The Problem with Trim Tabs

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The Problem with Trim Tabs

机译：修剪选项卡的问题

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In the 2011 fatal accident, the elevator trim tabs began fluttering due to wear on part of the linkage. With the loss of an effective trim system, the aircraft abruptly pitched up with as much force as 17 Gs, which caused the pilot to black out. (After the pitch up, the trim tab separated from the left elevator.) In 1998, the P-51 Voodoo Chile also lost its left elevator trim tab, pitching up with a 10-G force that incapacitated the pilot, though he came to in time to land safely.

机译：在2011年的致命事故中，由于连杆机构部分磨损，电梯装饰片开始飘动。由于缺少有效的修剪系统，飞机突然以高达17 Gs的力俯仰，这导致飞行员停电。（俯仰后，装饰片与左电梯分开。）1998年，P-51智利伏都教也失去了左电梯的装饰片，以10G的力向上倾斜，使飞行员无能为力，尽管他来了。及时降落。

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《Air and Space》 |2013年第6期|41-41|共1页
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2. Optimal trim control of a high-speed craft by trim tabs/interceptors Part I: Pitch and surge coupled dynamic modelling using sea trial data [J] . Ertogan Melek, Wilson Philip A., Tayyar Gokhan Tansel, Ocean Engineering . 2017,第jana15期

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The Problem with Trim Tabs

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