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Face Seal Gland Design, Static, O-Ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications
- Aerospace Standard
- AS6235B
- Revised
Sector:
Issuing Committee:
Language:
English
Scope
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 dash size range as AS4716 and AS5857 where applicable.
Rationale
AS6235 has been revised from Revision A to Revision B to:
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Reduce the groove edge breaks for pressures over 3000 psi (20690 kPa) to be similar to those in AS4716.
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Make some editorial improvements.
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Update references.
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Delete Appendices A, B, C, and E and include them in AIR7358; rename previous Appendix D to Appendix A herein.
Recommended Content
Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
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.
Reference
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