Showing posts with label Materials. Show all posts
Showing posts with label Materials. Show all posts

Tuesday, July 30, 2019

ISI Standards for Sheets, Plates and Bars - India




 The generally accepted meanings for  the terms, foil, sheet, strip and plate are as follows: 

Foil is sheet metal of varying widths having thickness not exceeding 1.6 mm. 

Strip is a metal rolled in any thickness between 1.6 mm and 10 mm and its widths vary from 100 mm to 1,550 mm. It is designated with letters ISST followed by the dimensions in mm in order of length, width and thickness. 

Sheet is a term used for metals having thickness lying between 0.4 mm to 4 mm and having a 
width varying from 1,800 mm to 4,000 mm. It is designated by letter ISSH followed by the dimensions in mm in order of length, width and thickness. 

Plates denote all widths of metals where the minimum thickness exceeds 5 mm and maximum upto 63 mm and all widths of metal and length varying from 2,200 mm to 13,500 mm. It is designated by letters ISPL followed by dimension in mm in order of length, width and thickness. 

18:1138-1958 gives sizes of metal strips, sheets, flats, plates, and bars round and square. Here the nominal sizes are given as well as the tolerances in the sizes kept in their manufacture are also specified. 

18:1731-1961 gives dimensions for steel flats, and their tolerances for structural and general engineering purposes while 18:1732-1961 gives dimensions for round and square steel bars for 
structural and general engineering purposes. 

Dimensions for steel plates, sheets and strips for structural and general engineering purposes are given in 18:1730-1961. The following 18 specifications also give the sizes of different structural 
sections made of steels for general purposes of engineering: 

18:808-1957 specification for rolled steel beams, channels and angle sections 

18 : 1173-1957 specification for rolled steel beams, channels and angle sections and for bars 

18:1250-1958 Specification for rolled steel beams, channels and angle sections, and bulb angles 

18:1863-1963 Dimensions for rolled steel bulb plates. 

All these structural steel sections are given combined in ISI standard handbook for structural engineers. 

18:6911-1972 gives dimensions of stainless steel plates, sheets and strips 

18:1079-1973 gives dimensions of hot rolled, carbon steel sheets and strip 

18:6527-1972 gives dimensions of stainless steel wire rods 

18:6528-1972 gives dimensions of stainless steel wire 

18:6529-1972 gives dimensions of stainless blooms, billets and slabs for forgings. 

18:6603-1973 gives dimensions of stainless steel bars and flats 



All sizes given in IS standards are not manufactured by companies. Only those sizes which are in large and continuous demand are made normally by them. So design engineers should refer to manufacturers' catalogues for the available sizes.

Saturday, July 27, 2019

Machine Element Materials - Fabrication Characteristics - Design for Manufacturability



Fabrication Characteristics and Processes of Fabrication - Materials Suited for Specific Fabrication Processes


The fabrication characteristics of metals are explained under the heads:  formability, castability,  machinability and weldability.

(a) Formability:


The ability of a metal to be formed is based on ductility of the metal. Ductility is based on its crystal structures. The metal that has the face centred cubic crystal structure is most ductile because the crystal has the greatest opportunity for slip in four distinct nonparallel planes and three directions of slip in each plane.

The other factors which control ductility of the material are grain size, alloying elements and softening heat treatments such as annealing and normalizing. The small grain sizes are recommended for shallow drawing of copper and relatively large grains for heavy drawing on the thicker gauges.

Hot and cold working, also have an effect on ductility. The high pressure applied in hot drawing distorts the grains which determine the ductility; cold working also results in distortion of crystals. Generally, cold worked crystals are more distorted and are usually less ductile than the hot worked crystals.

Alloying elements in a pure metal normally reduce its ductility, because if they replace the atoms of pure metal it reduces the number of slip planes as it occurs in steel, which is an alloy of carbon and iron and so steel is less ductile than iron. If the alloy finds its room in the spaces between the atoms of pure metal it offers increased resistance to slip, which happens in steel when iron carbide precipitates in slip planes when steel solidifies. By softening heat treatment such as annealing which consists of heating the metal to the re-crystallisation temperature at which at first the grains may be very small but they grow in size as long as the metal is exposed to the high temperature, when the desired size is obtained the metal is allowed to cool. During recrystallization ductility of metal is
restored because distorted crystals are reformed in re-crystallisation.

The processes using the property of formability of metal are under two major categories: (i) Hot working and (ii) Cold working.

Hot working processes:

Rolling, forging, extrusion and hot pressing are hot working processes. In hot working the metal is heated sufficiently to make it plastic and easily worked. The temperature of the heated metal or alloy should be above the re-crystallisation temperature. This temperature is different for different metals.

Hot rolling is used to create a bar of material of particular shape and dimensions. The principal rolled steel sections arc plates, angles, tees, channels and joists; round, hexagonal and square bars for forging and machining operations; sheets, rails, etc. All of them are available in many different sizes and in different materials. The materials most available in the hot rolled bar sizes are steel, aluminium and copper alloys. Tubes may be manufactured by hot rolling of strips or plates; the product may be butt welded or lap welded.

Forging is the hot working of metals by hammers, presses or forging machines. For small work forging is carried out with hand hammers but for large work hammers and forging machines are used. Forging alters the internal structure of metals which results in increased strength and ductility. Compared with castings, forgings have greater strength for the same weight. Forging should be
carried out within proper temperature range. If the temperature is too high the metal will be weak and brittle. If the temperature is too low, there will be internal stresses which may lead to distortion or cracking.

Many small parts are drop forged. In drop forging, solid lump with little or no previous treatment by hand is squeezed between dies to the shape required with one or more blows from a drop hammer. The component can be made to dimensions and with a good surface so that machining may be unnecessary. The limitations of this process are that the number of parts should be great (production volume has to be high) and complicated shapes cannot be produced as they can not be removed from dies.

Extrusion is a process where a heated blank is caused to flow through a restricted orifice under great pressure. Very complicated shapes may be produced by the extrusion process. The process is restricted to materials of low melting points such as brass, aluminium and certain alloys of tin, lead and other soft metals.

Hot pressing consists of forming metal to shape in a very rigid type of power press. A hot piece of metal is pressed and extruded in suitable dies into a smoothly finished piece to accurate dimensions. Automobile valves are formed by this process. 

Cold working processes:

In cold working is the forming of a metal is done usually at room temperature. In some cases, higher  temperatures are used but always, the temperature is lower than re-crystallisation temperature of the material. Cold working may vary from a simple bend to great deformation produced by deep pressing and tube drawing. The result of cold work is to increase hardness and tensile strength but to decrease ductility and shock resistance. Cold worked parts have a bright new finish, are more accurate and require less machining. Where cold work is considerable, the part may be annealed at some intermediate stage or stages of work. In cold working the surface of a material is very important as scale may be worked into the finished article with serious results. Some of cold working processes are drawing, heading, spinning, stamping, etc.

Drawing is a process by which the cross section of a metal is diminished by pulling it through an accurately formed hole in a drawing die. The operation is performed cold and only simpler forms can be produced without excessive resistance and tearing.

Heading is a cold working process in which the metal is gathered or upset . This  operation is commonly used to make screw and rivet heads. The blank is usually a piece of wire of suitable length and cross section; one end is cold forged in dies to form the desired shape of the head. Annealing may be required after cold heading.

Spinning is the operation of working sheet material around a rotating form into a circular shape. Pressure is applied to the sheet by means of a blunt nosed tool which presses it against the former. This is an economical method of forming parts if the quantities are small.

Stamping is the term used to describe punch press operations such as blanking, coining, forming and shallow drawing.

Powder metallurgy :

It is the art of making small components by heat treatment of compressed metallic powders, sometimes with inclusion of non-metallic material.

The powdered metals in desired proportions are compressed in moulds under a very high pressure varying from 700 to 14,000 kg/sq cm depending on the metal. The compacted part is heated at a temperature which is less than melting point of the major ingredient. T'he disadvantages of this method are (i) low strength of the component (ii) higher cost of material and (iii) the limited range of materials which can be used.

Filaments of refractory metals such as tungsten, self lubricating bearings, tungsten carbide tips for cutting tools and iron alloys for permanent magnets are examples of articles made from powdered metal. By this process small components can be made out of some metals whose melting point is too high to allow use of die casting.

(b) Castability:


Castability of a metal is judged to a large extent on the following factors: solidification rate, shrinkage, segregation, gas porosity, and hot strength.

Solidification Rate:

The ease at which a metal will continue (o flow after it has been poured in the mold depends on its analysis and pouring temperature. Some metals such as grey iron are very fluid and can be poured into thin sections of complex castings.

Shrinkage :

Shrinkage refers to the reduction in volume of a metal when it goes from a molten to a solid state. For steel, the amount of contraction amounts to about 6.9 to 7.4% by volume, or 2 cm per metre; grey  iron contracts half as much. This shrinkage factor has to be taken into account by the pattern maker and designer, not only to allow for the proper finished .size, but also to sec that undue strains will not be encountered during shrinkage due to the mould design. Various elements can be added to the alloy to control fluidity and shrinkage as discussed later in this chapter.

Segregation :

As the metal starts to solidify tiny crystal structures resembling pine trees and referred to as dendrites start to form at the mold edges. As they form, they tend to exclude alloying elements. Subsequent crystals that form are progressively richer in alloy content as the metal solidifies. Thus the surface of the casting is not of the same quality as that in the centre. This is overcome in part at least by subsequent heat treatment, or very slow cooling.

Gas Porosity:

Some metals in the molten state have a high affinity for oxygen and nitrogen. These gases become trapped as the metal solidifies creating voids or pinholes.

Hot Strength:

Metals are very low in strength right after solidification. This is especially true of the non-ferrous metals. Precautions must b(‘ taken at the lime of casting to avoid stress concentration that causes flaws and hot tears to develop as the metal solidifies .

Casting is the oldest form of metal shaping and is still the basic engineering process since most metals are melted and cast from ores. Castings are made of iron, steel, various brasses and bronzes, aluminium and its alloys and the various white metal alloys.

Patterns may be made of wood or metal and with its help the sand mould is formed in which molten metal is poured. The mould is dried before the metal is poured. Metal in cooling solidifies to the form outlined in the mould.

In die casting process the mould is usually made of steel and molten metal is poured or forced under pressure into the mould. This method is used for mass production only.

Non-ferrous alloys arc sometimes cast centrifugally. Molten metal is poured into a rapidly rotating cylindrical mould and is held against the mould by centrifugal force so that core is not required. On cooling the casting is complete. Such castings are generally denser and more homogeneous than ordinary sand castings. This process is limited to simple shapes and to fairly large quantities.

The following precautions should be observed in design of castings :

(i) All sections should be designed as far as possible with a uniform thickness.

(ii) All walls should be sufficiently thick to allow the molten metal to flow freely into all corners.

(iii) Adjoining sections should be designed with generous fillets or radii.

(iv) Parts should be designed so that patterns may be drawn readily from the moulds.

(v) A complicated part should be designed in two or more castings. These castings are assembled by fasteners.

(vi) Where the section uniformity is not possible, light sections should be blended into heavy sections.

Thickness of casting determined by calculations is often too small to permit production of good castings. Minimum values of the thicknesses for various castings are prescribed.


Material                                 Minimum thickness in mm


Grey cast iron                                    6

Malleable cast iron                           6

Steel casting                                     6

Brass                                                3

Bronze                                             3

Aluminium                                      3






(c) Machinability :


Machinability is the ease with which metal can be removed in operations such as turning, drilling, reaming, etc. Ease of metal removal requires that the forces acting against the cutting tools should be relatively low and the chips will be broken up, a good finish should result and the tools should last a reasonable period of time before it has to be replaced or resharpened. Machinability is also expressed as a machinability rating for each material. 

This rating is given for most ferrous metals using steels 13S25  in the cold drawn conditions as the basis of 100% machinability. This value involves turning at a cutting speed of 54.9 surface metre per minute for feeds upto 0.1778 mm per revolution and depths cut upto 6.35 mm using appropriate cutting fluid with high speed steel T70W18Cr4V1 tools. Machinability of other metals will be judged with respect to this basis.

This property plays a predominant role in deciding the selection of material for components manufactured using  machining on automatic machine for mass production. By adding alloying materials like sulphur and lead in steel its machinability can be increased, however, some reduction in tensile strength in takes place.

(d) Weldability:


It may be said that all metals are weldable by one process or another. However, the real criterion in deciding on the weldability of a metal is weld quality and the ease with which it can be obtained.

In deciding on weldability of a metal, the characteristics commonly considered are the heating and cooling effects on the metal, oxidation, and gas vaporization and solubility.

Heat and Cooling:

The effect of heat in determining the weldability of a material is related to the change in microstructure that results. For example, steels are sometimes considered weldable or not weldable on the basis of the hardness of the weld. The deposited weld metal may pick up carbon or other alloys and impurities from the parent metal that make it hard and brittle so that cracks result upon cooling.

The opposite effect may also be considered. A metal may have a certain hardness temper that will be changed by the heat of the weld. Although both of these conditions can be corrected by added precautions and heat treatment, they add to the cost and hinder the simplicity of the weld.

Hot shortness, a characteristic which is indicated by lack of strength at high temperature, may result in weld failures during cooling of certain metals.

Oxidation :

Oxidation of the base metal, particularly at elevated temperatures, is an important factor in rating weldability of a metal. Metals that oxidize rapidly, such as aluminium, interfere with the welding process. The oxide has a higher melting point than the base metal, thus preventing the metal from flowing. It also may become entrapped in the weld metal, resulting in porosity, reduced strength, and brittleness

Gas:

Large volumes of troublesome gases may be formed in the welding of some metals. These gases may become trapped in the weld because certain elements vaporize at temperatures below those needed for welding. Not only will this cause porosity, but some of the beneficial effects of these elements are lost.

Mechanical Properties of Materials Used in Machine Elements


Mechanical properties of materials 


The proper and efficient use (value engineering) of materials in machine elements requires considerable knowledge of their mechanical properties. The mechanical properties describe the behaviour of the material under use as a machine element in machine.  

The most important mechanical properties are creep,  ductility,  elasticity, hardness, machinability. malleability, resilience, stiffness, strength, and  toughness.

Strength


Strength is the ability of the material to resist stress without failure.  The measure of the strength is the ultimate stress. Ultimate strength refers to the force needed to fracture the material.

When materials are subjected to a pulling force (tensile force) they stretch as the stress increases. The stress-strain relationship can be graphed,  when test specimen is subjected to tensile load. The diagram is a graph between stress and % elongation. With the help of this diagram different-strengths of material can be defined.

When material is subjected to a pulling force the point where the stretch suddenly increases is known as the yield strength. In many design problems when the yield strength of materials is passed it is considered unsafe for further service. When mild steel is subjected to a pulling force it indicates a distinct point where the stretch suddenly increases. This is known as yield point. Some materials like high nickel alloys, monel metal and other similar non-ferrous materials do not show a definite break in the stress strain curve. In this case it is difficult to assign yield point for them. For such materials yield strength of material is defined at the point where 0.5% elongation takes place.

Proportional limit is the maximum stress under which a material will maintain a perfectly uniform rate of strain to stress. However, it is difficult to measure the exact proportional limit.

The maximum stress from which a material can recover is called the elastic limit. It is difficult to specify the elastic limit and so the idea of proof stress has been developed.

Proof stress is the maximum stress a material can withstand without taking more than small amount of set. The amount is usually specified as the smallest that can be measured by an extensometer.

The proportional limit is yield strength at 0.00% offset in the stress-strain relationship graph. Proof stress is yield strength at 0.01% offset and yield strength is yield strength at 0.2% offset on stress elongation curve under tensile load.

Several materials such as structural steel, copper, aluminium, etc. have equal strength in tension or compression, but their strength in shear is about two-thirds of the strength in tension while in grey cast iron the strength in tension and shear is a fraction of the strength in compression.

Shear strength is the force per unit area produced to fracture a specimen when it is impressed along the cross section of material. The material may be subjected to single shear or double shear. The shear strength of steels compared to their ultimate tensile strength ranges from about 50 to 80 per cent, the lower values for the harder materials.

Elasticity


Elasticity is the property of regaining original shape after deformation. All materials used in machine elements and structures (construction) are elastic but the degree of elasticity varies with different materials. This property is exceedingly important in precision tools and machines. Steel is highly elastic material.

Plasticity is the property that enables the formation of permanent deformation in a material. Stiffness is the property by virtue of which a material can resist deformation. Measure of stiffness is the modulus of elasticity. This property is desirable in materials used in machines, columns, beams and machine tools.

Ductility


Ductility is the property of material that enables it to be drawn out or elongated to an appreciable extent (subject to tensile force) before rupture occurs. The percentage elongation and the percentage of reduction of area before rupture of a test specimen are measures of ductility of the material.

Percentage elongation depends on gauge length and so gauge length is required to be stated when percentage elongation is given. Indian Standard Institution recommends gauge length of  5.65 SQRT( A) where A is the cross sectional area of the test specimen.

Brittleness is opposite to ductility. It shows lack of ductility. Brittle materials show little deformation before rupturing.

Materials with more than 15% elongation are usually considered ductile. Those with less than 5% elongation are considered brittle. Those between 5 and 15% elongation are of intermediate ductility. Property of ductility is desirable in machine parts which may be subjected to sudden and severe loads.

Mild steel, wrought iron, copper and aluminium are ductile materials. Cast iron is a brittle material. 

For a variety of engineering uses a material requires good combination of strength and ductility. Usually if two materials having the same strength and hardness the one that has the higher ductility is more desirable in engineering practice.

Malleability


Malleability is the property of a material that enables it to undergo great change in shape under compressive stress without rupture.Malleable materials may be hammered or rolled into any desired shape without rupture. 

Soft steel, wrought iron, copper and aluminium are malleable metals.

Hardness 


Hardness is that property of a material that enables it to resist penetration, indentation, abrasion or plastic deformation. 

In selecting a metal to withstand wear or erosion, mainly three properties are considered: ductility, toughness and hardness. However, the most important from wear resistance point is hardness Wear, which  may be either due to friction or erosion by steam, oil, and water  is resisted by materials having higher hardness. This property is decreased by heating.

Several methods have been developed for hardness testing. Those most often used are Brinell, Rockwell, Vickers, and Scleroscope. The first three are based on indentation tests and the fourth
on the rebound height of a diamond-tipped metallic hammer.

In order to relate one method of testing hardness with another, hardness conversion charts are available. 

Tensile strengths are often listed on hardness conversion charts. Although relationships exist between hardness, and tensile strength and yield strength, but there are chances for error. Therefore, use of tensile testing machine is preferred to determine strength.

Resilience


Resilience is that property of a material which enables it to store energy and resist shock and impact. The measure of resilience is the amount of energy that can be stored per unit volume after being stressed to elastic limit. This property is desirable in materials for springs.

Toughness


Toughness is the property which enables a material to be twisted, bent or stretched under a sudden impact or under a high stress before rupture. It is measured by the Izod test or Charpey test. The measure of toughness is the amount of energy that a unit volume of material has absorbed after being stressed up to the point of fracture. This property is decreased by heating.



Creep


Creep is expressed as the plastic behaviour of the metals or plastics under constant load and at constant temperature.Creep is observed as the material deforms slowly but progressively over a period of time under the same load and temperature. There are three stages of creep. In the first stage the material elongates rapidly but at a decreasing rate. In the second stage which is ordinarily of long duration the rate of elongation is constant. In the third stage the rate of elongation increases rapidly until the material fails.

Design engineers are  most concerned with second stage of creep, where elongation takes place at a constant specific rate. The percentage of elongation and time required are decided by the requirements of the particular application, viz, 0.1 per cent elongation in 10,000 hours. In rapidly rotating structural members such as rotors and blades of of steam and gas turbines, the clearances are extremely small and critical. The designer will be satisfied with nothing short of experimentally determined stress of 1 creep rate unit (CRU) or 1 per cent in 100,000 hours.


Determination of mechanical properties:


In order to determine the mechanical properties of the material,  tests are carried out in mechanical testing laboratories. These tests are carried out according to standard procedures laid down.  The simplest test that can be made on most materials is the static tensile test. The procedure to carry out this test is suggested by Indian Standards Institution. The values for the following properties are obtained from the test:

(i) Ultimate tensile strength

(ii) Proportional limit

(iii) Elastic limit or Proof Stress

(iv) Yield point or Yield strength

(v) Percentage elongation

(vi) Percentage reduction in area.


IS 1608 — 1960 is to be adhered to while carrying out the static tensile test.

Other tests commonly employed are compression, torsion, flexure, cold bending, hardness, impact and fatigue. Data of these various tests are usually shown graphically by the stress strain diagrams. 

Thursday, July 25, 2019

Steels


Steel is an alloy of iron and carbon and there are various steels with popular names with carbon content varying from 0.05% to 1.7%. Steels having only carbon as the additional element apart from iron are called plain carbon steels.

Steel is produced by oxidizing the impurities in molten pig iron and then adding the specified carbon which will give required combination of strength, ductility and hardness.

The processes used to produce steel are a) open hearth process b) the Bessemer Process and c) the electric furnace process. The finished molten steel is to poured into ingots in sizes suitable for used by rolling mills.

According to the World Steel Association, there are over 3,500 different grades of steel, encompassing unique physical, chemical, and environmental properties.

Dead Mild Steel

Dead mild steel contains carbon up to 0.1%. It is the softest and the most ductile material and possesses excellent machinability and weldability.  It is rolled into sheet and is also available in bar form. It is used for rivets and solid drawn steel tubes.




Steel Grades and Properties
What Are the Different Types of Steel?
January 27, 2019
https://www.thebalance.com/steel-grades-2340174

Pressure Vessel Steels - Tool Steel - Corrosion Resistant Steel - High Tensile Steel - Quenched and Tempered Steel - Abrasion / Wear Resistant Steel - Chrome Molybdenum Steel
http://www.shahalloys.com/alloy-special-steels-grade-spec.htm

Carbon content, steel classifications, and alloy steels
https://www.thefabricator.com/article/metalsmaterials/carbon-content-steel-classifications-and-alloy-steels

Tuesday, March 28, 2017

Magnesium and Its Alloys - Increasing Use in Products




Magnesium (Mg)  is  an  alkaline  earth  metal  having  atomic  number 12  with oxidation  number +2.

Density at 20°C (g/cm3) Magnesum 1.74 Aluminium  2.70 Iron 7.86


The cost of magnesium has been decreasing below the cost of the  aluminium since 2004. M
agnesium  melting  cost  is  2/3  compared  to  aluminium. In terms of productivity, magnesium provides    25%  higher  casting  productivity  compared  to  aluminium  pressure  die  casting,  300-  500% compared  to  aluminium  permanent  mold  casting,  and  200%  compared  to  polymer  injection molding.

Magnesium is considered to be a good choice material in the areas of defense and aerospace engineering for aircraft and missile components,  aircraft engine mounts,  control  hinges,  fuel  tanks,  wings.  In  automotive  sector  magnesium  is  used  for  wheels, housings, transmission cases, engine blocks, steering wheels and columns, seat  frames,  electronic goods  like  laptops,  televisions,  cell  phones  and  in  many  more  areas  (http://www.intlmag.org/).



ASTM  (American Society for Testing and Materials)  names the Magnesium alloys with two letters
defining  the  elements,  with  numbers  denoting  the  percentage  and  an  additional  digit  to indicate intermediate properties.


An ASTM code for magnesium’s alloying elements

Letter  Alloying Element     Letter  Alloying Element
A  Aluminum                      L  Lithium
B  Bismuth                         M  Manganese
C  Copper                           N  Nickel
D  Cadmium                       P  Lead
E  Rare Earths                    Q  Silver
F  Iron                                 R  Chromium
H  Thorium                         S  Silicon
Z  Zinc

For example, AZ 91 Mg alloy contain  aluminum  (Al) and  zinc (Zn) in 9%, 1% respectively in total and the rest by pure magnesium.

Source:
Magnesium and Its Alloys in Automotive Applications – A Review
D. Sameer Kumar, C. Tara Sasanka, K. Ravindra, K.N.S. Suman
American Journal of Materials Science and Technology
(2015) Vol. 4 No. 1 pp. 12-30


2017

Interviewed engineering graduates for four days during 28 to 31 March 2017. They do not know the usage of magnesium in mechanical engineering product components.


2016

Global demand for magnesium metal will reach 1,085 KT in 2016, representing market value worth US$ 3.13 Bn.
Magnesium’s applications in making automotive wheels, transmission cases, and engine blocks will continue to fuel demand in 2016 and beyond.
Application-wise, magnesium alloys and die-casting will continue to remain the largest segments, accounting for 349 KT and 302 KT respectively in 2016.
Magnesium will continue to witness stable demand from the aerospace sector, owing to its excellent properties as a reductant in manufacturing titanium.
The global magnesium metal market is anticipated to increase at a CAGR of 7.1% during 2016-2026, reaching 6.2 Bn in revenues by 2026.
http://www.futuremarketinsights.com/press-release/magnesium-metal-market

The automotive and transportation industries is one of the largest end-users for magnesium die-cast components such as assemblies, housings, and brackets. Average use of magnesium per vehicle is about two to three kilograms which could also go as high as 26 kilograms for some vehicles.
http://www.foundry-planet.com/equipment/detail-view/with-increasing-demand-from-auto-sector-global-magnesium-market-to-grow-by-573-by-2020/




Magnesium Alloys: The Future for Automotive Lightweighting?
Experts gathered at the University of Waterloo discussed the challenges and opportunities ultralightweight alloys pose
http://www.canadianmetalworking.com/article/metalworking/magnesium-alloys-future-automotive-lightweighting

2015
Magnesium Prices
http://www.metal-pages.com/metalprices/mangnesium/

2014



2013


Magnesium alloys are very attractive for a range of weight-sensitive applications. They have the largest strength-to-weight ratio of the common structural metals, are lighter than aluminum and are particularly favored for being easy to machine and for their ability to be die cast to net shape. Unfortunately, magnesium alloys tend to corrode too easily. A team at Monash University in Australia has now discovered a novel and potentially game-changing approach to the problem: poisoning the chemical reactions leading to corrosion of magnesium alloys by adding a dash of arsenic to the recipe.

Magnesium alloys are of great interest as lightweight replacements for aluminum, titanium, and steel components in a range of transportation and aerospace applications. However, magnesium alloys corrode easily, and this often prevents their use as substitute for noncorroding metals.  As a result, the use of magnesium alloys at present is less than a million tons per year, while nearly 50 million tons of aluminum alloys are used each year. The experimental demonstration of reduction in corrosion of magnesium is a welcome step.  The result was that addition of about one-third of a percent of arsenic to the magnesium alloy reduced its corrosion rate in a salt solution by a factor of nearly ten. In this initial study the intent was to prove the principle of the use of cathodic poisoning to reduce corrosion of Magnesium.

http://www.gizmag.com/stainless-magnesium-corrosion-monash/28856/


Updated 1 April 2017, 14 January 2015