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laminations
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Book Chapter
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002415
EISBN: 978-1-62708-193-1
... Abstract Knowledge of fatigue behavior at the laminate level is essential for understanding the fatigue life of a laminated composite structure. This article describes fatigue failure of composite laminates in terms of layer cracking, delamination, and fiber break and interface debonding...
Abstract
Knowledge of fatigue behavior at the laminate level is essential for understanding the fatigue life of a laminated composite structure. This article describes fatigue failure of composite laminates in terms of layer cracking, delamination, and fiber break and interface debonding. It discusses the fatigue behavior of composite laminates in the form of a relation between applied maximum fatigue stress and fatigue life. The article explains Weibull distribution and parameters estimation for fatigue data analysis and life prediction of composite laminates. It analyzes the fatigue properties and damage tolerance of fiber-metal laminates such as ARALL and GLARE laminates. The article concludes with a discussion on the effects of fatigue on notched and unnotched specimens.
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in Design and Fabrication of Inductors for Heat Treating, Brazing, and Soldering
> Induction Heating and Heat Treatment
Published: 09 June 2014
Fig. 16 Split-return coil with laminations on the center leg of the coil. Courtesy of Radyne Corporation, an Inductotherm Group Co.
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in Magnetic Flux Controllers in Induction Heating and Melting
> Induction Heating and Heat Treatment
Published: 09 June 2014
Fig. 3 Induction coil with laminations stacked between mechanical supports. Courtesy of Tucker Induction.
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in Systematic Analysis of Induction Coil Failures and Prevention
> Induction Heating and Heat Treatment
Published: 09 June 2014
Fig. 22 Laminations applied to a channel-type inductor function as a magnetic flux concentrator. Source: Ref 17
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in Systematic Analysis of Induction Coil Failures and Prevention
> Induction Heating and Heat Treatment
Published: 09 June 2014
Fig. 25 Laminations are particularly sensitive to aggressive environments such as quenchants and steam. Rusting and degradation result. Source: Ref 17
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in Systematic Analysis of Induction Coil Failures and Prevention
> Induction Heating and Heat Treatment
Published: 09 June 2014
Fig. 55 Degraded laminations resulting from excessive magnetic saturation and overheating due to improper design. Source: Ref 36
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Image
Published: 01 January 2006
Fig. 1 Typical laminations blanked and pierced from electrical sheet. (a) Laminations for rotating electrical machinery are blanked and pierced in single-station dies ( Fig. 3 ) or progressive dies ( Fig. 4 ). Slots can also be made in precut blanks, one at a time, with notching dies. (b
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Published: 01 January 2006
Fig. 2 Method for stacking laminations stamped in individual dies
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Published: 01 January 2006
Fig. 3 Sequence of operations for producing stator and rotor laminations using single-station dies. Operation 1, stock blanked and pierced; operation 2, stator lamination notched; operation 3, rotor lamination separated from stator lamination; operation 4, rotor lamination notched. Compare
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Published: 01 January 2006
Fig. 4 Blanking and piercing sequence for rotor and stator laminations in a five-station progressive die. Two pilot punches were used at each station. Station 1, pierce pilot holes, rotor slots, and rotor-shaft hole; station 2, pierce stator rivet holes and blank rotor; station 3, pierce
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Published: 01 January 2006
Fig. 5 Small-diameter laminations produced in progressive dies. Dimensions given in inches
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Published: 01 December 1998
Fig. 14 Typical laminations blanked and pierced from electrical sheet. (a) Laminations for rotating electrical machinery are blanked and pierced in single-station dies ( Fig. 15 ) or progressive dies ( Fig. 16 ). Slots can also be made in precut blanks, one at a time, with notching dies. (b
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Image
Published: 01 December 1998
Fig. 15 Sequence of operations for producing stator and rotor laminations using single-station dies. Operation 1, stock blanked and pierced; operation 2, stator lamination notched; operation 3, rotor lamination separated from stator lamination; operation 4, rotor lamination notched. Compare
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Image
Published: 01 December 1998
Fig. 16 Blanking and piercing sequence for rotor and stator laminations in a five-station progressive die. Two pilot punches were used at each station. Station 1, pierce pilot holes, rotor slots, and rotor-shaft hole; station 2, pierce stator rivet holes and blank rotor; station 3, pierce
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Published: 01 January 2005
Fig. 33 Laminations in rolled steel sheet resulting from insufficient cropping of the pipe from the top of a conventionally cast ingot. Courtesy of V. Demski, Teledyne Rodney Metals
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Published: 01 November 2010
Fig. 18 Degraded laminations resulting from excessive magnetic saturation and overheating due to improper design. Source: Ref 42
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in Crystallographic Analysis by Electron Backscatter Diffraction in the Scanning Electron Microscope
> Materials Characterization
Published: 15 December 2019
Fig. 12 Pole figures from iron-cobalt transformer laminations. (a) Discreet pole figure. RD, rolling direction; ND, normal direction; TD, transverse direction. (b) Contoured pole figure. Both show the presence of alpha and gamma fiber textures common in rolled and annealed body-centered cubic
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Published: 01 January 2002
Fig. 9 Laminations in rolled steel sheet resulting from insufficient cropping of the pipe from the top of a conventionally cast ingot. Courtesy of V. Demski, Teledyne Rodney Metals
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Published: 01 January 2002
Fig. 25 Porosity in GMAW core-plated silicon steel laminations. 100×
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Book Chapter
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003378
EISBN: 978-1-62708-195-5
... the development of the relations between mid-surface strains and curvatures and membrane stress and moment resultants. The article discusses the properties, such as thermal expansion, moisture expansion, and conductivity, of symmetric laminates and unsymmetric laminates. It describes the distribution...
Abstract
The properties of unidirectional composite (UDC) materials are quite different from those of conventional, metallic materials. This article provides information on the treatment of UDC stress-strain relations in the forms appropriate for analysis of thin plies of material. It explains the development of the relations between mid-surface strains and curvatures and membrane stress and moment resultants. The article discusses the properties, such as thermal expansion, moisture expansion, and conductivity, of symmetric laminates and unsymmetric laminates. It describes the distribution of temperature and moisture through the thickness of a laminate. Stresses caused due to mechanical loads, temperature, and moisture on the laminate are analyzed. The article concludes with information on interlaminar cracking, free-edge delamination, and transverse cracks of laminates.
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