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Kamis, 05 Maret 2009

AutoCad Block Harley Davidson


Inspired by Harley Davidson FXSTC Softail Custom


ENGINE
Engine : 1340cc,OHV V Evolution V-twin
Displacement : 1340cc
Bore x Stroke : 3.498 x 4.250 in.
Compression Ratio : 8.5:1

DIMENSIONS
Length : 94.92 in.
Weight : 613 lbs.
Ground Clearance : 5.94 in.
Wheelbase : 66.5 in.
Fuel Capacity : 5.2 gal.(includes .6 gal. reserve)
Seat Height : 26.70 in.

DRIVETRAIN
Transmission : 5-speed

Final Drive : Belt

BRAKES/WHEELS/TIRES
Brakes : Front: 11.5 in. x .20Rear: 11.5 in x .23

DRIVETRAIN
Suspension
Front: Travel 5.61 in.Rear: Travel 4.06 in.

BRAKES/WHEELS/TIRES
Tires
Front: MH90-21Rear: MT90B16

Donwload it on http://www.4shared.com/file/91376207/64fd2245/Harley_FXSTC.html

Rabu, 04 Maret 2009

CAD Block Jeep CJ7

Jeep CJ 7
First time look, i was impressed much. Powerfull and high utility. In indonesia, this jeep price is arround $3000 ~ $4500, production year 1980 ~ 1982. It depends on condition. Diesel version is more expensive $ 500.

Isometric View


Top View

Download it on http://www.4shared.com/file/90655371/5dd21d09/Jeep_Rio.html

Selasa, 03 Maret 2009

CAD Block Small Sedan

Inspired by Small BMW 318i m20 Series sedan, there is still many thing to be fix speceially the hood, well it is yours now


Left View


Isometeric View

Download it at http://www.4shared.com/file/90630050/a23bf4d6/Small_Sedan_Rio.html

Compact Car CAD Block

Free Auto Cad Block

There many more to come, and this compact sedan 1500 cc as a start
Compact sedan car

Left View

Isometric View

Please download it on http://www.4shared.com/file/90622438/6ada9285/Compact_Sedan_Rio.html

Senin, 16 Februari 2009

Grey Iron

Knowledge Article from www.Key-to-Steel.com

Cast irons are alloys of iron, carbon, and silicon in which more carbon is present than can be retained in solid solution in austenite at the eutectic temperature. In gray cast iron, the carbon that exceeds the solubility in austenite precipitates as flake graphite.

Gray irons usually contain 2.5 to 4% C, 1 to 3% Si, and additions of manganese, depending on the desired microstructure (as low as 0.1% Mn in ferritic gray irons and as high as 1.2% in pearlitics). Sulphur and phosphorus are also present in small amounts as residual impurities.

The composition of gray iron must be selected in such a way to satisfy three basic structural requirements:
1. The required graphite shape and distribution
2. The carbide-free (chill-free) structure
3. The required matrix

For common cast iron, the main elements of the chemical composition are carbon and silicon. High carbon content increases the amount of graphite or Fe3C. High carbon and silicon contents increase the graphitization potential of the iron as well as its castability. The combined influence of carbon and silicon on the structure is usually taken into account by the carbon equivalent (CE):

CE = %C + 0.3x(%Si) + 0.33x(%P) - 0.027x(%Mn) + 0.4x(%S)

Although increasing the carbon and silicon contents improves the graphitization potential and therefore decreases the chilling tendency, the strength is adversely affected. This is due to ferrite promotion and the coarsening of pearlite.

The manganese content varies as a function of the desired matrix. Typically, it can be as low as 0.1% for ferritic irons and as high as 1.2% for pearlitic irons, because manganese is a strong pearlite promoter.

The effect of sulfur must be balanced by the effect of manganese. Without manganese in the iron, undesired iron sulfide (FeS) will form at grain boundaries. If the sulfur content is balanced by manganese, manganese sulfide (MnS) will form, which is harmless because it is distributed within the grains. The optimum ratio between manganese and sulfur for a FeS-free structure and maximum amount of ferrite is:

%Mn = 1.7x(%S) + 0.15

Other minor elements, such as aluminum, antimony, arsenic, bismuth, lead, magnesium, cerium, and calcium, can significantly alter both the graphite morphology and the microstructure of the matrix.

In general, alloying elements can be classified into three categories.
1. Silicon and aluminum increase the graphitization potential for both the eutectic and eutectoid t
transformations and increase the number of graphite particles. They form colloid solutions in the matrix.
Because they increase the ferrite/pearlite ratio, they lower strength and hardness.

2. Nickel, copper, and tin increase the graphitization potential during the eutectic transformation, but
decrease it during the eutectoid transformation, thus raising the pearlite/ferrite ratio. This second effect is
due to the retardation of carbon diffusion. These elements form solid solution in the matrix. Since they
increase the amount of pearlite, they raise strength and hardness.

3. Chromium, molybdenum, tungsten, and vanadium decrease the graphitization potential at both
stages. Thus, they increase the amount of carbides and pearlite. They concentrate in principal in the
carbides, forming (FeX)nC-type carbides, but also alloy the aFe solid solution. As long as carbide formation
does not occur, these elements increase strength and hardness. Above a certain level, any of these elements
will determine the solidification of a structure with Fe3C (mottled structure), which will have lower
strength but higher hardness.

Generally, it can be assumed that the following properties of gray cast irons increase with increasing tensile strength from class 20 to class 60:
* All strengths, including strength at elevated temperature
* Ability to be machined to a fine finish
* Modulus of elasticity
* Wear resistance.

On the other hand, the following properties decrease with increasing tensile strength, so that low-strength irons often perform better than high-strength irons when these properties are important:
* Machinability
* Resistance to thermal shock
* Damping capacity
* Ability to be cast in thin sections. Successful production of a gray iron casting depends on the fluidity of the
molten metal and on the cooling rate, which is influenced by the minimum section thickness and on section
thickness variations.

Casting design is often described in terms of section sensitivity. This is an attempt to correlate properties in critical sections of the casting with the combined effects of composition and cooling rate. All these factors are interrelated and may be condensed into a single term, castability, which for gray iron may be defined as the minimum section thickness that can be produced in a mold, cavity with given volume/area ratio and mechanical properties consistent with the type of iron being poured.

Scrap losses resulting from missruns, cold shuts, and round corners are often attributed to the lack of fluidity of the metal being poured.

Mold conditions, pouring rate, and other process variables being equal, the fluidity of commercial gray irons depends primarily on the amount of superheat above the freezing temperature (liquidus). As the total carbon content decreases, the liquidus temperature increases, and the fluidity at a given pouring temperature therefore decreases. Fluidity is commonly measured as the length of flow into a spiral-type fluidity test mold.
The significance of the relationships between fluidity, carbon content, and pouring temperature becomes apparent when it is realized that the gradation in strength in the ASTM classification of gray iron is due in large part to differences in carbon content (~3.60 to 3.80% for class 20; ~2.70 to 2.95% for class 60). The fluidity of these irons thus resolves into a measure of the practical limits of maximum pouring temperature as opposed to the liquidus of the iron being poured.

The usual microstructure of gray iron is a matrix of pearlite with graphite flakes dispersed throughout. Foundry practice can be varied so that nucleation and growth of graphite flakes occur in a pattern that enhances the desired properties. The amount, size, and distribution of graphite are important. Cooling that is too rapid may produce so-called chilled iron, in which the excess carbon is found in the form of massive carbides. Cooling at intermediate rates can produce mottled iron, in which carbon is present in the form of both primary cementite (iron carbide) and graphite.

Flake graphite is one of seven types (shapes or forms) of graphite established in ASTM A 247. Flake graphite is subdivided into five types (patterns), which are designated by the letters A through E. Graphite size is established by comparison with an ASTM size chart, which shows the typical appearances of flakes of eight different sizes at l00x magnification.

Type A flake graphite (random orientation) is preferred for most applications. In the intermediate flake sizes, type A flake graphite is superior to other types in certain wear applications such as the cylinders of internal combustion engines.

Type B flake graphite (rosette pattern) is typical of fairly rapid cooling, such as is common with moderately thin sections (about 10 mm) and along the surfaces of thicker sections, and sometimes results from poor inoculation.

The large flakes of type C flake graphite are formed in hypereutectic irons. These large flakes enhance resistance to thermal shock by increasing thermal conductivity and decreasing elastic modulus. On the other hand, large flakes are not conducive to good surface finishes on machined parts or to high strength or good impact resistance.

The small, randomly oriented interdendritic flakes in type D flake graphite promote a fine machined finish by minimizing surface pitting, but it is difficult to obtain a pearlitic matrix with this type of graphite. Type D flake graphite may be formed near rapidly cooled surfaces or in thin sections. Frequently, such graphite is surrounded by a ferrite matrix, resulting m soft spots in the casting.

Type E flake graphite is an interdendritic form, which has a preferred rather than a random orientation. Unlike type D graphite, type E graphite can be associated with a pearlitic matrix and thus can produce a casting whose wear properties are as good as those of a casting containing only type A graphite in a pearluic matrix. There are, of course, many applications in which flake type has no significance as long as the mechanical property requirements are met.

Jumat, 13 Februari 2009

Grey Cast Iron DIN EN 1561

DIN EN 1561:1997 Grey Cast Iron

Grey cast iron is casting alloy, iron and carbon based, the latter element being present mainly in the form of lamellar graphite particles.
The properties of grey cast iron depend on the form distribution of the graphite and the structure of the matrix
This European standard deals with the classification of grey cast iron accordance with the mechanical properties of the material, either tensile strength hardness.

1. Scope
This standard specifies the properties of unalloyed and low alloyed grey cast iron used for castings, which have been manufactured in sand moulds with comparable thermal behavior.
This standard specifies the characterizing properties of grey cast iron by
Tensile strength of separately cast samples, or if agreed by manufacturer and the purchaser by the time of acceptance of the order, of cast-on samples or samples cut from casting
If agreed by the manufacturer and the purchaser by the time of acceptance of the order, the hardness of the material measured on castings or on cast-on knob

This standard does not apply to grey cast iron used for pipes and fittings according to EN 877-1.
This standard specifies six grey cast irons according to the tensile strength and six grey cast irons according to the brinell hardness

2. Definitions
2.1 Grey Cast iron
Iron-carbon material in which the free carbon is present as graphite, mainly in lamellar form

2.2 Relative hardness
Quotient of measured hardness to the hardness calculated from the measured tensile strength by means of an empirical relationship

2.3 Relevant wall thickness
Wall thickness for which the mechanical properties apply
Note : The relevant wall thickness is twice the modulus or twice the volume/surface ratio

3. Manufacture
The method of manufacturing of grey cast iron and its chemical composition shall be left to the discretion of the manufacturer, who shall ensure that the requirements defined in this standard are met for the material grade specified in the order

4. Requirements
4.1 Tensile properties

Table 1





(1) If cast-on sample is to be used the relevant wall thickness of the casting shall be agreed upon by the time of acceptance of the order
(2) If by the time of acceptance of the order proving of the tensile strength has been agreed, the type of the sample is also to be stated on the order. If this is lack of agreement type of sample is left to the discretion of the manufacturer
(3) For the purpose of acceptance the tensile strength of a given grade shall be between its nominal value n (position 5 of the material symbol) and (n+100) N/mm2.
(4) This column gives guidance to the likely variation in tensile strength for different casting wall thickness when a casting of simple shape and uniform wall thickness is cast in a given gray cast iron material. For castings of non-uniform wall thickness or castings containing cored holes, the table values are only an approximate guide to the likely strength in different sections, and casting design should be based on the measured tensile strength in critical parts of the casting.
(5) These values are guide-line values. They are not mandatory
(6) This value is included as the lower limit of the relevant wall thickness range
(7) The values relate to samples with an as-cast casting diameter of 30 mm, this corresponds to a relevant wall thickness 0f 15 mm


4.2 Hardness properties
If it is not possible to use the Brinell test method (EN 1003-1), alternative test methods may be used, which shall have correlated values with Brinell test.If a casting is ordered on the basis of hardness, the relevant wall thickness and the position of the test shall be agreed upon by the time of the acceptance of the order
Table 2





(1) For each grade, Brinell Hardness decreases with increasing wall thickness
(2) By agreement between the manufacturer and the purchaser a narrower hardness range maybe adopted at agreed position on the casting, provided that this is not less than 40 Brinell Hardness units. An example of such a circumstance could be castings for long series production









5 Sampling
5.1 Tensile test
5.1.1 Separately cast samples
The separately cast samples to establish the material grade shall be cast vertically. The moulds shall be either sand moulds or moulds with comparable thermal diffusivity. The moulds may be made for casting several samples simultaneously.



All dimensions are given in milimeters
The Length (L) shall be determined according to the length of the test piece and clamping divice used. Other dimensions of the mold should meet the dimensional requirements.
Samples of other dimensions and using other casting procedures may be agreed between the manufacturer and the purchaser for the purpose of representing the properties of particular castings.
Samples shall be made from the metal used to produce the castings which they represent and during the same period was when the castings are made.
The frequency of casting the separately cast samples shall be in accordance with the in-process quality assurance procedures adopted by the manufacture.
The sampels shall be stripped from the mould at temperature not exceeding 500 C.

5.1.2 Cast-on Samples
The test pices used for the tests shall be machined from a cast-on sample. The type of sample shall be chosen in such a way as to provide approximately the same cooling conditions as for the casting to be represented. The type of sample and the location of the sample on the casting shall be agreed between the manufacturer and the purchaser. If there is no such agreement, the manufacturer shall decide on the type of sample and it shall be located at a representative position on the casting.

* The small size set is used for casting less than 80mm thickness and the large size set is used for castings equal to or greater than 80 mm wall thickness

* Cast-on samples should only be used when casting is more than 20 mm thickness and th nass is more than 200 kg

5.1.3 Test Piece cut from a casting



All dimensions are in millimeters


Table 1 shows anticipated minimum values of tensile strength for test pieces cut from a casting with uniform section of sample shape


* Values obtained in castings of variable wall thickness can differ from those given in table 1











5.2 Hardness Test

Hardness test may be carried out on the separately cast samples
Alternatively, the brinell hardness test may be carried out, by agreement between the manufacturer and the purchaser, on a test piece ("Brinell knob") which is cast on to the casting as shown bellow. The position of the brinell knob. and its size and shape, shall be agreed between the manufacturer and purchaser by the time of acceptance of the order.
In order to carry out the brinell hardness test, the test piece is removed from the casting, ground on the cut surface and then tested on the ground surface


















6. Test Method
6.1 Tensile test
The tensile test shall be carried out in accordance with the requirements of EN 1002-1. The dimensions of the test piece shall conform to the dimensions given in table 3. The gripped parts may be either threaded or plain to suit clamping device


Common Metallurgical Defect on Grey Iron

Hydrogen Blowhole
Possible Causes :
1. High moisture content in charging or alloy element (including Rust)
2. High content of Alumunium and Titanium
3. High moisture content of molding sand
4. Buld-up of dead clay in greensand
5. Wet mold or core coating6. Cores have become old and pick up moisture
7. Use of damps refractories


Nitrogen Fissure
Possible Causes :
1. Use of high steel scrap content in cupola melted iron with high coke charges
2. Use of recarburizer with high nitrogen content
3. Use of high nitrogen containing resins or buld-up of nitrogen in the sand
4. Insufficient of Ti or Zr contens to neutralise free nitrogen
Compaction of Graphite Flakes

Possible Causes :
1. Use of steel scrap content in cupola melted iron with high coke charges
2. Use of recarburiser with high nitrogen content
3. Use of high nitrogen containing resins or buld-up of nitrogen in the sand
4. Insufficient of Ti or Zr contens to neutralise free nitrogen
Shringkage

Possible Causes :
1. Soft moulds or not properly cured binder
2. Insufficient clamping or weighting
3. Incorrect carbon content or carbon equivalent
4. Hot spot resulting from poor designed gates and riser system
5. Casting design causing large change in casting section size or sharp radii
6. Incorrect inoculation
Slag Inclusion
Possible Causes :
1. Inadequate slag removal during melting and pouring
2. Cold metal heels in ladles and recievers
3. Lack of slag traps of fitters
4. Low poring temperature
5. Excess addition of slag forming materials
6. Turbulent mould filling
Carbon Monoxida Blowhole

Possible Causes :
1. High sulphur in combination with high manganese content
2. Low pouring temperature
3. Improper slag seperation
4. Slag contaminated ladles and improper leaving a metal heel in the ladle
(Carbon monoxide blowhole is also known as the manganese sulphide blowhole)
Intercellular Carbide
Possible Causes :
1. Excessives of strong carbide promoter elements such as Cr, Ti, V and Mo
2. Low levels of graphite promoter elements such as Si and Ni in base iron
3. Insufficient inoculation
4. Superheating and long holding at base iron
5. Too high amount of steel scrap in the charge
Steadite

Possible Causes :
1. Excessive or high phosphorous content
2. Slow cooling in thicker section casting
(High phosphor content also increase the shringkage tendency and britelness of the iron)





Undercooled Graphite
Possible Causes :
1. Insufficient inoculation
2. Rapid solidification
3. Superheating or long holding of metal prior to pouring
4. High content of Ti
5. low carbon Equivalent
C Type Graphite

Possible Causes :
1. Found in condition of very slow cooling rate and near eutectic compositions
2. Under inoculation
(Also called kish graphite, is mainly found in iron with hyper eutectic composition)
Ferritic Rim

Possible Causes :
1. Too low content of volatiles in greensand moulds
2. Under inoculation
3. Slow pouring rate
4. Low Pouring temperature






























































































































































Kamis, 12 Februari 2009

Common Defects in Ductile Cast Iron

Common Metallurgical Defects in Ductile Cast Iron

C.M.Ecob
Customer Services Manager, Elkem AS, Foundry Products Division

Abstract
The objective of this paper is to provide an overview of some of the most common metallurgical defects found in the production of ductile cast iron today. The examples shown have all been determined during the examination of samples in Elkem’s Research facility in Norway. Whilst many foundries recognise the defects, an appreciation of the possible causes, and therefore cures, is not always apparent. The causes and cures for the different problems are examined in the paper. Emphasis is made on shrinkage problems, probably the most common problem seen by Elkem’s team of service engineers around the world.

Introduction
Metallurgical defects in ductile iron can be very costly to the foundry, not only because the part has to be remade or rectified, but due to the unfortunate fact that many defects are not revealed until after the expensive machining stage. Care in the selection of raw materials, good process control in the melting stage and proper metal handling procedures will go a long way to the prevention of defects. Further, a routine for logging and recording of defect occurrences will reveal which are the major problem areas, allowing for a systematic elimination of the defects. This paper will examine the most common defects, starting with shrinkage. Deterioration of affordable steel scrap qualities, use of incorrect inoculants and nodularisers plus the pressures to get castings out of the door as fast as possible has led to an increase in the incidences of shrink/porosity related cases seen by Elkem’s team of technical service engineers. Indeed, the ductile iron foundry, which truthfully claims not to have shrinkage concerns is the exception to the rule.
Other common defects may be divided into two basic categories:
- Those related to nodule shape and size, such as compacted graphite structures, exploded and chunky graphite,
graphite floatation, spiky graphite and nodule alignment.
- Those related to inclusions/abnormalities within the matrix, such as flake graphite surfaces, slag inclusions,
carbides and gas. These problem areas are described to aid recognition of the defect and causes are discussed
together with possible cures.
Shrinkage Control
There are many causes of shrinkage in ductile iron, experience globally has shown that about 50% of shrinkage defects are related to sand systems, feeding and gating. The other 50% may be attributed to metallurgical factors such as carbon equivalent, temperature, inoculation or high magnesium residuals.

Figure 1: Typical sub-surface shrinkage defect with dendrite arms partly covered with graphite sticking out.
When a shrink or porosity is detected in a casting, there are several immediate and simple steps that can be taken to identify the cause of the problem.
Firstly, the geometry of the casting should be examined to determine whether the location of the defect is close to a sharp radius or a potential hot spot. At the same time, the sand in the region of the shrink should be examined to look for any soft spots. Sand integrity accounts for a high proportion of shrinkage defects and a worn seal on the moulding machine, for example, resulting in a lower sand compaction can often be the cause of an unexplained sudden outbreak of shrinkage.
The second avenue of investigation should be the gating / runner designs and the feeding of the casting. Whilst many foundries have computer aided design systems, patterns are often altered slightly over the years at shop floor level and can be significantly different from the original design. Also, changes to the feeder specification can lead to different burn characteristics and metal solidification patterns. This can affect the amounts of feed metal available to different parts of the casting.
Metallurgically, there are many factors that can affect the shrinkage tendency.

Figure 2: Effect of magnesium content on shrinkage

Magnesium, apart from being one of the most powerful carbide stabilizers, has a marked effect on the shrinkage tendency of ductile irons. Foundries operating at the higher end of the magnesium range, 0.05% or above, will find that the iron is more prone to shrink than foundries operating at lower, but very acceptable, levels, say 0.035-0.04%. Both under-inoculation and over-inoculation can cause shrinkage. In the case of under- inoculation, not enough dissolved carbon is precipitated as graphite. Graphite nodules have a far lower density than the matrix and to precipitate the low density, high volume graphite has an overall expansion effect, which helps to counter the natural tendency of the iron to shrink. With over-inoculation, too many nucleation points are active early in the solidification, resulting in an early expansion and sometimes large mould wall movements. Later in the solidification, when feeders become inactive and contraction takes place, there is no graphite coming out from solution to counteract the contraction and the result is shrinkage between the eutectic cells. In many foundries, the microstructure shows even sized nodules (accounting for the fact that the section cuts through nodules in 2-dimensions). Many foundry men still consider this to be a good structure, even though the iron is prone to shrinkage. Nodularizers and specialist inoculants are available these days, which help to counter shrinkage by giving a skewed nodule distribution.

Figure 3: The same base iron treated with two different nodularisers resulting in a) Skewed nodule distribution b) Unskewed nodule distribution

A skewed nodule distribution indicates that some nodules are being created late in the solidification process and the drawing of graphite from solution at this stage is a very effective way to counter shrink. Most inoculants act almost instantaneously and this gives the even nodule size effect. Once the potency of the inoculant has gone, then there is no driver to create nodules late in the solidification and shrinkage can be the result. More recently, nodularisers have been developed by Elkem that have the same effect of producing the skewed and shrink reducing nodule distribution curve.
A low carbon equivalent, or metal that has been held for some time at temperature, due to a mechanical breakdown, for example, is also prone to shrinkage. In these cases, the inherent nuclei within the melt will be low and some preconditioning may be necessary to achieve a good level of nucleation.

Compacted Graphite within the structure. There are several causes of this, the most common being that the nodularisation process has partly failed. Incorrect weighing of the nodulariser or the use of the wrong nodulariser are possible reasons for the failure, although a long holding time in the ladle or excessive temperatures can be contributory factors.

Figure 4: Sample with compacted graphite present in the matrix due to partly failed
Nodularisation process
Another cause of CG particles in the matrix is an incorrect sulphur level in the base iron. Many foundries melt both grey and ductile charges and segregation of returns is essential. During the nodularisation process, the first reactions that take place are a desulphurisation and deoxidation, these elements combining preferentially with the magnesium. The base sulphur level must be accounted for in the calculation of MgFeSi charge weight. A note of caution here with regard to the addition of the MgFeSi to the ladle or treatment vessel. To add the MgFeSi early to a hot ladle and then hold the ladle for several minutes until the moulding line calls for metal is bad practise as the alloy will be burning or oxidising in the bottom of the ladle during this time. Higher and more consistent recoveries can easily be achieved by adding the alloy just before tap from the furnace.

Low Nodule Count
As the compacted graphite mentioned above may commonly be attributed to the nodulariser, then low nodule counts tend to be a function of the inoculant. Figure 5 shows a low count compared to the foundry’s normal practise. Avoiding long holding times in the furnace and prolonged pouring time post-inoculation will help to achieve consistent nodule counts, as will improving the responsiveness of the iron via preconditioning. The use of a specialist powerful inoculant will give the most consistent results.

Figure 5: Two casting with the same metal treatment resulting in a) low nodule count due to long pouring time and b) normal nodule count with normal practise.

Exploded graphite
Characteristically, exploded graphite looks exactly as the name might suggest that the graphite has been blown apart. Most MgFeSi alloys contain some rare earth metals, cerium, lanthanum, neodymium, praesodimium etc and these are beneficial in that they neutralise the effects of some detrimental tramp elements such as lead, bismuth, antimony, titanium etc..Rare earth elements are also nodularisers and aid the effects of the magnesium. In excess, however, rare earths can cause exploded graphite. This is more especially when high purity charges are used which are low in tramp elements. Exploded graphite is normally found in thicker section castings with slow cooling rates or at very high carbon equivalent levels.

Figure 6: Sample with exploded graphite present due to excess concentration of rare earth metals.
Care should be taken when using induction melting as rare earths can be cumulative in the iron. They tend to have very high melting points and do not volatilise, although some will be oxidised and come out in the slag. This is important to note if a low/zero RE containing nodulariser is substitutes to eliminate the problem as it may take time to dilute the residual RE out of the system. Should exploded graphite occur, then examination of the rare earth sources should be made – normally the MgFeSi. Melting a virgin charge with steel scrap, pig iron and no returns will quickly show if the returns and/or the MgFeSi are the problem. Latin America and countries in the Far East tend to use high levels of rare earth in the nodulariser. Reductions in the carbon equivalent may help to reduce exploded graphite.
Chunky graphite
The causes of chunky graphite are exactly the same as for exploded graphite with the addition that the defect is also found in thinner casting sections and is not as sensitive to the carbon equivalent as exploded graphite.

Figure 7: Sample with chunky graphite present due to excess concentration of rare earth metals.

Graphite floatation
This is caused when large, low density graphite nodules are formed during the solidification of thick section or otherwise slow cooling castings. The nodules, being of a lower density than the matrix, tend to float towards the surface of the casting and thus can have a negative effect on the mechanical properties (and surface finish) in that region. A reduction in the carbon equivalent will help to control this, as will a reduction in the pouring temperature or increasing the cooling rate of the casting by the use of chills. The inoculation system should also be examined, as it is likely that the large graphite nodules have been formed very early during the solidification process and an inoculant, which will generate more, smaller nodules, could be an advantage.
Figure 8: Sample with graphite floatation present due to high carbon equivalent.
Nodule Alignment
This is caused by large dendrites growing during the solidification with the nodules being precipitated between the dendrite arms. Thus the nodules appear to be aligned. Whilst not normally a serious problem, this can have detrimental effects on such properties as tensile strength or impact resistance. The normal causes are low carbon equivalent where not enough graphite is precipitated during the cooling, under inoculation or too high a pouring temperature.

Figure 9: Sample with nodule alignment caused by large dendrites growing during the solidification with the nodules being precipitated between the dendrite arms.
Spiky Graphite
The occurrence of spiky graphite in ductile iron is rare provided that the nodulariser used contains a small amount of rare earths. Normally, the rare earth metals neutralise such elements as lead, bismuth, titanium and antimony, as discussed in the section on exploded graphite, however the use of a rare earth-free nodulariser where traces of the deleterious elements are present results in spiky graphite. This is most commonly found in converter iron where the separate additions of RE have been left out by human error. The effect of spiky graphite is a dramatic reduction in the mechanical properties of the iron, the spikes provide points of weakness in the structure. The only cure for this type of defect is the addition of rare earths with the nodulariser.

Figure 10 Sample with spiky graphite present in the matrix due to too elevated level of Pb.

Flake Graphite on the Casting Surface This is commonly seen in foundries, however many ignore the flake graphite on the surface as it forms part of the machining allowance. The defect is illustrated in Figure 11 and clearly shows the thin layer of flake graphite adjacent to the mould. This is found mainly in greensand systems and is caused by a build up of sulphur in the sand, which reacts with the magnesium in the iron to form magnesium sulphides and effectively de-nodularise the iron. A higher Mg or Re in the nodulariser can overcome this, subject to shrinkage restrictions discussed earlier, but the most common remedy is to use an inoculant containing cerium. This has the effect of re-nodularising the iron locally.

Figure 11 Sample with flake graphite on the surface of the casting due to high sulphur content in he moulding sand.

Carbides In the production of ductile iron, it must be remembered that magnesium is one of the most powerful carbide promoters. Coupled with this, the violence of the magnesium reaction during the nodularisation process tends to destroy nuclei. For these reasons, inoculation requirements are heavier than for grey irons and under-inoculation or the use of the wrong inoculant are amongst the most common causes of chill or carbides in ductile iron. Poor inoculation is not the only cause of carbides, however, and all the potential reasons need to be explored to determine the reason behind carbide formation.