High Cycle Fatigue of Powder Metallurgy Materials

Total Page:16

File Type:pdf, Size:1020Kb

High Cycle Fatigue of Powder Metallurgy Materials VIII Congreso Nacional de Propiedades Mecánicas de Sólidos, Gandia 2002 195-204 HIGH CYCLE FATIGUE OF POWDER METALLURGY MATERIALS Herbert Danningera and Brigitte Weissb a Institute of Chemical Technologies and Analytics, Vienna University of Technology, A-1060 Wien, Austria b Institute of Materials Physics, University of Vienna, A-1090 Wien, Austria ABSTRACT: Powder metallurgy materials offer increased potential for manufacturing of special, often otherwise inaccessible, materials as well as for the mass production of complex-shaped components with high precision. Many PM products are subjected to fatigue loading in service, in part up to very high loading cycle numbers. In this paper the peculiarities of fatigue in PM materials and components are shown with focus to high cycle fatigue. It is stressed that for precision parts which are mostly ferrous the inherent porosity is the decisive factor; this porosity originates from the manufacturing process and is evenly distributed within the material. However, there is also the effect of singular defects such as large pores, pore clusters, slag inclusions, etc., and these defects become the more critical the lower the integral porosity is. For fully dense PM products such as powder forged components, tool steels, or extruded light alloys, the singular defects are the decisive feature in the material, and HC fatigue limit is controlled by the largest defect in the stressed volume. KEYWORDS: Powder metallurgy, high cycle fatigue; porosity; defects 1. INTRODUCTION Powder metallurgy implies production of solid metallic materials and components from predominantly metallic powder. This technology has encountered impressive growth in the last decades, and such indispensable products as cemented carbide tools are exclusively manufactured by powder metallurgy [1]. Also in the automotive industry, powder metallurgy components, mainly iron based precision parts, are increasingly being used [2]. Previously, PM automotive parts were geometrically precise but mechanically rather weak; however, this has drastically changed with the introduction of PM components for engines and transmissions. In this case, also fatigue and contact fatigue loading is quite common, and the fatigue behaviour of PM materials is therefore of high relevance for the applications. From the materials scientists’ viewpoint, the microstructure of PM materials is similar to that of cast and/or wrought counterparts. Form the engineer’s viewpoint however it has to be considered that there are much more manufacturing parameters relevant for production of PM materials. This also increases the number of microstructural parameters, e.g. pore related ones, to be taken into account most of which are also relevant for the fatigue behaviour. This makes the behaviour of PM materials more complex and difficult to understand [3]. PM materials can principally be split up into two groups according to manufacturing route and resulting microstructure: PM precision parts are produced by cold uniaxial pressing and subsequent pressureless sintering (to some extent also by powder forging). The residual pores are usually regarded to be the principal characteristic [4]. The most important parameters are total porosity and shape of pores/sintering contacts. Depending on total porosity - which is influenced primarily by the compacting pressure - and sintering conditions the sintering contacts can be isolated or interconnected [5]. In the matrix, the larger microstructural flexibility of PM materials is 195 Danninger and Weiss significant, e.g. distribution of the alloy elements - both homogeneous and inhomogeneous - can be adjusted more freely than with ingot metallurgy. Powder metallurgy full density products [6] are made by hot isostatic pressing (e.g. PM superalloys and tool steels), by extrusion (PM Al alloys) or by pressing with subsequent liquid phase sintering (hard metals, tungsten heavy alloys etc). Residual porosity should be low to negligible, and the microstructure is commonly homogeneous. The most important feature affecting the fatigue behaviour and resulting in marked differences to cast or wrought counterparts is the usually very fine and isotropic microstructure which gives uniform properties regardless of the orientation. On the other hand the materials are sensitive to inclusions the effect of which is further aggravated by the excellent properties of the basic material. Here, the fatigue behaviour of both types of materials is shown, and the common features as well as the differences are described. 2. INFLUENCE OF INTEGRAL POROSITY In pressed and sintered ferrous materials, e.g. for precision parts, the characteristic feature is the “integral” or “primary” porosity. This is in principle the porosity already present in the bulk powder, before compaction. Since the compaction of metal powders is commonly a cold working process, progressive work hardening occurs at the particle contacts and at some stage prevents further densification. Furthermore, the admixed organic pressing lubricant that is inevitable in uniaxial die compaction also absorbs considerable space in the compact and, being virtually incompressible, limits the densification of the metal skeleton. There remains an interconnecting network of pores, in part filled with lubricant, that is essential for the material during lubricant burnout in the initial stages of sintering (lubricant in isolated pores would inevitably result in blistering). During the sintering process, the metal powder particles weld together at the pressing contacts through diffusion processes and form stable metallic bonds. The typical microstructure of a sintered steel as depicted by metallographic techniques is shown in Fig.1 [7]. The sections however can be misleading: during sintering the pore structure remains interconnected in most cases, i.e. at the common density levels of up to 7.4 g.cm-3 for ferrous components (about 6% total porosity). Only through special pressing and / or sintering techniques or by powder forging density levels are attained where the interconnected pore network is dissolved into single isolated pores. Therefore, in most cases the sintered iron can be described through a “sponge” model, and only at rather high density levels the “swiss cheese” model, with isolated holes, applies. The structure of the pore network in sintered materials can be seen e.g. in resin replicas of the pore network, the iron skeleton having been etched away after resin impregnation [5]. The fact that the pores are mostly interconnected implies that the sintering contacts, which actually bear the load in the material (pores of course cannot be load-bearing), are isolated in these cases, and description of the microstructure has to focus at the sintering contacts. Furthermore, the pores form a very complex, 3-dimensional structure that is virtually impossible to depict in a single 2-dimensional metallographic section [8]. Therefore, it was shown rather early by Slesar [9] that fractographic techniques are more suited for describing the mechanical behaviour of sintered steels. If the fracture surfaces are obtained by a low deformation fracturing technique such as e.g. impact testing at 77K or high cycle fatigue testing, the fracture path runs through the weakest areas of the material, i.e. the thinnest parts of the sintering contacts, which are exactly those structural features that limit the mechanical resistance of the material [10]. Therefore, there should be a relationship between the total area of the sintering contacts in the weakest cross section – which can be defined as the “load bearing cross section” Ac – and the mechanical properties of the material. 196 VIII Congreso Nacional de Propiedades Mecánicas de Sólidos Figure 1. Schematic of the microstructure in ferrous PM components [7] If high strength sintered steels are e.g. impact tested at 77K, low-deformation fracture surfaces are obtained as typically shown in Fig.2a, c, e for varying total porosity levels. By suitable image analysing techniques [11], the area of the broken necks can be determined as a fraction of the total cross section, which yields the parameter Ac. In Fig.2b, d, f the broken contacts as analyzed by a specially developed routine are shown white. Here it stands out clearly that the load bearing cross section Ac is much lower than would be expected from the volume fraction of the metal phase. Even for the high porosity material in which the load bearing cross section is only about 0.15, i.e. only about 15% of the entire cross section consists of metallic contacts, still more than 70% of the volume is taken by the metallic phase. This of course results in comparatively low strength-to-weight ratio and indicates that increasing the relative density, i.e. lowering the porosity, is an essential measure to improve the mechanical behaviour of the material. In Fig.3a the fatigue endurance strength – push-pull mode at R = -1, determined by 8 ultrasonic techniques [12] at Nmax = 2.10 - of the Mo prealloyed sintered steel depicted in Fig.2 is shown as a function of the total porosity, and there is also the hypothetical function 1- P if Sw would follow the volume fraction of the metal phase. The much lower values for Sw compared to the function 1-P indicate the out-of-proportion effect of the porosity. This is still more noticeable if the specific endurance strength is given as in Fig.3b, once more in parallel to the absolute values; it is visible that the lower density of the porous specimens does not exert any significant effect on the trend of the fatigue endurance strength. 197 Danninger and Weiss Figure 2a/b: Ptot = 18.5% Figure 2c/d: Ptot = 12.3% Figure 2e: Ptot = 8.0% Figure 2. Fracture surfaces of high strength sintered steel Fe-1.5%Mo-0.7%C of varying porosity, heat treated. Impact testing at 77K: fracture surfaces analyzed through image processing system These results strongly confirm that it is not so much the total porosity that directly affects the mechanical properties but it must be a parameter that takes into account the real geometry of the microstructure. Here the load bearing cross section Ac seems to be well suited.
Recommended publications
  • Top Performance When the Going Gets Tough
    Top performance when the going gets tough The Alfa Laval DuroShell plate-and-shell heat exchanger Sub-headline coming soon DuroShell – plate-and-shell made tougher Alfa Laval DuroShell is a specially engineered plate-and-shell heat exchanger ideal for demanding duties and corrosive media. Able to withstand fatigue even at high temperatures and pressures, it outperforms not only traditional heat exchangers, but also other plate-and-shells. As flexible as it is strong DuroShell creates new possibilities through its com- pactness, efficiency and exceptional resistance to fatigue. Able to work with liquids, gases and two- phase mixtures, it stands out among heat exchangers in its duty range. DuroShell handles pressures up to 100 barg (1450 psig) in compliance with PED and ASME, and temperatures as high as 450 °C (842 °F). Built for your application DuroShell is fully welded and gasket-free, with internal features that make it still more robust. Plates are avail- able in 316L stainless steel, while the pressure vessel itself can be built in 316L stainless steel or carbon steel. Three different sizes are possible, with heat transfer surfaces ranging 2–235 m2 (21.5–2530 ft 2) in area. DuroShell RollerCoaster Robust and efficient performance. DuroShell PowerPack Optimized flow distribution and fatigue resistance. Learn more at www.alfalaval.com/duroshell Plate-and-shell benefits made better • More uptime and longer life due to • Installation savings through even greater fatigue resistance more compact, lightweight design • Higher operating pressures thanks • Greater reliability as a result of to robust, patented construction closed, fully welded construction • Operational gains created by 15–20 % higher thermal efficiency How it works Revolutionary technology Optimized flow DuroShell is a plate-and-shell heat exchanger, but one DuroShell operates with one media on the plate side with a unique internal design.
    [Show full text]
  • Fatigue Overview Introduction to Fatigue Analysis
    Fatigue overview Introduction to fatigue analysis • Fatigue is the failure of a component after several repetitive load cycles. • As a one-time occurrence, the load is not dangerous in itself. Over time the alternating load is able to break the structure anyway. • It is estimated that between 50 and 90 % of product failures is caused by fatigue, and based on this fact, fatigue evaluation should be a part of all product development. What is fatigue? In materials science, fatigue is the progressive and localized structural damage that occurs when a material is subjected to cyclic loading (material is stressed repeatedly). Clients tous différents Routes de qualités variables Contraintes Fatigue Design in Automotive Industry Conception fiable PSA (Peugeot Citroën) Résistances 3s 3s Dispersion matériau Dispersion de production Fatigue • Fracture mechanics can be divided into three stages: 1. Crack nucleation 2. Crack-growth 3. Ultimate ductile failure Introduction to fatigue analysis • Fatigue is the failure of a component after several repetitive load cycles. • As a one-time occurrence, the load is not dangerous in itself. Over time the alternating load is able to break the structure anyway. • It is estimated that between 50 and 90 % of product failures is caused by fatigue, and based on this fact, fatigue evaluation should be a part of all product development. Historical background • In comparison to the classical stress analysis, fatigue theory is a relative new phenomenon. The need to understand fatigue arose after the industrial revolution introduced steel structures. Three areas were particularly involved in early failures: Railway trains, Mining equipment and Bridges. Historical background • 1837: Wilhelm Albert publishes the first article on fatigue.
    [Show full text]
  • Corrosion Fatigue of Austenitic Stainless Steels for Nuclear Power Engineering
    metals Article Corrosion Fatigue of Austenitic Stainless Steels for Nuclear Power Engineering Irena Vlˇcková 1,*, Petr Jonšta 2, ZdenˇekJonšta 2, Petra Vá ˇnová 2 and Tat’ána Kulová 2 1 RMTSC, Material & Metallurgical Research Ltd., Remote Site Ostrava, VÚHŽ a.s., Dobrá 739 51, Czech Republic 2 Department of Materials Engineering, VŠB-Technical University of Ostrava, Ostrava 708 33, Czech Republic; [email protected] (P.J.); [email protected] (Z.J.); [email protected] (P.V.); [email protected] (T.K.) * Correspondence: [email protected]; Tel.: +420-558601257 Academic Editor: Hugo F. Lopez Received: 21 September 2016; Accepted: 8 December 2016; Published: 16 December 2016 Abstract: Significant structural steels for nuclear power engineering are chromium-nickel austenitic stainless steels. The presented paper evaluates the kinetics of the fatigue crack growth of AISI 304L and AISI 316L stainless steels in air and in corrosive environments of 3.5% aqueous NaCl solution after the application of solution annealing, stabilizing annealing, and sensitization annealing. Comparisons were made between the fatigue crack growth rate after each heat treatment regime, and a comparison between the fatigue crack growth rate in both types of steels was made. For individual heat treatment regimes, the possibility of the development of intergranular corrosion was also considered. Evaluations resulted in very favourable corrosion fatigue characteristics of the 316L steel. After application of solution and stabilizing annealing at a comparable DK level, the fatigue crack growth rate was about one half compared to 304L steel. After sensitization annealing of 316L steel, compared to stabilizing annealing, the increase of crack growth rate during corrosion fatigue was slightly higher.
    [Show full text]
  • Design for Cyclic Loading, Soderberg, Goodman and Modified Goodman's Equation
    Design for Cyclic Loading 1. Completely reversing cyclic stress and endurance strength A purely reversing or cyclic stress means when the stress alternates between equal positive and Pure cyclic stress negative peak stresses sinusoidally during each 300 cycle of operation, as shown. In this diagram the stress varies with time between +250 MPa 200 to -250MPa. This kind of cyclic stress is 100 developed in many rotating machine parts that 0 are carrying a constant bending load. -100 When a part is subjected cyclic stress, Stress (MPa) also known as range or reversing stress (Sr), it -200 has been observed that the failure of the part -300 occurs after a number of stress reversals (N) time even it the magnitude of Sr is below the material’s yield strength. Generally, higher the value of Sr, lesser N is needed for failure. No. of Cyclic stress stress (Sr) reversals for failure (N) psi 1000 81000 2000 75465 4000 70307 8000 65501 16000 61024 32000 56853 64000 52967 96000 50818 144000 48757 216000 46779 324000 44881 486000 43060 729000 41313 1000000 40000 For a typical material, the table and the graph above (S-N curve) show the relationship between the magnitudes Sr and the number of stress reversals (N) before failure of the part. For example, if the part were subjected to Sr= 81,000 psi, then it would fail after N=1000 stress reversals. If the same part is subjected to Sr = 61,024 psi, then it can survive up to N=16,000 reversals, and so on. Sengupta MET 301: Design for Cyclic Loading 1 of 7 It has been observed that for most of engineering materials, the rate of reduction of Sr becomes negligible near the vicinity of N = 106 and the slope of the S-N curve becomes more or less horizontal.
    [Show full text]
  • Very High Cycle Fatigue of Engineering Materials
    Faculty of Technology and Science Materials Engineering Vitaliy Kazymyrovych Very high cycle fatigue of engineering materials (A literature review) Karlstad University Studies 2009:22 Vitaliy Kazymyrovych Very high cycle fatigue of engineering materials (A literature review) Karlstad University Studies 2009:22 Vitaliy Kazymyrovych. Very high cycle fatigue of engineering materials - A literature review Research Report Karlstad University Studies 2009:22 ISSN 1403-8099 ISBN 978-91-7063-246-4 © The Author Distribution: Faculty of Technology and Science Materials Engineering SE-651 88 Karlstad +46 54 700 10 00 www.kau.se Printed at: Universitetstryckeriet, Karlstad 2009 Very high cycle fatigue of engineering materials (A literature review) V.Kazymyrovych* Department of Materials Engineering, Karlstad University SE-651 88, Sweden * Email address: [email protected] Abstract This paper examines the development and present status of the Very High Cycle Fatigue (VHCF) phenomenon in engineering materials. The concept of ultrasonic fatigue testing is described in light of its historical appearance covering the main principles and equipment variations. The VHCF behaviour of the most important materials used for very long life applications is presented, with particular attention paid to steels. In section 3 the VHCF properties of titanium-, nickel-, aluminium- and magnesium alloys are described. Furthermore, the typical fatigue behaviour and mechanisms of pure metals are presented. Section 4 examines the VHCF properties of various types of steels e.g. low carbon steel, spring steel, stainless steel, bearing steel as well as tool steel. In addition to this, the main material defects that initiate VHCF failure are examined in this study. Furthermore, the different stages characteristic for fatigue crack development in VHCF are described in section 5 in terms of relative importance and sequence.
    [Show full text]
  • Creep-Fatigue Failure Diagnosis
    Review Creep-Fatigue Failure Diagnosis Stuart Holdsworth Received: 22 October 2015 ; Accepted: 6 November 2015 ; Published: 16 November 2015 Academic Editor: Robert Lancaster EMPA: Swiss Federal Laboratories for Materials Science and Technology Überlandstrasse 129, Dübendorf CH-8600, Switzerland; [email protected]; Tel.: +41-58-765-47-32 Abstract: Failure diagnosis invariably involves consideration of both associated material condition and the results of a mechanical analysis of prior operating history. This Review focuses on these aspects with particular reference to creep-fatigue failure diagnosis. Creep-fatigue cracking can be due to a spectrum of loading conditions ranging from pure cyclic to mainly steady loading with infrequent off-load transients. These require a range of mechanical analysis approaches, a number of which are reviewed. The microstructural information revealing material condition can vary with alloy class. In practice, the detail of the consequent cracking mechanism(s) can be camouflaged by oxidation at high temperatures, although the presence of oxide on fracture surfaces can be used to date events leading to failure. Routine laboratory specimen post-test examination is strongly recommended to characterise the detail of deformation and damage accumulation under known and well-controlled loading conditions to improve the effectiveness and efficiency of failure diagnosis. Keywords: failure diagnosis; creep-fatigue; material condition; mechanical analysis 1. Introduction The diagnosis of failures invariably involves consideration of both the associated material condition and the results of a mechanical analysis of prior operating history. Material condition refers not only to a knowledge of the chemical composition and mechanical properties relative to those originally specified for the failed component, but also the appearance and extent of microstructural and physical damage responsible for failure.
    [Show full text]
  • Creep, Fatigue and Creep-Fatigue Interactions in Modified 9% Cr - 1% Mo (P91) Steels" (2013)
    University of Arkansas, Fayetteville ScholarWorks@UARK Theses and Dissertations 5-2013 Creep, Fatigue and Creep-Fatigue Interactions in Modified 9% rC - 1% Mo (P91) Steels Valliappa Kalyanasundaram University of Arkansas, Fayetteville Follow this and additional works at: http://scholarworks.uark.edu/etd Part of the Mechanics of Materials Commons, Structural Engineering Commons, and the Structural Materials Commons Recommended Citation Kalyanasundaram, Valliappa, "Creep, Fatigue and Creep-Fatigue Interactions in Modified 9% Cr - 1% Mo (P91) Steels" (2013). Theses and Dissertations. 692. http://scholarworks.uark.edu/etd/692 This Dissertation is brought to you for free and open access by ScholarWorks@UARK. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of ScholarWorks@UARK. For more information, please contact [email protected], [email protected]. CREEP, FATIGUE AND CREEP-FATIGUE INTERACTIONS IN MODIFIED 9% Cr – 1% Mo (P91) STEELS CREEP, FATIGUE AND CREEP-FATIGUE INTERACTIONS IN MODIFIED 9% Cr – 1% Mo (P91) STEELS A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy in Mechanical Engineering By Valliappa Kalyanasundaram Madurai Kamaraj University Bachelor of Engineering in Mechanical Engineering, 2004 University of Arkansas Master of Science in Mechanical Engineering, 2008 May 2013 University of Arkansas ABSTRACT Grade P91 steel, from the class of advanced high-chrome ferritic steels, is one of the preferred materials for many elevated temperature structural components. Creep-fatigue (C-F) interactions, along with oxidation, can accelerate the kinetics of damage accumulation and consequently reduce such components’ life. Hence, reliable C-F test data is required for meticulous consideration of C-F interactions and oxidation, which in turn is vital for sound design practices.
    [Show full text]
  • Analysis of Fatigue and Wear Behaviour in Ultrafine Grained Connecting Rods
    metals Article Analysis of Fatigue and Wear Behaviour in Ultrafine Grained Connecting Rods Rodrigo Luri, Carmelo J. Luis, Javier León, Juan P. Fuertes, Daniel Salcedo and Ignacio Puertas * Mechanical, Energetics and Materials Engineering Department, Public University of Navarre, Campus Arrosadía s/n, Pamplona 31006, Spain; [email protected] (R.L.); [email protected] (C.J.L.); [email protected] (J.L.); [email protected] (J.P.F.); [email protected] (D.S.) * Correspondence: [email protected]; Tel.: +34-948-169-305 Received: 3 July 2017; Accepted: 20 July 2017; Published: 29 July 2017 Abstract: Over the last few years there has been an increasing interest in the study and development of processes that make it possible to obtain ultra-fine grained materials. Although there exists a large number of published works related to the improvement of the mechanical properties in these materials, there are only a few studies that analyse their in-service behaviour (fatigue and wear). In order to bridge the gap, in this present work, the fatigue and wear results obtained for connecting rods manufactured by using two different aluminium alloys (AA5754 and AA5083) previously deformed by severe plastic deformation (SPD), using Equal Channel Angular Pressing (ECAP), in order to obtain the ultrafine grain size in the processed materials are shown. For both aluminium alloys, two initial states were studied: annealed and ECAPed. The connecting rods were manufactured from the previously processed materials by using isothermal forging. Fatigue and wear experiments were carried out in order to characterize the in-service behaviour of the components.
    [Show full text]
  • Assessment of Fatigue Damage and Crack Propagation in Ceramic Matrix Composites by Infrared Thermography
    ceramics Article Assessment of Fatigue Damage and Crack Propagation in Ceramic Matrix Composites by Infrared Thermography Konstantinos G. Dassios * and Theodore E. Matikas Department of Materials Science &Engineering, University of Ioannina, 45110 Ioannina, Greece; [email protected] * Correspondence: [email protected] Received: 20 March 2019; Accepted: 27 May 2019; Published: 10 June 2019 Abstract: The initiation and propagation of damage in SiC fiber-reinforced ceramic matrix composites under static and fatigue loads were assessed by infrared thermography (IRT). The proposed thermographic technique, operating in lock-in mode, enabled early prediction of the residual life of composites, and proved vital in the rapid determination of the materials’ fatigue limit requiring testing of a single specimen only. IRT was also utilized for quantification of crack growth in the materials under cyclic loads. The paper highlights the accuracy and versatility of IRT as a state-of-the art damage assessment tool for ceramic composites. Keywords: ceramics; composites; thermography; fatigue; crack growth 1. Introduction The highly desirable properties of ceramic matrix composites (CMC), including damage tolerance, fracture toughness, wear- and corrosion resistance, and crack growth resistance, allow them to withstand severe thermomechanical loading conditions [1]. As such, the materials are used today in aerospace applications, such as braking systems, structural components, nozzles, and thermal barriers. Glass–ceramic matrix composites reinforced with continuous SiC fibers have received particular scientific attention as they offer additional attractive properties, such as high strength and stiffness, low density, and chemical inertness at conventional and oxidative environments and over a wide range of temperatures [2]. The necessity of monitoring the structural integrity of aerospace composites and their structures is key to the prevention of failure as well as to the safe and economical operation of the structures.
    [Show full text]
  • Investigation of Corrosion Fatigue Phenomena in Transient Zone of Mechanical Drive Steam Turbines and Its Preventive Measures
    Proceedings of the Second Middle East Turbomachinery Symposium 17 – 20 March 2013, Doha, Qatar Investigation of Corrosion Fatigue Phenomena in Transient Zone of Mechanical Drive Steam Turbines and its Preventive Measures by Satoshi Hata Engineering and Design Division Mitsubishi Heavy Industries, Compressor Corporation Naoyuki Nagai Hiroshima Research & Development Center Mitsubishi Heavy Industries, Ltd. Norihito Fujimura MCO Saudi Arabia, LCC. (MCOSA) Mitsubishi Heavy Industries, Compressor Corporation Satoshi Hata ABSTRACT Satoshi Hata is a Group Manager For mechanical drive steam turbines, the investigation within the Turbo Machinery results of corrosion fatigue phenomena in the transient zone Engineering Department, Mitsubishi are introduced, including basic phenomena on expansion Heavy Industries, Ltd., in Hiroshima, line and actual design and damage experience. These results Japan. He has 30 year experience in were analyzed from the standpoint of stress intensity during R&D for nuclear uranium centrifuges, turbomolecular pumps, heavy-duty the start of cracking. In order to resolve such problems, gas turbines, steam turbines and preventive coating and blade design methods against fouling compressors. Mr. Hata has B.S., M.S. and corrosive environments are developed. Detailed and Ph.D. degrees (in Mechanical evaluation test results are given for coating performance Engineering) from Kyusyu Institute of using a unique test procedure simulating fouling phenomena Technology. and washing conditions. Finally, the results of the Naoyuki
    [Show full text]
  • Creep-Fatigue Deformation Behaviour of OFHC-Copper and Cucrzr Alloy with Different Heat Treatments and with and Without Neutron Irradiation
    Risø-R-1528(EN) Creep-Fatigue Deformation Behaviour of OFHC-Copper and CuCrZr Alloy with Different Heat Treatments and with and without Neutron Irradiation B.N. Singh, M. Li, J.F. Stubbins and B.S. Johansen Risø National Laboratory Roskilde Denmark August 2005 Author: B.N. Singh1), M. Li2), J.F. Stubbins3) and B.S. Johansen1) Risø-R-1528(EN) August 2005 Title: Creep-Fatigue Deformation Behaviour of OFHC-Copper and CuCrZr Alloy with Different Heat Treatments and with and without Neutron Irradiation Department: Materials Research Department 1)Materials Research Department, Risø National Laboratory DK-4000 Roskilde, Denmark 2)Metals and Ceramics Division, Oak Ridge National Laboratory Oak Ridge, Tennessee, USA 3)Department of Nuclear, Plasma and Radiological Engineering University of Illinois, Urbana, Illinois, USA ISSN 0106-2840 Abstract ISBN 87-550-3465-9 The creep-fatigue interaction behaviour of a precipitation hardened CuCrZr alloy was investigated at 295 and 573 K. To determine the effect of irradiation a number of fatigue specimens were irradiated at 333 and 573 K to a dose level in the range of 0.2 - 0.3 dpa and were tested at room temperature and 573 K, respectively. The creep-fatigue deformation behaviour of OFHC-copper was also investigated but only in the Contract no.: unirradiated condition and at room temperature. The creep-fatigue TW1-TVV-COP, TW2-TVM-CUCFA and interaction was simulated by applying a certain holdtime on both tension TW3-TVM-CUCFA2 and compression sides of the cyclic loading with a frequency of 0.5 Hz. Holdtimes of up to 1000 seconds were used.
    [Show full text]
  • Study on Wear and Fatigue Performance of Two Types of High-Speed Railway Wheel Materials at Different Ambient Temperatures
    materials Article Study on Wear and Fatigue Performance of Two Types of High-Speed Railway Wheel Materials at Different Ambient Temperatures Lei MA 1,* , Wenjian WANG 2, Jun GUO 2 and Qiyue LIU 2 1 School of Mechanical Engineering, Xihua University, Chengdu 610039, China 2 Tribology Research Institute, State Key Laboratory of Traction Power, Southwest Jiao Tong University, Chengdu 610031, China; [email protected] (W.W.); [email protected] (J.G.); [email protected] (Q.L.) * Correspondence: [email protected] Received: 14 January 2020; Accepted: 2 March 2020; Published: 5 March 2020 Abstract: The wear and fatigue behaviors of two newly developed types of high-speed railway wheel materials (named D1 and D2) were studied using the WR-1 wheel/rail rolling–sliding wear simulation device at high temperature (50 C), room temperature (20 C), and low temperature ( 30 C). The ◦ ◦ − ◦ results showed that wear loss, surface hardening, and fatigue damage of the wheel and rail materials at high temperature (50 C) and low temperature ( 30 C) were greater than at room temperature, ◦ − ◦ showing the highest values at low temperature. With high Si and V content refining the pearlite lamellar spacing, D2 presented better resistance to wear and fatigue than D1. Generally, D2 wheel material appears more suitable for high-speed railway wheels. Keywords: alpine region; high-speed wheel and rail materials; temperature; wear; fatigue damage 1. Introduction Railways play a vital role in the development of rail transportation. The environmental climate has a certain impact on wheel/rail systems exposed to the open air. Especially in China, wheel and rail materials may serve under extreme temperature conditions due to torridity and severe cold.
    [Show full text]