The invention relates to a testing device in the
aviation field, in particular to a
liquid drop and
solid plate
oblique collision testing device. The problems that an oil drop and
cavity wall collision
visual test cannot be carried out in an existing aircraft engine bearing cavity
test platform, the physical variance of the adjustment scopes of parameters such as
liquid drop sizes of other
liquid drop and
solid wall face collision testing devices and a bearing cavity project is large, the device is complex in structure and high in cost are solved. According to the technical scheme, the liquid drop and
solid plate
oblique collision testing device is built and comprises a supporting frame, a liquid drop generation component, an angle-adjustable solid plate component, an oil return component and a lighting pick-up
system, the dropping diameters of liquid drops are changed by changing
syringe needles of the liquid drop generation component, and the dropping speed of the liquid drops is changed by changing the distance between the liquid drop generation component and a collision plate in a sliding mode; oblique angles of the collision plate can be continuously changed. By means of the liquid drop and solid plate
oblique collision testing device, the splashing critical working condition caused after the liquid drop and solid plate oblique collision happens is conveniently determined,
visual observation on the oil drop and
cavity wall collision can be achieved, and cost is reduced.