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Training / Education
2015-04-20
Preventing future problems and troubleshooting existing problems in today's stamping plants requires greater stamping process knowledge. The link between inputs and outputs isn't as clear as many think, increasing the need for detailed understanding of the variables involved. This course discusses the key inputs and outputs associated with sheet metal stamping, including important elements for controlling the process and making it more robust. The course reviews sheet metal characteristics and their application, especially from a formability standpoint, using many automotive-related examples. Common issues such as springback, dent resistance, and process differences among mild steel, high strength steel, bake hardenable steel, and aluminum are discussed. Stamping die types and functions, in particular the types of dies used in draw forming, are explained. Mechanical presses and lubrication are briefly discussed as other variables in the process. Other processes, including tube and sheet hydroforming, and progressive dies are covered in less detail.
Standard
2014-07-22
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for parts requiring a high level of mechanical properties and resistance to exfoliation corrosion and moderate resistance to stress-corrosion cracking, but usage is not limited to such applications.
Standard
2014-07-22
This specification covers treated aluminum core material for structural sandwich construction.
WIP Standard
2014-07-15
Form: This specification covers an aluminum alloy in the form of plate products from 1.000 to 6.000 inches (152.40 mm) in thickness. Application: 7065-T7451 may be used in aerospace applications requiring high strength and fracture toughness, high resistance to stress-corrosion cracking and good resistance to exfoliation corrosion, but usage is not limited to such applications.
WIP Standard
2014-07-15
Form: This specification covers an aluminum alloy in the form of plate products from from 1.000 to 6.000 inches (152.40 mm) in thickness. Application: 7065-T7651 may be used in aerospace applications requiring high strength and good fracture toughness, good resistance to stress-corrosion cracking and to exfoliation corrosion, but usage is not limited to such applications.
Standard
2014-07-15
This specification covers aluminum in the form of sheet and plate.
Standard
2014-07-11
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for structural applications requiring material with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture-toughness, but usage is not limited to such applications.
WIP Standard
2014-06-25
This specification covers an aluminum alloy in the form of seamless, drawn tubing.
WIP Standard
2014-06-24
This specification covers an aluminum alloy in the form of drawn seamless tubing. This tubing has been used typically for parts, such as conduits and low-pressure fluid lines, where moderate strength, ductility, and good weldability are required, but usage is not limited to such applications.
Standard
2014-06-11
This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of investment castings.
WIP Standard
2014-06-09
This specification covers the specific requirements for 7075 aluminum alloy bar, rod, wire, and special shapes produced by rolling, drawing, or cold finishing.
WIP Standard
2014-05-28
This specification would cover an aluminum-lithium alloy in the extruded profiles form. These extrusions are typically used for parts where low density, high mechanical properties and good dimensional stability during the machining process are desired but is not limited in usage to such applications.
WIP Standard
2014-05-14
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock.
WIP Standard
2014-05-08
This specification covers an aluminum alloy in the form of extruded profiles such as angles, channels, tees, zees, I-beams, and H-beams.

These products have been used typically for parts requiring moderate strength, especially where such parts require brazing or welding during fabrication, but usage is not limited to such applications.

WIP Standard
2014-05-08
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.

These extrusions have been used typically for structural applications requiring a combination of high strength, good exfoliation-corrosion resistance, and stress-corrosion resistance, but usage is not limited to such applicaitons.

WIP Standard
2014-05-08
This specification covers an aluminum alloy in the form of sheet.

This sheet has been used typically for structural parts requiring the strength of 2024-T3 and lower density, but usage is not limited to such applications.

WIP Standard
2014-05-08
This specification covers an aluminum bronze alloy in the form of bars, rods, forgings, and forging stock. These products have been used typically for parts requiring strength and wear resistance at moderate temperatures, but usage is not limited to such applications.
WIP Standard
2014-05-08
This specification covers an aluminum or aluminum alloy in the form of sheet, laminated and edge bonded.
WIP Standard
2014-05-08
This specification covers aluminum in the form of foil and light gage sheet. These products have been used typically for capacitors, electronic components, and sound/vibration damping tape, but usage is not limited to such applications.
WIP Standard
2014-05-08
This specification covers an aluminum alloy in the form of die forgings and forging stock ordered to inch/pound units. These forgings have been used typically for parts requiring good resistance to stress-corrosion cracking but with lower strength than AMS4126, but usage is not limited to such applications.
Standard
2014-05-05
This specification covers an aluminum alloy in the form of coiled sheet supplied in the –T4 temper.
Standard
2014-05-05
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (See 8.8.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (See 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, 7475
WIP Standard
2014-05-02
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for structural applications requiring plate with high strength, moderate fatigue strength, and high fracture-toughness, but usage is not limited to such applications.
WIP Standard
2014-05-02
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.

These extrusions have been used typically for structural parts requiring high strength up to 500 degrees F (260 degrees C), but usage is not limited to such applications. May be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking.

WIP Standard
2014-05-02
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
WIP Standard
2014-05-02
This specification covers an aluminum alloy in the form of plate.

This plate has been used typically for parts requiring a high level of mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.

WIP Standard
2014-05-02
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes and tubing.

These products have been used typically for parts requiring good strength and where fabrication does not usually involve welding, but usage is not limited to such applications.

Certain design and processing procedures may cause these extrusions to be susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

Technical Paper
2014-04-28
Sujeet K Sah, Moqtik A Bawase, M R Saraf
Abstract Automobile industry is shifting towards lighter materials in order to meet the high strength to weight ratio as required for better performance, safety, and environmental concern. The objective of this review is to evaluate and compare the different advanced and light weight materials like advanced high strength steel (AHSS), Magnesium and Aluminium alloys, which will help in selection of appropriate materials for their intended application. In this paper comparison of materials on the basis of their current, applications, limitations, cost, potential future applications and percentage wise use in automotive vehicles are discussed. Solutions and suggestions are discussed to overcome the limitations of materials which will widen their future application. Case studies and charts for cost evaluation of different materials, on the basis of structural properties like stiffness and strength are also discussed.
WIP Standard
2014-04-27
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of bar, rod, tubing, and shapes.
Viewing 1 to 30 of 3599

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