The invention belongs to the technical field of
aviation, and particularly relates to an engine bearing cavity ventilation
system simulation calculation method considering pump suction performance, which is based on a flow
simulation calculation platform and adopts elements such as a cylindrical pipeline, an
elbow, a transition joint, a throttling hole, a flow source, a pressure source, a controller and a
signal collector. Components such as a pipeline, a sealing device, a bearing cavity and a lubricating
oil pump set are represented, an engine bearing cavity ventilation
system simulation calculation model considering pump suction characteristics is constructed, parameters such as pressure and ventilation quantity of the bearing cavity can be accurately calculated, and the influence mechanism of the parameters such as structures, flow, pressure and throttling hole diameters of different components on the ventilation
system is revealed. According to the scheme, modular elements are adopted, the system
layout and related parameters can be conveniently and rapidly adjusted, the design accuracy and calculation efficiency of the bearing cavity scheme are improved, and the high cost generated by redeveloping a new ventilation system is reduced.