Browse Topic: Iron
An optimized design, fabrication and testing solution is presented for flexible drive systems. A single piece welded drive shaft as well as a system consisting of sub and supercritical shafts, couplings and bearing hangers (for Tail Drive System in Helicopters and Interconnect Drive Systems in Tiltrotors) are included. This solution facilitates the qualification for flight of the drive shaft in airframes with reduced iron bird and expensive flight testing on the airframe. This solution also provides opportunities for improvements during the prototype phase such that potential deficiencies are identified and corrected before the drive shaft is put into service. An important part of the testing is accelerated testing, not in terms of operational life, but in terms of reliability. Theoretical Life of a flexible drive shaft is 'infinite' by design. 2.0
This specification covers an iron-nickel alloy in the form of strip 0.020 to 0.250 inch (0.51 to 6.35 mm) inclusive, in thickness (see 8.8).
This specification covers an iron-nickel alloy in the form of bars, forgings, flash-welded rings, and stock for forging, flash-welded rings, or heading.
The purpose of this SAE Information Report is to provide automotive engineers and designers with a concise statement of the basic characteristics of cast iron under elevated temperature conditions. As such, the report concentrates on general statements regarding these properties with limited illustrative data, anticipating that those who may be interested in more detail will want to use the bibliography provided at the conclusion of the report.
This standard describes general and detailed methods of sampling and testing for surface passivity of corrosion-resistant steel parts. These tests may also be useful to determine if there is a need for passivation.
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