The present invention relates to the field of
aviation technology, specifically to a transfer device for an aircraft lubricating oil
system, comprising a mounting seat, a stand fixed on the mounting seat, a filter box and a
heat sink, wherein a pump wheel 1 is fixed on the filter box, a
cantilever is fixed on the stand, a pump wheel 2 is fixed on the
cantilever, a shaft rod is connected to the
heat sink for fixed axis rotation, the upper end of the shaft rod is vertical and fixedly connected to one end of a swing rod, the pump wheel 1, the pump wheel 2, the filter box and the
heat sink are connected through pipelines, a filter purification mechanism is arranged in the filter box, a heat dissipation structure is arranged on the heat sink, a circulation mechanism is arranged on the stand, the pump wheel 1 and the pump wheel 2 are connected through a
sprocket assembly, the pump wheel 2 is connected to the filter purification mechanism, the
sprocket assembly is connected to the swing rod, and the circulation mechanism is connected through the swing rod. The transfer device for an aircraft lubricating oil
system can remove impurities in the lubricating oil and cool it down, thereby improving the service life and working reliability and stability of each component.