A plain-language guide to O-ring gland design: what squeeze, stretch and gland fill mean, the AS568 / ISO 3601 size and tolerance system, and the limits that keep a seal working.
AS568 (the US aerospace size standard) and ISO 3601 (its international counterpart) define the standard O-ring sizes — the inside diameters and cross-sections you can actually buy off the shelf — along with their dimensional tolerances. When someone specifies a "-214 O-ring," that dash number is an AS568 size. Designing a seal is mostly about choosing one of these standard rings and then cutting a groove (the "gland") around it that squeezes it the right amount.
Under pressure, an O-ring is pushed against the low-pressure side of the groove and tries to squeeze out through the clearance gap between the mating parts. Whether it survives depends on the clearance gap, the pressure, and the rubber hardness — a harder compound (higher Shore A) resists extrusion better. Design guides tabulate permissible extrusion clearances against those variables; exceed them and the ring shaves itself away.
A gland calculation stacks these effects: the standard AS568 / ISO 3601 size and its tolerance, the stretch from the groove diameter (which thins the effective cross-section), the resulting squeeze against the groove depth, and the gland fill against the groove width. A rigorous check runs the worst case — every tolerance stacked at its unfavourable limit simultaneously — because that's the combination that actually shows up on a bad-but-in-spec part. Tolerances come from the AS568 / ISO 3601-1 Class A tables; ISO 286 fits on the bore and groove add their own contribution.
A fully worked static radial-seal gland (stretch, effective cross-section, squeeze and fill), plus a checklist for specifying a gland that seals and survives.
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