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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