PULAOKHAO
Aerospace
- Jan 18, 2012
- 4
AS-5857A "GLAND DESIGN, O-RING AND OTHER ELASTOMERIC SEALS, STATIC APPLICATIONS", Table-6, page-37, lists 32 micro-inch max for O-ring groove dia & 63 micro-inch max for groove sides. It does not lists any restrictions on the min side.
Is anyone aware of any drawbacks for a radial, static O-ring seal in a gaseous system where the pressure difference across the seal does not exceed 1 atmosphere if the groove surface is very smooth [less than 1 micro-inch Ra]?
The squeeze is 27%; O-ring elastomer is butyl; 3.5 inch dia and 0.070 inch cross section
Is anyone aware of any drawbacks for a radial, static O-ring seal in a gaseous system where the pressure difference across the seal does not exceed 1 atmosphere if the groove surface is very smooth [less than 1 micro-inch Ra]?
The squeeze is 27%; O-ring elastomer is butyl; 3.5 inch dia and 0.070 inch cross section