This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 degree F (-54 to 71 degree C) at high cyclic speeds 300 cpm (13 fpm) for liners with a thickness less than 0.015 inch. The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qua
SAE AS 82819-2013由美国机动车工程师协会 US-SAE 发布于 2013-05-08。
SAE AS 82819-2013 在中国标准分类中归属于: V22 机械配件、构件,在国际标准分类中归属于: 49.035 航空航天制造用零部件。
* 在 SAE AS 82819-2013 发布之后有更新,请注意新发布标准的变化。
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