JOURNAL ARTICLE

De-icing Aircraft Wings with Inflatable and Deflatable Rubber Boot Systems: A Review.

  • Published In: International Scientific Journal of Engineering & Management, 2025, v. 4, n. 3. P. 1 1 of 3

  • Database: Applied Science & Technology Source Ultimate 2 of 3

  • Authored By: Tadvi, Sahil; Bhamare, Rudra; Srivastava, Rakesh Kumar 3 of 3

Abstract

The article reviews inflatable and deflatable rubber boot systems as a mechanical method for de-icing aircraft wings, focusing on their operation, benefits, limitations, and recent technological advances. These systems use pneumatic inflation to crack and shed ice buildup, offering a simple, reliable, and cost-effective solution particularly suited for smaller aircraft. Challenges such as ice bridging, aerodynamic disruption during inflation cycles, and material fatigue are noted, alongside ongoing research aimed at improving boot design, pneumatic control, and material durability. The review also highlights the transition in modern aircraft from vacuum pumps to advanced electronic instrumentation and optimized pneumatic systems, reflecting the evolving nature of de-icing technology to enhance aviation safety in cold-weather conditions.

Additional Information

  • Source:International Scientific Journal of Engineering & Management. 2025/03, Vol. 4, Issue 3, p1
  • Document Type:Article
  • Subject Area:History
  • Publication Date:2025
  • ISSN:25836129
  • DOI:10.55041/ISJEM02445
  • Accession Number:184897107
  • Copyright Statement:Copyright of International Scientific Journal of Engineering & Management is the property of International Scientific Journal of Engineering & Management and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

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