SAE 4340 Purpose: heavy machinery such as high load of axial, turbine shaft larger than 250 mm in diameter, a helicopter rotor shaft, turbojet engine turbine shaft, blade, high load transmission piece of moving parts, fasteners, crankshaft gear, etc. Also can be used for operating temperature more than 400℃ rotor shaft and blade, etc.; SAE 4340 steel can also into after nitriding processing, used to make special performance requirements of the important parts, after low temperature tempering or can be used for ultra-high strength steel after isothermal quenching.
SAE 4340 Chemical Compositions(%)
Grade | Chemical Compositions | |||||||
SAE 4340 | C | Si | Mn | S | P | Cr | Mo | Ni |
0.38~0.43 | 0.15~0.35 | 0.60~0.80 | ≤0.040 | ≤0.035 | 0.70~0.90 | 0.20~0.30 | 1.65~2.00 |
SAE 4340 Mechanical Properties
Grade | Tensile strength | Yield strength | Adjustable rate | Reduction of area | Impact energy | Impact toughness values |
SAE 4340 | (MPa) | (MPa) | (%) | (%) | J | (J/cm2) |
≥980 | ≥835 | ≥12 | ≥55 | ≥78 | ≥98 |
The corresponding steel grades to SAE 4340:40CrNiMoA,DIN 36CrNiMo4,DIN 1.6511,NF 40NCD3,JIS SNCM439,BS 816M40,AISI/4340,UNS G43400.
SAE 4340 Delivery status: by heat treatment (normalizing, annealing and high temperature tempering) or heat treatment state delivery, delivery status should be indicated in the contract.
SAE 4340 alloy steel Heat treatment: quenching 850 degrees; Coolant: oil; Tempering temperature 600 degrees; Coolant: water, oil; Or high temperature tempering steel annealing supply state brinell hardness GBW less than or equal to 269.
SAE 4340 Alloy Structure Steel Plate Specifications:
Steel Standard: SAE 4340
Thickness: 4.5 mm to 250 mm
Width: from 1.6 m to3.8m
Length: Up to 18 m
Katalor Enterprises has established a full set of strict quality control system, advanced manufacturing technique and equipments. As a SAE 4340 alloy structure steel plate stockist and supplier, if you have any demand of SAE 4340 alloy structure steel plate price, please do not hesitate to contact us .