Browse Topic: Metallurgy

Items (16,004)
Compressive residual stresses are very important at fatigue life, therefore this work has an objective to determine compressive residual stresses longitudinally, along a surface, with three levels of deflection causing tensile prestresses on the surface fibers, of 750 MPa, 1100 MPa and 1500 MPa, supported in one support position on the compression side, 150 mm, equidistant from the longitudinal center of the samples, which are made of EN 47 steel (DIN 51CrV4), with dimensions of 15 mm thick, 70 mm width and 1500 mm long. The samples are submitted to quenching, tempering, surface polishing and stress relief processes, with radius of 2500 mm and concavity downwards, and after they are immersed in a tank with mineral and conventional quenching oil compound, then the samples are tempered and the concave surfaces are polished to remove decarburization and took into the furnace to relieve stress caused by the surface polishing process. Next step, the samples are peened, with deflections of
Chiqueti, Cleber Michelde Almeida Benassi, AdrianoGomes, Bárbara Mirandados Santos, Marcosde Lima, Alexandre SantanaRolim, José Ronaldo Agostinhoda Silva, Fernando Vilanova
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) from 0.375 to 1.300 inches (9.53 to 33.02 mm) in diameter or thickness, produced with cross-sectional area of 22.5 square inches (145 cm2), maximum, and a circumscribing circle diameter (circle size) of 17.4 inches (44.2 cm), maximum (see 2.4 and 8.8).
AMS D Nonferrous Alloys Committee
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by hot isostatic pressing (HIP) (see 8.5).
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 0.002 inch (0.05 mm) and above in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion- and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification, in conjunction with the general requirements for steel heat treatment in AMS2759, establishes requirements for thermal stress-relief treatments of parts manufactured from the following materials: a Carbon and low-alloy steels b Tool steels c Precipitation-hardening, corrosion-resistant, and maraging steels d Austenitic corrosion-resistant steels e Martensitic corrosion-resistant steels
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant iron alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate from 0.006 to 3.000 inches (0.15 to 76.20 mm) in thickness, inclusive (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers the engineering requirements for producing brazed joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys using gold-nickel alloy filler metal.
AMS B Finishes Processes and Fluids Committee
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and foil.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the procurement of granular heat-treating salts suitable for use in the molten state.
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of plate 0.250 to 4.000 inches (6.35 to 101.60 mm), inclusive, in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an iron-nickel alloy in the form of strip 0.020 to 0.1874 inch (0.51 to 4.760 mm), inclusive, in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a high-strength, corrosion-resistant alloy in the form of bars up to 1.75 inches (44.4 mm) in diameter (see 8.2).
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a high-strength, corrosion-resistant alloy in the form of bar up to 1.75 inches (44.4 mm) in diameter (see 8.2).
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 6.000 inches (0.551 to 152.4 mm), inclusive, in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts and bite type flareless sleeves for use in aircraft fluid systems at an operating pressure of 5000 psi for the fittings and nuts and 3000 psi for the bite type sleeves.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers an aluminum alloy in the form of plate 0.750 to 1.500 inches, incl (19.05 to 38.10 mm, incl) in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
This specification establishes the engineering requirements for producing an anodic coating on titanium and titanium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
Friction stir surfacing is an advance surface modification technique, which is functionally evolved from the friction stir welding process. However, the fundamental reason behind the joining of Al/steel is difficult due to the formation of hard and brittle intermetallic compounds (IMC). To address the problem of IMC formation, the current study suggested an alternate production technique with solid-state friction surfacing deposition. In this work, the adhesion mechanism and metallurgical properties of solution-treated AA6061-T6 aluminum alloy cladding over a low-carbon steel IS2062 substrate were investigated. Impact procedural factors (axial frictional force, spindle speed, table traverse speed, consumable rod diameter, and substrate roughness) were examined. Push-off and hardness tests were used to inspect the mechanical properties of cladded samples. 67–77± HV hardness is observed at the interface of the cladded cross-section. A push-off strength of 9 kN was achieved, indicating
Badheka, Kedar HiteshkumarSharma, Daulat KumarBadheka, Vishvesh
This specification covers a corrosion-resistant steel in the form of cold-worked bars and wire up to 1.750 inches (44.45 mm), inclusive, in nominal diameter or least distance between parallel sides.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip 0.005 inch (0.13 mm) and over in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Standard covers normalized electric-resistance welded flash-controlled single-wall, low-carbon steel pressure tubing intended for use as pressure lines and in other applications requiring tubing of a quality suitable for bending, double flaring, beading, forming, and brazing. Material produced to this specification is not intended to be used for single flare applications, due to the potential leak path caused by the Inside Diameter (ID) weld bead or scarfed region. Assumption of risks when using this material for single flare applications shall be defined by agreement between the producer and purchaser. This specification also covers SAE J356 Type-A tubing. The mechanical properties and performance requirements of SAE J356 and SAE J356 Type-A are the same. The SAE J356 or SAE J356 Type-A designation define unique manufacturing differences between coiled and straight material. Nominal reference working pressures for this tubing are listed in ISO 10763 for metric tubing, and SAE
Metallic Tubing Committee
This research examined maraging steel (C300), which is widely used in the automotive industry. The study investigated how various 3D printing parameters—laser power (P), scanning speed (V), and layer spacing (H)—as well as post-processing heat treatment factors such as time (t) and temperature (T) affect the properties of C300 steel produced via selective laser melting (SLM). The primary properties assessed included relative density, porosity, hardness, and microstructure. The first part of the analysis focused on how processing parameters, time, and temperature influenced porosity types and manufacturing defects. Subsequently, ANOVA was employed to explore the sensitivity of relative density and microhardness to these parameters. The results revealed an optimal combination of parameters that improved both microstructural and mechanical properties. Additionally, the post-processing heat treatment was found to impact microhardness by modifying the microstructure and martensite lath size
Jaballah, OlaOmidi, NargesIltaf, AsimBarka, NoureddineEl Ouafi, Abderrazak
This specification covers the engineering requirements for producing brazed joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys by use of silver alloy filler metals and the properties of such joints.
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 32 square inches (206 cm2) in area (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers a leaded bronze in the form of sand and centrifugal castings (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum bronze alloy in the form of centrifugal and chill castings (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a nickel-aluminum-bronze alloy in the form of sand, centrifugal, and continuous castings (see 8.5).
AMS D Nonferrous Alloys Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, flash-welded rings, and stock for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for a hard anodic coating on magnesium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers an aluminum alloy in the form of plate 3.000 to 6.000 inches (76.20 to 152.40 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of round, non-welded tubing free from OD surface seams.
AMS E Carbon and Low Alloy Steels Committee
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