The invention discloses a normal
brake system used for an
airplane and having take-off line
brake capability. The normal
brake system comprises a
hydraulic brake valve, an electric valve, an electro-hydraulic
servo valve, an anti-slip control box, a hydraulic switch and a speed sensor, wherein the
hydraulic brake valve is mounted near a pedal mechanism under a bottom plate of a
cockpit, controlled by operation of stepping on a brake pedal by a
pilot and used for outputting a required
brake pressure; the electric valve is mounted on a hydraulic pipeline at the downstream part of the
hydraulic brake valve; the electro-hydraulic
servo valve is mounted on a hydraulic pipeline at the downstream part of the electric valve; the anti-slip control box is mounted in a main
landing gear cabin and powered by a power supply on the
airplane; the hydraulic switch is mounted on a hydraulic pipeline between the hydraulic brake valve and a first oil inlet of the electric valve. The normal brake
system can meet a braking demand of an existing normal brake system of the
airplane on a take-off line, is reasonable in structure, simple, convenient, feasible, consistent with a man-
machine engineering principle and favorable for reducing the burden of the
pilot, and eliminates accident potentials caused by false operation of switching on a take-off line brake switch.