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Method for detecting robustness in vibration of equipment in aircraft, involves applying one of two gaps determined from set of vibratory sections to equipment to detect robustness of equipment
Method for detecting robustness in vibration of equipment in aircraft, involves applying one of two gaps determined from set of vibratory sections to equipment to detect robustness of equipment
The method involves determining a gap in vibratory sections selected from a set of vibratory sections resulting from specifications by a determination unit. Another gap of other vibratory sections is determined from the former gap by transforming the former gap of the former vibratory sections into fatigue damage spectra using another determination unit. The latter gap of the latter vibratory sections is applied to an equipment to detect robustness of the equipment. An independent claim is also included for a device for detecting robustness in vibration of equipment, comprising a determination unit.
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