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Book: Powder Metallurgy
Series: ASM Handbook
Volume: 7
Publisher: ASM International
Published: 30 September 2015
DOI: 10.31399/asm.hb.v07.a0006106
EISBN: 978-1-62708-175-7
... Abstract Bronze and brass alloys are two key classes of materials in copper-base powder metallurgy applications. They are often compacted using mechanical or hydraulic pressing machines. This article provides an overview of the powder pressing process, providing information on the powder...
Abstract
Bronze and brass alloys are two key classes of materials in copper-base powder metallurgy applications. They are often compacted using mechanical or hydraulic pressing machines. This article provides an overview of the powder pressing process, providing information on the powder properties of bronze and brass and the roles of lubricant and compaction dies in the pressing process. It discusses the structural defects that originate during the compaction process. The article also describes the major factors that influence the sintering response in bronze, prealloyed bronze, brass, and nickel-silver.
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in Copper Powder Metallurgy Products
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 12 P/M brass components. (a) Brass rack guide for rack-and-pinion steering column of an electric outdoor motor. (b) Leaded brass rack for a stereo three-dimensional microscope. (c) Leaded brass objective mounts for a microscope. Courtesy of Metal Powder Industries Federation.
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Published: 01 June 2016
Fig. 20 Annealing curves of yellow brass (C27000, 65%Cu-35%Zn) and red brass (C23000, 85%Cu-15%Zn). Effect of annealing temperature (for 1 h) on (a) ultimate tensile strength, (b) grain size, (c) percent elongation of yellow wire, and (d) effect of annealing time on grain size of C27000
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Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002411
EISBN: 978-1-62708-193-1
... Abstract Copper alloys are classified by the International Unified Numbering System designations to identify alloy groups by major alloying element. This article presents the designations and compositions of various copper alloys, such as brasses, nickel silvers, bronzes, beryllium coppers...
Abstract
Copper alloys are classified by the International Unified Numbering System designations to identify alloy groups by major alloying element. This article presents the designations and compositions of various copper alloys, such as brasses, nickel silvers, bronzes, beryllium coppers, and spinodal alloys. It discusses the fatigue testing of the copper alloys and tabulates the tensile and fatigue strengths of the copper alloys. The article schematically illustrates S-N curves for the solid-solution (non-aging) strengthened alloys. It concludes with a discussion on the role of microstructure in the fatigue performance of beryllium copper alloys.
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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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Published: 01 January 1986
Fig. 16a Scanning electron micrograph of the aluminum/brass interface showing atomic number contrast. Analysis of numbered regions given in Table 5 . See also Fig. 16(b) , 16(c) , and 16(d) .
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Published: 01 January 1986
Fig. 16b X-ray dot map for aluminum at the aluminum/brass interface shown in Fig. 16(a) .
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Published: 01 January 1986
Fig. 16c X-ray dot map for zinc at the aluminum/brass interface shown in Fig. 16(a) .
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Published: 01 January 1986
Fig. 16d X-ray dot map for copper at the aluminum/brass interface shown in Fig. 16(a) . Source: Ref 27
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Published: 01 January 1986
Fig. 30 Representative Auger survey spectra from an α-brass sample cracked in a nontarnishing ammonia solution. (a) Ductile region. (b) Transgranular SCC facet
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Published: 01 January 1986
Fig. 31 Auger data from a series of points near the crack tip on an α-brass sample cracked in a nontarnishing ammonia solution. (a) Oxygen concentration versus distance from the transition zone. (b) Copper/zinc ratio versus distance from the transition zone
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Published: 01 January 1987
Fig. 54 Stress-corrosion fractures in a Cu-30Zn brass tested in distilled water at a potential of E = 0 V SCE (SCE, saturated calomel electrode). Brass containing 0.002% As fails by predominantly intergranular decohesion (a), and one with 0.032% As fails by a combination of cleavage
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Published: 01 January 1987
Fig. 55 Stress-corrosion fracture in a Cu-30Zn brass with 0.032% As tested in water containing 5 × 10 −3 % sulfur dioxide at a potential of E = 0.05 V SCE . The periodic marks are believed to be the result of a stepwise mode of crack propagation. Source: Ref 176
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Published: 01 January 2002
Fig. 47 AISI H13 mandrel used to pierce and extrude brass that failed after 298 pushes, about 30% of its expected life. The disk shown below, cut from the mandrel, was macroetched (10% aqueous nitric acid), revealing a heavily decarburized surface. The decarburization occurred during service.
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Published: 01 January 2002
Fig. 4 Failed aluminum brass condenser tube from a saltwater heat exchanger. The tube failed from pitting caused by hydrogen sulfide and chlorides in the feedwater. (a) Cross section of tube showing deep pits and excessive metal wastage. 2 3 4 ×. (b) Higher magnification view of a pit
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Published: 01 January 2002
Fig. 10 Failed admiralty brass heat-exchanger tubes from a refinery reformer unit. The tubes failed by corrosion fatigue. (a) Circumferential cracks on the tension (outer) surface of the U-bends. Approximately 1 1 4 ×. (b) Blunt transgranular cracking from the water side of tube 1. 40×
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Published: 01 January 2002
Fig. 38 Intergranular attack of Admiralty B brass in a hot water containing a small amount of sulfuric acid. 150×
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Published: 01 January 2002
Fig. 40 Views of a through-wall perforation of a chromium-plated α brass (70Cu-30Zn) tube removed from a potable water system due to dezincification. (a) Macroview of tube. (b) Inside diameter surface of the tube shown in (a), depicting localized green deposits at the areas of dezincification
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Published: 01 January 2002
Fig. 42 Effect of pH on time-to-fracture by SCC. Data are for brass in ammoniacal copper sulfate solution at room temperature.
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Published: 01 January 2002
Fig. 48 Micrographic montage of a longitudinal crack in a brass tube from a generator air cooler. The inside diameter of the tube is at the bottom. Etched in potassium dichromate. 100×
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