AS6235A Face Seal Gland Design, Static, O-ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications

Revised

12/19/2015

Features
Issuing Committee
Scope
Content
This SAE Aerospace Standard (AS) specifies standardized gland design criteria and dimensions for static face seals for internal pressure and external pressure applications for aerospace hydraulic and pneumatic applications using the same size range as AS4716 and AS5857 where applicable. Some small diameter sizes are excluded because they are not practical.
The glands have been specifically designed for applications using AS568 size elastomeric O-rings with related Class 2 tolerances at nominal system operating pressures up to 3,000 psi (20,680 kPa) utilizing no anti-extrusion (backup) rings.
While the gland dimensions herein have been designed for pressures up to 3,000 psi (20,680 kPa) these glands may be used for higher pressures, but extra precautions need to be taken and testing should be performed to ensure integrity of performance.
This specification covers the basic design criteria and recommendations for use with standard size elastomeric O-rings, however, these glands are also suitable for use with other elastomeric and polytetrafluoroethylene (PTFE) based seal geometries.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS6235A
Pages
78
Citation
SAE International Technical Standard, Face Seal Gland Design, Static, O-ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications, SAE Standard AS6235A, Revised December 2015, Issued September 2014, https://doi.org/10.4271/AS6235A.
Additional Details
Publisher
Published
Dec 19, 2015
Product Code
AS6235A
Content Type
Technical Standard
Status
Revised
Language
English

Revisions