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Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels
- Aerospace Standard
- AS666D
- Cancelled
Sector:
Issuing Committee:
Language:
English
Scope
This AS applies to the cavity design and the selection of O-rings for tubeless tire wheels.
Rationale
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.
Recommended Content
| Aerospace Standard | Thermal Sensitive Inflation Pressure Release Devices for Tubeless Aircraft Wheels |
| Aerospace Standard | Replacement and Modified Brakes and Wheels |
| Technical Paper | Tire Development by Dedicated Involvement |
Data Sets - Support Documents
No Datasets Available
Issuing Committee
Reference
| Number | Title |
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