The present invention relates to the field of high-altitude
simulation test equipment for aircraft engines, and discloses a
gas mixing device for air environment
simulation test, including a positive three-way
pipe fitting and a mixing structure, wherein the mixing structure is arranged in the positive three-way
pipe fitting, and a radial hanging plate is arranged in the main
pipe of the positive three-way
pipe fitting, and the end of the mixing structure is inserted from the
branch pipe of the positive three-way
pipe fitting, and contacts with the inner wall of the main pipe after passing through the hanging plate. The mixing structure includes a multi-layer mixing component arranged along the radial direction of the main pipe, a low-pressure gas channel is arranged between two adjacent
layers of mixing components, a high-pressure gas channel perpendicular to the low-pressure gas channel is arranged in the mixing component, and a spray structure connecting the low-pressure gas channel and the high-pressure gas channel is opened on the mixing component. The
gas mixing device of the present invention can solve the technical problems that the existing mixing device is prone to separation or vortex, the inlet air flow field is extremely uneven, etc., resulting in poor
mixing effect, and the mixing device has a large pressure loss and cannot meet the engine
inlet pressure requirement.