Avionics module anti-seismic detection device
The utility model discloses an avionics module anti-seismic detection device which comprises a test box body and a module to be detected arranged in the test box body, and the top surface and the bottom surface of an inner cavity of the test box body are correspondingly provided with at least one lo...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model discloses an avionics module anti-seismic detection device which comprises a test box body and a module to be detected arranged in the test box body, and the top surface and the bottom surface of an inner cavity of the test box body are correspondingly provided with at least one locking groove. The top and the bottom of the to-be-tested module are respectively provided with an elastic locking strip which is elastically clamped with the locking groove. An air inlet device is arranged at the top of the test box body, air duct baffles are arranged at the positions, located on the two sides of the locking groove, in the inner cavity of the test box body respectively, and an air duct communicated with the air inlet end of the air inlet device is formed between the two air duct baffles; one side of the test box body is provided with a circuit board installation box, and one side of the circuit board installation box is provided with an external aviation plug interface. According to the utility mod |
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