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cadmium plating
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Book: Surface Engineering
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001247
EISBN: 978-1-62708-170-2
... of cadmium plating with attention to the materials of construction and equipment used. The article provides a description of the selection of plating method with examples, applications, and several postplating processes of cadmium plating. anode system bath temperature brighteners cadmium plating...
Abstract
Electrodeposits of cadmium are used to protect steel and cast iron against corrosion. This article provides an overview of the surface preparation of, and brighteners used in, cyanide baths. It focuses on the anode system, current density, deposition rates, and bath temperature of cadmium plating with attention to the materials of construction and equipment used. The article provides a description of the selection of plating method with examples, applications, and several postplating processes of cadmium plating.
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Published: 01 January 1994
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Published: 01 January 1994
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Published: 01 January 1994
Fig. 4 Flow diagram showing cadmium plating operation relative to overall cleaning and post-treatment operations for steel and cast iron components Solution No. Composition Amount Temperature Immersion time °C °F 1 H 2 SO 4 8–12 vol% 71-93 160-200 10–120 s 2 HCl
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Published: 01 January 1994
Fig. 7 Application of shields to obtain shim having a uniform cadmium plating. The 305 mm (12 in.) long and 38 mm (1 in.) wide shim was plated to the required thickness of 13 ± 5 μm (520 ± 200 μin.).
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Published: 01 January 1994
Fig. 10 Thickness distribution for cadmium plating of 90 samples that were evaluated from a 5000-piece production lot
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Published: 01 January 2002
Fig. 12 Cadmium-plated 8740 steel aircraft-wing assembly nut that failed by hydrogen embrittlement. The nut was not baked after electroplating to release hydrogen. (a) Overall view. 5×. (b) Fracture surface. 9×. (c) Scanning electron micrograph of typical intergranular fracture shown in box
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Published: 01 January 2002
Fig. 13 Cadmium-plated alloy steel self-retaining bolts that fractured because of hydrogen damage. (a) Fractured and unused intact bolt. (b) Fractured bolt; brittle fracture surface is indicated by A and B. (c) and (d) Electron fractographs of surfaces A and B, respectively, showing brittle
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Published: 01 January 2002
Fig. 14 Cadmium-plated AISI 8740 alloy steel fasteners that failed by hydrogen embrittlement. See also Fig. 15 .
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Published: 01 January 2002
Fig. 16 Cadmium-plated 4140 steel nuts from a military jet engine that failed by LME. (a) Fragmented and cracked nuts. (b) Typical fracture surface. (c) Electron fractograph showing brittle intergranular fracture
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Published: 01 January 2002
Fig. 1 Cadmium-plated AISI 8740 steel nut that failed by hydrogen embrittlement. Failure occurred seven days after installation on an aircraft wing structure. See also Fig. 2. 5×. Courtesy of Lockheed-Georgia Company
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Published: 01 January 2002
Fig. 2 Fracture surface of failed cadmium-plated nut in Fig. 1 . (a) Macrograph of fracture surface; 15×. (b) Scanning electron micrograph of the area in the box in (a) showing typical intergranular fracture; 3950×. Courtesy of Lockheed-Georgia Company
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Published: 01 January 2002
Fig. 3 Service failure of a low-alloy steel nut by LMIE. Cadmium-plated, 4140 low-alloy steel (44 HRC) nuts were inadvertently used on bolts for clamps used to join ducts that carried hot (500 °C, or 930 °F) air from the compressor of a military jet engine. (a) The nuts were fragmented
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Published: 01 January 2002
Fig. 6 Failed Ti-6AI-4V shear fastener. The fasteners were cadmium plated for galvanic compatibility with the aluminum structure. (a) Photograph showing failure at the head-to-shank fillet. (b) Intergranular fracture morphology. Failure was attributed to LMIE caused by excessive temperature
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Published: 01 January 1994
Fig. 8 Couplings that were uniformly cadmium plated with the aid of a 6.4 mm ( 1 4 in.) diameter anode centered in the bore during the plating operation. Plating thickness ranges from 8 to 13 μm (320 to 520 μin.).
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Published: 15 January 2021
Fig. 1 Cadmium-plated AISI 8740 steel nut that failed by hydrogen embrittlement. Failure occurred seven days after installation on an aircraft wing structure. See also Fig. 2 . Original magnification: 5×. Courtesy of Lockheed-Georgia Company
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Published: 15 January 2021
Fig. 2 Fracture surface of failed cadmium-plated nut in Fig. 1 . (a) Macrograph of fracture surface. Original magnification: 15×. (b) Scanning electron micrograph of the area in the box in (a) showing typical intergranular fracture. Original magnification: 3950×. Courtesy of Lockheed-Georgia
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Published: 15 January 2021
Fig. 7 Failed Ti-6Al-4V shear fasteners. The fasteners were cadmium plated for galvanic compatibility with the aluminum structure. (a) Photograph showing failure at the head-to-shank fillet. (b) Intergranular fracture morphology. Failure was attributed to liquid-metal-induced embrittlement
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Published: 01 January 2003
Fig. 4 Embrittlement behavior of cadmium-plated 4340 steel. Specimens were tested in delayed failure at 300 °C (570 °F) and unplated steel in air at 300 °C (570 °F). Source: Ref 3
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Published: 01 January 2003
Fig. 5 Embrittlement behavior of cadmium-plated 4340 steel. Specimens were tested in delayed failure at temperatures ranging from 360 to 230 °C (680 to 445 °F). Source: Ref 3
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