The invention belongs to the field of product mechanical structure design, and discloses a pneumatic
servo control type fan air valve which comprises a channel butterfly plate
assembly, a
pilot valve
assembly, a
torque motor assembly, a filter assembly, an upper die cavity assembly, a lower die cavity assembly and a pressure guide
pipe. Gas introduced by a pressure guiding
pipe sequentially passes through the filtering assembly and the
pilot valve assembly to enter the
torque motor assembly, the
torque motor assembly adjusts the opening degree and exhausts the gas according to the magnitude of applied current, the gas flow subjected to opening degree adjustment enters the upper membrane cavity assembly, and a membrane type
differential pressure structure is formed between the upper membrane cavity assembly and the lower membrane cavity assembly. The lower die cavity assembly controls the opening degree of the channel butterfly plate assembly according to the air pressure in the upper die cavity assembly, and the channel butterfly plate assembly is arranged on an
airplane pre-cooling air path. According to the invention, the torque motor with extremely high precision and small adjustable flow is applied to the high-flow butterfly plate channel, so that stepless adjustment and high-precision adjustment of the temperature of the aircraft air
source system are achieved, and the adjustment precision far exceeds the use requirement of + / -6 DEG C of a civil aircraft air
source system, specifically, the adjustment precision can be within + / -1 DEG C. The valve is high in dynamic stability, rapid in response and stable and reliable in quality, and the product can meet the requirement for temperature adjustment of a civil aircraft air
source system and can meet the requirement for the civil aircraft air source
system.