多旋翼无人飞行器结冰与天然过冷云中液态水含量测量的相关性

IF 3.8 2区 工程技术 Q1 ENGINEERING, CIVIL Cold Regions Science and Technology Pub Date : 2024-06-27 DOI:10.1016/j.coldregions.2024.104262
Anna J. Miller , Christopher Fuchs , Nadja Omanovic , Fabiola Ramelli , Patric Seifert , Robert Spirig , Huiying Zhang , Emilie Fons , Ulrike Lohmann , Jan Henneberger
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引用次数: 0

摘要

大气结冰(冰在表面的累积)是航空业严重关切的问题。除冰和结冰预测工具是飞行员确保飞行安全所必需的,虽然大型飞机结冰已有成熟的技术,但小型无人驾驶飞行器(UAV)还需要更多的研究。在此,我们介绍了一架多旋翼无人飞行器在冬季低层云中 59 次飞行的测量结果,当时的温度在 -3 至 -10 °C 之间。无人飞行器配备了旋翼加热装置,可在结冰条件下飞行长达 10 分钟。结冰严重程度通过结冰期间电池电流的增加率进行量化,然后与液态水含量(LWC)的同步同位测量结果进行比较。液态水含量测量值(a)通过系留气球系统上的原位全息成像仪测量的云滴计算得出,(b)通过遥感观测(微波辐射计、气压计、云雷达)检索得出。我们的研究表明,在这些环境条件下,结冰与 LWC 在 0.02 至 0.5 g m-3 的范围内呈强烈的正相关,与温度和平均水滴大小无关,但直径为 50 μm 的水滴可能会导致结冰严重程度增加。我们还表明,从遥感中获取的 LWC 与现场测量结果非常吻合,这表明遥感测量可有效用于评估结冰状况。这些是已知的首次多旋翼无人飞行器结冰测量,并在自然云中进行了同位低纬度测量。
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Multirotor UAV icing correlated to liquid water content measurements in natural supercooled clouds

Atmospheric icing, the accumulation of ice on surfaces, is a severe concern for the aviation industry. Deicing and icing prediction tools are necessary for pilots to ensure flight safety, and while there is established technology for large aircraft icing, more research is needed for smaller uncrewed aerial vehicles (UAVs). Here, we present measurements from 59 flights of a multirotor UAV into wintertime low stratus clouds of temperatures between 3 and 10 °C. The UAV is equipped with rotor heating to allow flights up to 10 min in icing conditions. Icing severity was quantified by using the rate of increase in battery current during icing, and was then compared with simultaneous, co-located measurements of liquid water content (LWC). LWC measurements were (a) calculated from cloud droplets measured with an in situ holographic imager on a tethered balloon system and (b) retrieved from remote sensing observations (microwave radiometer, ceilometer, cloud radar). We show that, for these environmental conditions, icing was strongly positively correlated to LWC over an LWC range of 0.02 to 0.5 g m−3, independent of temperature and mean droplet size, though droplets >50 μm in diameter may contribute to increased icing severity. We also show that the LWC retrieved from remote sensing agrees well with the in situ measurements, indicating that remote sensing measurements can effectively be used to assess icing conditions. These are the first known measurements of multirotor UAV icing with co-located LWC measurements in natural clouds.

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来源期刊
Cold Regions Science and Technology
Cold Regions Science and Technology 工程技术-地球科学综合
CiteScore
7.40
自引率
12.20%
发文量
209
审稿时长
4.9 months
期刊介绍: Cold Regions Science and Technology is an international journal dealing with the science and technical problems of cold environments in both the polar regions and more temperate locations. It includes fundamental aspects of cryospheric sciences which have applications for cold regions problems as well as engineering topics which relate to the cryosphere. Emphasis is given to applied science with broad coverage of the physical and mechanical aspects of ice (including glaciers and sea ice), snow and snow avalanches, ice-water systems, ice-bonded soils and permafrost. Relevant aspects of Earth science, materials science, offshore and river ice engineering are also of primary interest. These include icing of ships and structures as well as trafficability in cold environments. Technological advances for cold regions in research, development, and engineering practice are relevant to the journal. Theoretical papers must include a detailed discussion of the potential application of the theory to address cold regions problems. The journal serves a wide range of specialists, providing a medium for interdisciplinary communication and a convenient source of reference.
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