The invention belongs to the technical field of aircraft
heat management, and particularly relates to an active flow control
stamping heat dissipation
system which comprises an S-shaped air
inlet flow channel, a
heat exchanger, a
heat exchanger outlet injection
nozzle, a
heat exchanger outlet flow channel and a heat exchanger outlet flow channel
grating. An inlet of the S-bent air
inlet channel protrudes out of the surface of an
airplane, and is responsible for introducing ram air flow into the heat exchanger from an outlet after passing through the S-bent air
inlet channel and
cooling fluid on the hot side of the heat exchanger as a cold source on the
cold side of the heat exchanger. According to heat exchanger outlet flow data obtained through flow calculation, a set of injection spray pipes are arranged on the side, with the low flow speed, of the outlet, and high-pressure gas led out of an engine or an auxiliary power device
gas compressor is sprayed out of a
nozzle after being conveyed through a connecting pipeline and mixed with cold edge air at the outlet of the heat exchanger; the air is discharged out of the
machine through the grid at the outlet of the exhaust runner; due to the injection effect of the high-pressure
airflow, the high-pressure
airflow sprayed out of the injection spray
pipe can accelerate cold-side air at an outlet of the heat exchanger, so that the cold-side flow of the heat exchanger is increased, and the overall heat dissipation performance of the heat exchanger is improved. The invention can effectively solve the problems of non-uniform
inlet pressure and insufficient flow of the heat exchanger in the existing
stamping heat dissipation
system.