatus for testing gears

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070058854A1 (en) * 2005-09-14 2007-03-15 Caskey Gregory T Gear pattern inspection system
CN104081173A (en) * 2012-01-30 2014-10-01 S.P.M.仪器公司 Apparatus and method for analysing the condition of a machine having a rotating part
CN103616303A (en) * 2013-12-02 2014-03-05 北京乐冶液压气动设备技术有限公司 Tension-compression and torsion vibration fatigue test device
CN104048825A (en) * 2014-05-28 2014-09-17 北京航空航天大学 Multi-sensor fusion type fault locating method for gearbox of wind turbine generator
CN107003207A (en) * 2015-03-13 2017-08-01 宝马股份公司 Method and apparatus for testing gears
CN106124198A (en) * 2016-06-17 2016-11-16 广西汽车集团有限公司 The main detection method by gear quality and system in a kind of main speed reducer of rear axle
CN106959211A (en) * 2017-03-15 2017-07-18 清华大学 The fatigue test device and its method of testing of a kind of gear engagement

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108533717A (en) * 2018-06-29 2018-09-14 重庆齿轮箱有限责任公司 A method of making double set gear teeth on Same Part
CN108533717B (en) * 2018-06-29 2019-11-08 重庆齿轮箱有限责任公司 A method of making double set gear teeth on Same Part
CN114216674A (en) * 2021-09-29 2022-03-22 中国航发湖南动力机械研究所 Gear fatigue test piece and manufacturing method thereof

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