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Engine components
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in Secondary Working of Bar and Billet[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
Fig. 10.2 Fan blades, compressor discs, and many other engine components use forged titanium parts.
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Image
Published: 01 June 2008
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2018
DOI: 10.31399/asm.tb.aceg.t68410009
EISBN: 978-1-62708-280-8
... Abstract This chapter is a brief account of various factors pertinent to the development of an engineering component. The discussion covers the disciplines and interactions of design development, engineering of component design, validation of design and process analysis, and matrix of design...
Abstract
This chapter is a brief account of various factors pertinent to the development of an engineering component. The discussion covers the disciplines and interactions of design development, engineering of component design, validation of design and process analysis, and matrix of design and manufacturing elements.
Image
Published: 01 October 2012
Image
in Aerospace Applications—Example Fatigue Problems
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060231
EISBN: 978-1-62708-343-0
... in Florida Fig. 10.2 Comparison of fatigue regimes encountered in the Space Shuttle Main Engines (SSMEs) and that encountered in aeronautical gas turbine engines Fig. 10.3 Cut-away view of the Space Shuttle Main Engine showing components and gas paths Fig. 10.4 Location...
Abstract
This chapter explains how the authors assessed the potential risks of creep-fatigue in several aerospace applications using the tools and techniques presented in earlier chapters. It begins by identifying the fatigue regimes encountered in the main engines of the Space Shuttle. It then describes the types of damage observed in engine components and the methods used to mitigate problems. It also discusses the results of analyses that led to changes in design or approach and examines fatigue-related issues in turbine engines used in commercial aircraft.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.tb.hpcspa.t54460277
EISBN: 978-1-62708-285-3
... and refurbishment of structural engineering components are also discussed. high-pressure cold spray process repair refurbishment aerospace industry oil and gas industry power-generation industry COLD SPRAY COATING TECHNOLOGY, as described in previous chapters, has the capability to provide surface...
Abstract
This chapter focuses on high-pressure cold spray applications pertaining to repair and refurbishment in the aerospace, oil and gas, and power-generation industries, the last specifically involving repair of gas turbine components. Advantages of cold spray coating in the repair and refurbishment of structural engineering components are also discussed.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060195
EISBN: 978-1-62708-355-3
...) and 100% relative humidity. a , distance from load point to initial crack tip; Δ a , growth during exposure. Source: Ref 4 Abstract This chapter focuses on tensile testing of three types of engineering components that undergo significant loading in tension, namely, threaded fasteners...
Abstract
This chapter focuses on tensile testing of three types of engineering components that undergo significant loading in tension, namely, threaded fasteners and bolted joints; adhesive joints; and welded joints. It describes the standardized tensile test for externally threaded fasteners and provides a brief background on relationships among torque, angle-of-turn, tension, and friction. The chapter also describes the test methods covered in the ASTM F 606M standard, namely, product hardness; proof load by length measurement, yield strength, or uniform hardness; axial tension testing of full-sized products; wedge tension testing of full-sized products; tension testing of machined test specimens; and total extension at fracture testing. Finally, the chapter covers tensile testing of adhesive and welded joints.
Image
Published: 01 October 2012
Fig. 1.13 Ti-6Al-4V engine nacelle component for the Boeing 757 aircraft. (a) Part as previously fabricated required 41 detail parts and more than 200 fasteners. (b) Superplastically formed part is formed from a single sheet. Courtesy of Metal Bellows Division of Parker Bertea Aerospace Group
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Image
Published: 01 August 2005
Fig. 3.4 A component made of an aluminum engineering alloy (type 6082), fabricated by fluxless brazing in a nitrogen flow furnace. The brazed joints exist at the interface between the web members and the face plates and also at the intersection of each web member. A similar component is shown
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Image
Published: 01 August 2005
Fig. 3.9 Tube-to-plate joint in aluminum engineering alloy components, torch brazed in air using a low-melting-point aluminum-base filler metal and commercially available flux
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2001
DOI: 10.31399/asm.tb.secwr.t68350001
EISBN: 978-1-62708-315-7
... is a multidisciplinary activity intended to tailor the properties of the surfaces of engineering components so that their function and serviceability can be improved. The ASM Handbook defines surface engineering as “treatment of the surface and near-surface regions of a material to allow the surface to perform...
Abstract
This chapter begins with a brief review of the different types of surface treatments and coatings used in industry and their effect on properties and performance. It then discusses the importance of corrosion and wear treatments and the consequences of failing to properly implement them in critical industries such as mining, energy production, transportation, and mineral and chemical processing. The chapter also describes basic approaches to dealing with corrosion and wear in steel.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2022
DOI: 10.31399/asm.tb.isceg.t59320049
EISBN: 978-1-62708-332-4
... at the best price and with the least time to bring the product to the market. 5.1 Component Development Disciplines and Interactions The three interrelated disciplines of design, material, and manufacturing contribute to engineering for functional performance ( Fig 5.1 ). The contributions of the three...
Abstract
This chapter provides an overview of how the disciplines of design, material, and manufacturing contribute to engineering for functional performance. It describes the interaction of product designers and casting engineers in product development. It discusses the consequences of component failure, uncertainty in data and assumptions, and selection of the factor of safety. The chapter also presents an overview of the functional requirements for product performance and provides an overview of product design development. It also presents a partial list of the different tests that are performed on prototypes and examples of product testing. The chapter describes the requirements of a traceability system.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2001
DOI: 10.31399/asm.tb.secwr.t68350195
EISBN: 978-1-62708-315-7
... surface-engineering solutions for seven operating conditions: Structural parts, for example, pipes, pump and valve bodies, casings, housings, supports, rigs, tanks, and so forth, subjected to corrosive conditions in various environments A part in static contact with another engineering component...
Abstract
This chapter provides helpful guidelines for selecting a surface treatment for a given application. It identifies important design factors and applicable treatments for common design scenarios, materials, and operating conditions. It explains why heat treatments and finishing operations may be required before or after processing and how to estimate or predict coating thickness, case depth, hardness, and the likelihood of distortion. It also addresses related issues and considerations such as part handling and fixturing, surface preparation and cleaning requirements, processability, aesthetics, and the influence of design features.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120139
EISBN: 978-1-62708-269-3
... is a semicommercial alloy developed by RMI Titanium Company in the 1960s to extend the use of titanium applications to 540 °C (1000 °F). Used for jet engine components Ti-6Al-2Sn-1.5Zr-1Mo-0.35Bi-0.1Si, UNS: none, Ti11 Developed by Timet for improved creep resistance Ti-11 was not commercially marketed because...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2018
DOI: 10.31399/asm.tb.aceg.9781627082808
EISBN: 978-1-62708-280-8
Book Chapter
Book: Systems Failure Analysis
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.tb.sfa.t52780147
EISBN: 978-1-62708-268-6
..., the additional tests or analyses identify where the design requires modification. Requirements Flowdown When the system-level requirements are understood, it is the engineers’ responsibility to take the system-level requirements and flow them down to subassembly and component-level requirements. Engineers...
Abstract
In some cases, the failure analysis team finds that all components meet their requirements, the system was properly assembled, and it was not operated or tested in an out-of-specification manner, yet it still failed. When this occurs, the only conclusion the failure analysis team can reach is that it missed something in its analysis or that the design is defective. This chapter focuses on the latter possibility by discussing the various factors that a failure analysis team should consider to identify the causes of defects in system design. These include requirements identification and verification, circuit performance, mechanical failures, materials compatibility, and environmental factors. Examples that illustrate the value of design analysis are also presented.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2022
DOI: 10.31399/asm.tb.tstap.t56040001
EISBN: 978-1-62708-428-4
... are easy to use, cost relatively little to operate, and have attributes that are beneficial to applications in almost all industries. The benefits of this environmentally friendly process are typically reduced cost, improved engineering performance, and/or increased component life ( Fig. 1 ). Figure 1...
Abstract
This article provides a high-level overview of thermal spray technologies and their applications and benefits. It is intended to educate members of government, industry, and academia to the benefits of thermal spray technology. The article describes the value of thermal spray technology with examples of application success stories. A few applications critical to thermal spray and market growth are briefly discussed. The article also summarizes the key research areas in thermal spray technology.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270019
EISBN: 978-1-62708-301-0
... engine components. Acoustic Microscopy High-frequency ultrasound in the GHz range is passed through the component of interest. The transmitted wave is detected by a rapidly scanning laser beam on the opposite surface. Transmission of these waves is interrupted by flaws present in the material...
Abstract
This chapter discusses the basic steps of a failure investigation. It explains that the first step is to gather and document information about the failed component and its operating history. It advises investigators to visit the failure site as soon as possible to record damages and collect test specimens for subsequent examination and chemical analysis. It also discusses the role of mechanical property testing, the use of nondestructive evaluation, and the final step of generating a report.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000001
EISBN: 978-1-62708-313-3
... because of their excellent formability and weldability. The next major engine components are the turbine vanes, which see slightly lower temperatures than the combustor, but oxidation resistance is still a significant consideration. The difference in pressure on the airfoil surfaces also causes...
Abstract
Superalloys, although not strictly defined, are generally regarded as high-performance alloys based on group VIII elements (nickel, cobalt, or iron, with a high percentage of nickel) to which a multiplicity of alloying elements have been added. The defining feature of a superalloy is its combination of relatively high mechanical strength and surface stability at high operating temperatures. This chapter provides a brief history of the development of superalloys and discusses their use in the gas turbine engines.
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