The invention relates to a fuel-tank
inert gas control device, which belongs to the field of aero-technology. The fuel-tank
inert gas control device comprises a small flow limit hole, a small flow pipeline, a small
check valve, a
safety valve, a large
check valve, a pressure
reducer, a large flow limit hole, a large flow pipeline, and a block valve and the like, wherein in the two
inert gas pipelines, one is used for controlling the normally-open feeding of the
inert gas with
low oxygen content and low flow under the action of the flow limit holes, and the other one is used for controlling the discontinuous feeding of the
inert gas with
high oxygen content and large flow according to the pressure demands of the
fuel tank through the cooperation of the flow limit holes, the pressure
reducer and the block valve. Through the cooperation among the flow limit holes and the pressure
reducer and the like, the fuel-tank
inert gas control device has the advantages of realizing the
oxygen content and pressure controls of the inert gas in the
fuel tank, and improving the working reliability. Meanwhile, the
oxygen content control of the inert gas in the
fuel tank has a larger margin and can reduce the requirements for
oxygen content of the feed gas when the plane drops, so the fuel-tank inert gas control device can reduce the scale of the air separator, and reduce the cost and weight thereof.