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extruding

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Published: 01 July 2009
Fig. 20.14 Backward extruding and upset forging of a beryllium part using a deformable steel ring to support the billet during forging. Source: ASM 1970 More
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Published: 30 September 2023
Figure 10.23: Complex canning arrangement, including composite billet for extruding tungsten tubes at 1210°C. More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2006
DOI: 10.31399/asm.tb.ex2.t69980009
EISBN: 978-1-62708-342-3
... Abstract The hot-working process extrusion is used to produce semifinished products in the form of bar, strip, and solid sections, as well as tubes and hollow sections. The first part of this chapter describes the composition, properties, and applications of tin and lead extruded products...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2006
DOI: 10.31399/asm.tb.ex2.t69980195
EISBN: 978-1-62708-342-3
... spectrum of materials to be extruded. This chapter focuses on the processes involved in the extrusion of semifinished products in various metals and their alloys, namely tin, lead, lead-base soft solders, tin-base soft solders, zinc, magnesium, aluminum, copper, titanium, zirconium, iron, nickel...
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Published: 01 December 2006
Fig. 2.44 Extruded cross-sectional geometry of the extruded external skin with integrated stringers. Source: Daimler Benz Aerospace Airbus More
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Published: 01 January 2017
Fig. 9.3 Stress-corrosion cracking in an extruded Mg-6Al-1Zn alloy tested in a salt-chromate solution, showing (a) intergranular crack propagation in the furnace-cooled alloy and (b) transgranular propagation in the water-quenched material. Source: Ref 9.26 More
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Published: 01 December 1984
Figure 1-21 Examples of segregation associated with central bursts in extruded AISI 1141 modified steel. The streaks, which consist of martensite, have a hardness of 46 to 58 HRC (Rockwell hardness on the C scale) while the matrix hardness is less than 20 HRC. More
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Published: 01 August 2005
Fig. 2.98 Stress-corrosion cracking in an extruded Mg-6Al-1Zn alloy tested in a salt-chromate solution. (a) Intergranular crack propagation in the face-cooled alloy. (b) Transgranular crack propagation in the water-quenched material. Source: Ref 2.72 More
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Published: 01 November 2011
Fig. 6.15 Shear welding: (a) and (b) extruded groove and tongue for shear welding, (c) assembled joint, (d) sandwich constructions assembled by shear welding of extruded aluminum profiles, and (e) air cooler. Source: Ref 6.8 More
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Published: 01 August 1999
Fig. 9 Transverse sections were taken from a 7075-T6 extruded shape and macroetched. Various specimen locations are also shown: A—tensile bar, longitudinal; B and C—tensile bar, long transverse; D—tensile bar, transverse; E—tensile bar, short transverse; F—C-ring, short transverse. Micrographs More
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Published: 01 November 2013
Fig. 31 Effect of tensile strength of steel being extruded on ram pressure required for backward and forward extrusion at different ratios. Source: Ref 10 More
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Published: 01 March 2000
Fig. 12 Direct press extrudes aluminum landing mats for aircraft from rectangular container. Source: Taber Metals L.P. More
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Published: 01 March 2000
Fig. 24 Photograph of tapered-seal hollow die. Source: Florida Extruded International, Inc. More
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Published: 01 March 2000
Fig. 30 Change of shape of the extruded aluminum alloy square tube (a) before die wear and (b) after die wear More
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Published: 01 March 2000
Fig. 2 Extruded aluminum shapes. Source: Cardinal Aluminum Co. More
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Published: 01 March 2000
Fig. 15 Classification of aluminum extruded section. Source: Ref 7 More
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Published: 01 March 2000
Fig. 31 Tube cross section from 6061 extruded at two different billet temperatures. (a) Normal billet temperature. (b) High billet temperature More
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Published: 01 July 2009
Fig. 13.13 Effect of heat treatment on the ductility of cast and extruded beryllium. Heat treatment at 780 °C (1435 °F) for 120 h. Source: Brown et al. 1960 More
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Published: 01 July 2009
Fig. 14.2 Longitudinal properties of as-extruded and heat treated (annealed) beryllium-aluminum alloy extrusions as a function of aluminum content. Source: London 1979 More
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Published: 01 July 2009
Fig. 21.3 Effect of various treatments on the fatigue life of extruded ingot beryllium. ▴, annealed, etched 0.46 mm (0.02 in.) deep; ▪, annealed, etched 0.46 mm deep (245 MPa, or 36 ksi); •, annealed, etched 0.05 mm (0.002 in.) deep (236 MPa, or 34 ksi); □, annealed (259 MPa, or 38 ksi More