Description |
1 online resource (vi, 247 pages) : illustrations |
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data file |
Physical Medium |
polychrome |
Bibliography |
Includes bibliographical references and index. |
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 -- 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. |
Access |
Use copy Restrictions unspecified MiAaHDL |
Reproduction |
Electronic reproduction. [Place of publication not identified] : HathiTrust Digital Library, 2010. MiAaHDL |
System Details |
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 |
Processing Action |
digitized 2010 HathiTrust Digital Library committed to preserve MiAaHDL |
Access |
Access restricted to Ryerson students, faculty and staff. CaOTR |
Local Note |
eBooks on EBSCOhost EBSCO eBook Subscription Academic Collection - North America |
Language |
English. |
Subject |
Aircraft gas-turbines -- Blades.
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Aircraft gas-turbines -- Blades. |
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Protective coatings.
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Protective coatings. |
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Gas-turbines -- Materials.
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Gas-turbines -- Materials. |
Genre/Form |
Electronic books.
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Electronic books.
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Added Author |
ASM International.
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Other Form: |
Print version: Tamarin, Y. Protective coatings for turbine blades. Materials Park, Ohio : ASM International, ©2002 0871707594 (DLC) 2002027690 (OCoLC)50124744 |
ISBN |
9781615030705 (electronic book) |
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1615030700 (electronic book) |
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0871707594 |
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9780871707598 |
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9780871707598 |
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0871707594 |
Standard No. |
9780871707598 |
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