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Rotor blades

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Published: 01 January 1987
Fig. 840 Fracture surfaces of the two broken turbine-rotor blades at the bottom in Fig. 839 . Fatigue beach marks are faintly visible at right on the fracture surface of the lower blade. The region between the parallel black lines on each blade was examined by electron microscopy. 6× More
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Published: 01 January 1987
Fig. 842 TEM p-c replica of a fracture surface of one of the turbine-rotor blades in Fig. 840 . This view is typical of all the areas examined. A patch of fatigue striations is faintly visible at center between arrows. The fatigue crack is believed to have been initiated by hot corrosion More
Image
Published: 01 January 2001
Fig. 4 EC-120 helicopter rotor application. (a) Rotor blade sleeve. The part is made of forged 2009/SiC/15p discontinuously reinforced aluminum (DRA). The scale below the part is 30 cm long. (b) Rotor assembly showing the DRA blade sleeves. Photos courtesy of DWA Aluminum Composites, Inc. More
Image
Published: 01 January 2002
Fig. 6 Fatigue cracking of a helicopter tail rotor blade. (a) Scanning electron micrograph of the blade showing lead wool ballast in contact with the 2014-T652 aluminum spar bore cavity wall at the failure origin ∼13×. (b) Greater magnification (∼63×) in this same area shows the multiple pits More
Image
Published: 01 January 1997
Fig. 11 Stress contour plot of first-stage silicon nitride turbine rotor blade for a natural-gas-fired industrial turbine engine for cogeneration. The blade is rotating at 14,950 rpm. Courtesy of Solar Turbines Inc. More
Image
Published: 01 January 1987
Fig. 841 A macroetched view of a cracked turbine-rotor blade near the arrow in Fig. 839 , displaying large columnar grains and a crack that initiated at the trailing edge (at left in this view) of the blade. This crack appears to have followed an intergranular path. Etched in 95 parts conc More
Image
Published: 15 January 2021
Fig. 6 Fatigue cracking of a helicopter tail rotor blade. (a) Scanning electron micrograph of the blade showing lead wool ballast in contact with the 2014-T652 aluminum spar bore cavity wall at the failure origin. Original magnification: ~13×. (b) Greater magnification (~63×) in this same area More
Image
Published: 01 January 2002
Fig. 28 Failed compressor rotor. Arrows indicate fractured portions of blades. 36× More
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Published: 15 January 2021
Fig. 21 Failed compressor rotor. Arrows indicate fractured portions of blades. Original magnification: 36 × More
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003467
EISBN: 978-1-62708-195-5
... deal mainly with structures that exhibit an initial material and/or manufacturing defect or failures that are most prevalent and most easily solved. The components include helicopter rotor blade, composite wing spar, and aircraft rudder. aircraft rudders composite wing spar helicopter rotor...
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Published: 01 January 1990
Fig. 1 Shaped holes, turbulators, pin fins, and other techniques used in turbine rotor blade cooling More
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Published: 01 December 2004
Fig. 12 Three pieces of honeycomb cut with a diamond wire saw. Note the absence of burrs and breakout. From left: titanium; section from helicopter rotor blade consisting of plastic, paper honeycomb, epoxy, stainless steel screws, and Kevlar; extruded ceramic honeycomb used in automotive More
Image
Published: 01 August 2018
Fig. 31 (a) Computed tomography (CT) image across a sample helicopter tail rotor blade showing outer fiberglass airfoil and center composite spar. (b) Planar reformation through the composite spar from a series of CT slices. The dark vertical lines are normal cloth layup boundaries, while More
Series: ASM Handbook
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...
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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...
Image
Published: 30 August 2021
Fig. 1 Failed gas turbine rotor. From left to right: first-, second-, and third-stage turbine blades. The failure originated in the second stage; fragments of the second-stage blades damaged the downstream third-stage blades. The first-stage blades were relatively undamaged. More
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
... been redesigned and replaced ( Ref 13 , 14 , 15 , 16 , 17 , 18 , 19 , 20 , 21 ). Many LP rotors with shrunk-on discs have been replaced by integral or welded rotors. Weld repair techniques for the disc-blade attachment areas were developed, including weld repair of the low-alloy steel disc...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003060
EISBN: 978-1-62708-200-6
... testing. Gas Turbine Components The successful performance of ceramic components has been demonstrated in gas turbine engines. The major efforts have been directed toward turbine rotor development, specifically one-piece rotor/blade components of both radial inflow and axial flow configurations...
Image
Published: 01 January 1987
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 for a view of the area near the arrow. See also Fig. 840 and 842 . 0.5× More