Re: LS1 midspan hinge repair
Vern,
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These center hinges have failed before. Steel is a lot better in fatigue than Al but if the inflight stress levels are close to the limit it is an insidious problem. It is obviously not a shear failure of they would be breaking upon loading. Reducing stress is the only answer. This is a materials problem. Either increase cross section, increase load transfer points, or redesign like Jay has done. Fatigue = repeated cyclic loading below the yield point internal material flaws move to high stress areas over time resulting in cracks and final failure at loads below the design point. My $0.02 worth of armchair analysis. Regards, On Monday, May 9, 2022, 4:47 AM, Frankenbird Vern <smeshno1@...> wrote:
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