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Plain Bearing Radial Limit and Ultimate Load Tests
- Aerospace Standard
Published November 12, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This test method outlines the recommended procedure for performing radial limit load and ultimate load tests on low speed airframe and high speed helicopter rotor head bearings.
This revision updates document formatting and document references to align with the latest publications.
|Aerospace Standard||Plain Bearing High Speed Oscillation Test|
|Aerospace Standard||Plain Bearing Lined Inside Diameter Plug Gaging|
|Aerospace Standard||Plain Bearing Low Speed Oscillation Test|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Table 1||Sample format of test data sheet|
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.|
|ISO 10012-1||This document is not part of the subscrption.|
|ISO10012/1||This document is not part of the subscrption.|
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