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Viewing 1 to 30 of 18576
2015-10-29 ...
  • October 29-30, 2015 (8:30 a.m. - 4:30 p.m.) - Troy, Michigan
Training / Education Classroom Seminars
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.
2015-09-14 ...
  • September 14-15, 2015 (8:30 a.m. - 4:30 p.m.) - Troy, Michigan
Training / Education Classroom Seminars
Advanced High Strength Steels (AHSS) are now commonly used in automotive body structural applications. The high strength of this grade classification is attractive to help reduce mass in the automotive body through reduction in thickness. Strength also supports improvements in safety requirements so that mass increases are minimized. In some specific grades of AHSS, energy absorption is possible in addition to the high strength. This course will review the definition and properties of AHSS and cover several common applications in automotive body structures.
2015-08-05 ...
  • August 5-7, 2015 (8:30 a.m. - 4:30 p.m.) - Troy, Michigan
  • December 16-18, 2015 (8:30 a.m. - 4:30 p.m.) - Troy, Michigan
Training / Education Classroom Seminars
There is a potential for metal fatigue in any situation where a component is subjected to cyclic loads. Fatigue failures of various types are a key concern in increasing the reliability of products. Problems involving fatigue have become more severe with the demand for lighter weight structures and components. The effective use of fatigue analysis and predictive tools is critical for reducing the development time of new products. Two methods of metal fatigue analysis will be covered. The first is the stress-life approach. This method is used for high cycle or very long life fatigue problems where loads have fairly constant amplitude.
2015-06-15
Technical Paper
2015-01-2136
Francisco José Redondo
Due to weight constraints, the engine air intake for the Airbus A400M Transport Airplane will be all made in aluminum, and by specification, the intake is protected against ice accretion by a hot air system. In order to assure a fatigue life of the element for the life of the airplane, the temperature of the air supplied must be controlled to a maximum value consistent with aluminum characteristics. A system has been designed wherein hot air is bled and cooled by coolant air from inside the nacelle with a jet pump.While maximum temperature was a constraint for the design of the system, several other constraints appeared during the detailed design of the system; - the tight space allocation inside the nacelle limited the length of the jet pump, - the low temperature provided by the engine bleed in flight idle limited the secondary flow used to cool the engine bleed, and - the complex air distribution needed to supply air to the intake areas. Two variants of the system were developed.
2015-06-15
Journal Article
2015-01-2188
Zhaohui Sun, Glen Steyer, Chih Hung Chung, Gregory Kopp
Abstract This paper discusses approaches to properly design aluminum axles for optimized NVH characteristics. By effectively using well established and validated FEA and other CAE tools, key factors that are particularly associated with aluminum axles are analyzed and discussed. These key factors include carrier geometry optimization, bearing optimization, gear design and development, and driveline system dynamics design and integration. Examples are provided to illustrate the level of contribution from each main factor as well as their design space and limitations. Results show that an aluminum axle can be properly engineered to achieve robust NVH performances in terms of operating temperature and axle loads.
2015-06-09
Event
The advanced composites community in Australia has been a strong contributor for more than two decades to the research, development and production of carbon fibre composite components, particularly for the global aerospace industry. In this presentation a review of current Australian activities in the field will be provided, including the latest on implementing new technologies in areas ranging from oil & gas to aerospace & defence. Particular emphasis will be placed on the transition of research undertaken in the Cooperative Research Centre for Advanced Composite Structures (CRC-ACS) into production.
2015-06-09
Event
This session will focus on the latest technology developments in materials used for aerospace design, from structures to skin, to include new alloys and composites.
2015-06-09
Event
This paper focuses on a case study solution for setting up and monitoring the process capability of machined parts at an aircraft OEM. By creating standardized measurement plans and automating the analysis of the measured output, users can understand individual machine process performance and overall process performance in real time, as well as through automated reporting. By showing outputs and set up, reinforced by customer data, DCS will demonstrate the method of creating actionable reporting and quality tracking for process capability at a major aerospace OEM.
2015-06-09
Event
2015-06-09
Event
2015-05-21
Standard
AMS03_20
This SAE Standard specifies the requirements for the electro-deposition of zinc on non-corrosion resisting steel items for protection against corrosion, and on copper-base alloy items and corrosion resisting steel items for the reduction of contact corrosion of less noble metallic materials. Zinc coatings shall not be used on items which are liable to be subjected to temperatures exceeding 350 °C.
2015-05-21
Standard
AMS03_27
This SAE Standard specifies the requirements for the nickel-plating of ferrous metals, copper alloys, aluminum alloys and zinc alloys for one or more of the following purposes: a. the production of wear-resistant surfaces; b. the building up of worn or over-machined surfaces; c. corrosion resistance; d. to provide an undercoat for subsequent deposits, e.g., chromium.
2015-05-21
Standard
AMS03_28PT1
This SAE Standard covers the requirements for coatings of high purity aluminum on low alloy steels, high strength steels, corrosion-resisting steels, aluminum alloys and titanium alloys and other materials where appropriate.
2015-05-21
Standard
AMS03_28PT2
This SAE Standard covers the requirements for the deposition of cadmium coatings on carbon steel, low alloy steels, high strength steels, corrosion resisting steels and other materials where appropriate.
2015-05-21
Standard
AMS03_25
This SAE Standard specifies the properties of sulphuric acid anodizing of aluminum and aluminum alloys.
2015-05-19
Standard
AS9132B
This standard defines uniform quality and technical requirements relative to metallic parts marking performed using "data matrix symbology" within the aviation, space, and defense industry. ISO/IEC 16022 specifies general requirements (e.g., data character encodation, error correction rules, decoding algorithm). In addition to ISO/IEC 16022 specification, part identification with such symbology is subject to the requirements in this standard to ensure electronic reading of the symbol. The marking processes covered by this standard are as follows: - Dot Peening - Laser - Electro-Chemical Etching Further marking processes will be included, if required. Unless specified otherwise in the contractual business relationship, the company responsible for the design of the part shall determine the location of the data matrix marking. Symbol position should allow optimum illumination from all sides for readability. This standard does not specify information to be encoded.
2015-05-13
WIP Standard
AMS5934/H1000
This specification covers a corrosion-resistant steel product in the solution and precipitation heat treated (H1000) condition 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides (See 8.2).
2015-05-11
Event
2015-05-07
Standard
J2975_201505
This procedure describes a method for generating, preparing and analyzing samples of new and unused brake friction materials for their chemical constituents.
2015-05-07
Standard
AMS5503F
This specification covers a corrosion resistant steel in the form of sheet, strip, and plate.
2015-05-06
WIP Standard
AMS2631E
This specification covers the procedure for ultrasonic inspection of wrought titanium and titanium alloy products 0.25 inch (6.4 mm) and over in cross-section (thickness) or diameter.
2015-05-06
Standard
AMSQQA200/8A
This specification covers the specific requirements for aluminum alloy 6061 bar, rod, shapes, tube, and wire produced by extrusion.
2015-04-30
WIP Standard
J2947
This SAE Recommended Practice defines and establishes mechanical property ranges for six grades of continuously cast high strength automotive sheet steels that can be formed, welded, assembled, and painted in automotive manufacturing processes.
2015-04-30
Standard
J1453/2_201504
The three parts of SAE J1453 cover material, dimensional, and performance requirements of steel O-ring face seal (ORFS) connectors for tubing and the O-ring face seal interface and nut portion of hose stem assemblies for nominal tube diameters of 6 mm through 38 mm and for nominal hose diameters 6.3 mm through 38 mm. SAE J1453-2 covers the requirements for “metric based” O-ring face seal connectors to metric stud ends along with the associated adapters, bulkhead and union connectors. Metric hex wrenching flats are used throughout this standard.
2015-04-30
Standard
AMS03_17
This SAE Standard specifies the requirements for the electro-deposition of gold on ferrous-base materials, copper-base materials, aluminum-base materials, zinc-base materials and nickel-base materials for MOD use. It is primarily intended for use on electrical and electronic items which are to be plated with gold to: a. Increase the electrical conductivity of the surface. b. Provide a solderable surface. This Standard does not cover the gold plating of threaded items.
Viewing 1 to 30 of 18576

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