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Gland Design, O-ring and Other Seals
- Aerospace Standard
Published December 12, 2017 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Standard (AS) provides standardized gland (groove) design criteria and dimensions for O-ring seal glands for static and dynamic applications, and other seals.
Revision C of this document reflects various technical and editorial corrections and improvements identified during its Five-Year Review.
|Aerospace Standard||Gland Design, O-Ring and Other Elastomeric Seals, Static Applications|
|Aerospace Standard||Hydraulic and Pneumatic Retainers (Backup Rings), Polytetrafluoroethylene (PTFE) Resin|
|Aerospace Standard||Gland Design: Nominal 3/8 Inch Cross Section for Compression-Type Seals|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Table 1A||Standard gland dimensions and O-ring squeeze in inches|
|Table 1B||Standard gland dimensions and O-ring squeeze in millimeters|
|Table 2A||Standard groove width for zero, one, and two backup in inches|
|Table 2B||Standard groove width for zero, one, and two backup in millimeters|
|Table 3||Groove wall angle details|
|Table 4||Groove break edge details|
|Table 5||Standard groove corner radius dimensions in inches and millimeters|
|Table 6||Surface roughness requirements|
|Unnamed Dataset 11|
|Table 7A||Standard gland diametral clearance dimensions in inches|
|Table 7B||Standard gland diametral clearance dimensions in millimeters|
|Table 8||Run-out for standard glands in inches and millimeters|
A6C2 is responsible for the development of standards, processes, and practices related to Seals, Scrapers and Bearings used in actuation systems for Commercial and Military air vehicles. The panel provides a forum for government engineers, prime contractors, OEMs and suppliers to exchange technical information, regulatory updates, recent technology developments, issues related to system development and in service operation and lessons learned.
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