Progress in Aircraft Engines Materials and Their Properties

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Authors: Sugandh Gupta, Virinder Kumar, Parminder Singh, Rinku, Harmehar Singh
Cited by: 0

Abstract

This chapter explores the development of materials in aircraft engines in terms of performance, safety, and efficiency improvements that characterizes modern aviation. This chapter follows the historical development and the current status of aircraft engine materials from the early 20th-century dependence on wood, steel, and aluminum to the present high-performance alloys and composites. It highlights the severe requirements imposed on aircraft engines, like mechanical loads and corrosive atmospheres, as well as extreme temperatures and the resultant requirement for higher-performance materials like titanium and nickel-based superalloys, ceramic matrix composites (CMCs), and carbon–carbon composites. These materials exhibit high strength-to-weight ratios, thermal resistance, and durability under stress. The chapter also addresses particular materials for specific engine components and the importance of protective coatings in increasing component lifespan. It also highlights the shift to cleaner, lighter, and more efficient designs due to increasing environmental and economic pressures. With the help of advanced manufacturing processes and material advancements, aircraft engines now have higher thrust-to-weight ratios, better fuel efficiency, and longer operational lifespans, defining the future of aerospace propulsion.

Fields of Study & Subjects

Material Properties and Applications High Temperature Alloys and Creep Material Selection and Properties

Publication details

Journal / source
CRC Press eBooks
Pages
40–56
Publication date
12 February 2026
Language
EN
Document type
Book chapter