Dynamic monitoring device for fatigue cracks of aircraft engine on hightemperature test rig
AssigneeEddysun (Xiamen) Electronics Co., Ltd.
InventorsJunming Lin, Zesen Lin
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AssigneeEddysun (Xiamen) Electronics Co., Ltd.
InventorsJunming Lin, Zesen Lin
Estimating the term…
A dynamic monitoring device for fatigue cracks of an aircraft engine on a high-temperature test rig includes a profiled housing, an eddy current testing sensor, a signal processing module, a wireless communication module, and a miniature centrifugal cooler which are encapsulated inside the profiled housing. A detection end face of the profiled housing includes a plurality of miniature air film holes, and the plurality of miniature air film holes cooperate with the miniature centrifugal cooler to form a cooling air film. An inner side wall and an outer side wall of the profiled housing respectively includes a built-in water cooling pipe and an external wind-guide channel to enhance a cooling effect. The eddy current testing sensor includes a ferrite core and insulated wires wound around the ferrite core, which can effectively detect tiny fatigue cracks.
A dynamic monitoring device for fatigue cracks of an aircraft engine on a test rig configured to use a testing method of a monitoring device and a test spindle forming asynchronous relative motion under simulated high-speed rotation, wherein:
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