The invention discloses an
air bridge balance air inlet and return
system integrated structure, a design method and an
assembly method, and belongs to the technical field of wind tunnel tests. The wind tunnel model structure design problem caused by the fact that an
air bridge balance air inlet and return
system is difficult to integrally arrange due to insufficient model space is solved. Two high-pressure air inlet pipelines and two low-pressure air return pipelines of the
air bridge pipeline are embedded into a
fuselage force-bearing piece in a gooseneck type air bridge
layout form, the high-pressure air inlet pipelines are connected with a flow
control unit, the flow
control unit is connected with a ventilation wing, the ventilation wing is connected with the low-pressure air return pipelines, and the low-pressure air return pipelines are connected with the low-pressure air return pipelines. And the high-pressure air inlet pipeline, the low-pressure air return pipeline and the internal strain balance are respectively connected with the supporting piece. According to the air bridge balance air inlet and return
system integrated structure, the design method and the
assembly method, the technical capability of
power simulation wind tunnel tests such as a TPS
nacelle and an air motor driving
propeller can be remarkably improved, and the air bridge balance air inlet and return system integrated structure plays an important role in improving the applicability and reliability of an air inlet and return air bridge system.