VST-Technology Trends.Indd

Total Page:16

File Type:pdf, Size:1020Kb

VST-Technology Trends.Indd Vacuum/Surface Treating Technology Trends in Vacuum Heat Treating Part Two: Processes and Applications Daniel H. Herring – The HERRING GROUP, Inc., Elmhurst, Ill. Vacuum thermal processing is key for aerospace component manufacturers due to industry demands for the highest possible quality. Brazing and surface treatment are two process areas where vacuum technology is utilized by the aerospace industry. art two of this series contin- ues our discussion of vacuum heat-treating processes and P applications. Brazing The volume of work produced by vacuum brazing far exceeds that of any other pro- cess in which vacuum furnaces are being utilized. The transportation (automotive and aerospace) industry has provided the impetus for the increasing use of vacuum furnaces for brazing, and the use of light- weight, high-strength materials have also contributed to the popularity of brazing. As with all brazing, variables that need to be controlled to produce mechanically sound braze joints include base-metal selec- Fig. 1a. Jet engine turbine blades brazed in a horizontal vacuum furnace tion and characteristics, fi ller-metal selection and characteristics, component design, joint design and clearance, surface preparation, fi ller-metal fl ow characteristics, temperature and time, and rate and source of heating. Some factors affect the ability to pro- duce a metallurgically sound braze joint by infl uencing the behavior of the brazed joint, while others affect the base-metal properties, while still others infl uence the interactions between the base metal and fi ller metal. Effects on the base metal include carbide precipitation, hydrogen embrittlement, the nature of the heat- affected zone, oxide stability and sulfur embrittlement. Filler-metal effects include vapor pressure, alloying, phosphorous em- brittlement and stress cracking. Interac- tion effects include post-brazing thermal Fig. 1b. Various aerospace components brazed in a bottom-loading vacuum furnace IndustrialHeating.com - November 2008 57 Vacuum/Surface Treating Fig. 3. Family of aerospace, automotive and industrial components illustrating the Fig. 2. Typical honeycomb seals versatility of low-pressure vacuum carburizing treatments, corrosion resistance and dis- silver-base brazing alloys are used for the furnace is fi rst evacuated to a low pressure similar-metal combinations. fi ller metal. Generally, alloys that contain 10-2 to 10-4 mbar (10-2 to 10-4 torr) to re- Vacuum furnaces can be either hori- easily vaporized elements for lowering the move residual air. The temperature is then zontal or vertical in design (Figs. 1a, 1b) melting points are avoided. With respect raised to approximately 955°C (1750°F) to and have technical advantages including: to the heat treatment of steel, the copper allow outgassing and to remove any sur- • The process permits brazing of com- and the nickel-base brazing alloys are the face contamination. Finally, the furnace plex, dense assemblies with blind pas- most widely used fi ller metals. is heated to brazing temperature normally sages that would be almost impossible 1100–1120°C (2000–2050°F) under a to braze and adequately clean using at- Aluminum and Aluminum Alloys partial pressure of inert gas up to 1 mbar mospheric fl ux-brazing techniques. In the brazing of aluminum components, it (7.5x10-1 torr) to inhibit evaporation of • Vacuum furnaces operating at 10-5 to 10-4 is important that vacuum levels be main- the copper. When brazing is completed, mbar (10-5 to 10-4 torr) remove essential- tained in the 10-5 mbar (10-5 torr) range usually within minutes after the set-point ly all gases that could inhibit the fl ow of or better. Parts are heated to 575–590°C temperature has been reached, the work brazing alloy, prevent the development (1070–1100°F) depending on the alloy. is allowed to slow cool to approximately of tenacious oxide fi lms and promote the Temperature uniformity is critical, typi- 980°C (1800°F) so that the fi ller metal wetting and fl ow of the braze alloy over cally ±5.5°C (±10°F) or better, and multi- will solidify. Parts can then be rapidly the vacuum-conditioned surfaces. ple-zone temperature-controlled furnaces cooled by gas quenching, typically in the • Properly processed parts are unloaded are common. Cycle times are dependent range of 2 bar. in a clean and bright condition, often on furnace type, part confi guration and avoiding additional processing. part fi xturing. Longer cycles are required Nickel-Base Alloys • A wide variety of materials ranging for large parts and very dense loads. Brazing with nickel-base alloys is usually from aluminum, cast irons, stainless done without any partial pressure at the steel, steels, titanium alloys, nickel al- Copper and Copper Alloys vacuum levels in the range of 10-3 to 10-5 loys and cobalt-base superalloys are Copper fi ller metal applied to the base mbar (10-3 to 10-5 torr). Normally, a pre- brazed successfully in vacuum furnaces metal either as paste, foil, clad or solid heat soak at 920–980°C (1700–1800°F) without the use of any fl ux. copper can be vacuum brazed recognizing is used to ensure that large workloads that the high vapor pressure of copper at are uniformly heated. After brazing, the Many different types of nickel, nick- its melting point causes some evaporation furnace temperature can be lowered for el-base, copper, copper-base, gold-base, and undesirable contamination of the fur- additional solution or hardening heat palladium-base, aluminum-base and some nace internals. To prevent this action, the treatments before gas cooling and un- loading. Table 1. Honeycomb Materials Component AMS Specifi cation Major Constituents Aerospace Brazing Process Example Honeycomb 5536 5878 Ni, Cr, Co, Mo A honeycomb seal (Fig. 2) is a jet engine component designed to in- Rings and Details 5662 5596 5706 Ni, Cr, Mo, Cb, Ti crease engine effi ciency by surround- Filler Metal 4777 4779 4782 Ni, Si, Cr, B ing the airfoil or turbine blade and 58 November 2008 - IndustrialHeating.com Vacuum/Surface Treating Fig. 4. Heavy-duty truck shafts low-pressure vacuum carburized Fig. 5. Automotive transmission gears low-pressure vacuum and oil quenched carburized and high-pressure gas quenched prevent airfl ow around the blade tips. Honeycomb seals are timate contact and achieve a sound joint during brazing. All di- made from a variety of nickel and cobalt superalloys (Table 1) mensions are set during the tacking process. Braze tolerances of designed to withstand the harsh service environments of jet en- 0.25–0.50 mm (0.010–0.020 inch) are common. Proper cleaning gine applications. is another critical pre-braze step. Every effort should be made to Rolling and tacking are the two most important steps in the ensure the part is clean and free of all oxides, contaminants and pre-braze assembly process. Firm tack is necessary to ensure in- oils prior to braze preparation. Where industry turns to turn up the heat Thermcraft is the leader in high performance heat treating technology • superior thermal engineering • heavy duty design • maintenance free operation • custom systems • fast heat up and cool down • single and multi zone Front Loading Box Furnace with pneumatic, vertical lift door Batch Oven Thermcraft also has the heaters you need for high temperature applications that demand high performance Hinged Split Customized Tube Furnace Recirculating Oven P.O. Box 12037 • Winston-Salem, NC 27117 • Phone: (336) 784-4800 • Fax: (336) 784-0634 Website: www.thermcraftinc.com Email: [email protected] Major credit cards accepted. 60 November 2008 - IndustrialHeating.com The furnace cycle is equally as critical as part preparation to Case Hardening by Nitriding and Nitrocarburizing the success of the brazing operation. Parts that ramp too fast are Plasma (ion) nitriding (Fig. 6) using pulsed power generators is at risk for distortion and uneven temperature throughout the as- an option to the traditional gas nitriding process. Nitriding is sembly. Parts that are not stabilized will not see proper braze fl ow. used in many applica- If the assembly quenches too rapidly, there is risk for distortion, tions for increased wear quench cracking of the braze joint and splatter. resistance and improved Brazing of these high-temperature nickel alloys is typically per- sliding friction as well formed at 1040–1200°C (1900–2200°F) in a vacuum level of 10-4 to as in components where 10-5 mbar (10-4 to 10-5 torr). Brazing is performed 40–65°C (100– increased load-bearing 150°F) above the braze-alloy melting point. capacity, fatigue strength Common problems include splatter of the braze alloy, quench and corrosion resistance cracking and distortion. All of these problems can be prevented are important. Corrosion by controlling cleanliness of the part, using proper setup tech- resistance can be especial- nique, designing a proper brazing recipe and operating the fur- ly enhanced by a plasma nace properly. Multiple re-brazes can be performed using shorter post-oxidation treatment. brazing cycles at slightly higher temperatures. Stop-off paints such Dimensional changes are as alumina oxide (preferred) can be applied to reduce the risk of minimal, and the masking unwanted braze fl ow. process for selective nitrid- ing is simple and effective. Case Hardening by Carburizing and Carbonitriding Plasma nitriding uses Low-pressure vacuum carburizing (LPC) or low-pressure vacuum nitrogen gas at low pres- Fig. 6. Plasma nitriding of automo- carbonitriding (LPCN) combined with either high-pressure gas sures in the range of 1–10 tive crankshafts (Photograph Cour- quenching (HPGQ) or oil quenching (OQ) has become increas- mbar (0.75–7.5 torr) as tesy of Surface Combustion) ingly popular over the past decade, with industries such as aero- space, automotive and commercial heat treating spearheading the use of this technology.
Recommended publications
  • Troubleshooting Decorative Electroplating Installations, Part 5
    Troubleshooting Decorative Electroplating Installations, Part 5: Plating Problems Caused Article By Heat & Bath Temperature Fluctuations by N.V. Mandich, CEF, AESF Fellow Technical Technical In previous parts of this series, emphasis was given The fast-machining steels must then be carburized to troubleshooting of the sequences for pre-plating or case-hardened to obtain a surface with the hardness and electroplating over metals, Parts 1 and 2;1 required to support the top chromium electroplate. the causes, symptoms and troubleshooting for Case hardening is the generic term covering several pores, pits, stains, blistering and “spotting-out” processes applicable to steel or ferrous alloys. It changes phenomena, Part 3;2 and troubleshooting plating on the surface composition of the top layer, or case, by plastic systems, Part 4.3 Here in Part 5, causes and adsorption of carbon, nitrogen or a mixture of the two. some typical examples of problems that occur in By diffusion, a concentration gradient is created. The electroplating as a result of a) thermal, mechanical heat-treatments and the composition of the steel are surface treatments, b) the metallurgy of the part to additional variables that should be addressed and taken be plated or c) effects of plating bath temperature into account in the electroplating procedure. on plating variables and quality of the deposits When discussing the effect of heat-treatment on are discussed. subsequent electroplating processes it is necessary to zero in on the type of heat-treatment involved. We Nearly every plater has at one time or another had the can defi ne the heat-treatment process as changing the experience of trying to plate parts that simply would characteristics of the parts by heating above a certain not plate.
    [Show full text]
  • Aluminum Brazing with Non-Corrosive
    Aluminium Brazing with Non-corrosive Fluxes State of the Art and Trends in NOCOLOK® Flux Technology Dr. Hans – Walter Swidersky Solvay Fluor und Derivate GmbH Hans-Boeckler-Allee 20 – 30173 Hanover, Germany Presented at the 6th International Conference on Brazing, High Temperature Brazing and Diffusion Bonding (LÖT 2001), Aachen, Germany (May 2001) – Revised Text Abstract This paper summarises the general development and the current status of aluminium brazing with non-corrosive fluxes. Based on the most common manufacturing practices, present-day brazing operations are described. Numerous improvements to aluminium brazing technology have been made in recent years. The most significant devel- opments and trends are addressed, particularly process reengineering (e.g., cleaning, flux application), cost savings (e.g., water, flux, energy), and aluminium alloy improvements (e.g., high strength, good formability, and long-life). Table of contents Success or failure in CAB production relies on several • Introduction factors. The starting point is good product fit-up. Parts 1. Cleaning and Flux Application to be metallurgically joined must have intimate contact 2. Flux Application Methods at some point along the joint. An adequate (but not 3. Wet Flux Application excessive) quantity of filler metal must be available to 4. Dry/ Electrostatic Flux Application fill the joints. Capillary forces pull the filler into the 5. Post Braze Flux Residue joints. The gap tolerance is 0.1 to 0.15 mm for non-clad 6. Filler Metal Alloys components. When clad products are used, intimate 7. Brazing Alloys and Brazing Sheet contact is recommended; the clad layer(s) will act as a 8.
    [Show full text]
  • Ats 34 and 154 Cm Stainless Heat Treat Procedure
    ATS 34 AND 154 CM STAINLESS HEAT TREAT PROCEDURE This is an oil hardening grade of steel which will require oil quenching. The oil should be a warm, thin quenching oil that contains a safe flash point. Olive oil has been used as a sub­ stitute. As a rule of thumb, there should be a gallon of oil for each pound of steel. For , warming the oil before quenching, you may heat a piece of steel and drop it in the oil. 1.) Wrap blades in stainless tool wrap and leave an extra two inches on each end of the package. (This will be for handling purposes going into the quench as described below.) We suggest a double wrap for this grade. The edges of the foil should be double crimped, being careful to avoid hav­ ing even a pin hole in the wrap. 2 . ) Place in the furnace and heat to 1900"F. After reaching this temperature, immediately start timing the soak time of 25-30 minutes. 3.) After the soak time has elapsed, very quickly and carefully pull the package out with tongs~ place over the quench tank and snip the end of the package allowing the blades to drop into the oil. You should have a wire basket in the quench tank for raising and lowering the blades rather than have them lie s till. Gases are released in the quench and would form a "trap" around the steel unless you keep them movi~g for a minute or so. *IMPORTANT--It is very important that the blades enter the oil quench as quickly as possible after leaving the furnace ! Full hardness would not be reached if this step is not followed.
    [Show full text]
  • Aluminum Alloy AA-6061 and RSA-6061 Heat Treatment for Large Mirror Applications
    Utah State University DigitalCommons@USU Space Dynamics Lab Publications Space Dynamics Lab 1-1-2013 Aluminum Alloy AA-6061 and RSA-6061 Heat Treatment for Large Mirror Applications T. Newsander B. Crowther G. Gubbels R. Senden Follow this and additional works at: https://digitalcommons.usu.edu/sdl_pubs Recommended Citation Newsander, T.; Crowther, B.; Gubbels, G.; and Senden, R., "Aluminum Alloy AA-6061 and RSA-6061 Heat Treatment for Large Mirror Applications" (2013). Space Dynamics Lab Publications. Paper 102. https://digitalcommons.usu.edu/sdl_pubs/102 This Article is brought to you for free and open access by the Space Dynamics Lab at DigitalCommons@USU. It has been accepted for inclusion in Space Dynamics Lab Publications by an authorized administrator of DigitalCommons@USU. For more information, please contact [email protected]. Aluminum alloy AA-6061 and RSA-6061 heat treatment for large mirror applications T. Newswandera, B. Crowthera, G. Gubbelsb, R. Sendenb aSpace Dynamics Laboratory, 1695 North Research Park Way, North Logan, UT 84341;bRSP Technology, Metaalpark 2, 9936 BV, Delfzijl, The Netherlands ABSTRACT Aluminum mirrors and telescopes can be built to perform well if the material is processed correctly and can be relatively low cost and short schedule. However, the difficulty of making high quality aluminum telescopes increases as the size increases, starting with uniform heat treatment through the thickness of large mirror substrates. A risk reduction effort was started to build and test a ½ meter diameter super polished aluminum mirror. Material selection, the heat treatment process and stabilization are the first critical steps to building a successful mirror. In this study, large aluminum blanks of both conventional AA-6061 per AMS-A-22771 and RSA AA-6061 were built, heat treated and stress relieved.
    [Show full text]
  • Heat Treating of Aluminum Alloys
    ASM Handbook, Volume 4: Heat Treating Copyright © 1991 ASM International® ASM Handbook Committee, p 841-879 All rights reserved. DOI: 10.1361/asmhba0001205 www.asminternational.org Heat Treating of Aluminum Alloys HEAT TREATING in its broadest sense, • Aluminum-copper-magnesium systems The mechanism of strengthening from refers to any of the heating and cooling (magnesium intensifies precipitation) precipitation involves the formation of co- operations that are performed for the pur- • Aluminum-magnesium-silicon systems herent clusters of solute atoms (that is, the pose of changing the mechanical properties, with strengthening from Mg2Si solute atoms have collected into a cluster the metallurgical structure, or the residual • Aluminum-zinc-magnesium systems with but still have the same crystal structure as stress state of a metal product. When the strengthening from MgZn2 the solvent phase). This causes a great deal term is applied to aluminum alloys, howev- • Aluminum-zinc-magnesium-copper sys- of strain because of mismatch in size be- er, its use frequently is restricted to the tems tween the solvent and solute atoms. Conse- specific operations' employed to increase quently, the presence of the precipitate par- strength and hardness of the precipitation- The general requirement for precipitation ticles, and even more importantly the strain hardenable wrought and cast alloys. These strengthening of supersaturated solid solu- fields in the matrix surrounding the coher- usually are referred to as the "heat-treat- tions involves the formation of finely dis- ent particles, provide higher strength by able" alloys to distinguish them from those persed precipitates during aging heat treat- obstructing and retarding the movement of alloys in which no significant strengthening ments (which may include either natural aging dislocations.
    [Show full text]
  • Effect of Forming Temperature and Sheet Temper on the Brazing Characteristics of Aluminum Alloy Sheet
    Effect of Forming Temperature and Sheet Temper on the Brazing Characteristics of Aluminum Alloy Sheet by Michael J. Benoit A thesis presented to the University of Waterloo in fulfillment of the thesis requirement for the degree of Doctor of Philosophy in Mechanical and Mechatronics Engineering Waterloo, Ontario, Canada, 2018 © Michael J. Benoit 2018 Examining Committee Membership The following served on the Examining Committee for this thesis. The decision of the Examining Committee is by majority vote. External Examiner DAVID WILKINSON Distinguished University Professor, McMaster University Supervisor MARY WELLS Professor, University of Waterloo Supervisor CAROLYN HANSSON Professor, University of Waterloo Internal Member NORMAN ZHOU Professor, University of Waterloo Internal Member MICHAEL WORSWICK Professor, University of Waterloo Internal-external Member ALEXANDER PENLIDIS Professor, University of Waterloo ii Author’s Declaration This thesis consists of material all of which I authored or co-authored: see Statement of Contributions included in the thesis. This is a true copy of the thesis, including any required final revisions, as accepted by my examiners. I understand that my thesis may be made electronically available to the public. iii Statement of Contributions The research contained within this thesis was conducted as part of a Natural Sciences and Engineering Research Council of Canada Collaborative Research and Development grant (NSERC CRD), in collaboration with Dana Canada Corporation and CanmetMATERIALS. Furthermore, the results presented in Chapters 3 to 6 have been adapted from manuscripts which are published, or are to be published. As a result, a number of co-authors have contributed to the current work. However, all measurements which were not performed by me were conducted either under my direct supervision, or were co-ordinated by me.
    [Show full text]
  • Brazing Compilation of Literature References from 1973 to 1978
    OCTOBER 1979 BRAZING COMPILATION OF LITERATURE REFERENCES FROM 1973 TO 1978. BY J.C. RÖMER N et hf^rlfi rids E norqy R o soa re h \ oundation ECN does not assume any liability with respect to the use of, or for damages resulting from the use of any information, apparatus, method or process disclosed in this document. Netherlands Energy Research Foundation ECN P.O. Box 1 1755 ZG Petf.n(NH) The Netherlands Telephone (0)2246 - 62».. Telex 57211 ECN-7* OCTOBER 1979 BRAZING COMPILATION OF LITERATURE REFERENCES FROM 1973 T01978. BY J.C. ROMER -2- ABSTRACT This report is a compilation of published literature on high temperature brazing covering the period 1973-1978. The references are listed alphabetically with regard to the base material or combination of base materials to be brazed. Trade names are treated as base materials. The report contains approximately 1500 references, of which 300 are to patents. KEYWORDS BRAZING BRAZING ALLOYS FILLER METALS JOINING - 3 CONTENTS ABSTRACT 1. ALUMINIUM 2. ALUMINIUM (FLVXLESS) 3. ALUMINIUM - BERYLLIUM 4. ALUMINIUM/BORON COMPOSITES 5. ALUMINIUM - COPPER 5.1. Aluminium - graphite 5.2. Aluminium - nickel alloys 5.3. Aluminium - niobium 5.4. Aluminium ~ molyldenum 5.5. Aluminium - stainless steel 5.6. Aluminium - steels 5.7. Aluminium - tantalum 5.8. Aluminium - titanium 5.9. Aluminium - tungsten 6. BERYLLIUM 7. BORONNITRIDE• 8. BRASS 8.1. Brass - aluminium 8.2. Brass - steels 9. BRONZE 9.1. Bronze - stainless steels 10. CERAMICS 10.1. Ceramics - metal - 4 - CERMETS 61 11.1. Cermets - stainless steels 62 COBALT 63 COPPER ALLOYS 64 13.1. Copper alloys - brass 68 13.2.
    [Show full text]
  • ALUXCOR 4047 Aluminum Flux Cored Braze Filler Metal
    TECHNICAL INFORMATION SHEET ™ ALUXCOR 4047 ALUMINUM FLUX CORED BRAZE FILLER METAL DESCRIPTION Brazing Range 1080°F- 1120°F (582°C - 605°C) Electrical Conductivity: 40 (%IACS) Aluxcor 4047 flux cored brazing wire is designed for manual and Weight in ft./lb. (0.090 dia.) 184.5 semi-automatic aluminum flame brazing. A common application is brazing HVAC aluminum components including return bends, AVAILABLE FORMS headers, tube assemblies, and distributors. The flux core eliminates the need for a separate flux application and the core Standard diameters in coils, rods, spools, and formed rings. cross section is designed to release a measured amount of flux into the capillary. This ensures good oxidation protection and SPECIFICATION COMPLIANCE suitable capillary fill by the melted aluminum metal. Metal – AWS A5.8 Classification BAlSi-4 Aluxcor 4047 is available with different flux compositions. Each ISO 17672 Code Al 112 flux chemistry and ratio is designed to provide brazing Flux – Conforms to Harris Products Group engineering standard characteristics engineered for your specific application. for cored brazing material. Formula 15.1 is a potassium fluroaluminate salt with a SAFETY INFORMATION melting range of 1049 ° - 1061° F, (564° - 572°C). WARNING: PROTECT yourself and others. Read and understand this Formulas 15.2, 15.3 and 15.4 are cesium fluoroaluminate information. blends which lower flux activity temperature and corresponding FUMES AND GASES can be hazardous to your health. brazing temperature. Inclusion of this compound also allows HEAT RAYS, (infrared radiation) from flame or hot metal can injure eyes. brazing of magnesium containing base metals like 6063. Before use, read and understand the manufacturer’s instructions, Material Safety Data Sheets (MSDS), and your All flux core compositions are non-hygroscopic so post braze employer's safety practices.
    [Show full text]
  • Soldering and Brazing of Copper and Copper Alloys Contents
    Soldering and brazing of copper and copper alloys Contents 1. Introduction 4 5. Quality assurance 47 2. Material engineering fundamentals 9 6. Case studies 48 2.1. Fundamentals of copper and copper alloys 9 6.1 Hot-air solder levelling of printed circuit boards 48 2.2 Filler materials 10 6.2 Strip tinning 49 2.2.1 Soft solder 11 6.3 Fabricating heat exchangers from copper 49 2.2.2 Brazing filler metals 13 6.4 Manufacture of compact high-performance 2.3 Soldering or brazing pure copper 16 radiators from copper 49 2.4 Soldering / brazing copper alloys 18 2.4.1 Low-alloyed copper alloys 18 7. Terminology 50 2.4.2. High-alloyed copper alloys 22 8. Appendix 51 3. Design suitability for soldering/brazing 26 References 57 4. Soldering and brazing methods 29 Index of figures 58 4.1 The soldering/brazing principle 29 4.2 Surface preparation 30 Index of tables 59 4.3 Surface activation 32 4.3.1 Fluxes 33 4.3.2 Protective atmosphere / Shielding gases 35 4.4 Applying the solder or brazing filler metal 36 4.5. Soldering and brazing techniques 37 4.5.1 Soldering with soldering iron 38 4.5.2 Dip bath soldering or brazing 38 4.5.3 Flame soldering or brazing 40 4.5.4 Furnace soldering or brazing 40 4.5.5 Electric resistance soldering or brazing 43 4.5.6 Induction soldering or brazing 44 4.5.7 Electron beam brazing 45 4.5.8 Arc brazing 45 4.5.9 Laser beam soldering or brazing 46 2 | KUPFERINSTITUT.DE List of abbreviations Abbreviations Nd:YAG laser Neodymium-doped yttrium aluminium garnet laser SMD Surface-mounted device PVD Physical vapour deposition RoHS
    [Show full text]
  • Effect of Homogenization on Recrystallization and Precipitation
    Materials Transactions, Vol. 49, No. 2 (2008) pp. 250 to 259 #2008 The Japan Institute of Metals Effect of Homogenization on Recrystallization and Precipitation Behavior of 3003 Aluminum Alloy Hsin-Wen Huang, Bin-Lung Ou and Cheng-Ting Tsai Department of Mechanical Engineering, National Central University, Chung-Li, Taiwan 320, R.O. China This investigation studies 3003 aluminum alloys for automobile heat exchangers. The effects of precipitation in homogenization treatments, recrystallization in extrusion and brazing on extrusion forming ability and final material properties are examined. At first, fine second phase particles were precipitated during the 460C Â 9 h homogenization treatment and coarse particles were precipitated by homogenization treatments with 600C Â 9 h. Second, when the precipitation were not plentiful and fine enough during extrusion, the amount of solution dominated the extrusion breakout pressure, and recrystallization was easier; on the contrary, the domination state was replaced by plentiful and fine precipitated particles, and recrystallization became more difficult. Additionally, the hardness after extrusion was lower in the complete recrystallization position, and higher in the incomplete recrystallization position. Finally, in brazing, the sample under the 460C Â 9h condition (a) underwent full recrystallization from partial recrystallization with a reduction in strength; the local position of the edge of the sample under the 600C Â 9h ! 460C Â 3 h condition (c) exhibited a second recrystallization and a significant drop in hardness. [doi:10.2320/matertrans.MRA2007615] (Received June 19, 2007; Accepted November 26, 2007; Published January 25, 2008) Keywords: 3003 aluminum alloy, homogenization, precipitation, extrusion, brazing, recrystallization, second recrystallization 1. Introduction brazing were determined.
    [Show full text]
  • The Brazing Guide GH Induction Atmospheres
    The Brazing Guide GH Induction Atmospheres Turnkey Heating Solutions GH Induction Atmospheres • 35 Industrial Park Circle, Rochester New York 14624 USA • Tel: 585.368.2120 • Fax: 585.368.2123 • [email protected] • www.inductionatmospheres.com The Brazing Guide Brazing is a method of joining two pieces of metal together with a third, molten filler metal. Of all the methods available for metal joining, brazing may be the most versatile. The process is relatively fast and economical, requires relatively low temperatures and is highly adaptable to automation and lean manufacturing initiatives. Brazed joints have great tensile strength – they are often stronger than the two metals being bonded together. Brazed joints repel gas and liquid, withstand vibration and shock and are unaffected by normal changes in temperature. Because the metals to be joined are not themselves melted, they are not warped or otherwise distorted and retain their original metallurgical characteristics. Use this guide to learn about the different aspects of brazing and the many advantages offered by this unique process. Brazing Overview ..............................................................................................pg 2 Topics include brazing basics, when brazing works best, heat sources for brazing and types of braze joints. Basic Procedures .......................................................................................................pg 4 Describes the basic process and offers recommendations to improve your brazing techniques. Induction Brazing ...............................................................................................pg
    [Show full text]
  • Fundamentals of Heat Treating and Plating
    SEMINARS FOR ENGINEERS Fundamentals of Heat Treating and Plating Fasteners and Other Small Components About the Seminar: Benefits of Attending This two-day seminar was developed for engineers and technical Gain an understanding of what is occurring when a fastener is heat treated personnel to gain a high level, broad understanding of why and Become familiar with the common heat treating processes how fasteners and other similar items are heat treated and plated for fasteners or coated. The demands on today’s fasteners are ever increasing Understand when to specify specific processes or equipment and these two process steps play a critical role in how well the Recognize potential failures modes fastener will perform its intended function. Gain an understanding of the benefits of different platings and coating This seminar will begin by exploring the fundamental metallurgical Understand when to specify certain plating or coating pro- transformations and principals that yield the mechanical changes cesses desired by the fastener designer or engineer. Each process will Gain insight into plating and coating performance and rela- be examined in greater detail to understand how the process tive cost to achieve these goals achieves these underlying principals and what practical effects it Explore current issues in regulation and environmental protection has on the fastener. Control points will be investigated to gain an understanding of, not only how the process remains in control, but also how it can go wrong and the consequences when it does. Concepts Covered Day two will explore platings and coatings. There are a multitude Metallurgical transitions of good options today and this seminar shall look at those favored Hardenability by large fastener consuming industries.
    [Show full text]