Residual Stresses in Railway Axles

Similar documents
MTS Restan. Automatic System for Residual Stress Measurement by Hole-Drilling

Numerical simulation of radial compressor stages with seals and technological holes

Analysis of pressure losses in the diffuser of a control valve

Using Experimental Procedure to Improve the Efficiency of the Two Stand Reversing Cold Mill

Modeling of thin strip profile during cold rolling on roll crossing and shifting mill

Certification of AMS acc. EN 15267, Part 3 - Overview and First Experience -

DETERMINATION OF THE DEPTH OF CLOSED BLIND CRACKS IN NON-METAL CHECK SAMPLES AND TEST PANELS FOR PENETRANT TESTING

The Use of ILI In Dent Assessments

LOW-CYCLE FATIGUE LIFE OF AW 1050 ALUMINIUM ALLOY FSW AND TIG WELDED JOINTS

Design and Analysis of Rotary Lawn Mower

Engineering Practice on Ice Propeller Strength Assessment Based on IACS Polar Ice Rule URI3

PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADE WITH WINGLETS ON ROTATING CONDITION USING WIND TUNNEL

machine design, Vol.6(2014) No.3, ISSN pp

Tapered Roller Bearings in X-life quality Customer Information. Business Unit TRB Schweinfurt, 2013

3.3 Other processes - performance 3 PROCEEDINGS

J. J. Daly Metal Improvement Company Paramus New Jersey USA

Study to Establish Relations for the Relative Strength of API 650 Cone Roof Roof-to-Shell and Shell-to- Bottom Joints

Other Si min/max. Cr min/max. 0.4/ / / / Bal.

Analysis of dilatometer test in calibration chamber

Determination of the wind pressure distribution on the facade of the triangularly shaped high-rise building structure

intended velocity ( u k arm movements

Analysis of Shear Lag in Steel Angle Connectors

Mechanical Stabilisation for Permanent Roads

Torrild - WindSIM Case study

STRIP EDGE SHAPE CONTROL

Prof. B V S Viswanadham, Department of Civil Engineering, IIT Bombay

Procedia Engineering Procedia Engineering 2 (2010)

Calibration and Validation of the Shell Fatigue Model Using AC10 and AC14 Dense Graded Hot Mix Asphalt Fatigue Laboratory Data

A Low Cost Digital Angle Gage, version 3

Paper 2.2. Operation of Ultrasonic Flow Meters at Conditions Different Than Their Calibration

P Oskarshamn site investigation. Borehole: KAV01 Results of tilt testing. Panayiotis Chryssanthakis Norwegian Geotechnical Institute, Oslo

STRESS ANALYSIS OF BELL CRANK LEVER

POWER Quantifying Correction Curve Uncertainty Through Empirical Methods

Conventional Ship Testing

Stress and deformation of offshore piles under structural and wave loading

Low Profile Load Cells

University of Huddersfield Repository

MIKE NET AND RELNET: WHICH APPROACH TO RELIABILITY ANALYSIS IS BETTER?

Fatigue Analysis of a LUG Assembly

Comparing the calculated coefficients of performance of a class of wind turbines that produce power between 330 kw and 7,500 kw

Aerodynamic Analyses of Horizontal Axis Wind Turbine By Different Blade Airfoil Using Computer Program

P-04 Stainless Steel Corrugated Hoses and Metal Bellows Expansion Joints

3. Load Rating and Life

Hardware Triaxial and Consolidation Testing Systems Pressure Measurement and Control

Calibration Procedure

A Review of the Bed Roughness Variable in MIKE 21 FLOW MODEL FM, Hydrodynamic (HD) and Sediment Transport (ST) modules

Investigation of Inspection Performance on Cracked Railway Axles

Experimental investigation of the check valve behaviour when the flow is reversing

Variable Face Milling to Normalize Putter Ball Speed and Maximize Forgiveness

Design and Analysis of Pressure Safety Release Valve by using Finite Element Analysis

ITTC Recommended Procedures and Guidelines

Moyno ERT Power Sections. Operational Guidelines

Návrh vratného kanálu u dvoustupňového kompresoru Return channel design of the two stage compressor

Offshore platforms survivability to underwater explosions: part I

BAM - 3.2: Section Pressure Equipment Pressure Receptacles; Fuel Gas Storage Systems 26 th September 2014

Beamex. Calibration White Paper. Weighing scale calibration - How to calibrate weighing instruments

3 1 PRESSURE. This is illustrated in Fig. 3 3.

A Study on the Punch Shape for Improving Tool Life in Shearing AHSS

RESIDUAL EXPANSION OF CYLINDERS. INTERMEDIATE TEST RESULTS

Evaluation of aerodynamic criteria in the design of a small wind turbine with the lifting line model

Thin strip profile control capability of roll crossing and shifting in cold rolling mill

Calculating Total Uncertainty of Temperature Calibration with a Dry Block. Calibration White Paper. Beamex.

Numerical Simulation of Flow and Determination of Aerodynamic Forces in the Balanced Control Valve

SEMATECH Provisional Test Method for Pressure Cycle Testing Filter Cartridges Used in UPW Distribution Systems

Traceable calibration of automatic weighing instruments in dynamic operation

Safety and Longterm Accuracy of Bourdon Tube Pressure Gauges

DEVELOPMENT OF A ROBUST PUSH-IN PRESSUREMETER

Special edition paper

Risk-Based Condition Assessment and Maintenance Engineering for Aging Aircraft Structure Components

Analysis of fatigue failure in D-shaped karabiners

Tightening Evaluation of New 400A Size Metal Gasket

OMS Technical Information Technical data

Optimization of rotor profiles for energy efficiency by using chamber-based screw model

Chapter 12 Practice Test

THEORETICAL EVALUATION OF FLOW THROUGH CENTRIFUGAL COMPRESSOR STAGE

pren CEN standard-draft pr EN 12261

New Highly Productive Phased Array Ultrasonic Testing Machine for Aluminium Plates for Aircraft Applications

Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA , United States.

Figure 1 - JPIF proposal for ISO standardisation of the CAI test method

Modal Analysis of Barrels for Assault Rifles

Power efficiency and aerodynamic forces measurements on the Dettwiler-wind turbine

for Cold-Formed Steel Framing Products

Aalborg Universitet. Published in: Proceedings of Offshore Wind 2007 Conference & Exhibition. Publication date: 2007

THIN CYLINDERS AND SHELLS

Pressure coefficient on flat roofs of rectangular buildings

23 RD INTERNATIONAL SYMPOSIUM ON BALLISTICS TARRAGONA, SPAIN APRIL 2007

Wind Regimes 1. 1 Wind Regimes

The below identified patent application is available for licensing. Requests for information should be addressed to:

MIL-STD-883H METHOD EXTERNAL VISUAL

Level 3 Cambridge Technical in Engineering 05822/05823/05824/05825/05873 Unit 3: Principles of mechanical engineering

Study on wind turbine arrangement for offshore wind farms

Organisation Internationale de Métrologie Légale

PVP Copyright 2009 by ASME

ScienceDirect. Relating baseball seam height to carry distance

Irrigation &Hydraulics Department lb / ft to kg/lit.

INFLUENCE OF MEASURING PROCESS AUTOMATION ON UNCERTAINTY OF MASS STANDARD AND WEIGHTS CALIBRATION.

Certificate of Accreditation

Available online at ScienceDirect. Procedia Engineering 112 (2015 ) 40 45

TRACEABILITY FOR ROUNDNESS MEASUREMENTS OF ROLLS - European Metrology Research Programme, project No. IND62

Displacement-based calculation method on soil-pile interaction of PHC pipe-piles

Transcription:

Residual Stresses in Railway Axles ŘEHA BOHUSLAV 1,a,*, VÁCLAVÍK JAROSLAV 2,b NÁVRAT TOMÁŠ 3,c and DAVID HALABUK 3,d 1 GHH-BONATRANS GROUP a.s., Revoluční 1234, 735 94 Bohumín, Czech Republic 2 Výzkumný a zkušební ústav Plzeň s.r.o., Tylova 1581/46, 31 Plzeň, Czech Republic 3 Faculty of Mechanical Engineering, Brno University of Technology, Technická 2896/2, 616 69 Brno, Czech Republic a bohuslav.reha@ghh-bonatrans.com, b vaclavik@vzuplzen.cz, c navrat@fme.vutbr.cz, d david.halabuk@vutbr.cz Keywords: Residual Stresses, Railway Axle, Hole-Drilling Method, X-Ray Diffraction Abstract. The companies producing railway axles are obliged to demonstrate a level of residual stresses in their products based on the specification of standard EN 13261 in which the applicable methods are suggested and the allowable values of residual stresses are specified. An objective of this contribution is to arouse a discussion whether the requirements of the standard can be met by means of the suggested measuring methods - hole-drilling (according to ASTM E837-13 standard) or X-ray diffraction. It especially applies to the ability to determine the residual stress distribution in the depth of 2 mm below the surface. The mentioned issue is demonstrated by means of both measuring methods under various measurement conditions. Background The railway axles are exposed to the high operating stress. It especially includes the high-cycle fatigue where the high tension stresses reduce the material fatigue limit. At the same time, unevenly distributed residual stresses may cause the deformation of an axle and increase the stress amplitude originating during the axle rotation. These both values also refer to the quality of heat treatment and the manufacture of the axle. The demonstration of the low level of the residual stress is one part of the existing standards dealing with checking the quality of railway axles EN 13261 [1] and EN 1326 [2]. Both standards require that surface tension residual stresses measured in the depth of.1 mm below the axle surface are lower than 1 MPa. The standards also specify three sections where the measurements shall be carried out (Fig. 1). In each section there is requirement for two measurements in the angular separation by 12. In addition, the standard EN 13261 requires that the mutual deviation of the residual stresses measured at 6 points separated by the angle of 6 in the central section of the axle (a difference of the maximal and minimum values) must be within the interval up to 4 MPa (Fig. 1, section A). All the tests shall be carried out by means of a strain gauge or an X-Ray method. At the present time a new version of the EN 13261 standard is being prepared where in addition to the conventional strain gauge techniques such as the layer removal method and the sectioning method, the hole-drilling method according to ASTM E837-13a [3] standard is recommended. Measurement Methods Hole-Drilling Method. A hole is drilled into the centre of the strain gauge rosette in the steps by means of an end mill or a high speed turbine at the revolutions ranging from 2, to 4, rpm and the residual stress is calculated from the released strains using calibration constants. Content from this work may be used under the terms of the Creative Commons Attribution 3. license. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI. Published under license by Materials Research Forum LLC. 95

A B C 195 164 12 992 72 559 2156 A B C 6 3 12 24 12 12 18 Fig. 1 The points being measured on a railway axle according to the requirement of [1]. The level of the surface residual stresses are demonstrated at three sections (A, B, C). In the centre (A), the evenness of the residual stress is tested at another 6 points by 6 along the perimeter. (a) (b) Fig. 2 The equipment used for measuring residual stresses by means of the hole-drilling method RESTAN (a) and for measuring by means of the X-Ray method (b) The ASTM E837 standard specifies these constants for the Vishay rosettes of the sizes D 1/32, 1/16 and 1/8 inches. Using the largest rosette it is possible to determine the residual stresses to the depths up to 2 mm. The minimum depth is within the range from.25 to.1 mm according to a size of the rosette. Thus it would look like the minimum and maximal depths met the requirements of the standard for the tests of the railway axles. However, applying this standard is questionable in several aspects. No other shape of the strain gauge rosette than the one specified in the standard can be used as no calibration constants are specified for it. The hole must be drilled coaxially with the rosette centre with the accuracy of ±.4D (i.e..16 mm for the largest rosette) which sometimes is difficult to keep. The standard does not state any method for correcting the misalignment. The radial clearance angles on the end face of the cutting tool should not exceed the value of 1, however, the standard does not give any possibility how to correct the fact that the value would be greater. In the standard the calibration constants are set for a theoretical diameter of the hole being drilled. For the actual diameter of the drilled hole it is recommended to correct them using the quadratic interpolation. Uncertainty of the Hole-Drilling Method. According to [3] the uncertainty of determination of the uniform stresses by means of the power-series method is ±1%. It is not determined for the 96

integral method. In [4] an extensive analysis of a measuring error is carried out based on the uncertainties of the most of the input parameters. The main source of the uncertainties specified herein is the eccentricity of the hole being drilled (5 %), stress induced by drilling (5.5 %), a diameter of the hole being drilled and the material constants. When using the integral method, the error is the maximal on the surface due to the influence of the high uncertainty of the input parameters (misalignment, presence of large strain gradients, smaller gauge outputs in the first drilling steps, identification of the zero reference surface) and in the last step of the hole drilling when the uncertainty of the input parameters is increased due to the method lowest sensitivity. In [5] the effect the hole-bottom fillet radius for the case of using the power-series method is investigated however, the calculated measuring error for the first drilled depth is valid also in case of the evaluation by the integral method. A deviation of the released relative deformation for the radius of 5% of the hole diameter is estimated to be 1%. The diameter of a railway axle is approx. 2 mm. The derived error when we use the coefficients for flat surface is shown at Fig. 3a for the 1/8 and 1/16 inch rosettes. The released strain and the calculated residual stress are always lower on the curved surface at the surface layer. We derived also the error we would make if we use the correction of the standardized sensitivity coefficients by the quadratic approximation recommended by the standard [3] for the actual diameter of the drilled hole. The resultant error of the released relative deformation is shown at Fig. 3b where the comparison is carried out for the standardized hole diameter of D = 4 mm. The approximation of coefficients is carried out for the other diameters. The error increases with the depth being drilled and with a higher deviation from the standardized diameter. The maximal error is in the maximal depth being drilled. It is obvious from the considerations performed that the uncertainty of determination of the residual stresses on the axle surface and in the depth of 2 mm below the surface is very high and very hard to identify. We estimate that it can reach even 3% and more of the measured value depending on the stress state of the axle. For roll burnished or surface hardened axles the measuring error is increased due to the tri-axial stress state by additional at least 5% especially in bigger depth being drilled [6]. δε [%] 1-1 -2 1/16 inch rosette δσ HMH [%] 2 15 1 5 3,2 3,4 3,6 3,8 4 4,2-3 1/8 inch rosette -5-4,1,2,3,4,5 z/d [ ] -1,2,4,6,8 1 z/d [ ] a) b) Fig. 3 The dependence of the released relative deformation on the standardized depth below the surface. Due to the curvature of the surface the maximal error for the axle diameter D = 2 mm is reached on the surface (a). Due to the recalculation of the calibration coefficients to the actual diameter of the hole being drilled for the deviation from the hole diameter 4 mm (b) the error is the maximal in the maximal depth being drilled. Results An influence of the drilling steps. An example of the distribution of the measured residual stress on the surface-hardened axle is shown at Fig. 4. Three sets of measurements were carried out 97

with a 1/8 inch rosette (HBM RY61-3.2/12S, an electric motor of 2, rpm) with three different steps of drilling Δz =.25 mm (96 steps),.5 mm (48 steps) and.1 mm (24 steps) always to the final depth of 2.4 mm (An evaluation is carried out always for 2 depths). σ max, min [MPa] -1-2 -3-4 -5-6 σax.25mm σax.5mm σax.1mm σtang.25mm σtang.5mm σtang.1mm -7,5 1 1,5 2 z [mm] Fig. 4 An influence of the size of drilling steps Δz =.25,.5 and.1 mm on the distribution of the evaluated residual stresses by making the step finer the curve becomes smoother and correspond more to the reality. It is obvious that the resultant residual stress depth profile is not so warped for a finer step of the material drilling which rather corresponds to the reality. For the roughest step specified by the standard [3] the profile is the most warped especially at the place of the maximal depth being drilled. This is an undesirable effect, especially in case we evaluate a deviation of the residual stress in the depth of 2 mm at 6 points in one section of the axle. The hole drilling was carried out to the depth of 2.4 mm, not to the depth of 2 mm as required by the standard [3]. If the drilling is carried out only to the depth of 2 mm, then the dispersion of the residual stress value is very high probably for the reason that when the curve is smoothed, there is a lack of the values of bigger depths. Therefore we recommend carrying out the measurements to the depth bigger by approx. 4 steps than for which the evaluation is carried out. Stress variation around the axle. It was examined what was the mutual deviation of the evaluated residual stresses in the centre of the axle in the depth of 2 mm. The measurement was carried out with a 1/8 inch rosette again at six points separated by an angle of 6 and the result is shown at Fig. 5a where a double standard deviation of the evaluated stresses is given. The measurement was carried out for 4 axles made of the material A1N (R e = 52 MPa), A4T (R e = 58 MPa), for the surface-hardened axle and for the roll-burnished axle, the material OS (according to GOST 4728). The angular deviation of the residual stress for the axles made from the materials A1N and A4T is low and the requirement of the standard [1] can be reached. The results for the hardened and roll-burnished axle significantly exceed the permissible deviation of 4 MPa. This fact may be caused not only by a big measuring error which is increased with the measured value of the residual stress but also by the fact that the level of the residual stresses in both axles approximates to the yield point of the material. The stresses drawn at Fig. 5a are not corrected to the elastic-plastic stress state as there is no reliable method for integral method. A reliable method for the correction of the stresses approximating the yield point is derived for the uniform stress distribution through the depth [4]. This correction is presented at Fig. 5b for one measured point for the roll-burnished axle A1N. The profiles of non-corrected and corrected stresses measured both by a small 1/16 inch rosette (serving for measuring the residual stress on the axle surface), and by a big 1/8 rosette for determining the values in the depth of 2 mm are plotted here. The depth of the roll-burnished layer is approx. 5 mm and a drop of the 98

stress to the depth of 2 mm is very low so in our opinion the power-series method can be used for the evaluation although the requirement of the stress uniformity given in the previous versions [3] (e.g. ASTM E837-8) is not met. By the use of the power-series method in drilling to the depth of 4 mm we obtain a rough estimate of the average value of the residual stresses for the mean depth of 2 mm. This value does not show any significant dispersion and it can be used for the demonstration of the requirement of the standard for the uniformity [1]. -18,,5 1, 1,5 2, 2,5 z [mm] a) b) Fig. 5 The maximal deviation of the axial component of the residual stresses measured in the axle centre for two standard materials of the axles and for the hardened and roll-burnished axles (values non-corrected to the elastic-plastic stress state). An example of such correction of the residual stresses approximating to the yield point (b) represents shifting the distributions of the mean stresses towards the lower values (power-series method). σ [MPa] -2-4 -6-8 -1-12 -14-16 σmax, PS σmin, PS σmax, PS, Cor σmin, PS, Cor σmax, PS, 1/16 σmin, PS, 1/16 σmax, PS, 1/16, Cor σmin, PS, 1/16, Cor σ ax [MPa] 1-1 -2 HD HD 1 HD 2 X-Ray X-Ray 1 X-Ray 2-3 -4-5 -6-7 -8,5,1,15,2,25,3 z r [mm] Fig. 6 Comparison of the surface stresses measured by the hole-drilling method (HD) and the X- Ray method on the original () and 2 new surfaces (1, 2) after removing 2 1 mm layers. Another way how to avoid the high uncertainty of the determination the residual stress in the depth of 2 mm is the measurement on the removed layers. The investigation was carried out on the surface-hardened axle A4T on the original not machined surface and after that twice on the new surface where layers of the material of the thickness of 1 mm were removed successively by lathe-turning. The measurement was also carried out by the X-Ray method in several gradually etched depths from these surfaces. At Fig. 6 there is a comparison of the subsurface residual stresses using the 1/16 inch rosette and the X-Ray method. Three measurements on three layers overlapping one another are presented. The residual stress was induced by the lathe-turning in the surface layer but the results are steady for all the layers from the depth of approx..1 mm. 99

Summary The hole-drilling strain-gauge method is an acceptable method to demonstrate the level of the residual stresses in the railway axles required by the standards EN 13 26+A1 and EN 13261 under certain circumstances. i) The evaluation of the residual stresses for reducing the measurement uncertainty requires carrying out the calculation corrections which are not contained in the standard ASTM E837-13. Therefore the new version of the standard EN 13 26 + A1 being prepared should contain that the measurement of residuals stress shall be carried out in compliance with the methodology of ASTM E837-13 instead of directly using this standard in order to avoid problems with this formulation during the accreditation of the measurement method. ii) Then, the demonstration of the requirements of the EN 13 26 + A1 standard can be implemented without any problems for the axles made of the standard materials A1N and A4T with the level of the residual stresses up to 1 MPa. iii) In order to evaluate the residual stresses of the hardened or roll-burnished railway axles in the depth of 2 mm below the surface we recommend using the method of layers removing or the power-series method with the correction to the elastic-plastic stress state as the distribution of state of stress in the subsurface layer is roughly homogeneous. It is problematic to use the integral method for the reason of a high uncertainty comparable with the requirement of the standard for the inspection of the railway axles. iv) The measurement of the residual stresses in the depth of.1 mm by the hole-drilling method is also burdened with a big error. The demonstration of the level lower than the demanded tensile 1 MPa according EN 13 26 + A1 standard usually is without any problems if all the necessary corrections are carried out as the residual stresses in the existing axles are nearly always compressive. The article has originated in the framework of the institutional support of the long-term conceptual development of the research organization. References [1] EN 13 261+A1 Railway applications Wheelsets and bogies Axles Product requirements (21). [2] EN 13 26+A1 Railway applications Wheelsets and bogies Wheelsets Product requirements (21). [3] ASTM E837-13a Determining Residual Stresses by the Hole-Drilling Strain-Gage Method. American Society for Testing and Materials, West Conshohocken, PA (213). [4] M. Scafidi, E. Valentini, B.Zuccarello, Error and Uncertainty Analysis of the Residual Stresses Computed by Using the Hole Drilling Method, Strain 47 (211) 31-312. https://doi.org/1.1111/j.1475-135.29.688.x [5] M. Scafidi, E. Valentini, B.Zuccarello, Effect of the Hole-Bottom Fillet Radius on the Residual Stress Analysis by the Hole Drilling Method, JCPDS-International Centre for Diffraction Data (29) 263-27. [6] D. Halabuk, T. Návrat, The Effect of Third Principal Stress in the Measurement of Residual Stresses by Hole-drilling Method, DMEE 218, in print. 1