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WASHER, FLAT, COUNTERSUNK CORROSION AND HEAT RESISTANT STEEL (UNS S66286)

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS9768
  • Current
Published 2019-12-27 by SAE International in United States

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PIN, STRAIGHT, HEADLESS, DOWEL - CORROSION AND HEAT RESISTANT STEEL (UNS S66286), STANDARD AND OVERSIZE

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS9390D
  • Current
Published 2019-12-27 by SAE International in United States

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Design Methodology for Motor Thermal Management in Vehicle Electrification

NISSAN AUTOMOTIVE TECHNOLOGY CO., LTD.-Kengo Sakao
Nissan Motor Co., Ltd.-Yoshikazu Tsuruoka, Masaaki Kubo, Tsuyoshi Yamamuro
  • Technical Paper
  • 2019-01-2368
Published 2019-12-19 by SAE International in United States
In order to improve the accuracy of the coil temperature prediction, detailed fundamental experiments have been conducted on thermal resistances that are caused by the void air gap and contact surfaces. The thermal resistance of the coil around the air gap can be calculated by an air gap distance and air heat conductivity. Contact surface thermal resistance between the core and the housing was constant regardless of the press-fitting state in this experiment. Prediction accuracy of the coil temperature is improved by including the heat resistance characteristics that is obtained by the basic experiment to conjugate heat transfer analysis model.
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Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steels and Alloys Wrought Products and Forging Stock

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS2371L
  • Current
Published 2019-12-17 by SAE International in United States

This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable material specification requirements of wrought corrosion and heat-resistant steel and alloy products and of forging stock.

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Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 74Ni - 15.5Cr - 8.0Fe

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5665P
  • Current
Published 2019-12-17 by SAE International in United States

This specification covers a corrosion and heat resistant nickel alloy in the form of round bars over 2.50 to 4.50 inches (over 63.5 to 114.3 mm), inclusive, in nominal diameter, forgings over 2.50 inches (63.5 mm) in nominal thickness, other bars and forgings, flash welded rings, and stock for forging or flash welded rings (see 8.6).

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Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing, 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) 0.90Ti - 0.50Al - 18Fe, Consumable Electrode Remelted or Vacuum Induction Melted, 1775 °F (968 °C) Solution Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5589G
  • Current
Published 2019-12-13 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD with nominal wall thickness 0.015 inch (0.38 mm) and over (see 8.6).

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Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings, 57Ni - 20Cr - 10Co - 8.5Mo - 2.1Ti - 1.5Al - 0.005B, Vacuum Induction and Consumable Electrode Melted, Solution Heat Treated, Precipitation Heat Treatable

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5915A
  • Current
Published 2019-12-02 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and stock for forging.

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Titanium Alloy, Sheet and Strip 4Al - 2.5V - 1.5Fe Electron Beam Single Melted. Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6949A
  • Current
Published 2019-11-25 by SAE International in United States
This specification covers a titanium alloy in the form of sheet and strip up to 0.143 inches (3.63 mm), inclusive, in nominal thickness.
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Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Cold Drawn, and Aged

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5834E
  • Current
Published 2019-11-25 by SAE International in United States
This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.001 to 0.140 inch (0.025 to 3.56 mm) inclusive in nominal diameter supplied in straight lengths or coils (see 8.6).
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Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Solution Heat Treated and Cold Drawn

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5833E
  • Current
Published 2019-11-25 by SAE International in United States
This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.001 to 0.140 inch (0.025 to 3.56 mm) inclusive in nominal diameter supplied in straight lengths or coils (see 8.5).
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