Aircraft engine fuel nozzle sealing detection device
The utility model discloses a sealing detection device for a fuel nozzle of an aircraft engine, which comprises a rack, a water tank and a water pump are fixedly mounted on one side of the rack, a liquid inlet of the water pump is connected with the water tank through a pipeline, a liquid outlet is...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model discloses a sealing detection device for a fuel nozzle of an aircraft engine, which comprises a rack, a water tank and a water pump are fixedly mounted on one side of the rack, a liquid inlet of the water pump is connected with the water tank through a pipeline, a liquid outlet is fixedly connected with a water outlet hose, two sliding rails are fixedly mounted on the rack, and a detection table is arranged on the sliding rails. The bottom parts of two ends of the detection platform are provided with slide blocks which are clamped on the slide rails in a sliding manner, the rack is provided with a driving mechanism which drives the slide blocks to move horizontally, the detection platform is provided with a plurality of nozzle clamping grooves which are used for clamping and placing fuel nozzles, and the rack is fixedly provided with a support. The sealing detection device of the aircraft engine fuel nozzle solves the problems that in the prior art, fuel nozzles are not suitable for being de |
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