Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels(Cancelled Jan 2011) AS666D

DOI: https://doi.org/10.4271/AS666D

Issuing Committee: A-5A Wheels, Brakes and Skid Controls Committee

Publisher: SAE International

Pages: 5

Rationale:This document has not been maintained. The document's primary purpose was to provide instructions for designing a static seal gland and o-ring for the wheel halves. Modern wheel static seal gland & o-ring design must take into account the wheel size, use, environment and type (for example demountable flange). The designs depend on these factors such that the designs will vary for different applications as opposed to having one design for all applications as AS 666 specifies.