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Two Aileron Types

机译:两种副翼类型

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摘要

To help reduce the likelihood of wing tip stall and adverse yaw, engineers developed differential ailerons. As the name implies, they deflect by different amounts: When the stick or yoke is moved to the right, for example, the aileron on the right (descending) wing is deflected up much more than the left (ascending) wing's aileron is deflected down. This basic design is depicted in Figure 2, at right. The reason differential aileron movement works is that deflection of an aileron upward can't do much harm; it is the aileron deflected downward that can be the "troublemaker," i.e., the one possibly precipitating a wing-tip stall. Additionally, a design incorporating differential aileron deflection works to minimize adverse yaw, the tendency of the ailerons to pull the airplane's nose around to the opposite side of the intended direction of turn.
机译:为了帮助减少机翼尖端失速和不利偏航的可能性,工程师们开发了差分副翼。顾名思义,它们会偏转不同的角度:例如,当棍子或or架向右移动时,右侧(下降)机翼的副翼向上偏转的幅度要大于左侧(上升)机翼的副翼向下偏转的幅度。 。此基本设计如图2所示。副翼差动原理起作用的原因是,副翼向上偏转不会造成太大伤害。向下偏转的副翼可能是“麻烦制造者”,即可能使机翼尖端失速的机翼。此外,结合差动副翼偏转的设计可最大程度地减少不利的偏航,即副翼将飞机机头拉向预期转弯方向的相反侧的趋势。

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    《Aviation safety》 |2014年第11期|9-9|共1页
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