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The sukitsudo slide prevention braking system by the deceleration which possesses directional stability

机译:具有方向稳定性的减速的寿喜堂防滑制动系统

摘要

(57) Abstract Dextral and the sukitsudo sliding prevention braking system for the aircraft where directional stability is superior the inside of the left brake pedal deceleration instruction (19 and 119) keeps being chosen making use of the common deceleration instruction (16) is offered. Alteration the common deceleration instruction (16) which is chosen making use of each brake pedal deceleration instruction (19 and 119), each side wheel speed instruction is granted, differential braking function (36 and 136) is granted, when using each deceleration instruction because of this the left of the aircraft and vis-a-vis the dextral wheel brake, the instability which has the fear which it occurs is removed.
机译:(57)<方向>方向稳定性优于飞机的右手侧和寿喜堂防滑动制动系统,始终使用通用减速度指令(16)选择左制动踏板减速度指令(19和119)内部提供。更改使用每个制动踏板减速指令(19和119)选择的通用减速指令(16),授予每个侧轮速度指令,授予差动制动功能(36和136),因为使用每个减速指令是因为在飞机的左侧和右手轮制动器之间,消除了可能发生的不稳定性。

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