Ice Accretion on Rotary-Wing Unmanned Aerial Vehicles—A Review Study

Abstract

Ice accretion on rotary-wing unmanned aerial vehicles (RWUAVs) needs to be studied separately from the fixed-wing UAVs because of the additional flow complexities induced by the propeller rotation. The aerodynamics of rotatory wings are extremely challenging compared to the fixed-wing configuration. Atmospheric icing can be considered a hazard that can plague the operation of UAVs, especially in the Arctic region, as it can impose severe aerodynamic penalties on the performance of propellers. Rotary-wing structures are more prone to ice accretion and ice shedding because of the centrifugal force due to rotational motion, whereby the shedding of the ice can lead to mass imbalance and vibration. The nature of ice accretion on rotatory wings and associated performance degradation need to be understood in detail to aid in the optimum design of rotary-wing UAVs, as well as to develop adequate ice mitigation techniques. Limited research studies are available about icing on rotary wings, and no mature ice mitigation technique exists. Currently, there is an increasing interest in research on these topics. This paper provides a comprehensive review of studies related to icing on RWUAVs, and potential knowledge gaps are also identified.

Conceptual Design of Cost-Effective Ice Detection System Based on Infrared Thermography

“…In aviation, supercooled water droplets convert into ice upon surface impingement and change the aerodynamics of aircraft (Muhammed and Virk, 2022;Szilder and Yuan, 2017;Muhammed and Virk, 2023a). Rotorcrafts endure ice accretion on propellers and vital engine parts (Cao and Chen, 2016;Muhammed and Virk, 2023b). In railways, precipitation icing may cause flashovers and derailment and hence disruption to rolling stock (Network Rail, n.d.;Kandelin, 2021;Qi et al, 2022).…”