MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Extreme Materials from MCAM
Visit Mitsubishi Chemical Advanced Materials for Extreme Materials - high performance plastic machining stock engineered to replace metals such as nickel alloys or stainless steel.

(Viewing data as-entered. Click here to return)
Haynes 282® Nickel Alloy Sheet, Solution Annealed and Cold Worked
Categories: Metal; Nonferrous Metal; Nickel Alloy
Material Notes: Excellent High Temperature Strength

HAYNES® 282® alloy is a wrought, gamma-prime strengthened superalloy developed for high temperature structural applications, especially those in aero and land-based gas turbine engines. It possesses a unique combination of creep strength, thermal stability, weldability, and fabricability. The alloy has excellent creep strength in the temperature range of 1200 to 1700°F (649 to 927°C), surpassing that of Waspaloy alloy, and approaching that of R-41 alloy.

Easily Fabricated: This high level of creep strength in HAYNES 282 alloy has been attained at a relatively low volume fraction of the strengthening gamma-prime phase, resulting in outstanding resistance to strain-age cracking (normally a problem with superalloys in this creep strength range). Additionally, slow gamma-prime precipitation kinetics allow for the alloy to have excellent ductility in the as-annealed condition. Consequently, HAYNES 282 alloy exhibits superior weldability and fabricability.

Product Forms: HAYNES 282 alloy is designed for use in the form of plate, sheet, strip, foil, billet, bar, wire welding products, pipe, and tubing.

Heat Treatment: HAYNES 282 alloy is provided in the solution-annealed condition, in which it is readily formable. The typical solution annealing temperature is in the range of 2050 to 2100°F (1121 to 1149°C). After component fabrication, a two-step age hardening treatment is required to put the alloy into the high-strength condition. The treatment includes 1850°F (1010°C) / 2 hours / AC (air cool) + 1450°F (788°C) / 8 hours / AC.

Applications: Suitable for critical gas turbine applications, such as sheet fabrications, seamless and flash butt-welded rings, and cases found in compressor, combustor, and turbine sections. In augmented aircraft gas turbines, it is useful for exhaust and nozzle components. In land-based gas turbines, HAYNES 282 alloy is a good candidate for transition sections and other hot-gas-path components.

Machining: HAYNES 282 alloy has similar machining characteristics to other nickel alloys used at high temperatures. Rough machining should be carried out prior to age-hardening, using the following guidelines. Final machining or finish grinding may be done after age-hardening.

Data provided by the manufacturer, Haynes International, Inc.
Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

Click here to view all available suppliers for this material.

Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Density 8.27 g/ccSolution Annealed Only
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 2610% Cold-worked
 3320% Cold-worked
 3830% Cold-worked
 4140% Cold-worked
 4350% Cold-worked
Tensile Strength, Ultimate 909 MPa
@Thickness 3.20 mm		10% cold reduction
 999 MPa
@Thickness 3.20 mm		20% cold reduction
 1141 MPa
@Thickness 3.20 mm		30% cold reduction
 1270 MPa
@Thickness 3.20 mm		40% cold reduction
 1382 MPa
@Thickness 3.20 mm		50% cold reduction
 1485 MPa
@Thickness 3.20 mm		60% cold reduction
Tensile Strength, Yield 605 MPa
@Strain 0.2 %,
Thickness 3.20 mm		10% cold reduction
 790 MPa
@Strain 0.2 %,
Thickness 3.20 mm		20% cold reduction
 963 MPa
@Strain 0.2 %,
Thickness 3.20 mm		30% cold reduction
 1093 MPa
@Strain 0.2 %,
Thickness 3.20 mm		40% cold reduction
 1204 MPa
@Strain 0.2 %,
Thickness 3.20 mm		50% cold reduction
 1312 MPa
@Strain 0.2 %,
Thickness 3.20 mm		60% cold reduction
Elongation at Break 5.6 %
@Thickness 3.20 mm		60% cold reduction
 6.6 %
@Thickness 3.20 mm		50% cold reduction
 8.9 %
@Thickness 3.20 mm		40% cold reduction
 15.5 %
@Thickness 3.20 mm		30% cold reduction
 31.5 %
@Thickness 3.20 mm		20% cold reduction
 46.7 %
@Thickness 3.20 mm		10% cold reduction
Modulus of Elasticity 140 GPa
@Temperature 1000 °C		Dynamic
 154 GPa
@Temperature 900 °C		Dynamic
 166 GPa
@Temperature 800 °C		Dynamic
 175 GPa
@Temperature 700 °C		Dynamic
 183 GPa
@Temperature 600 °C		Dynamic
 190 GPa
@Temperature 500 °C		Dynamic
 196 GPa
@Temperature 400 °C		Dynamic
 202 GPa
@Temperature 300 °C		Dynamic
 209 GPa
@Temperature 200 °C		Dynamic
 213 GPa
@Temperature 100 °C		Dynamic
 217 GPa
@Temperature 25.0 °C		Dynamic
Poissons Ratio 0.319
@Temperature 25.0 °C
 0.326
@Temperature 100 °C
 0.335
@Temperature 200 °C
 0.335
@Temperature 300 °C
 0.337
@Temperature 400 °C
 0.341
@Temperature 500 °C
 0.346
@Temperature 600 °C
 0.352
@Temperature 700 °C
 0.355
@Temperature 800 °C
 0.357
@Temperature 900 °C
 0.363
@Temperature 1000 °C
Shear Modulus 51.0 GPa
@Temperature 1000 °C		Dynamic
 57.0 GPa
@Temperature 900 °C		Dynamic
 61.0 GPa
@Temperature 800 °C		Dynamic
 65.0 GPa
@Temperature 700 °C		Dynamic
 68.0 GPa
@Temperature 600 °C		Dynamic
 71.0 GPa
@Temperature 500 °C		Dynamic
 73.0 GPa
@Temperature 400 °C		Dynamic
 76.0 GPa
@Temperature 300 °C		Dynamic
 78.0 GPa
@Temperature 200 °C		Dynamic
 80.0 GPa
@Temperature 100 °C		Dynamic
 82.0 GPa
@Temperature 25.0 °C		Dynamic
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.0001261 ohm-cm
@Temperature 25.0 °C
 0.0001278 ohm-cm
@Temperature 100 °C
 0.0001299 ohm-cm
@Temperature 200 °C
 0.0001299 ohm-cm
@Temperature 1000 °C
 0.0001318 ohm-cm
@Temperature 300 °C
 0.0001326 ohm-cm
@Temperature 900 °C
 0.0001334 ohm-cm
@Temperature 400 °C
 0.0001345 ohm-cm
@Temperature 800 °C
 0.000135 ohm-cm
@Temperature 500 °C
 0.0001355 ohm-cm
@Temperature 700 °C
 0.0001362 ohm-cm
@Temperature 600 °C
 
Thermal PropertiesOriginal ValueComments
CTE, linear 12.1 µm/m-°C
@Temperature 25.0 - 100 °C
 12.4 µm/m-°C
@Temperature 25.0 - 200 °C
 12.8 µm/m-°C
@Temperature 25.0 - 300 °C
 13.1 µm/m-°C
@Temperature 25.0 - 400 °C
 13.5 µm/m-°C
@Temperature 25.0 - 500 °C
 13.7 µm/m-°C
@Temperature 25.0 - 600 °C
 14.2 µm/m-°C
@Temperature 25.0 - 700 °C
 14.9 µm/m-°C
@Temperature 25.0 - 800 °C
 15.9 µm/m-°C
@Temperature 25.0 - 900 °C
 16.9 µm/m-°C
@Temperature 25.0 - 1000 °C
Specific Heat Capacity 0.436 J/g-°C
@Temperature 25.0 °C
 0.463 J/g-°C
@Temperature 100 °C
 0.494 J/g-°C
@Temperature 200 °C
 0.522 J/g-°C
@Temperature 300 °C
 0.544 J/g-°C
@Temperature 400 °C
 0.563 J/g-°C
@Temperature 500 °C
 0.581 J/g-°C
@Temperature 600 °C
 0.594 J/g-°C
@Temperature 700 °C
 0.650 J/g-°C
@Temperature 800 °C
 0.668 J/g-°C
@Temperature 900 °C
 0.676 J/g-°C
@Temperature 1000 °C
Thermal Conductivity 10.3 W/m-K
@Temperature 25.0 °C
 12.0 W/m-K
@Temperature 100 °C
 14.1 W/m-K
@Temperature 200 °C
 16.3 W/m-K
@Temperature 300 °C
 18.5 W/m-K
@Temperature 400 °C
 20.5 W/m-K
@Temperature 500 °C
 22.6 W/m-K
@Temperature 600 °C
 24.8 W/m-K
@Temperature 700 °C
 26.1 W/m-K
@Temperature 800 °C
 27.3 W/m-K
@Temperature 900 °C
 28.9 W/m-K
@Temperature 1000 °C
Melting Point 1300 - 1375 °C
Solidus 1300 °C
Liquidus 1375 °C
 
Processing PropertiesOriginal ValueComments
Annealing Temperature 2050 - 2100 °FTypical for solution annealing
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 1.5 %
Boron, B 0.0050 %
Carbon, C 0.060 %
Chromium, Cr 20 %
Cobalt, Co 10 %
Iron, Fe <= 1.5 %
Manganese, Mn <= 0.30 %
Molybdenum, Mo 8.5 %
Nickel, Ni 57 %as balance
Silicon, Si <= 0.15 %
Titanium, Ti 2.1 %
 
Descriptive Properties
Thermal Diffusivity0.0288 cm2/s25°C
 0.0315 cm2/s100°C
 0.0348 cm2/s200°C
 0.0381 cm2/s300°C
 0.0413 cm2/s400°C
 0.0444 cm2/s500°C
 0.0473 cm2/s600°C
 0.0488 cm2/s800°C
 0.0498 cm2/s900°C
 0.0509 cm2/s700°C
 0.0521 cm2/s1000°C

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
Haynes 282® Nickel Alloy Sheet, Solution Annealed and Age-hardened
Haynes 282® Nickel Alloy Sheet, Plate and Bar, Solution Annealed
Special Metals INCONEL® Alloy 625
Haynes 282® Nickel Alloy Sheet, Gamma-Prime Strengthened
Nimonic 263, Nimocast 263 Superalloy

NHAY986b / 162650

Rulon Bearings




Searches:   Advanced  •   Composition  •   Property  •   Material Type  •   Manufacturer  •   Trade Name  •   UNS Number
Other Links:   Advertising  •   Submit Data  •   Database Licensing  •   Web Design & Hosting  •   Trade Publications
Supplier List  •   Unit Converter  •   Reference  •   Links  •   Help  •   Contact Us  •   Site Map  •   FAQ  •   Home
 
Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at webmaster@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2024 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.