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        ?

        Updating of CNC programs for improving accuracy of roll-bending forming

        2015-11-03 00:49:55SergeiBelykh
        關(guān)鍵詞:共青城軋輥軋機(jī)

        Sergei V.Belykh

        (Aviation Technology Komsomolsk-on-Amur State Technical University, Komsomolsk-on-Amur 6810132, Russia)

        ?

        Updating of CNC programs for improving accuracy of roll-bending forming

        Sergei V.Belykh

        (Aviation Technology Komsomolsk-on-Amur State Technical University, Komsomolsk-on-Amur 6810132, Russia)

        The work on correcting control programs for the NC roll bevel-bending machine ГМС-1 is a continuation of a complex of works on designing software. This paper covers possible reasons for the occurrence of finished extruded section-shaped piece deviations from its electronic analogue in computer-aided bending by rolling on a NC roll machine. A mathematical description for the procedure of correcting NC programs according to component results is presented. A design of a checking device providing optimal quality and accuracy of finished part geometrical measurements is proposed.

        NC; roll bending; pre-stressed state; numerical analysis

        CLC:TG174.4

        Aricle ID:2095-7262(2015)05-0570-03 Document code:A

        0 Introduction

        When automating elasto-plastic deformation processes, many development engineers run into a serious of processing problems. Whatever the accuracy of mathematical models of deformation process-ses is, the accurate manufacture of parts fully corresponding to their electronic models or standard samples, as a rule, is impossible. This is primarily due to the fact that, depending on a batch of work parts, a supplier and conditions of manufacture, storage and shipment of work parts as well as parameters of metal thermal treatment, if any in accordance to the manufacturing process, work part parameters may be inconsistent with tabled values used in designing NC programs. Variations in work-part cross-sectional geometrical parameters within tolerance limits according to reference books and classifications can markedly affect the results of a deformation process[1]. Variations in material mechanical characteristics can cause even greater errors and, for revealing actual parameters of a material, at least one work part from the batch should to be sent to a metrological examination, which may be a problem in conditions of the present-day production and cause an increase in time for a process design. The severity of taking into account for all mentioned above features hardly hinders the process of production automation in the filed of material deformation.

        Similar problems have occurred in designing software for the roll machine ΓCM-1 for bending extruded products. A part made with an NC program designed with using tabled cross-sectional geometrical parameters and characteristics of a material may be inconsistent with its actual shape specified in detailed engineering drawings. To solve the above-mentioned problem, it has been decided to use a system of NC program correction according to the first component results.

        1 Cross-sectional geometrical parameters

        Let us assume that, for some normalized work part with certain cross-sectional geometrical parameters and made of a material with required mechanical characteristics, there is a dependenceM(χ) charac-terizing values of a bending force and a resultant curvature. For the case of elasto-plastic work of a material, this dependence is defined by the following expression[2-3]:

        Mz=χ·E·J+χn·K·Jpl.

        (1)

        Atthegivendegreeofstress-strainedstateafterrelievinganactiveload,amaterialelasticrestitution[4-5]takesplaceandtheresidualcurvatureinacross-sectionisdefinedbythefollowingexpression[2-3]:

        (2)

        Arealworkpartmaygenerallydifferfromanormalizedonewithaveragedcharacteristicstakenfromareferencebookorclassificationbothovergeometricalparametersandmechanicalcharacteristicsofitsmaterial.Asaconsequence,thestiffnesscharacteristics[EJ]=f(χ)ofarealworkpartandnormalizedonewillbedifferent.Accordingly,thecurvatureofarealworkpartafterelasticrestitutionwilldifferfromtheratedonebysomevalueΔχwhichisfindfromthecomponentresults:

        Δχ=χ0-χ′,

        (3)

        whereχ0istheexpectancecurvaturevalueafterspringbackandχ′istheactualcurvaturevalueafterspringback.

        Δχ=0orχ0=χ′.

        (4)

        2 Cross-sectional model

        Adeviationofthegeneralizedstiffnesscharacteristic[EJ]=f(χ)ofarealworkpartwillbeconsiderednotgreatandthedependenceM(χ)forarealworkpartbesimilartoananalogdependenceforanormalizedworkpart.

        Let,byananalogywiththedependenceσ-εintheformofalinearpowerfunctionforelasto-plasticworkofamaterial[2-6],theM(χ)functionapproximationalsoberepresentedasalinearpowerfunction.Assumingequalstiffnesscross-sectionalcharacteristicsintheelasticdeformationzoneforarealworkpartandnormalizedone(Fig.1)

        [EJ]r=EJ,

        weobtain

        (5)

        Fig. 1 M(χ) dependence approximation

        WefindthevaluesAandmfromthelinearfunctionM=A(χ′)mgoingthroughtwopoints:

        (1)thepointofchangingelasticstrainsinthecross-sectionbeingconsideredintoplasticones:

        (6)

        Taking,asaninitiationofplasticstrains,thecurvature,atwhichplasticstrainsoccurinthelayerfarthestremovedfromtheneutralcross-sectionalline,wewrite:

        Thevalueh1-ynisfindfromthemodelforacomplexcross-section(Fig.2).

        Fig. 2Elasto-plasticbendforacompound-sectioncomponent

        or, taking into account (3),

        (7)

        ExpressingAfrom(6)andsubstitutingitinto(7),weobtain

        (8)

        Thelinearpowerdependencedescribedbyexpressions(5)and(8)characterizesthebehaviorofarealworkpartunderdeformation.

        Accordingto(5),asthebendingforceMinsomesectionofarealworkpartisachieved,thecurvaturethereinforelasto-plasticloadingisdefinedas

        (9)

        Afterelasticrestitutionwithrelievinganactiveload,thecurvaturewillchangebythevalue

        And the residual curvature is equal to

        (10)

        TocorrectanNCprogram,werecalculatetheinitialworkpartcurvaturesobtainedininvestigatingtheworkpartgeometryinthebendingplaneintonewvaluescorrespondingtotherealbehavioroftheworkpartunderdeformationwithconsiderationforitsactualstiffnesscharacteristics.

        ThecorrectedbythismeansNCprogramwillgivefarmoreaccu-rateresults,whichmakesitpossibletoreduceaninfluenceofparame-tersneglectedindesigningandtolessenlaborinputinfinishingworkswhichareinevitableinmakingcomplexhigh-precisionparts.

        Forcheckingafinishedpartgeometrydeviationfromitselectronicanalogueonecanuseacheckingdevicewhichconsistsinasetoflongitudinalmembers(gages)mountedatthesamebasealongthelengthofthepartandtherebyformingthepart-surfacegeneratinglineattheprescribedpoints(Fig.3).

        Fig. 3 A checking device

        3 Conclusion

        Theuseofthiskindofcheckingdevicewillmakeitpossibletopreventshapedeformationsbygravity,whichisinevitablewithothermethodsofchecking,thusimprovingaccuracyofasubsequentNCprogram

        correction. The readjustability of the device allows to check a wide range of standard parts at low expenses. The deviation may be measured both on coordinate-measuring machines and multi-purpose inspection tools. The selection of a measuring way and a tool depends on a required accuracy of measurements.

        [1]Вдовин С И. Методы расчета и проектирования на ЭВМ процессов штамповки листовых и профильных заготовок [M].С И Вдовин - М: Машиностроение, 1988.

        [2]Выгодский М Я, Справочник по высшей математике[M].М Я Выгодский- М: Наука, 865-872 .

        [3]Белых С В, Станкевич А В, Кривенок А А. Особенности автоматизированного изготовления стрингеров летательного аппарата с использованием роликового оборудования оснащенного ЧПУ [J]. Авиационная промышленность 2009:30-44.

        [4]Феоктистов С И, Белых С В, Кривенок А А. Перевалов. Аппроксимация геометрии контура дугами при контроле точности изготовления деталей летательных аппаратов[M].С И Феоктистов, - Комсомольск-на-Амуре: КнАГТУ, 2010:150-156.

        [5]Феоктистов С И. Автоматизация проектирования технологичес-ких процессов оснастки заготовительно-штамповочного производства авиационной промышленности[M]. Владивосток: Дальнаука, 2001.

        [6]Белых С В, Феоктистов С И, Станкевич А В.Аппроксимация геометрии контура дугами при контроле точности изготовления деталей летательных аппаратов[J].Ученые записки Комсомольского-на-Амуре государственного технического университета,2010:9-15.

        (編輯李德根)

        2015-01-06;修改日期:2015-07-06

        Sergei V. Belykh(1978-),男,阿穆?tīng)柟睬喑侨?,副教?工學(xué)博士,研究方向:數(shù)控加工,E-mail:belykhsv@knastu.ru。

        提高成形軋輥撓度的CNC程序校正研究

        Sergei V.Belykh

        (阿穆?tīng)柟睬喑菄?guó)立技術(shù)大學(xué) 飛行器制造系, 阿穆?tīng)柟睬喑?6810132, 俄羅斯 )

        針對(duì)數(shù)控滾機(jī)床ГМС-1工序校正控制程序設(shè)計(jì)復(fù)雜的問(wèn)題,分析發(fā)生擠壓塊偏離其彎曲數(shù)控滾軋機(jī)的原因,給出輥軋過(guò)程的數(shù)學(xué)描述。結(jié)果表明:校正的數(shù)控程序能夠根據(jù)組件檢查設(shè)備的狀態(tài),可以提高零件的幾何精度。

        NC; 軋輥撓度; 預(yù)應(yīng)力狀態(tài); 數(shù)值分析

        TG174.4

        10.3969/j.issn.2095-7262.2015.05.021

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