The invention relates to the field of aero-engines, in particular to an aero-engine lubricating oil monitoring structure and method. The structure includes a housing, an insulating sleeve, a fusible sheet, a
gasket, a sealing ring, an insulating bush, a stop ring, an
electrode, a
magnet, and an outer
bushing. Pin 3 of the cable plug is connected to the
magnet, and the cable plug The No. 2 pin in the outer
bushing is connected to the outer
bushing, the
magnet is fixed in the outer bushing, the outer bushing and insulating sleeve connected to each other are connected to the shell, and the fusible sheet is installed inside the outer bushing and outside the magnet in sequence from inside to outside ,
Gasket, sealing ring, insulating bushing and
electrode, fusible sheet,
gasket, sealing ring, insulating bushing and
electrode are fixed by the stop ring in the electrode collar groove. The invention realizes the simultaneous monitoring of the magnetic
metal shavings in the oil and the temperature of the oil by setting the
magnetic poles and the fusible sheet, and can be overlapped with an online detection
system, and can be applied to the monitoring of lubricating oil at key parts of various types of engines.