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Rotor blade shrouds

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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
... specimen toward and into the bladed rotor. Incursion rates, the speed at which the specimen is moved into the rotor, can be adjusted 1 to 2000 μm/s (0.04 to 79 mils/s). Either real turbine blades or blade dummies, as shown in Fig. 14 , can be tested. While the use of original blades provides the advantage...
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 Many LP rotors with shrunk-on discs have been replaced by integral or welded rotors.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 Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005737
EISBN: 978-1-62708-171-9
... are the combustor, transition liners, first-row stationary airfoils (also called the first-stage vanes or the nozzle guide vanes), first-stage rotating airfoils (sometimes called first-stage buckets or blades), later stator and rotor stages, and disks or wheels to which the rotating airfoils are attached. Many...
Series: ASM Handbook
Volume: 18
Publisher: ASM International
Published: 31 December 2017
DOI: 10.31399/asm.hb.v18.a0006428
EISBN: 978-1-62708-192-4
... filters past the struts and inlet guide vane (IGV) into a high-pressure compressor ( Ref 1 ). The compressor broadly consists of alternating stages of compressor blades and vanes which decrease in size as one goes from front to aft stages. The blades are attached to a rotor in the form of blade or bucket...
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...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003485
EISBN: 978-1-62708-195-5
... The Eurocopter France EC120 and N4 helicopters are used for civilian law enforcement and search and rescue in Europe, the United States, and in many other countries. The large centrifugal loads of each rotor blade (the N4 has five blades) are supported by a blade sleeve, which holds the rotor blade to the drive...
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
.... In cases where material is released in the turbine flow path, such as a broken airfoil, downstream components typically suffer secondary damage, and so the first component to fail is typically at the upstream end of the damaged zone ( Fig. 1 ). Fig. 1 Failed gas turbine rotor. From left to right...
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: 18
Publisher: ASM International
Published: 31 December 2017
DOI: 10.31399/asm.hb.v18.a0006429
EISBN: 978-1-62708-192-4
..., and the surfaces of the vane and the grooves of the rotors. In particular, the parts between the vane and the cam ring and between the vane and the side plates are essential ( Ref 31 ) and the oil temperature ( Ref 32 ) is important for the vane pump performance. For the vane pump test ( Ref 33 ), fourteen...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003500
EISBN: 978-1-62708-180-1
... Distress damages Vibration Short/open circuit Failed components Sleeve bearing Seal Coupling Shaft Pinion/ball/turning gear Casing Rotor Impeller Shroud Piston Diaphragm Wheel Blades; foil, root, shroud Labyrinth Thrust bearing Pivoted pad bearing Roller/ball bearing Cross-head piston Cylinder...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006753
EISBN: 978-1-62708-295-2
... revealed both the compressor rotor and the shaft sustained fatigue failures. Fig. 21 Failed compressor rotor. Arrows indicate fractured portions of blades. Original magnification: 36 × Fig. 22 Compressor blade fracture surface showing fatigue origins on low-pressure (i.e., right) side...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003061
EISBN: 978-1-62708-200-6
... entrained in fluids or gases striking a surface of a wear plate. Examples would be coal, gravel, ore, or grain striking a chute, an elbow, or a fan blade in a materials handling system. Rubbing wear involves sliding abrasion of two materials in contact with each other, with or without abrading particles...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005730
EISBN: 978-1-62708-171-9
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006785
EISBN: 978-1-62708-295-2
... for steam turbine rotors/discs, carbon and alloy steel components in boilers Residential and industrial water-delivery systems: Stainless steel PEX clamps (described earlier) and brass components General Characteristics of Stress-Corrosion Cracking The phenomenological characteristics of SCC...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003091
EISBN: 978-1-62708-199-3
..., and rotor steels have higher quality requirements and tighter composition control than plain carbon or ordinary low-alloy steels. The production of special-quality steels requires vacuum-based induction or electric remelting and refining capabilities. The article explores the types and characteristics...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003350
EISBN: 978-1-62708-195-5
... U.S. tactical fighter aircraft, the F-22. Over 24% of the F-22 structure is OMCs. The B-2 bomber, shown in Fig. 2 , is constructed using an even higher percentage of composites, as are current helicopter and vertical lift designs. For example, the tilt- rotor V-22 Osprey is over 41% composite...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001072
EISBN: 978-1-62708-162-7
... applications led to the development of Nimonic alloy 80 and Nimonic alloy 80A during the 1940s ( Ref 8 ) The development of the turbo-supercharger for aircraft engines, which operated at temperatures ranging from 650 to 815 °C (1200 to 1500 °F) as the rotor turned at speeds of 20,000 to 30,000 rpm, led...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005227
EISBN: 978-1-62708-187-0
..., high specific modulus, wear resistance, low coefficient of thermal expansion, and high specific conductivity, which make them very attractive for automotive, electronic packaging, and space applications. Several MMC components are currently being used as automotive components, such as brake rotors...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001105
EISBN: 978-1-62708-162-7
.... Unfortunately, these goals were not fulfilled, despite a major effort in the United States and Europe during the 1950s. The degree of ductility and toughness imparted by the metallic binder phase remains inadequate for most critical applications, such as turbojet and stationary gas turbine blades or nozzle...
Series: ASM Handbook
Volume: 7
Publisher: ASM International
Published: 30 September 2015
DOI: 10.31399/asm.hb.v07.a0006079
EISBN: 978-1-62708-175-7
... and toughness are required to 595 °C (1100 °F); cutting tools, shear blades, reamers, dies, ingot tongs Iron-manganese Low (similar to carbon steel) Excellent Low yield point deformation Poor; grind if required Austenite saturated with carbon; iron-manganese carbides at grain boundaries in thin, flat...