Anti- and de-icing Methods tor rotorcraft applications: a critical review

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TypeTechnical Report
Series titleLaboratory Technical Report; no. LTR-SMPL-2004-0175
Physical description61 p.
AbstractIn-flight and ground icing has historically posed a significant problem for all types of aircraft, and has been determined to be the cause of numerous accidents. Canadian airspace is especially hazardous as air temperatures are typically sub-zero, leading to ripe conditions for the onset of icing. Ice accretion on the leading edge and other areas of wings, fuselage, windows, engine inlets, and sensors degrade the aerodynamic form of the aircraft, and results in decreased lift and a higher stall velocity. Multiple solutions to this problem have been developed and applied to fixed-wing and, to a lesser extent, rotary aircraft. Most of these applications have shown promise and some have already seen limited service time. However, all current applications have considerable disadvantages, specifically in terms of weight and power requirements. Rotorcraft are known to be particularly sensitive to in-flight icing due to the large effective distance the rotor blades travel compared to the effective distance that any component of a fixedwing aircraft travels. The lift generated by the rotor blades is extremely sensitive to the effective shape of the blade itself; therefore, it is imperative that ice is either prevented from forming, or effectively removed once formed. The majority of today's civil and military helicopters certified to fly in icing conditions are equipped with electro-thermal ice protection systems. Due to their proven record of reliability, durability and effectiveness versus the complete spectrum of other de-icing technologies developed, electro-thermal de-icing remains the favored solution after decades of research and development. However, due to the weight and considerable power consumption demands of an electro-thermal system, alternate anti- and de-icing methods have been intensely studied. This paper summarizes the numerous anti-/de-icing methods that have been studied and/or applied to rotorcraft to replace the electro-thermal systems and explores the feasibility of using shape memory alloy actuated systems as a more efficient means of rotorcraft de-icing.
Publication date
PublisherNational Research Council Canada. Institute for Aerospace Research
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
NoteStructures, Materials and Propulsion Laboratory
Peer reviewedNo
NPARC number23000207
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Record identifier2ba09001-874b-40ca-bc6d-e012e10ec31a
Record created2016-06-20
Record modified2016-10-03
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