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Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels
- Aerospace Standard
Published January 06, 2011 by SAE International in United States
This AS applies to the cavity design and the selection of O-rings for tubeless tire wheels.
This document has not been maintained. The document's primary purpose was to provide instructions for designing a static seal gland and o-ring for the wheel halves. Modern wheel static seal gland & o-ring design must take into account the wheel size, use, environment and type (for example demountable flange). The designs depend on these factors such that the designs will vary for different applications as opposed to having one design for all applications as AS 666 specifies.
|Aerospace Standard||Thermal Sensitive Inflation Pressure Release Devices for Tubeless Aircraft Wheels|
|Technical Paper||Tire Development by Dedicated Involvement|
|Technical Paper||Mechanical Properties of Radial-Ply Aircraft Tires|
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