Steel Nitralloy 135 Modified

Annealing Procedure

Heat to 1700 F and slow cool or subcritical anneal at 1250-1300F.

Applications

Aircraft applications, including gears, crankshafts, cams and bolts.

Forgeability

Heat evenly to 2000-2025 F. Do not work below 1700F. Forgings should be air cooled.

Heat Treatability

Normalize by heating to 1800 F and hold for 1 to 4 hours, followed by air cooling. Austenitize by heating to 1700-1750 F for 1/2 hour per inch of cross section and quench in oil or water.

Principle Design Features

Nitralloy 135 Modified, as it is commonly known, is a low alloy nitriding steel grade with moderate hardenability. It was designed to provide a high case hardness and maintain its core strength during nitriding. VAC-ARC and VIM-VAR melting procedures tend to yield the most prefered ingot solidification, as well as superior cleanliness.

Tempering Procedure

Heat to 1000-1300 F depending on the desired end hardness. Temper material one hour for each inch of thickness

Known Forms

Angle

Angle

Billet

Billet

Cee

Cee

Channel

Channel

Coil

Coil

Disc

Disc

Drill Rod

Drill Rod

Flat Bar

Flat Bar

H-Beam

H-Beam

Half Round

Half Round

Hexagon Bar

Hexagon Bar

Hollow Bar

Hollow Bar

Octagon Bar

Octagon Bar

Piling

Piling

Pipe

Pipe

Plate

Plate

Precision Ground Bar

Precision Ground Bar

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Square Tube

Square Tube

Standard Beam

Standard Beam

Strip

Strip

Tee

Tee

Treadplate

Treadplate

Wide Beam

Wide Beam

Zee

Zee

Additional Data

Specifications

6470,6471,6472,A355 (A),A519 (E7140),S-6709,K24064,K24065

Chemical Elements

Carbon0.4 nom
Chromium1.2 nom
IronBalance
Manganese0.6 nom
Molybdenum0.2 nom
Silicon0.3 nom

Physical Properties

Density: 0.283lb/in³Density