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AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings

AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings

500 INR/Kilograms

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AMS 6308 Bars, AMS 6308 Rods & AMS 6308 Rings Price And Quantity

  • 500 INR/Kilograms
  • 1 Kilograms

Product Description

AMS 6308 is an aerospace-grade, high-performance, low-alloy carburizing steel specification established by SAE International. It is commercially known as Pyrowear 53 (UNS K71040) and is produced via premium double-vacuum or triple-vacuum melting processestypically Vacuum Induction Melting followed by Vacuum Arc Remelted (VIM-VAR or VIM-VAR-VAR) or Electroslag Remelted (ESR)to achieve maximum micro-cleanliness, tight chemical control, and high fatigue resistance.

Below is an engineering breakdown of AMS 6308 in its standard supply forms: Bars, Rods, and Rings.

1. Material Properties & Characteristics

AMS 6308 is specifically engineered for components that operate under extreme cyclic loads and high temperatures.

  • High Temper Resistance: Unlike standard carburizing steels (such as AISI 9310 or 8620) which soften dramatically above $300^\circ\text{F}$ ($149^\circ\text{C}$), AMS 6308 maintains its surface hot hardness and core fracture toughness at elevated service temperatures up to $450^\circ\text{F}$ ($232^\circ\text{C}$).

  • Core Toughness: It features exceptionally high impact strength and fracture toughness in the core alongside high case fatigue life.

  • Ultra-Clean Microstructure: Double or triple vacuum melting minimizes non-metallic inclusions, crucial for resisting subsurface-initiated rolling contact fatigue (RCF).

Nominal Chemical Composition (%)

Carbon (C) Silicon (Si) Chromium (Cr) Nickel (Ni) Molybdenum (Mo) Copper (Cu) Vanadium (V) Manganese (Mn)
0.07 0.13 0.60 1.20 0.75 1.25 1.60 2.40 3.00 3.50 0.35 max 0.05 0.15 0.25 0.50

2. Product Form Specifications

AMS 6308 Bars & Rods

Bars and rods represent the primary stock for subsequent machining, centerless grinding, or secondary forging.

  • Supply Conditions: Typically supplied in the annealed, cold-finished, or hot-rolled condition, optimized for high machinability before the component undergoes the carburizing and heat-treatment cycle.

  • Common Size Profiles: Standard rounds range from 1.500 to 7.000 in diameter, though smaller precision rod diameters and custom large-diameter bars are produced based on the mill run.

  • Quality Controls: Subject to strict aerospace standards for decarb depth limits, surface finish, macroetch limits (per ASTM A604), and premium aircraft-quality magnetic particle inspection (AMS 2300).

AMS 6308 Rings

For seamless, high-integrity circular components, AMS 6308 is processed into forged and rolled rings.

  • Manufacturing Process: Produced via seamless rolled ring forging to realign the grain flow circumferentially. This maximizes the tangential fatigue strength and structural integrity under high radial loads.

  • Applications: Primarily utilized for bearing races, output shaft couplings, internal ring gears, and retaining rings.

3. Industrial Applications

AMS 6308 is selected almost exclusively for mission-critical drive systems where component failure is not an option:

  • Aerospace & Rotorcraft: Main rotor transmission gearboxes, tail rotor drive gears, and planetary gear systems for helicopters and defense aircraft.

  • Jet Engines: High-temperature accessory gearboxes, shafts, and bearing housings.

  • High-Performance Motorsports: Heavily loaded drivetrain gears and pinions operating under thermal stress.

4. Heat Treatment & Carburizing Notes

To unlock its targeted properties, components machined from AMS 6308 stock are processed using a tailored thermochemical sequence:

  1. Carburizing: Typically gas or vacuum carburized at temperatures between $1650^\circ\text{F}$ and $1750^\circ\text{F}$ ($899^\circ\text{C}$ to $954^\circ\text{C}$).

  2. Core Hardening & Quenching: Often oil or gas quenched from a solution temperature to develop high core strength.

  3. Sub-Zero Treatment: Deep freezing at $-100^\circ\text{F}$ to $-120^\circ\text{F}$ ($-73^\circ\text{C}$ to $-84^\circ\text{C}$) to eliminate retained austenite in the case.

  4. High Tempering: Tempered at elevated temperatures (often around $400^\circ\text{F}$ to $500^\circ\text{F}$ / $204^\circ\text{C}$ to $260^\circ\text{C}$) to match its inherent high temper resistance, yielding a typical case hardness of 6064 HRC with superb core fatigue limits.

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