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Inconel 600 PDF Print E-mail
Wednesday, 20 September 2006
(Click on the tabs for information on specific properties)

Overview

Inconel® Alloy 600 is a non-magnetic nickel-chromium alloy perfect for use at high temperatures when corrosion resistance is important. Often used in chemical and food processing, Alloy 600 has demonstrated it's use for nuclear engineering, furnace components and gas turbine components.

Inconel® 600 is a versatile alloy that can be annealed, cold drawn, hot worked, welded and formed by conventional methods.

It is resistant to many corrosive agents, including: chlorine ion stress-corrosion cracking, high purity water, and organic acids. Alloy 600 is also resistant to carburizing and ammonia bearing atmospheres.

We supply Inconel® 600 in a variety of forms including round, hexagon, flats, pipe, tube, plate, sheet, strip, and wire.

 

Chemical Composition

Chemical Composition (%)
Element Minimum Maximum
Carbon (C) -- 0.15
Chromium (Cr) 14 17
Copper (Cu) -- 0.5
Iron (Fe) 6 10
Manganese (Mn) -- 1
Nickel (Ni) 72.0
Balance
Silicon (Si) -- 0.5
Sulphur (S) -- 0.015

Mechanical Properties

Mechanical Properties (Annealed)
Tensile Strength
95,000 psi     655 N/mm2
Yield Strength
45,000 psi  310 N/mm2
Elongation
40%

Physical and Thermal Data

Physical and Thermal Data
Density
0.306 lb /in  8.47 Mg/m3
Melting Range
2470-2575 ºF 1354-1413 ºC
Specific Heat
0.106 (Btu/lb · ºF) 444 (J/kg · ºC)
Curie Temperature
-192  ºF -124  ºC
Permiability
1.010  (at 200 oerstad (15.9 kA/m)
Coefficient of Expansion
7.4 (70-200 ºF , 10-6  in/in · ºF) 13.3 (21-93ºC, µm/m · ºC
Thermal Conductivity
103 (Btu · in/ft2 · h · ºF) 14.9 (W/m · ºC)
Electrical Resistivity
602  (ohm·circ mil/ft) 1.03 (µΩ · m)

Inconel is a registered trademark of Inco Alloys International

 
6AL-4V (ELI) Titanium PDF Print E-mail
Tuesday, 29 August 2006
(Click on the tabs for information on specific properties)

Overview

6Al-4V ELI is one of the most widely used Titanium alloys in the medical industry. It's properties of corrosion resistance, high strength, and toughness make it especially suitable for implants and other medical devices.

It's excellent strength to weight ratio also makes it ideal for aerospace applications.

We supply 6AL-4V ELI in a variety of forms including bar, wire, plate, and sheet.

Chemical Composition

Chemistry Data
Element Minimum Maximum
Carbon -- 0.08
Nitrogen  -- 0.05
Hydrogen -- 0.012
Iron -- 0.25
Oxygen -- 0.13
Aluminum 5.5 6.5
Vandium 3.5 4.5
Titanium -- Balance

Physical Data

Physical Data
Density 0.160 lb / cu. in.
Electrical Resistivity 1.71 µohms-m
Thermal Conductivity 6.6-6.8 W/mK
Modulus of Elasticity  16.5 psi x 10(6)

Specifications

  • AMS 4907
  • AMS 4931
  • ASTM F136
  • ASTM F467 (TI-5)
  • ASTM F468 (5)
  • ASTM F468 (S)
  • MIL F-83142
  • MIL T-9046
  • MIL T-9047
  • SPS M618
  • UNS R56401
 
15-5PH Stainless PDF Print E-mail
Tuesday, 29 August 2006
(Click on the tabs for information on specific properties)

Overview

15-5PH Stainless Steel is a martensitic, precipitation hardenable alloy used often in aircraft components.

It's properties of corrision resistance, high strength, hardness, toughness, and ductility make it a good choice for shafts, gears, fittings, fasteners, and valves.

Chemical Composition

Chemistry Data
Element Minimum Maximum
Carbon -- 0.07
Chromium  14 15.5
Copper  2.5 4.5
Iron -- Balance
Manganese -- 1
Nickel 3.5 5.5
Niobium 0.15 0.45
Phosphorus -- 0.04
Silicon -- 1
Sulphur -- 0.03

Physical Data

Physical Data
Density 0.285 lb / cu. in.
Specific Gravity 7.8
Specific Heat 0.11 (Btu/lb/Deg F - [32-212 Deg F])
Modulus of Elasticity Tension 29
 
17-4PH Stainless Steel PDF Print E-mail
Friday, 25 August 2006
(Click on the tabs for information on specific properties)

Overview

17-4PH is a very widely used precipitation hardened stainless steel alloy with a toughness especially suited for the aerospace, nuclear energy, and chemical processing industries.

This alloy features good corrosion resistance, hardness, toughness and strength. It is soft and ductile when solution annealed, yet can achieve high properties through precipitation or aging treatment.

These properties make it especially useful for aircraft engines, gears, fittings, fasteners, and valves. 17-4PH is also widely used in nuclear reactor components, paper mill equipment, and oil field parts.
 
We handle 17-4 PH in a wide variety of forms.

Chemical Composition

Chemistry Data
Element Minimum Maximum
Carbon -- 0.07
Chromium  15 17.5
Copper  3 5
Iron -- Balance
Manganese -- 1
Nickel 3 5
Niobium 0.15 0.45
Phosphorus -- 0.04
Silicon -- 1
Sulphur -- 0.03

Physical Data

Physical Data
Density 0.28 lb / cu. in.
Specific Gravity 7.74
Specific Heat 0.11 (Btu/lb/Deg F - [32-212 Deg F])
Electrical Resistivity 588 (microhm-cm (at 68 Deg F))
 
13-8 MO VM Stainless Steel PDF Print E-mail
Wednesday, 16 August 2006
(Click on the tabs for information on specific properties)

Overview

 

13-8MO VM  is a precipitation hardened, vacuum melted stainless steel alloy with a toughness especially suited for the aerospace and nuclear energy industries. It's ability to be heat treated makes it extremely valuable when hardness and stress corrosion in severe conditions are the main concern.

This alloy features excellent strength and hardness, high resistance to both general and stress corrosion, and high ductility.

These properties make it especially useful for aircraft engine and landing gear parts, fittings, pins, fasteners, and valves. 13-8MO is also widely used in nuclear reactor components.
 
We handle 13-8 MO in a wide variety of forms, including:  plate, rod, and bar.

 

Chemical Composition

Chemistry Data
Element Minimum Maximum
Aluminum 0.9 1.35
Carbon -- 0.05
Chromium 12.25 13.25
Iron -- Balance
Manganese -- 0.2
Molybdenum 2 2.5
Nickel 7.5 8.5
Nitrogen -- 0.01
Phosphorus -- 0.01
Silicon -- 0.1
Sulphur -- 0.008

Physical Data

Physical Data
Density 0.28 lb / cu. in.
Specific Gravity 7.76
Specific Heat 0.11 (Btu/lb/Deg F - [32-212 Deg F])
Electrical Resistivity 613 (microhm-cm (at 68 Deg F))
Modulus of Elasticity Tension 28.3
 
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