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aluminum alloy forging
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Published: 01 January 2002
Fig. 12 Fracture surface of a high-strength aluminum alloy forging that failed from stress corrosion. Progression marks similar to those observed in fatigue fractures are evident. Source: Ref 13
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Published: 01 January 2002
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Published: 01 January 2005
Fig. 18 No-draft, close-tolerance aluminum alloy forging for a stabilizer support fitting. Detail A shows a rib 0.125 in. wide with an h : w ratio of 23 to 1. Dimensions given in inches
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Image
Published: 01 January 2005
Fig. 20 Partial close-tolerance aluminum alloy forging for sponson attachment fittings that was forged in a tilted position to produce a rib 2.5 mm (0.10 in.) thick with a maximum height-to-width ratio of 17 to 1 (section A-A). Dimensions given in inches
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Image
Published: 01 January 2005
Fig. 21 Conventional aluminum alloy forging for a wing front spar terminal fitting, with a dorsal rib that was preblocked as a web and then blocked and finished as a rib. Dimensions given in inches
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Published: 01 January 2005
Fig. 8 Finished conventional aluminum alloy forging for engine removal door support (a). The face of the bottom insert for the blocker forging used in making the forging is shown in (b). Sections of the insert used to contain flash are shown in (c). See Example 5 . Dimensions given in inches.
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Published: 15 January 2021
Fig. 51 Micrograph of stress-corrosion cracking in an aluminum alloy forging. Original magnification: 277×
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Published: 15 January 2021
Fig. 52 Macrograph of stress-corrosion cracking in an aluminum alloy forging that exhibits widening of stress-corrosion cracks adjacent to the exposed surface. Original magnification: 11×
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Image
Published: 01 January 1989
Fig. 15 Rough and finish boring of a heat-treated aluminum alloy forging. Dimensions in figure given in inches Speed, at 1200 rev/min, m/min (sfm) 97 (318) Feed, mm/min (in./min) 35.6 (1.4) Cutting fluid Kerosene plus proprietary oil Production rate, pieces/h 9 Tool life
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Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0003996
EISBN: 978-1-62708-185-6
... Abstract This article begins with discussion on forgeability and the factors affecting the forgeability of aluminum and aluminum alloys. It describes the types of forging methods and equipment and reviews critical elements in the overall aluminum forging process: die materials, die design...
Abstract
This article begins with discussion on forgeability and the factors affecting the forgeability of aluminum and aluminum alloys. It describes the types of forging methods and equipment and reviews critical elements in the overall aluminum forging process: die materials, die design, and die manufacture. The article discusses the critical aspects of various manufacturing elements of aluminum alloy forging, including the preparation of the forging stock, preheating stock, die heating, lubrication, trimming, forming and repair, cleaning, heat treatment, and inspection. It concludes with a discussion on the forging of advanced aluminum materials and aluminum alloy precision forgings.
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Published: 01 January 2005
Fig. 9 Aluminum alloy forgings for which the use of knockout pins was optional. (a) Vertical fin attachment with 3° draft. (b) Window frame with 1° draft. Dimensions given in inches.
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Published: 01 January 2005
Fig. 10 Aluminum alloy forgings that incorporate design draft. (a) Pylon bulkhead forging. (b) Stabilizer support forging. Dimensions given in inches.
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Image
Published: 01 January 2005
Fig. 14 Conventional aluminum alloy forgings for gimbal ring: ring-rolled (a) and finished by closed-die forging (b). See Example 8 . Dimensions in figure given in inches Item Conventional closed-die forging (revised) Material and temper Aluminum alloy 2014-T6 (a) Forging
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Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006721
EISBN: 978-1-62708-210-5
... Abstract This datasheet provides information on composition limits, fabrication characteristics, processing effects on physical and tensile properties, and applications of aluminum forging alloy 6151. Tensile property limits for aluminum alloy 6151 is also provided. aluminum forging alloy...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006493
EISBN: 978-1-62708-207-5
... such as workpiece and die temperature, strain rate, and deformation mode. The article describes the relative forgeability of the ten most widely used aluminum alloys, and reviews common forging equipment, including hammers, mechanical and screw presses, and hydraulic presses. It also discusses postforge operations...
Abstract
This article examines aluminum forging processes, including open-die, closed-die, upset, roll, orbital, spin, and mandrel forging, and compares and contrasts their capabilities and the associated design requirements for forged parts. It discusses the effect of key process variables such as workpiece and die temperature, strain rate, and deformation mode. The article describes the relative forgeability of the ten most widely used aluminum alloys, and reviews common forging equipment, including hammers, mechanical and screw presses, and hydraulic presses. It also discusses postforge operations such as trimming, forming, repairing, cleaning, and heat treatment.
Image
Published: 01 January 2005
Fig. 7 Aluminum alloy hinge forging shown as (a) a finished forging and (b) as a blocker forging. Section A-A includes the outline for a tapered fairing, which was removed before finish forging, and shows the design of the flash cavity. See Example 4 . Dimensions given in inches.
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Image
Published: 01 January 1987
Fig. 980 Fatigue fracture of an aluminum alloy 2014-T6 heat-treated forging. Details of the heat-treatment procedure were not available. Some machining was carried out on the forging prior to heat treatment. The aircraft structural component cracked in service. The horizontal lines
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Published: 01 January 1987
Fig. 1004 An aluminum alloy 7075-T736 aircraft main landing gear forging, similar to that described in Fig. 1002 and 1003 , which was shot peened on its inner-diameter surface to enhance fatigue resistance. The shot-peened part withstood cycles far beyond the number required for acceptance
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Published: 01 January 2002
Fig. 14 Beach marks on a fatigue fracture in aluminum alloy 7075-T73 forging. The light-colored reflective bands are zones of fatigue crack propagation. At high magnifications, thousands of fatigue striations can be resolved within each band. The dull, fibrous bands are zones of crack
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Image
Published: 01 January 2002
Fig. 39 Opened crack in part of an aluminum alloy aircraft undercarriage forging. Note suggestion of beach marks in the fracture, indicating that, in later stages, crack propagation occurred in a series of steps. −0.04×
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