[Aerospace-related Contracted Vibration Test Case] Electronic Components

Conducted a random 3-axis simultaneous vibration test! A case where the cause of electronic component failure was clarified.

We would like to introduce a case study of vibration testing related to aircraft that our company conducted. For electronic components used in aircraft that experienced operational failures, we verified whether the issues could be reproduced through a three-axis simultaneous vibration test, which is closer to real environmental conditions, rather than a single-axis vibration test. While conducting a random three-axis simultaneous vibration test with the electronic component under power, we observed failures in the signal transmission of the electronic component. This verification allowed us to clarify the cause of the failure of the electronic component in question. [Test Specimen] ■ Name: Electronic Component for Aircraft ■ Weight: 17kg (including mounting fixture) ■ Dimensions: Approximately 300mm(W) x 200mm(D) x 150mm(H) *For more details, please refer to the PDF document or feel free to contact us.

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