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ICE DETECTION CAPABILITIESUNDER AIRCRAFT POST DEICING CONDITIONS

机译:飞机后冰状况下的冰探测能力

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Human visual and tactile ice detection capabilities while inspecting deiced aircraft surfaces have not beenquantified. Six male professional deicers from AeroMag 2000 Montreal participated in the experiment. Weused a cold chamber to simulate one of the conditions experienced in the operational deicing environment.Ice samples were created by APS Aviation on white painted aluminum panels. Ice thicknesses ranged from0.2 mm to 1.0 mm and were covered with aircraft deicing fluid. We used a two-alternative forced-choiceprocedure in which we showed a deicer a panel, then a second panel, and finally asked him to indicate onwhich of the two ice was present. Our data showed that, within the range of thicknesses we presented,deicers were unable to visually detect ice of any thickness on the white painted panels, but could easilydetect ice using a tactile check.
机译:在检查飞机除冰表面时的人眼视觉和触觉冰检测能力尚未量化。来自AeroMag 2000 Montreal的六位男性专业除冰剂参加了实验。我们使用了一个冷室来模拟在操作除冰环境中遇到的条件之一。冰样是由APS Aviation在涂有白色油漆的铝板上制成的。冰的厚度范围为0.2毫米至1.0毫米,并覆盖有飞机除冰液。我们使用了两种选择的强制选择程序,在该程序中,给除冰器显示一个面板,然后显示第二个面板,最后让他指出两个冰中的哪个出现。我们的数据表明,在我们介绍的厚度范围内,除冰器无法在白色烤漆板上目视检测到任何厚度的冰,但可以通过触觉检查轻松检测到冰。

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