This Aerospace Information Report (AIR) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 steel, AMS 4944 titanium and MIL-T-7081 aluminum alloy, mounted as free-free resonant beams. Of particular advantage are the inherent simplicity of test setup, minimum restraint from a test fixture, low power requirements, short test duration and ease of varying stress level.
SAE AIR 1529A-1989由美国机动车工程师协会 US-SAE 发布于 1989。
SAE AIR 1529A-1989 在中国标准分类中归属于: V21 管件、卡箍、密封件,在国际标准分类中归属于: 49.080 航空航天用流体系统和零部件。
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