Influence of Shot Peening Parameters on Residual Stresses in Flake And
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Controlled Shot Peening Preventing Failures
MIC Services INNOVATORS IN TECHNOLOGY Metal Improvement Company Subsidiary of Curtiss-Wright Corporation Controlled shot peening Preventing failures Enhancing the performance of metals and materials www.metalimprovement.co.uk Controlled shot peening - preventing failures Metal Improvement Company (MIC) is a Component failure is often related to residual tensile stress global organisation specialising in metal and DESIGN CONSIDERATIONS - COST OF PERFORMANCE CRITERIA material surface treatments which enhance induced during manufacture. Subsequent severe working performance and extend the life of critical and/or unexpected conditions can eventually lead to Parameter selection - the choice of process have to be accurately and Intensity control components, enabling component designs to shot peening parameters is dependant repeatedly controlled. achieve their maximum potential. premature failure. on a variety of conditions: Shot peening intensity is the measure Controlled shot peening is different of the energy of the shot stream. It is Established in 1945, MIC has over 60 l knowledge of the application of the from most manufacturing processes in one of the essential means of ensuring operating divisions in Europe, USA, Canada Typical examples of premature failure are: The shot peening process - how it component that there is no non-destructive method process repeatability. The energy of the and Asia with on-site processing worldwide. works l component geometry to confirm that it has been performed shot stream is directly related to the We offer a quality controlled and cost l Metal fatigue to the proper specification. Techniques compressive stress that is imparted into l manufacturing method effective service, working in partnership to Controlled shot peening is the such as x-ray diffraction require the a component. -
Residual Compressive Stress Strengthens Brittle Materials
Residual Compressive Stress Strengthens Brittle Materials Effect of retained residual compressive stress on the ductility of the still hot and ductile subsurface the surface layer of brittle materials in reducing applied surface glass. As cooling continues, the sub tensile stress. Spring test data demonstrate the beneficial effect surface glass contracts against the rela tively cool and rigid surfaces, resulting of residual compressive stress in· the surface of hard steel. in residual tensile stress in the core and corresponding resiqual compres sive stress in the surface.' JOHN 0. ALMEN with glass specimens. Among the · ad The relative static strength of a Research Consultant vantages of glass for evaluating resid specimen of normal glass, which was ual stresses is that at ordinary tem carefully annealed to avoid residual UNDER CONDITIONS of br:ttlc fracture, peratures glass is completely brittle. stresses, and that of a similar glass specimen surfaces are weaker than For this reason, the residual stress pat specimen_that had been quenched on sound subsurface material. When such tern remains unaltered by plastic flow both surfaces as described in the pre relatively weak surfaces are residually to the instant of fracture. Also, any c:!ding paragraph is shown in Fig. 1. stressed in compression, the specimens apparent unorthodox behavior of glass As shown by the insert in Fig. 1, these will support greater tensile loads and will not mistakenly be attributed to specimens were ordinary -! in. plate will exhibit greater ductility because cold work or altered structure. glass, 3 in. wide and 18 in. long. Each the applied surface tensile stress is re Residual compressive stress in glass was placed on supports spaced 12 in. -
Peening Weld Surfaces with Steel Shot Induces Compressive Stresses That Raise Resistance to Fatigue and Corrosion
Peening weld surfaces with steel shot induces compressive stresses that raise resistance to fatigue and corrosion. By Tom Floyd hot peening improves Testing shot-peened parts, re- Built-in compressive stresses property performance searchers have demonstrated that raise resistance to stress corrosion of welds and weld- peening raises fatigue resistance of by counteracting tensile stresses. mentsS by cancelling residual tensile fillet welds in carbon steel and butt Stress corrosion occurs when tensile stresses that develop in surfaces as welds in constructional alloy steel stresses break up oxide layers that welds cool and replacing them with by 20 to 40 percent, and can double normally protect surfaces of chro- compressive stresses. Compressive fatigue resistance of butt welds in mium-containing alloys. Though stresses raise resistance to fatigue, aluminum plate and 18-percent Ni bare metal re-oxidizes to form fresh stress corrosion, and intergranular maraging steel. Researchers at Rock- oxide coatings, recurring cycles of corrosion. well International (Atomic Di- tensile stresses continually rupture A cold-working process, shot vision) found that shot peening pre- these layers. peening bombards a metal work- vents stress corrosion cracking of As for intergranular corrosion, piece with spherical pellets, com- weldments in austenitic stainless characteristic of stainlesses sensi- monly steel shot. Each impact steel. tized at weld temperatures, peening stretches and densifies surface lay- Fatigue resistance improves be- before welding helps to prevent it ers. Because subsurface material re- cause, when service imposes tensile by breaking up surface grains. This mains unstretched, it exerts an op- stresses in a part, the built-in com- action provides a multitude of nu- posing force, trying to restore the pressive stresses counteract them. -
Shot Peening Overview
H:\docs\training\SPO_08_28_2000.wpd Shot Peening Overview by Jack Champaigne Electronics Inc 1428 W. 6TH Street Mishawaka, In 46544 http://www.shotpeener.com Last Revised January 18, 2001 With special thanks to Metal Improvement Co for their technical contributions http://www.metalimprovement.com Shot Peening Overview 1. INTRODUCTION ............................................................... 3 1.1 Shot Peening Described ................................................... 3 1.2 Residual Stresses ....................................................... 3 1.3 Load Stress Profiles ...................................................... 6 2. MANUFACTURING PROCESSES - EFFECT ON FATIGUE LIFE .......................... 8 2.1 Beneficial Manufacturing Processes .......................................... 8 2.2 Detrimental Manufacturing Processes ........................................ 8 2.2.2ElectroDischargeMachining(EDM)....................................... 10 3. SERVICE EFFECTS REMEDIED BY SHOT PEENING ................................. 16 3.1CavitationDamage ..................................................... 16 3.2FrettingandFrettingFatigue .............................................. 17 3.3 Galling ............................................................... 18 3.4Pitting ............................................................... 18 3.5CrackArrest........................................................... 20 3.6StressCorrosionCracking................................................ 21 4. PRODUCTS BENEFITTING FROM SHOT PEENING -
Improvement of Hardened Surface by Shot P
IMPROVEMENT OF HARDENED SURFACE BY SHOT P M. Ohsawa, Honda R & D Co., LTD. T. Yonemura, Parker Netsushori Co., LTD. --ABSTRACT In the application of shot peening to automotive parts, this process has been the com- monly used. surface treatment for springs. Today, a tend among automobile manufacturers is to use this process for other parts, e. g. transmission gears, with the aim of in- creasing durabi 1 i ty . The authors have recent 1y conducted severa 1 experiments on the effect of this process on soft-nitrided parts which are now undergoing remarkable devel- opment, and on widely used plated parts after they have been case-hardened by carbu- rizing. These experirnen ts have proven that the fatigue strength of sof t-ni trided or casehardened surface is increased, and that reduction of the strength of hardened surf - face after plating is avoided, contributing greatly to reduction of the weight of such parts wi thou t loss of strength. KEYWORDS; Sof t-Ni triding, Tuff triding, Cr-plating, Residual stress, Fatigue strength. 1 OUTLINE OF TEST RESULTS 1-1 Effect of Shot peening on Sof t-Ni trided Parts Soft-ni triding which is also called as Gas Sof t-Ni triding, Liquid Ni triding known as Tufftride process has the features shown in Table 1 and is in wide use for various automotive parts. This treatment, however, may not be applicable to common carbon steel where high performance is desired because of shallow case depth and lower surface hardness. This paper deals with our observations on the effect of shot peening on sof t-ni trided steel to see how its mechanical properties are improved. -
In-Situ Measurement and Numerical Simulation of Linear
IN-SITU MEASUREMENT AND NUMERICAL SIMULATION OF LINEAR FRICTION WELDING OF Ti-6Al-4V Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University By Kaiwen Zhang Graduate Program in Welding Engineering The Ohio State University 2020 Dissertation Committee Dr. Wei Zhang, advisor Dr. David H. Phillips Dr. Avraham Benatar Dr. Vadim Utkin Copyrighted by Kaiwen Zhang 2020 1 Abstract Traditional fusion welding of advanced structural alloys typically involves several concerns associated with melting and solidification. For example, defects from molten metal solidification may act as crack initiation sites. Segregation of alloying elements during solidification may change weld metal’s local chemistry, making it prone to corrosion. Moreover, the high heat input required to generate the molten weld pool can introduce distortion on cooling. Linear friction welding (LFW) is a solid-state joining process which can produce high-integrity welds between either similar or dissimilar materials, while eliminating solidification defects and reducing distortion. Currently the linear friction welding process is most widely used in the aerospace industry for the fabrication of integrated compressor blades to disks (BLISKs) made of titanium alloys. In addition, there is an interest in applying LFW to manufacture low-cost titanium alloy hardware in other applications. In particular, LFW has been shown capable of producing net-shape titanium pre-forms, which could lead to significant cost reduction in machining and raw material usage. Applications of LFW beyond manufacturing of BLISKs are still limited as developing and quantifying robust processing parameters for high-quality joints can be costly and time consuming. -
Effect of Shot Peening on Fatigue Strength of Maraging Steel
Transactions on Engineering Sciences vol 39, © 2003 WIT Press, www.witpress.com, ISSN 1743-3533 Effect of shot peening on fatigue strength of maraging steel N. ~awa~oishi',T. ~a~ano~ & M. ~ori~arna~ I Faculty of Engineering, Kagoshima University,Kagoshima, Japan 2 Miyakonojyo National College of Technology, Miyakonojyo, Japan Abstract Rotating bendmg fatigue tests were carried out for a shot-peened maraging steel in order to investigate the effects of shot peening on the fatigue strength and the fracture mechanism focusing on the effect of surface roughness. Fatigue strength was markedly improved by shot peening because of hardening and generation of compressive residual stress in the surface layer. The origin of fatigue fracture changed from the specimen surface at high stress levels to an inclusion in the interior of specimen at low stress levels. And at the middle stress levels, both fracture modes were observed. Consequently, the shape of the S-N curve of shot- peened specimen was complex, corresponding to the change of fracture mode. In the region where surface fracture occurs, polishing the specimen surface and double shot peening using superhard fine particles were effective to improve the fatigue strength through the decrease in stress concentration due to smoothening the specimen surface. Transactions on Engineering Sciences vol 39, © 2003 WIT Press, www.witpress.com, ISSN 1743-3533 100 Surface Twatment V1 1. Introduction Maraging steel is an ultra-high strength steel which has both high tensile strength and high ductility [1],[2]. However, fatigue strength is relatively low in comparison with the hgh static strength [3]. Therefore, the study on the improvement of fatigue strength of maraging steel is important. -
United States Patent [191 [111 4,354,371
UnitedO States Patent [191 [111 4,354,371 Johnson [45] Oct. 19, 1982 [54] METHOD OF PRESTRESSING THE 4,214,923 7/1980 Price ............................... .. 29/421 R WORKING SURFACES 0F PRESSURE 4,230,426 10/ I980 Avery . .. 72/53 ERS 0R ERS Primary Examiner-Gene Crosby [75] lnventol‘l Daniel E- 30111180111 Dallas, TBX- Attorney, Agent, or Firm—Stephen A. Roen; Arthur L. [73] Assignee: Metal Improvement Company, Inc., Fredenck - Paramus, NJ. [57] ABsTRAcr [21] Appl‘ No" 200,767 A method of prestressing the working surface of pres 2 Filed; Oct, 27 1980 sure chambers or cylinders comprising the steps of ?rst [2 1 ’ s h o t peemng' th eir' wor king sur races t o rorm compres [gé] clci3 ............................................ "hr/1325161115 sive residual stresses’ and then applying ?uid pressure at [ 1 .' ' ' """""""""""""""""" " ’ a predetermined magnitude to cause tensile stresses in [58] Field of Search ................. .. 72/53, 40, 61; 148/4, the working surfaces The magnitude of compressive 148/141; 29/421; 51/319 residual stresses established on their outer working sur [55] References Cited faces 'is made substantially equal to the tensile stress U_s_ PATENT DOCUMENTS applied to these surfaces during the pressure phase of 454 592 6/1891 Jackson 72/61 the process‘ 3,4ss1073 12/1969 Burney .. 4,034,585 7/1977 Straub ................................... .. 72/53 6 Claims, 2 Drawing Figures 4,354,371 1 2 the plastic from the elastic zone in said substrate. This .METHOD OF PRESTRESSING THE wouxnwc tension component, unless neutralized, can produce SURFACES or PRESSURE CHAMBERS on microscopic fractures in the internal surface of the CYLINDERS chamber wherein defects exist therein. -
Laser Peening Fact Sheet
Hepburn and Sons LLC “Trusted advisors to the American Maritime Industry” TECHNOLOGY FACT SHEET – Laser Shock Peening TECHNICAL CHALLENGE 10X Compressive residual stress • Aluminum shipbuilding on the rise in the Navy, leading to benefits over other peening materials problems like stress corrosion cracking (SCC) and methods and treatments sensitization • Repair yards tasked with these substantial repairs • Aluminum repair has significant rework, as it is difficult to work with • Welding repairs impart large stresses on and deform the 48X aluminum SCC on aluminum ship Lifetime extension of • Flame straightening not permitted on marine grade aluminum superstructure sensitized aluminum when laser shock peened versus • Common aluminum forming methods are laborious, costly, and no treatment time-consuming TECHNOLOGY OVERVIEW • High-energy pulsed laser directed at material surface to generate pressure pulses • Shock wave plastically yields and cold works the 1-5 mm material to generate deep compressive stresses Range of compressive residual stress depth as a • Residual stress layers are orders of magnitude result of laser shock peening deeper than that achievable with shot peening • Highly predictive and deterministic stress Laser peening a metal surface profiles • Used successfully in the aerospace industry for nearly 20 years • Significantly improves aluminum lifespan • 20 years Arrests crack growth and mitigates stress Length of time that laser corrosion cracking shock peening has been successfully used in the • Mitigates aluminum sensitization -
Laser Peening for Prevention of Fatigue Failures
LASER PEENING FOR PREVENTION OF FATIGUE FAILURES David F. Lahrman Peter A. Gaydos LSP Technologies, Inc. United States ABSTRACT Laser peening is an innovative commercially-available surface enhancement process for increasing the fatigue life of metal components. The process produces deep residual compressive stress into treated surfaces, typically five to ten times deeper than conventional metal shot peening. These deep compressive residual stresses inhibit the initiation and propagation of fatigue cracks. Laser peening has been particularly effective in increasing the resistance to fatigue crack propagation initiated from foreign object damage in titanium alloy fan and compressor blades of aircraft gas turbine engines. [1,2,3,4] However, the potential application of this process is much broader, encompassing automotive parts, orthopedic implants, tooling and dies, and others. Significant progress has been made to lower the cost and increase the throughput of the process, making it affordable for numerous applications. This paper reviews the status of laser peening technology, material property enhancements, and potential applications. KEYWORDS Laser shock peening, fatigue, life, residual stress, surface, enhancement HOW LASER PEENING WORKS Laser peening drives a high amplitude shock wave into a material surface using a high energy pulsed laser. The effect on the material being processed is achieved through the mechanical “cold working” effect produced by the shock wave, not a thermal effect from heating of the surface by the laser beam. The laser system is a high-energy, pulsed neodymium-glass laser system having a wavelength of 1.054 µm. The laser peening system produces very short laser pulses, selectable from 8 to 40 nanoseconds, with a pulse energy of up to 50 joules. -
11283: Engineered Residual Stress to Mitigate Stress Corrosion Cracking
Paper No. 2011 11283 Engineered Residual Stress to Mitigate Stress Corrosion Cracking of Stainless Steel Weldments Jeremy E. Scheel, N. Jayaraman, Douglas J. Hornbach Lambda Technologies 5521 Fair Lane Cincinnati, OH, 45227-3401 USA ABSTRACT Stress corrosion cracking (SCC) is the result of the combined influence of tensile stress and a corrosive environment on a susceptible material. Austenitic stainless steels including types 304L and 316L are susceptible alloys commonly used in nuclear weldments. An engineered residual stress field can be introduced into the surface of components that can reliably produce thermo-mechanically stable, deep compressive residual stresses to mitigate SCC. The stability of the residual stresses is dependant on the amount of cold working produced during surface enhancement processing. Three different symmetrical geometries of weld mockups were processed using low plasticity burnishing (LPB) to produce the desired compressive residual stress field on half of each specimen. SCC testing in boiling MgCl2 was performed to compare the LPB treated and un-treated 304L and 316L stainless steel weldments. X-ray diffraction residual stress analyses were used to document the respective residual stress fields and percent cold working of each condition. Testing was performed to quantify the thermo-mechanical stability of the residual stresses. The un-treated weldments suffered severe SCC damage due to the residual tension from the welding operation. The results show conclusively that LPB completely mitigated SCC in the tested weldments and provided thermo-mechanically stable, deep residual compression. KEYWORDS: Stress Corrosion Cracking, Low Plasticity Burnishing, Residual Stress, Weldments, Nuclear Reactor, Stainless Steel. ©2011 by NACE International. Requests for permission to publish this manuscript in any form, in part or in whole, must be in writing to NACE International, Publications Division, 1440 South Creek Drive, Houston, Texas 77084. -
Effect of Tensile Residual Stress on Brittle Fracture of Ferritic Steel
INFLUENCE OF RESIDUAL STRESSES ON BRITTLE FRACTURE OF FERRITIC STEELS A. Mirzaee Sisan, C. E. Truman and D. J. Smith Department of Mechanical Engineering, University of Bristol, Queen’s Building, University Walk, Bristol, BS8 1TR, UK. ABSTRACT An experimental and numerical study is presented which demonstrates the significant effect of tensile residual stress fields on the brittle fracture of ferritic steels. A residual stress field was introduced into laboratory specimens, specifically single edge notched bend, SEN(B), and round notched bars, RNB, using in-plane compression. In-plane compression consists of applying a compressive load along the longitudinal axis of a specimen containing a shallow notch and then unloading at room temperature. The specimens were then cooled to a temperature of -150oC and reloaded to fracture after introduction of a sharp notch. Numerical analyses utilizing ABAQUS finite element code were carried out to simulate the process of in-plane compression. The numerical studies demonstrated that a high tensile residual stress region was created at the notch tip. A considerable decrease in fracture stress and fracture toughness was observed as a result of in- plane compression. The results emphasise the significant role of residual stresses in the fracture behaviour of ferritic steels. 1 INTRODUCTION Residual stress fields have significant effect on the fracture load of structures [1]. Welding is one of the major causes of residual stresses. The magnitude of weld residual stress can be as high as the yield strength of the material [2]. The tensile residual stress field can be combined with in- service stresses and promote failure [2,3].