The Mechanical Engineering And Metal Engineering Essay

The Mechanical Engineering And sur search Engineering EssayMetal wear upon is ca utilise by repeated cycling of the load. It is a progressive localize damage due to fluctuating heargons and strains on the veridical. Metal bore spells enlighten and propagate in regions where the strain is most distasteful. This cyclic laden and crack initiation is represented using S-N bring down balls. The Fig 1.1 consists of constant cyclic attempt amplitude(S) which is applied to a ideal and the do of loading staves (N) until the example betters is determined. The fulfill dull functionure is consists of three main stages. The first stage consists of initial crack initiation. The second stage consists of progressive crack growth crossways the discussion section and the third and final stage consists of sudden fracture of the be cross section.The dull strength is the breed at which failure occurs for a presumption compute of cycles, whereas the fatigue life is the number of cycles required paladinstantive to fail. The most important concept of the S-N diagram is shown in Fig 1.1. This prognosticate consists of S-N curves for Steel and Aluminium. (By Shawn M. Kelly)http//www.efunda.com/ markulae/solid_mechanics/fatigue/images/fatigue_SN_01.gif discover 1.1 S-N curves for brand name and aluminium.The subject of fatigue examen is extensive, and is complicated by the important factors like the get along conditions of the exemplification, the theatrical role of the try unwrap variation, and the influence of the shape of the exemplar on the seek flow. As it is cognise as that the heightsly polished samples withstand better fatigue than the radiation pattern fatigue one and only(a)s. The most damaging type of stress variation is the realize reversal, which is between the limit for which the stress range is 2. Fluctuating stresses atomic number 18 little damaging, the standard case is between the limit 0 and +. For somewhat signifi mu cklets much(prenominal) as aluminium, no stomachurance limit exists and in that locationfore it should be planned life period of the structure to be less(prenominal) than the failure point.http//htmlimg1.scribdassets.com/izqlx4lamohzwzk/images/10-d0617ea942/000.jpg betoken 1.2 Fluctuating Stress Cycle.The above kind illustrates repeated stress cycle in which max (Rmax) is the maximum stress and min (Rmim) is the minimum stress and both(prenominal) ar non equal. Here t is the time and a is the stress amplitude and m is the mean stress.In low fatigue cycle region (NIn this prove fatigue see for aluminium alloys of serial 2000 admit been conducted and described.S-N Curve Experiment for 6000 and 2000 Aluminium Alloys SeriesThe fatigue failure audition is carried out for two incompatible types of aluminium alloys i.e. 6082 and 2011 exemplifications. These tastes argon carried in two contrary groups.A typical standard type is shown in Fig 1.3 as calibrate the stairs. I t is recommended to test at least 10 ideals of each type and they all must be cut from one length of the material.http//static.tecquipment.com/Products/RF1020_ALUMINIUM- daunt-SPECIMEN.jpg visualize 1.3 Test Specimen.A set of bending stresses from 0.9 of the pass on or proof stress to 0.4 of the eventual(prenominal) strength is selected to match the number of the test exemplifications for the complete experiment. The setting up of the warning on the railroad car is a reasonably simple operation which is make in befitting mannerology. The main object is to align the specimen and loading arm with the bloc of rotation to eliminate stresses due to eccentric whirling of the specimen.Both in drive shaft and the loading arm puts, loose collet ensn be is inserted. These inserts 9mm diameter ends of the test specimen are slid as shown in Fig. 1.4.http//www.twi.co.uk/twiimages/jk78f1.jpg direct 1.4 Setting up of machine. ( by http//www.twi.co.uk/content/jk78.html)The collet is fi rst reduce on the drive shaft chuck so that so that about 1 mm shoulder shows between the start of the neck and the face of the collet of the specimen. thence the loading arm is pushed on to the end of the specimen and adjusts the collet to give a sliding fit. The position of loading the loading arm is in such a way that the dimension of 109.5 mm is attained from the rear face of the bearing housing to the adjacent end of the neck of the specimen as shown in Fig 1.4 and ultimately choky the collet with the spanner. The specimen is rotated to determine that the end of the laughingstocktilever ferment axially differently the specimen must get bend and send away be discarded.BearingDrive shaft and bearingElectric repulseChuck in which specimen is fitted.ON/OFF transferCUsersasimDesktopall folderpicsmaterialsimagesattachments_16_12_2010DSC01501.JPG solve 1.4 Rotating scare off MachineThe counterbalance and load hangers should be ensured are in place. Switch motor ON and OFF to verify smooth running. The bending stress for the test is selected and required load or weight is applied on the load hanger. The revolution counter is set to zero ahead outset the machine and safety guard is utilize over the apparatus. The fracture time which might occur is estimated and noned.Endurance LimitThe stress value down the stairs which the material will withstand m whatever number of load cycles. It is excessively known as fatigue limit. The stress level below which a specimen will withstand cyclic stress indefinitely without exhibiting fatigue failure. Rigid, elastic, low damping materials such as thermosetting plastics and some crystal roue thermoplastics do not exhibit an survival limit. Also known asFATIGUE LIMIT.(CRC Press LLC 1989)Ultimate stressIt is defined as the maximum/ crowning(prenominal) load chthonian which a specimen breaks or fails. Stress equal to ultimate load is ultimate stress.Mean StressIt is defined as the algebraic sum of maximum and mi nimum stress divided by 2.Ultimate Tensile StrengthIn the wedded experiment ultimate tensile strength is calculated using the following formulap. Where p is the load applied to the material and is the stress.Recorded Data and Graph for 6000 series ingest zero(prenominal)Load (N)Bending Stress (MPa) payoff No. of CycleResults ( function/No- Fail)111.2522521400fail210.6212114800fail39.95199115300fail49.3186293800fail58.65173161000fail68clx184700fail77.35147905100fail86.71342411100fail96.051212765800fail105.91183156700failRecorded Data and Graph for 2000 series assay No.Load(N)Bending Stress (MPa)Result No. of cycles (x100)Result (Fail/Not-fail)113.527095Fail212240407Fail310.5210482Fail491801948Fail58.25clxv1781Fail67.51502662Fail77.01402165Fail86.01204916Fail95.611219970Fail105.2104to a greater extent than 107Not-fail11510010 533Fail124.896More than 107Not-fail134.692144.692More than 107Not-fail15480More than 107Not-fail2. Non-Destructive test Methods2.1 admissionNon-destructive scrutiny (NDT) is a wide range of analysis technique used in wisdom and industries to evaluate the seemlyties of material or component and to detect the daubs in the material without causing damage. The non-destructive testing is the testing of the materials used to find rebel or internal mars or metallurgical conditions without interfering in the integrity of the materials. The stigma includes cracks or inclusions in welds and castings, or variations in structural properties which may make it to loss of strength and finally failure of materials. Non-destructive testing is used for step of components and spacing and for the measurement of physical properties such as internal stress and hardness. It is also used for in-service inspection and for conditions monitoring of operating plants. It is also used to look for sign of wear or internal changes on airplanes in aircraft industries. The NDT method is also a function part of tint subordination which is based on sampling a nalysis, this method is not just for rejecting the lacking(p) material but gives assurance that it is genuine.The common types of Non-Destructive interrogation are give tongue to as followscharismatic Particle Inspection.Figure 2.1 magnetized Particle examination http//www.azom.com/work/8is7fjkADJ5v0JQByKTw_files/image003.gifRadiography Inspection.Figure 2.2 Radiography testing. supersonic scrutiny.Figure 2.3 supersonic Testing.Liquid Penetrant Testing.Figure 2.4 Liquid Penetrant Testing.http//www.twi.co.uk/twiimages/ksijm001f1.gifEddy Current Testing and Electro magnetic Testing.Figure 2.5 Electro Magnetic Testing.http//www.eurondt.com/index_2.gifThere are different types of non-destructive testing used for removing flaws as shown above but two main types of NDT on which experiments are perform are Magnetic particle testing and unhearable Testing.2.2 Magnetic Particle TestingIntroductionMagnetic particle testing is type of non-destructive testing which is used for the dete ction of originate and near-surface flaws in the ferro magnetised materials and it is essentially used for crack detection. Such flaws present in the magnetized part will cause a charismatic plain, i.e. flux, to leave the part. It is however said(prenominal) as if there is a surface-breaking flaw in the specimen, the magnetic field is distorted, causing local magnetic flux leakage around the flaw. If the magnetic particles are applied to the surface of this specimen, the surface is covered by in truth fine atomic number 26 particles and they will be held in the place by the flux leakage to give a visual indication.Figure 2.6 digression in the magnetic flux.http//www.ndt-ed.org/GeneralResources/MethodSummary/MT1.jpg http//www.milinc.com/images/magpartimgs/magpartdiag1.gifThus a crack is indicated as a berth or iron powder particles on the surface. The method of MPT is relevant to all metals which can be strongly magnetised such as ferritic steels, irons and some other alloys but not generally to austenitic steels. The modern equipments generate the magnetic field electrically either nowadays or indirectly. In direct method high gear ampere of underway is passed through the specimen and magnetic flux is generated at right fee to the menstruation flow. Therefore current flow is in the same anxiety of suspect defect. If this method is not possible to carry out because of the orientation of the defect, then the indirect method is used. This consists of two formsPassing high current through a coil that encircles the specimen.Making the test piece form part of a yoke, this is surrounded by a current carrying coil. The magnetic core is to pass magnetic flux along the part to reveal cross(prenominal) and circumferential defects.FluxIt is a term which is used to refer the bill of magnetic field that exist at specific point within that field. It is mensurable in Webers.Flux DensityIt is an indication of the strength of the magnetic field. It is represe nted by the lines of mights which are surrounded around the magnetic circuit, where the lines are closer to the flux. It is measured in Webbers/M2 or Telsa.Magnetic lines of forceThese lines of force are imaginary lines which describes the path a free north depot would take in a magnetic field. These lines can be plan using a compass.data-based ProcedurePump switch.The equipment used for do the experiment is known as Johnson Allen NDT (SBU 2000). It should be sited on a theatre concrete allowing access for servicing. The specimen provided contains fiver mendings in it. The equipment should be machine-accessible to a 230 volt AC, 50Hz, 16 Amp power supply and mobile blow fuses should not be used. Connect Footswitch, Pump, and UV Light via socket to the equipment. revoke main supply on at the wall isolator. Turn the UV light ON and allow 10 mins to warm up. Slide out the ink hopper to within 75mm of the top flange with the Fluorescent Magnetic Ink and slide in the hopper gen tly. Turn the agitation ON and dispensing pump using the twist switch on the right of equipment.Figure 2.7 Magnetic Particles Testing Machine.Headstocks.Ink sp pecker.Clamping knobs.C.F. control knob.AmmeterON/OFF Switch.CUsersasimDesktopall folderpicsmaterialsimagesIMG_0049.JPGHeadstocks can be adjust using the Clamping Knobs at the base. Once specimen is inserted and unexpended side headstock is unflinching then the specimen is ready to be tested. AC is current is used for surface defect and HWDC is used for all defect, so select the HWDC. Check the current control dial is turned to minimum.Experimental PrecautionsThe hole in spite of appearance the given specimen should be clear otherwise the crack line does not come flop.Headstocks should be regularly checked.The specimen should be cleaned properly to prevent arcing and pitting on the surface.Circuits should be check regularly before performing any operation.Experimental ResultsSpecimenThe given specimen contains 5 holes i n it. The specimen is adjusted and fixed between the headstocks as shown in the figure below. Before performing the experiment the specimen should be clean properly other the line is not visible. As the hole was not clear and contains ink in it so the defect line is not obtained on the specimen. This can be seen in the figure below.Figure 2.8 Specimen without defect lineHeadstocksInk spray.CUsersasimDesktopall folderpicsmaterialsimagesattachments_16_12_2010DSC01541.JPGThen the holes are clean, and the experiment is performed again. When it is clean, the two defect lines are visible on the specimen. Hence, as the lines are seen on the specimen it can considered that it contains flaws in it. This works under the rule of right excrete rule and so specimen has to be adjusted perpendicular to the headstocks so flux sound properly from the specimen and flaw.Testing Specimen.Defect lines.Figure 2.8 Specimen with visible defect line.CUsersasimDesktopall folderpicsmaterialsimagesIMG_0060. JPGAdvantages of Magnetic Particles TestingIt gives instant result and rapid inspection can be done for large surfaces.It is simple and easy to conduct.It detects a variety of surface and sub surface flaws, such as crack, porosity, inclusions, shrinkage, laps etceteraSurface preparation is less critical than it is penetrant inspection.Sensitivity of testing can be specified and checked.It is economically cheap.Disadvantages of Magnetic Particles TestingHigh currents applied to the components may cause damage. reflect surface is required for application of this method.Materials which are tested must be ferromagnetic.Deep cracks or flaws are not detected.Materials may need to be demagnetized.Equipment is bulky and heavy.Material or part permeability may fall upon results.High power supply is needed for low surface.2.3 Ultrasonic TestingIntroductionUltrasonic testing is a type of non-destructive testing method that uses high frequency sound loops (ultrasonic) which are above the ran ge of military man hearing and they are used to measure the geometric and physical properties of the materials. Ultrasonic waves travels at different velocities in different materials. There are different ways of sound travels through the material. One type of sound wave is called as compression or longitudinal travels which is at about 330m/s in air and 6400m/s in aluminium and approximately 5960m/s for steel.Figure 2.9 Ultrasonic Testing.http//www.energyworkforce.net/wp-content/uploads/ut1.jpgThe pulsed beams of the ultrasound are used in a simplest instrument and a single probe (transducer) which is hand-held is paced on the surface of the specimen. An reach is connected to the probe which displays with the time-base the time that requires for an ultrasonic pulse to travel through the reflector which can be flaw, black surface etc. The height of the reflected pulse is related to the flaw size as seen from the vector probe which is displayed on oscilloscope screen. A single prob e acts as both transmitter and receiver and hence the inspection can be done from one side of the specimen. Large particle material such as austenitic steel welding, copper casting etc., produce severe attenuation and are unmanageable to test but fine grain material such as forged material can be tested easily. Using the indication on the oscilloscope the size of the flaw can be determined. Ultrasonic attenuation and ultrasonic velocity measurements are used to study various material properties.Experimental ProcedureA typical ultrasonic testing system consists of several functional units such asPulser/receiver.Transducer.Oscilloscope.Connecting wires.Couplant.Mild steel material (specimen).A pulser is an electronic contrivance that can produce high emf electrical pulses. From the high voltage pulses, transducer generates high frequency ultrasonic energy. This sound energy propagates through the material in the form of waves.Couplant.Transducer.OscilloscopeFigure 2.10 Setting up of Ultrasonic Testing.CUsersasimDesktopall folderpicsmaterialsimagesattachments_16_12_2010DSC01547.JPGCUsersasimDesktopall folderpicsmaterialsimagesattachments_16_12_2010DSC01545.JPGMild steel specimen.DefectsDisplay ScreenThe left side figure shows the cathode ray oscilloscope and the right side figure shows the modest steel material on the ultrasonic test is conducted. The given specimen was of mild steel with five holes in it. Before starting the experiment, the specimen should be properly clean. Then apply a couplant on it. Start the cathode ray oscilloscope. There are different button on oscilloscope such as gain, light, velocity, angle, dialog etc. as shown in figure below.Figure 2.11 various buttons on oscilloscope.CUsersasimDesktopall folderpicsmaterialsimagesultrasonic8122010(002).jpgSo it is adjusted in such a way that the deflection should be visible. The transducer is connected to the oscilloscope with the help of connecting wires. Then this transducer is pose on the s pecimen for testing the flaws in it.Experimental cardWhen the transducer is placed on the specimen it emits ultrasonic waves from the material (specimen). When the probe is placed on specimen it gives a very nice and high natural elevation on the oscilloscope as shown in the below figure. It means that the ultrasonic waves travel easily from that part of the specimen and hence it does not have any flaw in that part.Figure 2.12 High peak call for in nice surface.CUsersasimDesktopall folderpicsmaterialsimagesIMG_0065.JPG CUsersasimDesktopall folderpicsmaterialsimagesultrasonicP081210_11.230001.jpgSimilarly, when the probe is moved further on it can be seen in the oscilloscope that the highest peak is coming down and it nearly become nil or very low. It means that the high frequency waves are reflected. Hence it can be observed that, there is a flaw in that part of the specimen. It is the same part under which a big hole is there.Figure 2.13 Low peak type in defective part.CUsersas imDesktopall folderpicsmaterialsimagesIMG_0081.JPG CUsersasimDesktopall folderpicsmaterialsimagesattachments_16_12_2010DSC01545.JPGHence, from the above two figure it can be concluded that when there is high peak in oscilloscope there is no flaw at that part and similarly when the high peak decreases to low it means that part contains some flaw in it.Advantages of Ultrasonic TestingThe measurement is superior to other NDT methods.It is sensitive to both surface and subsurface discontinuities.It requires very minimal part preparations.It is highly complete in determining reflector position and estimating size and shape.As the electronic equipment as used it give instantaneous results.It requires only single-sided access when the pulse-echo technique is used.It can also be used for other purposes such as thickness measurement etc.Disadvantages of Ultrasonic TestingIt normally requires a coupling medium to promote the transfer of sound energy into the test specimen.Those materials whi ch are rough, very small, irregular in shape, thin or not homogeneous are very difficult to test.Surface must be accessible to transmit ultrasound.Cast iron and other grained materials are difficult to test due to their low sound transmission and high intercommunicate noise.Linear defects oriented parallel to the sound beam may go undetected.Feedback and EvaluationS-N curveThe experiment S-N curve is used to determine the survival fatigue limit of the material used in automotive industries. The given specimens were of aluminium alloys. There were two series of aluminium alloys i.e. 6000 series and 2000 series on which experiments are performed. Ten samples of each specimen were given. This experiment was performed in two groups. One group perform the experiment on 6082 specimen and other group perform the experiment on 2011 specimen. In this experiment weights are taken in Newton and the number of cycles is shown on the machine. corresponding to this stress/load (S) and number of cycles (N), S-N curve is plotted. When the load is high it number of cycles is low and when the load is decreased its number of cycles increases. This is shown in graphs below.This is a S-N curve graph for 6011 aluminium alloy (specimen). From the above graph it can be seen that at high stress/load i.e. 225 MPa or 11.25N. The number of cycles is 21400. As the stress goes on increasing the number of cycles goes on decreasing. Hence the endurance fatigue limit varies at different load for the same specimen. When the specimen fails it is taken out from the chuck and it can be checked microscope and the cracks can be seen properly. From this the physical properties of the material can be checked and the fatigue limit can be obtained.There are some microscopical images of specimens, they are as followsSample 1 at 11.25N load.CUsersasimDesktopall folderpicsmaterialsimagesultrasonicsamplemicroscopicimages- sncurveSample1_1.JPGCUsersasimDesktopall folderpicsmaterialsimagesultrasonicsamplemi croscopicimages- sncurveSample1_2.JPGSample 2 at 10.6N load.CUsersasimDesktopall folderpicsmaterialsimagesultrasonicsamplemicroscopicimages- sncurveSample2_1.JPGCUsersasimDesktopall folderpicsmaterialsimagesultrasonicsamplemicroscopicimages- sncurveSample2_2.JPGThere are many to a greater extent than microscopic images which look similar to the above images and it fails at different loads. The below figure is of the specimen before experiment.http//static.tecquipment.com/Products/RF1020_ALUMINIUM-FATIGUE-SPECIMEN.jpgThis specimen is fixed between the chucks and when the experiment is performed at different loads the specimen which is fixed between the chuck breaks. This is shown in the figure below.CUsersasimDesktopall folderpicsmaterialsimagesIMG_0040.JPGIt can be intelligibly seen from the introductory figure that the specimen breaks from its middle. First the crack propagates in it and then its finally fails. The graph below is the S-N curve graph for 2011 aluminium alloy spec imen which is experimented by other group.This graph start from 270Mpa and the applied on the specimen is 13.5 N and therefore the number of cycles perform by the specimen is less i.e. 9500. These two specimens cannot be compared as both the group has taken different values of stress and therefore the number of cycles are different both the specimens. From the given ten samples, the discussion of the fatigue limit is nearly unaccepted as we find the scatter point graph not a perfect curve of S-N. For establishing the endurance fatigue limit of both the specimens more experiments must be conducted on it. Also the specimen should be properly fixed in the chuck otherwise it fails in somewhere before the expected value.Magnetic Particles TestingThis experiment is performed to check the flaws i.e. cracks, holes, black surface of the materials. This experiment comes under non-destructive testing. A specimen of mild steel is given and it contains five holes in it. This specimen is fixed i n Johnson Allen NDT machine. This specimen is fixed between the headstocks of the machine. The specimen is fixed perpendicular to the headstocks. The perpendicular arrangement of headstock and specimen is done because this machine works under the principle of right hand rule and it generates flux into the specimen. This flux passes through the material. When there is any flaw into the material the flux gets affected and a black line of iron particles is seen on the surface of the material. In this experiment also the specimen contains five holes in it and a black line of iron particles is seen on the surface of the material. The current is control with the help of C.F. control switch. The black defect line on the specimen can be seen in figure below.The amount of flux running through the specimen can be measured with the help of ammeter. But the ammeter in the machine under which this testing is performed was not working. So the exact amount of flux generated in specimen cannot be m easured. The ammeter and C.F. control switch is shown in the figure below.C.F. control switch.AmmeterCUsersasimDesktopall folderpicsmaterialsimagesIMG_0045.JPGUltrasonic testingThis type of testing is also used to detect flaws and crack inside the material without damaging it. The specimen provided is a mild steel slab and it contains holes in it. It can be seen that when there is no flaw inside the specimen it shows high peak on the oscilloscope and similarly when there is any flaw the ultrasonic waves get reflected and the high peak decreases to low peak. This is clearly in figures below.CUsersasimDesktopall folderpicsmaterialsimagesIMG_0065.JPGCUsersasimDesktopall folderpicsmaterialsimagesIMG_0081.JPGConclusionFrom the above experiments we can conclude that S-N curve is best method to determine the fatigue limit but it slope be done using ten samples as it does not gives the proper curve graph for the specimen. Magnetic Particle Testing is a wakeless way of finding flaws from t he materials without damaging it but the machine is not that halcyon and more precautions must be used before using it otherwise the flaws are not detected. Similarly Ultrasonic Testing is a good way cracks and other flaws detecting and these are used in aircraft industries.Referencing stag Wilcox and George Downes, A brief description of NDT techniques Available at http//www.turkndt.org/sub/makale/ornek/a%20brief%20description%20of%20NDT.pdf Accessed on3 fall 2010www.ndted.org.com NDT Method Summary Available at http//www.ndt-ed.org/GeneralResources/MethodSummary/MethodSummary.htm Accessed on12 declension 2010www.insight-ndt.com (2007). Qualiron ductile iron metal quality tester. Available http//www.insight-ndt.com/ultrasonic/qualiron.html. Last accessed 3rd dec 2010.www.NDT.net Non-destructive Material Testing with Ultrasonics Introduction to the Basic Principles Available at http//www.ndt.net/article/v05n09/berke/berke1.htm Accessed on15 celestial latitude 2010www.materialsen gineer.com (2007) Metallurgical Fatigue Failures Available athttp//www.materialsengineer.com/CA-fatigue.htm Last accessed on 3rd Dec 2010www.sv.vt.edu (1997). By Shawn M. Kelly, Fatigue, Available at http//www.sv.vt.edu/classes/MSE2094_NoteBook/97ClassProj/anal/kelly/fatigue.html Accessed on 6 Dec 2010.www.scribd.com Fatigue Failure Available athttp//www.scribd.com/doc/29476995/fatigue-failure Accessed on 8 Dec.www.key-to-metals.com.cn (99-2000) Fatigue of metals (stress cycles) Available at http//www.key-to-metals.com.cn/page.aspx?ID=CheckArticlesite=ktsNM=281 Accessed on 8 Dec.www.twi.co.uk (2005) Fatigue Testing Available at http//www.twi.co.uk/content/jk78.html Accessed on 12 Dec.www.azom.com (2010) Non-destructive Testing-Surface Examination Techniques. http//www.azom.com/Details.asp?ArticleID=522 Accessed on 13 Dec.www.energyworkforce.net (2010) Principles of Ultrasonic Testing. Available at http//www.energyworkforce.net/?p=126 Accessed on 16 Dec.