SAE AS666D
Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels
SAE International , 01/06/2011
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This document has been declared "CANCELLED" as of January 2011. By this action, this document will remain listed in the Numercial Section of the Aerospace Standards Index.
This document has not been maintained. The documents 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.
This document has not been maintained. The documents 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.
Product Information
Published:
01/06/2011
File Size:
1 file , 530 KB
Language:
English
Note:
This product is unavailable in Ukraine, Russia, Belarus
