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Thermal Shock
TEACHER INSTRUCTIONS Thermal Shock Objective: To illustrate thermal expansion and thermal shock. Background Information: In physics, thermal expansion is the tendency of matter to increase in volume or pressure when heated. For liquids and solids, the amount of expansion will normally vary depending on the material’s coefficient of thermal expansion. When materials contract, tensile forces are created. When things expand, compressive forces are created. Thermal shock is the name given to cracking as a result of rapid temperature change. From the laboratory standpoint, there are three main types of glass used today: borosilicate, quartz, and soda lime or flint glass. Borosilicate glass is made to withstand thermal shock better than most other glass through a combination of reduced expansion coefficient and greater strength, though fused quartz outperforms it in both respects. Some glass-ceramic materials include a controlled proportion of material with a negative expansion coefficient, so that the overall coefficient can be reduced to almost exactly zero over a reasonably wide range of temperatures. Improving the shock resistance of glass and ceramics can be achieved by improving the strength of the materials or by reducing its tendency to uneven expansion. One example of success in this area is Pyrex, the brand name that is well known to most consumers as cookware, but which is also used to manufacture laboratory glassware. Pyrex traditionally is made with a borosilicate glass with the addition of boron, which prevents shock by reducing the tendency of glass to expand. Demo description: Three different types of glass rods will be heated so that students can observe the amount of thermal shock that occurs. -
Area Array Packages with Known Reliably and Mitigation Risks, Allowing Greater Processing Power in a Smaller Board Footprint and Lower System Weight
National Aeronautics and Space Administration Reliability of CGA/LGA/HDI Package Board/Assembly (Revision A) Reza Ghaffarian, Ph.D. Jet Propulsion Laboratory Pasadena, California Jet Propulsion Laboratory California Institute of Technology Pasadena, California JPL Publication 12-3 2/12 National Aeronautics and Space Administration Reliability of CGA/LGA/HDI Package Board/Assembly (Revision A) NASA Electronic Parts and Packaging (NEPP) Program Office of Safety and Mission Assurance Reza Ghaffarian, Ph.D. Jet Propulsion Laboratory Pasadena, California NASA WBS: 724297.40.43 JPL Project Number: 104593 Task Number: 40.49.02.02 Jet Propulsion Laboratory 4800 Oak Grove Drive Pasadena, CA 91109 http://nepp.nasa.gov This research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, and was sponsored by the National Aeronautics and Space Administration Electronic Parts and Packaging (NEPP) Program. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not constitute or imply its endorsement by the United States Government or the Jet Propulsion Laboratory, California Institute of Technology. Copyright 2013. California Institute of Technology. Government sponsorship acknowledged. Acknowledgments The author would like to acknowledge many people from industry and the Jet Propulsion Laboratory (JPL) who were critical to the progress of this activity. The author extends his appreciation to program managers of the National Aeronautics and Space Administration Electronics Parts and Packaging (NEPP) Program, including Michael Sampson, Ken LaBel, Drs. Charles Barnes and Douglas Sheldon for their continuous support and encouragement. ii OBJECTIVES AND PRODUCTS Commercial-off-the-shelf column grid array (COTS CGA) packaging technologies in high-reliability versions are now being considered for use in a number of National Aeronautics and Space Administration (NASA) electronic systems. -
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. -
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. -
MATERIAL SCIENCE Module 3 Thermal Shock Thermal Shock DOE-HDBK-1017/2-93 TABLE of CONTENTS
Department of Energy Fundamentals Handbook MATERIAL SCIENCE Module 3 Thermal Shock Thermal Shock DOE-HDBK-1017/2-93 TABLE OF CONTENTS TABLE OF CONTENTS LIST OF FIGURES .................................................. ii LIST OF TABLES ................................................... iii REFERENCES .................................................... iv OBJECTIVES ..................................................... v THERMAL STRESS ................................................ 1 Thermal Shock ............................................... 1 Summary ................................................... 5 PRESSURIZED THERMAL SHOCK .................................... 6 Definition ................................................... 6 Evaluating Effects of PTS ....................................... 6 Locations of Primary Concern ..................................... 8 Summary ................................................... 8 Rev. 0 Page i MS-03 LIST OF FIGURES DOE-HDBK-1017/2-93 Thermal Shock LIST OF FIGURES Figure 1 Stress on Reactor Vessel Wall .................................... 4 Figure 2 Heatup Stress Profile .......................................... 7 Figure 3 Cooldown Stress Profile ........................................ 7 MS-03 Page ii Rev. 0 Thermal Shock DOE-HDBK-1017/2-93 LIST OF TABLES LIST OF TABLES Table 1 Coefficients of Linear Thermal Expansion ............................ 2 Rev. 0 Page iii MS-03 REFERENCES DOE-HDBK-1017/2-93 Thermal Shock REFERENCES Academic Program for Nuclear Power Plant Personnel, Volume -
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. -
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. -
Thermal Shock-Resistant Cement
BNL-101087-2012-IR Thermal Shock-resistant Cement T. Sugama, T. Pyatina, S. Gill February 2012 Sustainable Energy Technologies Department/Energy Conversion Group Brookhaven National Laboratory U.S. Department of Energy DOE office of Energy Efficiency and Renewable Energy Notice: This manuscript has been authored by employees of Brookhaven Science Associates, LLC under Contract No. DE-AC02-98CH10886 with the U.S. Department of Energy. The publisher by accepting the manuscript for publication acknowledges that the United States Government retains a non-exclusive, paid-up, irrevocable, world-wide license to publish or reproduce the published form of this manuscript, or allow others to do so, for United States Government purposes. 1 DISCLAIMER This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, nor any of their contractors, subcontractors, or their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or any third party’s use or the results of such use of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof or its contractors or subcontractors. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof. -
Corrosion Science 173 (2020) 108828
Corrosion Science 173 (2020) 108828 Contents lists available at ScienceDirect Corrosion Science journal homepage: www.elsevier.com/locate/corsci The oxidation effect on the cracking behavior of a Co-based alloy under thermal shocks T Junxia Wena,b,c,d, Rui Caoa,b,*, Hongyan Chee, Hao Donge, Haiyan Zhanga,b, Yingjie Yana,b, Yanfei Gaoc,**, Peter K Liawc,** a State Key Laboratory of Advanced Processing and Recycling of Non-ferrous Metal, Lanzhou University of Technology, Lanzhou, 730050, Gansu, China b School of Materials Science and Engineering, Lanzhou University of Technology, Lanzhou, 730050, Gansu, China c Department of Materials Science and Engineering, The University of Tennessee, Knoxville, TN, 37996, USA d School of Mechanical and Electrical Engineering, Liuzhou Vocational & Technical College, Liuzhou 545006, Guangxi, China e Advanced Technology & Materials Limited Company, China Iron & Steel Research Institute Group, Beijing, 100081, China ARTICLE INFO ABSTRACT Keywords: Oxidation and cracking behavior during thermal-shock experiments of a new Co-based alloy were analyzed in Co-based alloy the present work. Comparing to the static conditions, the oxidation behavior during thermal shocks is stress- Thermal shock assisted and crack-accelerated. Cracks during the thermal shocks were initiated from the sample surfaces and Oxidation their growth are driven by various stresses, including those induced by volume change, mismatch of coefficients Crack of thermal expansion (CTEs), and temperature gradient between the matrix and the internal oxides. It is found Thermal fatigue that the crack propagation correlates to these stresses in the classic Paris’ law. 1. Introduction also different from that in the static oxidation. The cyclic oxidation behavior of the Co-based alloy has been well investigated by Barrett The Co-based alloy has a good combination of high-temperature and Lowel [13]. -
Theoretical Research on Thermal Shock Resistance of Ultra-High Temperature Ceramics Focusing on the Adjustment of Stress Reduction Factor
Materials 2013, 6, 551-564; doi:10.3390/ma6020551 OPEN ACCESS materials ISSN 1996-1944 www.mdpi.com/journal/materials Article Theoretical Research on Thermal Shock Resistance of Ultra-High Temperature Ceramics Focusing on the Adjustment of Stress Reduction Factor Dengjian Li 1, Weiguo Li 1,*, Dingyu Li 1, Yushan Shi 1 and Daining Fang 2 1 State Key Laboratory of Coal Mine Disaster Dynamics and Control, College of Resources and Environmental Science, Chongqing University, Chongqing 400030, China; E-Mails: [email protected] (De.L.); [email protected] (Di.L.); [email protected] (Y.S.) 2 State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University, Beijing 100871, China; E-Mail: [email protected] * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel.: +86-023-6546-8932; Fax: +86-023-6546-8932. Received: 27 November 2012; in revised form: 30 January 2013 / Accepted: 31 January 2013 / Published: 18 February 2013 Abstract: The thermal shock resistance of ceramics depends on not only the mechanical and thermal properties of materials, but also the external constraint and thermal condition. So, in order to study the actual situation in its service process, a temperature-dependent thermal shock resistance model for ultra-high temperature ceramics considering the effects of the thermal environment and external constraint was established based on the existing theory. The present work mainly focused on the adjustment of the stress reduction factor according to different thermal shock situations. The influences of external constraint on both critical rupture temperature difference and the second thermal shock resistance parameter in either case of rapid heating or cooling conditions had been studied based on this model. -
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. -
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.