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Compressors
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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
... Abstract Pumps and compressors are representative fluid machineries, which are indispensably important industrial equipment for water supply systems, chemical processing and reactions, and fluid power systems. This article addresses friction, lubrication, and wear of components in several types...
Abstract
Pumps and compressors are representative fluid machineries, which are indispensably important industrial equipment for water supply systems, chemical processing and reactions, and fluid power systems. This article addresses friction, lubrication, and wear of components in several types of machines such as positive displacement pumps including hydraulic pumps, turbo-pumps including centrifugal pumps, vacuum pumps, and compressors including the positive displacement type and turbo type.
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Published: 01 August 2013
Fig. 13 High-pressure compressor blades coated with physical vapor deposition process for improved wear resistance. Source: Ref 22
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Published: 01 August 2013
Fig. 9 Relationship between clearance and efficiency of compressor
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Published: 01 January 2006
Fig. 2 Compressor coating. The coating is composed of an aluminum-filled inorganic phosphate with a polytetrafluoroethylene (PTFE) layer on top. Beneath the PTFE layer is an ion-reactive primer that inhibits corrosion, which otherwise would cause delamination of this top layer. As-polished
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in Fabrication of Near-Net Shape Cost-Effective Titanium Components by Use of Prealloyed Powder and Hot Isostatic Pressing
> Powder Metallurgy
Published: 30 September 2015
Fig. 16 Selectively net shape Ti-6Al-4V compressor casing as (a) hot isostatic pressed and (b) final limited machining. Source: Courtesy of Rolls-Royce
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Published: 01 December 2004
Fig. 16 Transverse section of a forged compressor disc, Ti-17 alloy. Flow lines and variations in grain size are revealed. Section is approximately 25 cm (10 in.) high; scale is in inches. Etched in 15 mL HNO 3 (conc.), 10 mL HF (48%), and 75 mL H 2 O at room temperature. Courtesy of F
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 9 1000-h creep rupture strength of turbine rotor and compressor blade alloys. Source: Ref 14
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 10 Yield strength at 0.2% offset of five candidate compressor blade alloys compared with that of 12Cr-0.6Mo steel. Source: Ref 14
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Published: 01 January 2005
Fig. 3 Wrought gamma titanium products. (a) Compressor blades. (b) Subscale isothermally forged disk. (a) and (b) Source: D.U. Furrer, Ladish Company. (c) Large, conventionally (pack) rolled sheet. Source: Battelle Memorial Institute, Air Force Research Laboratory
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Published: 01 January 2005
Fig. 13 Compressor disk forgings of original and revised designs, showing machined contours in phantom. See Example 1. Dimensions in figure given in inches Item Revised design Material AMS 5613 (type 410 stainless steel) (a) Forging equipment 35 kN (8000 lbf) hammer (b) 50
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Published: 01 January 1987
Fig. 86 Alloy steel compressor disk that cracked from overheating during forging. (a) Macrograph of disk (cracking at arrow). 0.4×. (b)Fracture surface of a specimen from the disk that was normalized, quenched, and tempered to 321 to 341 HB. The treatment revealed facets indicative
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Published: 01 January 1987
Fig. 739 High-cycle fatigue fracture of the end cap for a high-pressure compressor used in a polyethylene process. The forging was made of Armco 15-5PH (UNS S15500), quenched and tempered to the H1075 condition. The end cap was located between the crosshead and plunger of the compressor, where
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Published: 01 January 2002
Fig. 28 Failed compressor rotor. Arrows indicate fractured portions of blades. 36×
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Published: 01 January 2002
Fig. 29 Compressor blade fracture surface showing fatigue origins on low pressure (i.e., right) side of blade, as indicated by the arrows. 13×
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Published: 01 January 2002
Fig. 30 Failed compressor rotor shaft. Fracture occurred at radius between large and small diameters. Arrows indicate some of fatigue origins. 1×
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Published: 01 January 2002
Fig. 16 4340 steel compressor shaft that fractured because of peeling-type fatigue cracking. (a) Configuration and dimensions (given in inches). (b) and (c) Photographs showing crack path, failure origin, and beach marks on fracture surfaces of shaft and key
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Published: 01 January 2002
Fig. 46 Tube sheet from an air compressor aftercooler that failed by SCC. (a) Configuration of tube sheet. (b) Micrograph of a specimen etched in 10% ammonium persulfate solution showing intergranular crack propagation. 250×. (c) Macrograph of an unetched specimen showing multiple branching
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Published: 01 January 2002
Fig. 40 Freon-compressor shaft of 4140 steel that failed by fretting corrosion in the bearing area (Example 2). (a) Shaft and bearing assembly. (b) Failed region of shaft, at 2×, showing disturbed metal and partly closed keyway. (c) Shaft side of bearing inner ring, at 3×, showing pitting
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in Nondestructive Evaluation of Pressed and Sintered Powder Metallurgy Parts[1]
> Nondestructive Evaluation of Materials
Published: 01 August 2018
Fig. 10 Automotive air conditioner compressor part examined by resistivity measurement. (a) Actual part. (b) Cross section showing flawed area. (c) Six-location test fixture. Source: Ref 6
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