Duralumin By Group 2.

Slides:



Advertisements
Similar presentations
Metals All metals belong to one of these two groups.
Advertisements

Coat Hook Revision Notes
Aluminium A large Aluminium billet from which wrought products will be produced.
Duralumin By Group 2.
Characteristics of Metals AG 221 – Metals and Welding.
Bulk Deformation Processes in metal forming Chapter 19 Part 4- Wire and Bar Drawing Manufacturing Processes, MET1311 Dr Simin Nasseri Southern Polytechnic.
Bachelor of Technology Mechanical
Annealing Processes All the structural changes obtained by hardening and tempering may be eliminated by annealing. to relieve stresses to increase softness,
VMA - vehicle assembly and manufacturing The Energy Cost of Making an Automobile Presentation in 2015 FGS (Weizmann Inst.) Guided Reading Course Energy.
Application of ultrasonic excitation to metal forming processes M. Rosochowska Manufacturing Engineering Research Group.
Romina Javadianfard Period: 3. Alloys Alloy is a solid combination of atoms of two or more metals. Alloy is a solid combination of atoms of two or more.
Metal Alloys Manufacturing Processes © 2013 Su-Jin Kim, GNU Nonferrous Alloys ( 비철금속 ) More expensive than ferrous metals. Applications: aluminium for.
Physical Metallurgy Design alloys for aircraft engine.
DURALUMIN 7G GROUP2 BRIAN GO WILLIAM CO SEAN BRAGANZA GRANT TAN MATTHEW ANG.
Metals GROUP 2.
Sheet metal processing
B. Titanium-based Alloys Titanium is hcp at room temperature – and transform to the bcc structure on heating to 883 o C. Alloying elements are added to.
Metals All metals belong to one of these two groups. Ferrous metals are metals, which are mainly made of iron with small amounts of other metals or elements.
Traditional Manufacturing Processes Casting Forming Sheet metal processing Cutting Joining Powder- and Ceramics Processing Plastics processing Surface.
Heat treatments Produced by Neil Liggett
UNIT III Bulk Deformation Process. Bulk Deformation Processes Characterized by significant deformations and massive shape changes "Bulk" refers to workparts.
TOPIC : NON-FERROUS METALS AND ALLOYS. GROUP MEMBERS : 1) : Bhoya sandip k. 2) : Chaudhari ankit z. 3) : Gamit.
Aluminum Alloy 6061 – Composition, Properties, Temper and Applications of 6061 Aluminum.
Subject: Design of Machine Elements Presentation On ALLOYING ELEMNTS ADDED TO STEEL AND EFFECTS Mechanical: 5 th B-2 Prepared by: Guided by: 1. Mohak Maniar
Brake Booster. INTRODUCTION  In Automobile Vehicles, Brake Boosters are used only on power brakes, not Manual Brakes.  The Booster’s Function is to.
Metals Unit 212/255 – Principles of Fabrication and Welding Technology.
Bulk deformation Processes II
Dr. Owen Clarkin School of Mechanical & Manufacturing Engineering Summary of Material Science Chapter 1: Science of Materials Chapter 2: Properties of.
Nonferrous Metals & Alloys. Nonferrous Metals Ferrous Alloys – alloys contain iron Nonferrous Metals – metals do not contain iron such as Copper (Cu),
Materials Engineering
Numbering Systems for Alloys
Basic Aircraft Structure
Unit 13: Non-ferrous metals Dr
Metals All metals belong to one of these two groups.
Characteristics of Metals
Alloys and Its Application
PROPERTIES OF Al6063 BY USING EQUAL CHANNEL ANGULAR PRESSING PROCESS
Identification terminology various aircraft hardware
Chapter 13: Non-ferrous metals
NON – FERROUS ALLOYS.
Titanium 6AL-4V in Aircraft
Types of Bronze alloys Super Metal Industries
BEARING MATERIALS.
Noteworthy advantages of using aluminum alloys
INTERMETALLIC COMPOUNDS.
Metals All metals belong to one of these two groups.
Aerospace System Prototyping and Validation- Lecture 2
Forging of Metals.
Friction Welding Welding Technology/ 3.5 Friction Welding.
7G GROUP2 BRIAN GO WILLIAM CO SEAN BRAGANZA GRANT TAN MATTHEW ANG
Forging Aluminum for Aerospace Pressure Vessels
BTE 1013 ENGINEERING SCIENCEs
Manufacturing Processes
Metals All metals belong to one of these two groups.
Building Materials Metals.
PLASTIC FORMING PROCRSSES
Aluminium &Aluminium Alloys Properties: (i)It is ductile and malleable due to FCC structure. (ii)It is light in weight (iii)It has very good thermal and.
Heat treatment of steel
Status of the PANDA Solenoid Magnet Production in BINP
by Norman E. Dowling. ISBN
Modern Automotive Technology PowerPoint for by Russell Krick
Chapter 7 Ionic and Metallic Bonding 7.3 Bonding in Metals 7.1 Ions
Basic Aircraft Structure
7G GROUP2 BRIAN GO WILLIAM CO SEAN BRAGANZA GRANT TAN MATTHEW ANG
Metals There are two categories of metal Ferrous & Non Ferrous
METALLIC STRUCTURAL MATERIALS
CHAPTER 9 Engineering Alloys 1.
HEAT TREATMENT OF NON-FERROUS METALS AND ALLOYS BY JITENDRA.
Chapter 6: Mechanical Properties of Metals
Mechanical Properties of Metals - I
Presentation transcript:

Duralumin By Group 2

History of Duralumin Duralumin was developed by the German metallurgist Alfred Wilm at Dürener Metallwerke Aktien Gesellschaft. In 1903, Wilm discovered that after quenching, an aluminium alloy containing 4% copper would slowly harden when left at room temperature for several days. Further improvements led to the introduction of duralumin in 1909. The name is obsolete today, and mainly used in popular science to describe the Al-Cu alloy system, or 2000 series as designated by the International Alloy Designation System (IADS) originally created in 1970 by the Aluminum Association.

Duralumin It is strong and hard. It is an alloy of aluminum that is 4 percent copper and contains small amounts of magnesium, manganese, and copper: used for applications requiring lightness and strength.

It is used for...... making aircraft frames making the frames of automobiles and speedboats making household articles

Future uses * 2011: Wire, rod, and bar for screw machine products. Applications where good machinability and good strength are required. * 2014: Heavy-duty forgings, plate, and extrusions for aircraft fittings, wheels, and major structural components, space booster tankage and structure, truck frame and suspension components. Applications requiring high strength and hardness including service at elevated temperatures.

* 2024: Aircraft structures, rivets, hardware, truck wheels, screw machine products, and other miscellaneous structural applications. The first age-hardened alloy ever discovered. * 2036: Sheet for auto body panels. * 2048: Sheet and plate in structural components for aerospace application and military equipment. * 2141: Plate in thicknesses of 40 to 150 mm (1.5 to 6.0 in.) for aircraft structures. * 2218: Forgings; aircraft and diesel engine pistons; aircraft engine cylind

Sources http://www.britannica.com/EBchecked/topic/1741 06/duralumin http://wiki.answers.com/Q/What_are_the_possibl e_uses_of_duralumin