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Rolling Element Test Method for Axial Limit and Fracture Load Testing
- Aerospace Standard
Published October 10, 2007 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This test method outlines the recommended procedure for performing static axial limit and ultimate load tests on rolling element bearings used in airframe applications. Bearings covered by this document shall be antifriction ball bearings and spherical roller bearings in either annular or rod end configurations.
ARP5483/4 is a conversion of the MIL-STD-2159 (which had only been issued previously in draft form).
Data Sets - Support Documents
|Unnamed Dataset 1|
ACBG Rolling Element Bearing Committee
The objective of the Airframe Control Bearing Group (ACBG)is to provide industry experience and state of the art technology for airframe bearings, and issue as appropriate, published documents known as SAE Aerospace Standards. The focus of the Committees is present and future aircraft airframe control systems, bearings, and associated components.The ACBG shall be responsible for the preparation, development, maintenance and promotion of all relevant specifications, standards, and requirements for airframe bearings, control system components, and associated hardware used in the design and construction of aerospace mechanical systems and subsystems. The ACBG shall also coordinate with other organizations for lubricants, control cables, and locking devices and shall utilize and promote the use of specifications published by those organizations. The ACBG shall function as a forum for technology transfer as it affects the Airframe bearing and control systems industry and for the enhancement of distribution channels.
|ANSI/NCSLZ540-1||This document is not part of the subscrption.|
|ASTME4||This document is not part of the subscrption.|
|ASTME83||This document is not part of the subscrption.|
|ISO10012||This document is not part of the subscrption.|
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