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63/32bearing dimensions
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63/32bearing
Minimum Longitudinal Tensile Properties: PropertyValue Tensile Strength260 ksi Yield Strength 0.2% offset217 ksi Elongation10% Reduction of Area30%
Chemical Composition: SymbolElementMin %Max % CCarbon0.38%0.43% MnManganese0.65%0.90% SiSilicon0.15%0.35% PPhosphorus0.01% SSulfur0.01% CrChromium0.70%0.90% NiNickel1.65%2.00% MoMolybdenum0.20%0.30% CuCopper0.35%
63 32simplified
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Mechanical Properties: Bar SizeTemperature * Tensile StrengthYield Strength Elongation in 2"Reduction of Area 3.5" Dia.400° F (204° C)276 ksi222 ksi11.0%35.0% 7.5" Dia.500° F (260° C)265 ksi222 ksi8%25.0% 10.5" Dia.1100° F (593° C)165 ksi150 ksi18%60.0%
63/28 bearing dimensions
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Service Steel Aerospace is one of the largest distributors / suppliers of 4340 Alloy Steel available in several forms including round bar, flat bar, and square bar as well as block, and billet. See below for product size ranges stocked.
62/32 bearing dimensions
Common Trade Names: Lescalloy 4340 Vac-Arc European Designation 36CrNiMo4 4340 Chrome-Nickel-Molybdenum Steel SAE 4340 AISI 4340 4340 CEVM 4340 ESR
Hardenability Requirements: Jominy: J 12/16 inch: 53 RC Hardness min Jominy: J 20/16 inch: 32 RC Hardness min For Material Normalized 1600° F (871° C) with Test Specimen Austenitized 1550° F (843° C)
Tempering Data: TemperatureHardness (approx) 400° F (204° C)52 HRC 500° F (260° C)49 HRC 600° F (316° C)47 HRC 700° F (371° C)45 HRC 800° F (427° C)41 HRC 900° F (482° C)38 HRC 1000° F (538° C)35 HRC 1100° F (593° C)30 HRC 1200° F (649° C)25 HRC
Heat Treatment: TypeProcess Normalize1600° - 1700° F (871° – 927° C), then air cool Auestenitize1475° – 1575° F (802° – 857° C), then quench in oil Temper400° – 1200° F (204° – 649° C) depending on desired strength. For Ultimate Tensile Strength above 260ksi, temper between 400° – 500° F (204° – 260° C)
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4340 VAR: AS9100 Mill Producers Dunkirk Specialty Steel, a Universal Stainless company Electralloy a G.O. Carlson Inc. Co Gloria Material Technology Corp. Carpenter Technology Corp. Latrobe Specialty Metals Liberty Speciality Steels Ltd Universal Stainless & Alloy Products
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Fabrication: ForgingForge between 1950° – 2250° (1066° – 1232° C). Preheating or furnace cooling in ash or lime is recommended MachinabilityNormalize, then temper at approx. 1200° F (649° C) for optimum condition for machining WeldingCan be welded by gas or arc fusion methods. Alloy is capable of air hardening, and should be either Annealed or Normalized and Tempered after welding
63/22 bearing dimensions
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4340 VAR AMS 6414 Common Specifications: AMS 6414 VAR (CEVM) AMS 6414 ESR AMS 6415 (Air Melt) AMS 6409 MIL-S-5000, AMS-S-5000 (Both are cancelled and superseded by AMS 6415) MIL-S-8844 299-947-055 Bell Helicopter SS 9702 Sikorsky DMS 1555 Boeing (Previously McDonnell Douglas) HMS 6-1121 (for 4340 ESR Only) BPS 4807 (for 4340 ESR Only)
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4340 VAR AMS 6414 Stocked Sizes: Rounds: 39 sizes 0.500” through 10.00” diameter Flats & Blocks: 12" x 23" block to cut-to-size Custom thicknesses & widths available saw-cut Billets: 7” and 14" billet for conversion to special sizes Note: Stocked as Normalized and Tempered
4340 VAR AMS 6414 is a low alloy Chromium-Nickel-Molybdenum steel capable of being heat treated to high strength levels. This specification is for a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. Service Steel Aerospace stocks Premium Aircraft Quality produced double melted in an Electric Furnace, followed by VAR, or Vacuum Arc Remelt (also known as CEVM, or Consumable Electrode Vacuum Arc Remelting). This results in a much cleaner steel meeting the magnetic particle test requirements of AMS-2300. It is a steel of the highest quality with excellent transverse ductility and toughness at high strength levels. It has good shock and impact resistance as well as wear and abrasion resistance in the hardened condition. Standard Aircraft Quality air-melted AMS 6414 Air Melt material is available on request. 4340 ESR, or Electroslag Remelted material is also available on request.
4340 has been used typically for parts requiring a through-hardening capability up to 3.5 inches (89 mm) in nominal thickness at time of heat treatment and subject to rigid magnetic particle inspection standards, but usage is not limited to such applications. Premium Aircraft Quality is intended for use in the manufacturing of highly stressed parts at higher strength levels, such as 260/280,000 psi and where a much cleaner steel is desired.
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