Development of Novel High Temperature Aluminum Alloys
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Hiduminium Technical Data
HIDUMINIUM TECHNICAL DATA HIGH DUTY ALLOYS LTD SLOUGH F oreword Extensive research carried out in recent years, com bined with an increasing demand for " H ID UM IN IUM " high tensile aluminium alloys, has necessitated the revision and increase of the series of data sheets pre viously issued by the Company. As before, our aim is to place before designers and constructors the fullest possible particulars regarding the physical and mechanical properties of " H ID U M IN IU M ," which will enable them to select the materials most suitable for their requirements and to adapt their designs in accordance with the outstanding character istics of this range of alloys. " HIDUMINIUM" is produced under conditions of strict scientific control and progressive inspection and a staff of expert Metallurgists, Research W orkers and Technicians is always ready to give advice on all problems connected with the use of these alloys. Fresh data, as it is revealed by further research, will be issued on additional sheets. This will ensure that all information contained in this volume is up-to-date and may thus be referred to at all times with complete confidence. HIGH DUTY ALLOYS LIMITED 3 CONTENTS Page Index to Specifications 6-9 Hiduminium 15 10-11 Hiduminium 23 12-13 Hiduminium 33 14-15 Hiduminium 35 16-17 H iduminium 40 & 42 18-19 Hiduminium 45 20-21 Hiduminium R.R. 50 22-23 Hiduminium R.R. 53 24-26 Hiduminium R.R. 53.C 27-29 Hiduminium R.R. 56 30-32 H iduminium R.R. 59 33-35 Hiduminium 72 36-37 Hiduminium R.R. -
Studies on Properties of Al–Sic Metal Matrix Composite Material for Making IC Engine Valves
Proceedings of the World Congress on Engineering 2018 Vol II WCE 2018, July 4-6, 2018, London, U.K. Studies on Properties of Al–SiC Metal Matrix Composite Material for Making IC Engine Valves Nilamkumar S. Patel, Ashwin D. Patel, Ritesh Kumar Ranjan, Vikas Rai Abstract-Automobile industries are using material substitution the matrix also helps to transfer load among the composite for to build lighter weight, and fuel efficient engines, offering is compound material which differs from alloy due to fact better properties materials of engine components, including that all the individual component retain its characteristic. engine poppet valves and valve seats. Valves and valve seats are very important components that are used at high operating II. EXPERIMENTAL SET-UP temperature to control the flow and volumetric efficient at desired level of engine performance. The present work Stir casting process is liquid state processing. It is simple describes that Al-SiC composite as possible alternate materials and flexible process. In this process, there is mixing of with its unique capacity to give required properties for engine matrix and reinforcement. poppet valves and valve seats. Al-SiC MMC is prepared by In this process, reinforcement particles are added into the powder metallurgy and various casting techniques. In the research a composite is developed by stir casting process by molten matrix metal. And then the proper mixture is done using aluminium alloy with silicon carbide Nano particles and by hand stirring as well as Mechanical stirring. And then substitute sintering operation at 600oC temperature for one this mixture is allowed to pour into the mould shape. -
A Review on Comparison of Aluminium Alloy LM-25 with Al/Sic
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 01 | Jan-2018 www.irjet.net p-ISSN: 2395-0072 A review on comparison of Aluminium alloy LM-25 with Al/Sic Rahul Ushir1 , Kunal Gandhi2, Gaurav Dahe3, Vijay Bidgar4, Prof. Vishal Thakre5. 1,2,3,4 BE student Mechanical, SND COE & RC, YEOLA, Maharashtra, India 5Prof. Mechanical, SND COE & RC, YEOLA, Maharashtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract- Many industries suffered a great loss of materials and procedures to decrease the wear of devices manufacturing process due to collapse of manufacturing and designing segments. These incorporate change of mass machines due to wear and fail of lubrication. Friction is main properties of the materials, surface medications and cause of wear and energy dissipation. Improving friction can utilization of covering, and so on. In the course of the most make substantial saving. It is obvious that enormous amount recent couple of years, numerous endeavors have been made of the worlds resources are used to overcome friction in the to comprehend the wear conduct of the surfaces in sliding form or another. Lubrication is an effective means of contact and the instrument, which prompts wear. The controlling wear and reducing friction. Hence, for the survival applications of aluminium and its alloys for the machine of machine wear and friction must be decreased parts are increasing day to day in the industry. However, and/controlled carefully. little has been reported on the wear behaviour of aluminium and its alloys with the addition of grain refiner and modifier. Key words: Silicon Carbide(Sic) , aluminium LM25,scanning electron microscope ( SEM ) , metal PROBLEM DEFINITION: matrix composite ( MMCs) . -
Aluminium Products Coil
Helping manufacturers across the globe achieve sustainable leaner manufacturing processes Aluminium Coil, Foil, Products Sheet & Wire Commercially Pure Aluminium Alloys Series 1000 Series 2000 Series 3000 Fast Series 4000 Series 5000 Turnaround Series 6000 Processing Series 7000 Series 8000 Clad Aluminium WIDE STOCK RANGE Low Width Thickness Ratio 3:1 unique to the industry (normal minimum is 8:1) Over 75 years Experience Knight Group Visit our websites: Main: www.knight-group.co.uk Offcuts: www.ksmdirect.co.uk www.pmdirect.be Head Office Linkside, Summit Road Cranborne Industrial Estate Potters Bar, Hertfordshire EN6 3JL United Kingdom Main Office : +44(0)1707 650251 Fax: +44(0)1707 651238 [email protected] Knight Strip Metals Ltd Sales, Processing & Warehouse Saltley Business Park Cumbria Way, Saltley Birmingham B8 1BH United Kingdom Telephone: +44 (0)121 322 8400 Fax: +44 (0)121 322 8401 Sales 08456 447 977 [email protected] Precision Metals EU Industriezone Mechelen-Noord (D) Omega Business Park Wayenborgstraat 25 2800 Mechelen Belgium Telephone: +32 (0) 15 44 89 89 Fax: +32 (0) 15 44 89 90 [email protected] The information contained herein is given in good faith and is based on our present knowledge and experience. However, no liability will be accepted by the Knight Group and its subsidiaries in respect of any action taken by any third party in reliance thereon. Any advice given by the Company to any third party is given for that party’s assistance only and without any liability on the part of the Company. The contents of this brochure are subject to change and the most recent edition of all Knight Group documentation can be found on our website or by written request. -
Maec.19 70 (University of London) London
COMPLEX & INCREMENTAL STRESS CREEP OF A HIGH STRENGTH ALUMINIUM ALLOY AT ELEVATED TEMPERATURES (ALLOY: HIDUMINIUM RR58 SPECIFICATION DTD 731) by SURINDAR BAHADUR MATHUR Thesis presented in the Department of Mechanical Engineering for the Award of the Doctor of Philosphy in Mechanical Engineering of the University of London. Mechanical Engineering Department Imperial College of Science and Technology mAec.19 70 (University of London) London. ABSTRACT A theory for creep rates under complex and incremental stresses is deduced from experimental data concerning complex creep at elevated temperatures for the test material HIDUMINIUM RR 58 - Specification DID 731. The most important results are for tubular specimens tested at 150°C and 250°C under incremental loads. The analysis of results relates to steady state creep only. Modified relationships in stress equivalence and strain equivalence are proposed to account for thermal softening, polygonization, recrystallization and the resulting exaggerated flow in the direction of the applied shear. (The original equations are based on the hypothesis of Von Mises). A further relationship is suggested between the immediate total energy of distortion and the subsequent creep work rate. Results of the static tests and the results of the tests for creep behaviour under complex loading are presented and compared with the results of static torsion and simple incremental torsion creep tests on the basis of the proposed equations. An appendix describes the complex creep testing machine, furnace, extensometers -
Review on Multi-Pass Friction Stir Processing of Aluminium Alloys
Preprints (www.preprints.org) | NOT PEER-REVIEWED | Posted: 22 July 2020 doi:10.20944/preprints202007.0514.v1 Review Review on Multi-Pass Friction Stir Processing of Aluminium Alloys Oritonda Muribwathoho1, Sipokazi Mabuwa1* and Velaphi Msomi1 1 Cape Peninsula University of Technology, Mechanical Engineering Department, Bellville, 7535, South Africa; [email protected]; [email protected] * Correspondence: [email protected]; Tel.: 27 21 953 8778 Abstract: Aluminium alloys have evolved as suitable materials for automotive and aircraft industries due to their reduced weight, excellent fatigue properties, high-strength to weight ratio, high workability/formability, and corrosion resistance. Recently, the joining of similar and dissimilar metals have achieved huge success in various sectors. The processing of soft metals like aluminium, copper, iron and nickel have been fabricated using friction stir processing. Friction stir processing (FSP) is a microstructural modifying technique that uses the same principles as the friction stir welding technique. In the majority of studies on FSP, the effect of process parameters on the microstructure was characterized after a single pass. However, multiple passes of FSP is another method to further modify the microstructure in aluminium castings. This study is aimed at reviewing the impact of multi-pass friction stir processed joints of aluminium alloys and to identify a knowledge gap. From the literature that is available on multi-pass FSP, it has been observed that the majority of the literature focused on the processing of plates than the joints. There is limited literature reporting on multi-pass friction stir processed joints. This then creates a need to study further on multi-pass friction stir processing on dissimilar aluminium alloys. -
Extruded Aluminium Profiles
Aluminium Al Product format: Extruded Technical characteristics : Flats, rods, tubes and extruded aluminium profiles www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 1050 PURE ALUMINIUM (99,5%) EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. FRANCE UNITED KINGDOM ITALY OTHERS Al-99,5 L-3051 Al-99,5 Al-99,5 A5 1B 9001/2 17010 Puraltok 99,5 3,0255 1S Durcilium T 4007 WG-1S Hiduminium A1 1150/55 Impalco 0,5 Aluran 99,5 EQUIVALENCES 1200 PURE ALUMINIUM (99 %) EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. FRANCE UNITED KINGDOM ITALY OTHERS Al 99,0 L-3001 Al 99,0 2S 1100 A-4 1C 3567 4010 Puraltok 99 3,0205 2S 1100 5090 WG-2S Birmetal 2 9001/1 17005 90 Hiduminium-1C 1008 1010 NA-2S 1191 2584 A0 Aluran 99 www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 2007 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES SPAIN GERMANY FRANCE SUIZA L-3121 DIN 1725 A U4Pb Al-CuMgPb Cobreltok 07 DIN 1746 Al-CuMgCd DIN 1747 Decotal 200 Tordal 1970 Aludur D 505 Spanal 320 MFK Aludur 570 A Automat EQUIVALENCES 2011 ALUMINIUM-COPPER COMMERCIAL EQUIVALENT SPAIN CANADA E.E.U.U. FRANCE SUIZA ITALY UNITED KINGDOM L-3192 CB 60 2011 A-U5PbBi Decotal 500 Recidal 11 28 S 28-S CSA HA,5 ASTM B 211 Fortal 2011 28 S QQ-R-225/3 QQ-R-365 WW-P-471 Ty III QQ-R-566 www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 2030 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES SPAIN GERMANY FRANCE SUIZA L-3121 Al CuMgPb A U4Pb Al-CuMgPb 3,1645 NF A 57.350 Al-CuMgCd DIN 1725 Fortal D Decotal 200 DIN 1746 Fortal 2030 Aludur D 505 DIN 1747 Carbium al Pbl MFK Tordal 1970 Duralumin DE Spanal 320 Aludur 570 A Automat EQUIVALENCES2014 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. -
The Effect of Cooling Rate on the Microstructure of A356 Aluminium Alloy
SVOA MATERIALS SCIENCE & TECHNOLOGY (ISSN: 2634-5331) Research https://sciencevolks.com/materials-science/ Volume 2 Issue 4 The Effect of Cooling Rate on the Microstructure of A356 Aluminium Alloy Maftah H. Alkathafi1*, Abdalfattah A. Khalil2, Ayad O. Abdalla3 Affiliations: 1Mechanical Engineering Department, Faculty of Engineering, Sirte University, Libya 2Materials Science Department, Faculty of Engineering, Omer Al-Mukhtar University, Libya. 3College of Mechanical Engineering Technology, Benghazi-Libya. *Corresponding author: Maftah H. Alkathafi* Mechanical Engineering Department, Faculty of Engineering, Sirte University, Libya Received: December 10, 2020 Published: December 31, 2020 Abstract: In this study a fast-cooling technology is employed for a cast iron mould to prepare cast A356 aluminium alloy by solidifica- tion of the molten metal. The cooling rate is achieved by pouring the molten alloy into a preheating permanent mould at different temperatures (25, 100, 200, 300 and 4000C) for cast samples with 40 mm inside diameter and 200 mm height. The samples considered are analyzed by optical microscopy, scanning electron microscopy (SEM), and EDS X-ray analysis (EDS). The effects of cooling rate on the morphology of α – aluminum and eutectic silicon of A356 alloy have been studied. The results showed that the dendritic structure of α-phase was broken and converted into a somewhat globular grain structure and the coarse acicular eutectic silicon trend to be broken and converted into short sticks or small rounded in other cases. Keywords: A356 Aluminum alloy, Grain refinement, Cooling rate, SEM, EDS, Microstructure. 1. Introduction Aluminium alloys have attractive physical and mechanical properties. They are lightweight, low costs production, easy to machine and have good recycling possibilities up to 95 % [1]. -
Aluminium Alloy - 6262 - T6 Extrusions
Aluminium Alloy - 6262 - T6 Extrusions SPECIFICATIONS CHEMICAL COMPOSITION Commercial 6262 BS EN 573-3:2009 Alloy 6262 EN 6262 Element % Present Magnesium (Mg) 0.80 - 1.20 Aluminium alloy 6262 is a heat treatable alloy with Copper (Cu) 0.15 - 1.40 very good corrosion resistance and strength. Additions of bismuth to the alloy mean that 6262 has excellent Silicon (Si) 0.40 - 0.80 machinability and surface finish. Lead (Pb) 0.40 - 0.70 High-speed steel or carbide tooling can be used to obtain smooth finishes. Heavy cutting requires oil Bismuth (Bi) 0.40 - 0.70 lubricant but light cutting can be done dry. Iron (Fe) 0.0 - 0.70 Alloy 6262 can be used in place of 2011 when higher corrosion resistance and better anodising response is Zinc (Zn) 0.0 - 0.25 required. Chromium (Cr) 0.04 - 0.14 Applications Titanium (Ti) 0.0 - 0.15 6262 is commonly used in the manufacture of: Manganese (Mn) 0.0 - 0.15 Screw machine products Camera parts Others (Total) 0.0 - 0.15 Nuts Other (Each) 0.0 - 0.05 Couplings Aluminium (Al) Balance Marine fittings Decorative hardware and appliance fittings Hinge pins Oil line fittings ALLOY DESIGNATIONS Valves and valve parts Aluminium alloy 6262 also corresponds to the following standard designations and specifications but may not PLEASE NOTE: Due to European Environmental be a direct equivalent: Protection Directives: AA6262 # 2000/53/CE-ELV – For the automotive sector Al 1.0Mg 0.6Si Pb # 2002/95/CE-RoHS – For the electrical and A96262 electronics sector This alloy has been replaced by Alloy 6026 which has a PLEASE NOTE: Due to European Environmental lower Lead content. -
Fatigue Behavior of 2618-T851 Aluminum Alloy Under Uniaxial and Multiaxial Loadings
Open Archive Toulouse Archive Ouverte (OATAO) OATAO is an open access repository that collects the wor of some Toulouse researchers and ma es it freely available over the web where possible. This is an author's version published in: https://oatao.univ-toulouse.fr/24572 Official URL : https://doi.org/10.1016/j.ijfatigue.2019.105322 To cite this version : BenaÕssa, Malek and Mabru, Catherine and Chaussumier, Michel Fatigue behavior of 2618-T851 aluminum alloy under uniaxial and multiaxial loadings. (2020) International Journal of Fatigue, 131 (105322). 1-9. ISSN 0142-1123 Any correspondence concerning this service should be sent to the repository administrator: [email protected] Fatigue behavior of 2618-T851 aluminum alloy under uniaxial and multiaxial loadings ⁎ Benaïssa Malek, Catherine Mabru, Michel Chaussumier Université de Toulouse, Institut Clément Ader (ICA), UMR CNRS 5312, UPS/INSA/ISAE/ Mines Albi, 3 Rue Caroline Aigle, 31400 Toulouse, France ABSTRACT Keywords: AA2618 aeronautical aluminum alloy has been largely used in the past, especially in well-known Concorde AA2618-T851 aircraft, developed during sixties decade. In more recent aircraft, this alloy has been largely replaced by others Multiaxial fatigue such as 7075 which present greater fatigue resistance. Forgotten for a time, AA2618 comes back in new aircrafts Roughness for structural parts submitted to fatigue loading at high temperature because of only a slight decrease of fatigue Crossland criterion resistance of this alloy compared to room temperature fatigue resistance. In this paper, a complete fatigue characterization of 2618-T851 aluminum alloy is presented: fatigue tests under uniaxial tensile or torsion cyclic loadings, with mean tensile or shear stress have been realized; fatigue tests under combined tensile-torsion, in or out-of-phase have also been conducted as well as some combined tensile-torsion-internal pressure fatigue tests. -
Tribological Behavior and Hardness Properties of Heat Treated Al 7075-Beryl-Graphene Hybrid Metal Matrix Composites
International Journal of Recent Technology and Engineering (IJRTE) ISSN: 2277-3878, Volume-8 Issue-3, September 2019 Tribological Behavior and Hardness Properties of Heat Treated Al 7075-Beryl-Graphene Hybrid Metal Matrix Composites Shanawaz Patil, Mohamed Haneef mirror frames, house members, serving trays and cooking Abstract— The emerging technologies and trends of the utensils. Even in the field of engineering applications, the present generation require downsizing the unwieldy structures to aluminum and its alloys plays vigorous role as an aerospace, lightweight structures. Aluminum matrix composites are tailored space, and automotive components material of increasing candidate materials for aerospace applications due to their outstanding greater strength to weight ratio and low wear rate. In value because of its properties which includes diverse range this study, Al7075 alloy-Beryl-Graphene hybrid composites are of uses are appearance, lightweight and has a low density of developed by using stir casting process. Graphene weight range 2.7 to 2.8 gm/cm3 which is almost one-third of steel percentage was varied from 0 wt. % to 2 wt. % in steps of 0.5 wt. %. (7.83 gmcm3)[-,5]. One of the foremost usually used metal Whereas for Beryl 6 wt. % is used thorough out the study. The alloy for structural application is Al7075 due to its enticing casted specimens were heat-treated at T6 solutionizing wide-ranging properties like low density, improved strength, temperature of 530±5oC for 8 hours. After the heat treatment the specimen are quenched in boiling Water and Ice. The ductility, toughness, and resistance to fatigue. Al7075 alloy microstructure of the newly developed hybrid MMCs has been has been extensively used in aircraft structure elements and investigated by TEM and SEM. -
Abstracts from the Scientific and Technical Press Titles And
December, ig4j Abstracts from the Scientific and Technical Press " (No. 117. October, 1943) AND Titles and References of Articles and Papers Selected from Publications (Reviewed by R.T.P.3) TOGETHER WITH List of Selected Translations (No. 63)' London : "THE ROYAL AERONAUTICAL SOCIETY" with which is incorporated "The Institution of Aeronautical Engineers" 4, Hamilton Place, W.I Telephone: Grosvenor 3515 (3 lines) ABSTRACTS FROM THE SCIENTIFIC AND TECHNICAL PRESS. Issued by the Directorate's of Scientific Research and Technical Development, Ministry of Air craft Production. (Prepared by R.T.P.3.) No. 117. OCTOBER, 1943. Notices and abstracts from the Scientific and Technical Press are prepared primarily for_ the information of Scientific and Technical Staffs. Particular attention is paid to the work carried out in foreign countries, on the assumption that the more accessible British work (for example that published by the Aeronautical Research Committee^ is already known to these Staffs. Requests from scientific and technical staffs for further information of transla tions should be addressed to R.T,P.3, Ministry of Aircraft Production, and not to the Royal Aeronautical Society. Only a limited number of the articles quoted from foreign journals are trans lated and usually only the original can be supplied on loan. If, however, translation is required, application should be made in writing to R.T.P.3, the requests being considered in accordance with existing facilities. ' NOTE.—As far as possible, the country of origin quoted in the items refers to the original source. The Effect of Nitrogen on the Properties of Certain Austenitic Valve Steels.