| Description |
1 online resource (vi, 247 pages) : illustrations |
| Contents |
Choosing Optimum Coatings for Modern Aircraft Engine Turbine Blades -- Conditions of Turbine Blade Operation -- Requirements Imposed on Turbine Blade Coatings -- Principles of Choosing Coatings for Aircraft Engine Turbine Blades -- Causes of Coating Failures on Aircraft-Engine Turbine Blades -- Technological Processes for Deposition of Protective Coatings to Turbine Blades -- Diffusion Coatings -- Overlay Coatings -- Phase Composition and Structure of Coatings on Superalloys -- Phase Composition and Structure of Diffusion Coatings -- Phase Composition and Structure of Ni-Cr-Al, Ni-Co-Cr-Al, and Co-Ni-Cr-Al Alloys and Overlay Coatings Made of Them -- Phase Composition and Structure of Overlay Coatings -- Phase and Structural Changes in Coatings during High-Temperature Tests -- Changes of Phase Composition and Structure in Diffusion Coatings -- Changes of Phase Composition and Structure in Overlay Coatings at High-Temperature Tests -- Turbine Blade Coating Protective Properties -- Protective-Properties Evaluation Methods -- Heat Resistance of Aluminides and Alloys for Overlay Coatings -- Heat Resistance of Coated Superalloys -- Resistance of Overlay-Coated Alloys to Hot Corrosion -- Resistance of Coated Superalloys to Hot Corrosion -- The Effect of Protective Coatings on the Mechanical Properties of Superalloys -- Thermal Expansion Coefficients and Elasticity Modulus of Coating Alloys -- Mechanical Properties of Coating Alloys -- Thermal Stresses in Superalloy Coatings -- Effect of Coatings on High-Temperature Strength of Superalloys |
| Summary |
This book addresses the problem of surface protection for aircraft engine turbine blades. It is based on the author's 30+ years of work on the development and application of coatings to protect against oxidation and hot corrosion. It describes and details a methodology for optimizing turbine blade surface protection. The distinctions of this book from other publications on this topic include: The performance of protective coatings is assessed and evaluated by the complex interconnections of their chemical and phase composition, structure, and physical-mechanical properties; The properties of overlay coatings are given for the wide range of compositions, including the possible coatings states after their production and long-term service; The principles for calculating the stresses and strains for coated turbine blades are reviewed |
| Bibliography |
Includes bibliographical references and index |
| Notes |
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL |
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English |
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Print version record |
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digitized 2010 HathiTrust Digital Library committed to preserve pda MiAaHDL |
| Subject |
Aircraft gas-turbines -- Blades.
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Protective coatings.
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Gas-turbines -- Materials.
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Protective coverings.
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protective coating.
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TRANSPORTATION -- Aviation -- General.
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Protective coverings
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Aircraft gas-turbines -- Blades
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Gas-turbines -- Materials
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Protective coatings
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Gasturbine
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Rotorblatt
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Schutzschicht
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| Form |
Electronic book
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| Author |
ASM International.
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| LC no. |
2002027690 |
| ISBN |
9781615030705 |
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1615030700 |
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0871707594 |
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9780871707598 |
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