Aircraft structure surface inspection system and method for aircraft strength test
The invention belongs to the technical field of whole aircraft strength tests, and particularly relates to an aircraft structure surface inspection system and method for aircraft strength tests, and the system comprises two-dimensional code labels arranged in corresponding detection areas; the track...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention belongs to the technical field of whole aircraft strength tests, and particularly relates to an aircraft structure surface inspection system and method for aircraft strength tests, and the system comprises two-dimensional code labels arranged in corresponding detection areas; the track inspection system is provided with a track and a sliding mechanism; an MEC server; the control end is used for controlling the MEC server to send out the test inspection task information; and the visual identification module is arranged on the sliding mechanism and is used for scanning the two-dimensional code label, carrying out two-dimensional shooting and 3D scanning on the corresponding detection area, superposing a shot image with time and position information and then transmitting the superposed image to the MEC server. According to the aircraft structure surface inspection system and method, the inspection result and the inspection position are fused and stored to facilitate retrieval and inspection, rapid |
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