The performance of aviation lubricating oil gear pumps in high-altitude environments is crucial for the safe and reliable operation of aircraft. To obtain the high-altitude characteristic curves of lubricating oil gear pumps and analyze their influencing factors, a performance test platform for aviation lubricating oil gear pumps capable of simulating high-altitude environments from 0 to 12 km was established to investigate the high-altitude characteristics of the lubricating oil pumps. The results indicate that as the inlet pressure decreases, the flow rate exhibits a linear decline across different pressure conditions, while both torque and flow pulsation demonstrate a linear increase. Notably, when the inlet pressure is less than or equal to 30 kPa (corresponding to an altitude of ≥8.5 km) and the outlet pressure exceeds 2.2 MPa, the flow rate decreases sharply, accompanied by a sudden rise in torque and pulsation, along with a rapid increase in the internal lubricating oil temperature. As the rotational speed increases, the flow rate, volumetric efficiency, and torque under different inlet pressures exhibit linear growth. However, when the inlet pressure is less than or equal to 30 kPa (corresponding to an altitude of ≥8.5 km) and the rotational speed exceeds 1800 r/min, the flow rate and torque demonstrate slow growth, while the volumetric efficiency decreases sharply. Concurrently, the flow pulsation increases abruptly to 11.2 %. The high-altitude characteristic inflection points of the lubricating oil gear pump are determined to be approximately 1800 r/min and 30 kPa.
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