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turbine blade alloys

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Published: 01 January 1990
Fig. 9 1000-h creep rupture strength of turbine rotor and compressor blade alloys. Source: Ref 14 More
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004133
EISBN: 978-1-62708-184-9
...) and ultrasupercritical (USC) power plants. These components include high-pressure steam piping and headers, superheater and reheater tubing, water wall tubing in the boiler, high-and intermediate-pressure rotors, rotating blades, and bolts in the turbine section. The article reviews the boiler alloys, used in SC and USC...
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Published: 01 January 1987
Fig. 105 Fracture surface of a cast aluminum alloy A357-T6 air-turbine blade. (a) Overall view of the fracture surface showing a large inclusion (dark) near the tip of the blade. Approximately 0.4×. (b) and (c) Decohesion at the interfaces between the inclusion and the aluminum matrix More
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Published: 01 January 2002
Fig. 9 Gamma-prime overaging in a nickel-base alloy turbine blade material. (a) SEM micrograph of the blade material, showing the breakdown of the eutectic gamma prime (5) and the spreading of the coarse gamma prime. Smaller particles of fine aging gamma prime (4), which would appear between More
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Published: 01 January 2002
Fig. 11 Hot corrosion attack of René 77 nickel-base alloy turbine blades. (a) Land-based, first-stage turbine blade. Notice deposit buildup, flaking, and splitting of leading edge. (b) Stationary vanes. (c) A land-based, first-stage gas turbine blade that had type 2 hot corrosion attack. (d More
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Published: 01 January 2006
Fig. 11 Microstructures of nickel-base Alloy 713C turbine blades. (a) Original structure prior to service. (b) Coarsening of γ' precipitates and elimination of secondary γ' caused by 5000 h of service More
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Published: 01 August 2018
Fig. 30 Digital radiograph of an aircraft engine turbine blade (nickel alloy precision casting) from an industrial computed tomography system More
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003517
EISBN: 978-1-62708-180-1
... are exposed to elevated temperatures for long times. Typical metallurgical instabilities for turbine blades include carbide coarsening, gamma-prime formation, and hot corrosion. For steel alloys used for tubes and piping, carbide spheroidization and coalescence, sigma-phase formation, sensitization...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004155
EISBN: 978-1-62708-184-9
..., and turbine cylinders, and only a few major changes have been introduced in the last two decades ( Ref 2 , 6 ). These materials are listed in Table 1 . Titanium alloy blades are slowly being introduced for the last low-pressure stages. Also, improved melting practices, control of inclusions and tramp...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006824
EISBN: 978-1-62708-329-4
.... The effects of more modest temperature excursions may be limited to incipient melting, where only the grain boundaries melt as a result of local differences in alloy chemistry and surface tension at the grain boundaries. Example 3: Localized Melting of Turbine Blades An industrial gas turbine operating...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005738
EISBN: 978-1-62708-171-9
...); typical examples are the aforementioned polymeric and elastomeric materials ( Ref 8 , 9 , 10 ) (mostly fan/inlet applications), honeycombs (NiCrAlY and FeCrAlY alloys) commonly used in low-pressure turbine applications where large radial displacements are experienced against shrouded blade seals...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005737
EISBN: 978-1-62708-171-9
... of an airfoil section and a dovetail joint. The dovetail joint connects the blade to the turbine disk. The rotating blades are under more stress than the vanes due to the centrifugal forces exerted on the blades. Creep can be a problem, which is why new alloys and processing techniques have resulted...
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001051
EISBN: 978-1-62708-161-0
... in turbine rotor blade cooling For the past 28 years, high-pressure turbine blades and vanes have been made from cast nickel-base superalloys. The higher-strength alloys are hardened by a combination of approximately 60 vol% γ′ [Ni 3 (Al,Ti)] precipitated in a γ matrix, with solid-solution...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004158
EISBN: 978-1-62708-184-9
... of an industrial gas turbine blade. Below the tip, a coating is protecting the base metal. (b) Micrograph of the oxidation shown in (a). There is an external oxide E; a layer of fully oxidized base metal, F; an internally oxidized layer, I; and an alloy-depleted layer, A. The alloy-depleted layer includes...
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Published: 30 August 2021
of mid-airfoil trailing edge of stage 1 blade. The sulfide particles are the light-gray particles in the alloy-depleted layer (light); the darker-gray particles near the surface are oxides. Etched with chromic acid, electrolytic. (d) Outer-airfoil trailing edge of second-stage turbine vane showing More
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003570
EISBN: 978-1-62708-180-1
... alloying elements, depending on the manufacturer. High magnetomechanical damping is a key property of 12% Cr steel, which serves admirably as blading in high-purity steam. Some turbines have been fitted with precipitation-hardened stainless steel (17-4 PH) blades in the next-to-last row of the low-pressure...
Image
Published: 01 January 1987
Fig. 109 Porosity in a fracture of a cast aluminum alloy A357 blade from a small air turbine. The blade fractured by overload from an impact to its outer edge. More
Series: ASM Handbook
Volume: 24A
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.hb.v24A.a0007019
EISBN: 978-1-62708-439-0
... development of a 13 m (43 ft) wind turbine blade mold using AM ( Fig. 3 ) by Oak Ridge National Laboratory (ORNL) in collaboration with Sandia National Laboratories, TPI Composites, and National Renewable Energy Laboratory (NREL) ( Ref 23 ). At that time, several benefits were identified that would justify...
Series: ASM Handbook
Volume: 18
Publisher: ASM International
Published: 31 December 2017
DOI: 10.31399/asm.hb.v18.a0006378
EISBN: 978-1-62708-192-4
... of the distinctions between the different forms of erosion. It discusses steam turbine blade erosion, aircraft rain erosion, and rain erosion of wind turbine blades. The article describes the mechanisms of liquid impact erosion and time dependence of erosion rate. It reviews critical empirical observations regarding...
Series: ASM Handbook Archive
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000616
EISBN: 978-1-62708-181-8
..., crescent-shaped fatigue-crack area visible in Fig. 835 , to ductile dimples. SEM, 225× Fig. 839 A gas-producer turbine rotor cast of alloy 713LC that fractured after 440 h of service, as the result of hot corrosion fatigue. Fracture was abrupt, with three blades being thrown off. See Fig. 841...