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in X-Ray—Radiography and Computed Tomography in Additive Manufacturing
> Additive Manufacturing Design and Applications
Published: 30 June 2023
Fig. 9 Sheet-based gyroid lattice structure showing the sheet thickness evaluation using computed tomography data
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Image
Published: 01 January 2006
Fig. 3 Fracture limit of an aluminum sheet (AlMg0.4Si1.2-ka; sheet thickness, 1.25 mm or 0.05 in.) in straight flanging. Source: Ref 4
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Image
Published: 01 January 2006
Fig. 3 Hole punching parameters. (a) Allowable sheet thickness-to-punch diameter for hole punching as a function of material shear strength. (b) Minimum punch diameter (hole size) as a function of material thickness for three materials: A, 195 MPa (28 ksi) copper; B, 345 MPa (50 ksi) steel; C
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Image
Published: 01 January 2006
Fig. 20 Schematic of springback in a bending operation. t is sheet thickness, R 0 and, α 0 are the die radius and bend angle, and R f and α f are the part radius and bend angle after springback.
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Published: 01 January 2006
Fig. 8 Stretch-formed specimen. Material: MgAl3Zn1 (AZ31); initial sheet thickness, s 0 : 1.3 mm (0.051 in.); forming temperature: 250 °C (480 °F). Source: Ref 15
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Image
Published: 01 January 2006
Fig. 12 As-rolled-dependent flow curves of MgAl3Zn1 (AZ31) (initial sheet thickness, s 0 =1.0 mm, or 0.039 in.) determined in the uniaxial tensile test at temperatures of 20 and 200 °C (70 and 390 °F). ε ˙ , strain rate
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Image
Published: 01 January 2006
Fig. 11 Alloy 25 welded cylinder (sheet thickness, 1.7 mm, or 0.066 in.) in position for explosive forming. Dimensions given in inches
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Published: 01 January 2006
Fig. 12 The ratio of supported length l to sheet thickness t determines whether or not a blankholder is required for deep drawing.
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Published: 01 January 2006
Fig. 11 Comparison of sheet thickness predicted by the sine law and a simplified modeling approach (SMA) with experimental data. Source: Ref 2
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Published: 01 January 1986
Fig. 14 Copper alloy 26000 (cartridge brass, 70%) sheet, hot rolled to a thickness of 10 mm (0.4 in.), annealed, cold rolled to a thickness of 6 mm (0.239 in.), and annealed to a grain size of 0.120 mm (0.005 in.). At this reduction, grains are basically equiaxed. Compare with Fig. 15
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Image
Published: 01 December 2004
Fig. 22 Copper alloy 26000 (cartridge brass, 70%) sheet, hot rolled to a thickness of 10 mm (0.4 in.), annealed, cold rolled to a thickness of 6 mm (0.230 in.), and annealed to a grain size of 0.120 mm (0.005 in.). At this reduction, grains are basically equiaxed. Compare with Fig. 23
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in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 45 Sheet samples with an initial width-to-thickness ratio of 6. (a) Single local neck (sample with tensile strength of 1586 MPa, or 230 ksi). (b) Two local necks (sample tensile strength of 827 MPa, or 120 ksi). (c) Fracture of specimen in (a)
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Published: 01 January 2006
Fig. 11 Correlation between sheet thinning and bending. The final thickness ( t f ) depends on initial thickness ( t 0 ) and bending angle (θ). Source: Ref 26
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Published: 01 January 2006
Fig. 37 Schematic of the concept of forming a sheet material that has a thickness profile before forming
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Published: 01 November 2010
Fig. 5 Cross sections of side-trimmed edge sheet of thickness 0.147 mm for 15° rake angle. Unit shown is 400 μm. Clearance: (a) 0, (b) 0.30, (c) 0.43, and (d) 0.50 mm
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Book Chapter
Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005179
EISBN: 978-1-62708-186-3
... Abstract This article introduces process factors that influence die wear and lubrication for metal forming operations such as bending, spinning, stretching, deep drawing, and ironing. It discusses the effects of part shape, sheet thickness, tolerance requirements, sheet metal, and lubrication...
Abstract
This article introduces process factors that influence die wear and lubrication for metal forming operations such as bending, spinning, stretching, deep drawing, and ironing. It discusses the effects of part shape, sheet thickness, tolerance requirements, sheet metal, and lubrication on shallow forming dies. The article describes the wear of material for dies to draw round and square cup-shaped metal parts in a press. It also discusses the effect of process conditions on the shallow forming dies.
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Published: 01 December 1998
Fig. 1 Typical mechanical properties of low-carbon steel sheet shown by the range of properties in steel furnished by three mills. Hot-rolled sheet thickness from 1.519 to 3.416 mm (0.0598 to 0.1345 in., or 16 to 10 gage); cold-rolled sheet thickness from 0.759 to 1.519 mm (0.0299 to 0.0598
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in Carbon and Low-Alloy Steel Sheet and Strip
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 1 Typical mechanical properties of low-carbon steel sheet shown by the range of properties in steel furnished by three mills. Hot-rolled sheet thickness from 1.519 to 3.416 mm (0.0598 to 0.1345 in., or 16 to 10 gage); cold-rolled sheet thickness from 0.759 to 1.519 mm (0.0299 to 0.0598
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Image
Published: 31 October 2011
Fig. 2 (a) Lap seam weld, (b) mash seam weld with flat electrodes, and (c) mash seam weld with radiused (contoured) electrodes. Flat electrodes in mash seam welding should not be used when sheet thickness is less than 1mm (0.040 in.). Radiused electrodes can be used for sheet thicker than 1mm
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Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005101
EISBN: 978-1-62708-186-3
... and expansion, and (c) piercing. Source: Ref 1 Hole Size The size of holes that can be punched is limited by the sheet material strength and thickness. As is evident in Fig. 1 , the hole-making punch is subjected to a compressive load, which is equal to the force required to cause the shearing...
Abstract
Sheet-forming processes provide considerable geometric and material flexibility in meeting these requirements, and design of parts for sheet forming must take into account these benefits as well as the limitations of the processes. This article reviews the basic forming operations and their general geometric features. These operations include hole making, flanging, bead and rib forming, and stretching and drawing for shallow or deep recesses. The article illustrates the general approach to design for sheet forming and the considerations that must be made for material savings and manufacturing ease, in addition to part function. It concludes with information on reducing the amount of scrap in sheet-forming operations.
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