An Electro‑thermal De‑icing Model and Simulation Analysis Considering Ice Shedding
The electro‑thermal anti/de-icing systems have high heating efficiency and relatively simple structures, marking them as a key development direction for future icing protection. Existing simulation algorithms for electro-thermal de-icing seldom delve into comprehensive ice accretion-melting-deicing models that account for ice shedding. Therefore, the detachment behavior of ice layers during the heating process requires in-depth research and discussion. This paper physically models the phenomenon of ice shedding, incorporates the detachment behavior of ice layers during heating, improves the existing mathematical model for electro-thermal de-icing calculations, establishes an ice accretion-melting-deicing model for electro-thermal de-icing systems, and conducts numerical simulation, verification and optimization analysis of electro-thermal de-icing considering ice shedding. Through multi-condition de-icing numerical simulations of a specific wing model, it is found that ambient temperature can serve as a factor for adapting the electro heating anti/de-icing strategy to the environment. An optimization of heating heat flux density and heating/cooling time is conducted for the wing de-icing control law under the calculated conditions. The improved electro-thermal de-icing model and algorithm developed in this paper provide solid technical support for the design of electro-thermal de-icing systems.
Institutions
- Aviation Industry Corporation of China (China) (CN)
- Beihang University (CN)
Publication Details
- Journal
- SHILAP Revista de lepidopterología
- Published
- 2025-04-01
- DOI
- https://doi.org/10.16356/j.1005-1120.2025.02.002
- Primary Topic
- Icing and De-icing Technologies
- Type
- article
- Field-Weighted Citation Impact
- 0.00