AS6235B Face Seal Gland Design, Static, O-Ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications
Revised
11/09/2021
- Features
- Issuing Committee
- 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 dash size range as AS4716 and AS5857 where applicable.
- Content
- 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.
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- Citation
- SAE International Technical Standard, Face Seal Gland Design, Static, O-Ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications, SAE Standard AS6235B, Revised November 2021, Issued September 2014, https://doi.org/10.4271/AS6235B.