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Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003665
EISBN: 978-1-62708-182-5
... Abstract Exfoliation is a structure-dependent form of localized intergranular corrosion that follows grain boundaries in the rolling direction of wrought materials, particularly aluminum alloys. Highly cold-worked materials with elongated grain boundaries tend to be most affected. The article...
Abstract
Exfoliation is a structure-dependent form of localized intergranular corrosion that follows grain boundaries in the rolling direction of wrought materials, particularly aluminum alloys. Highly cold-worked materials with elongated grain boundaries tend to be most affected. The article provides information on accelerated salt spray and total-immersion testing methods to help rate the exfoliation corrosion susceptibility of various aluminum alloys and alloy compositions. It also discusses visual assessment challenges and identifies several ASTM designations and where and how they apply.
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Forms of corrosion in aircraft. (a) Exfoliation corrosion. (b) Microbiologi...
Available to PurchasePublished: 01 January 2006
Fig. 12 Forms of corrosion in aircraft. (a) Exfoliation corrosion. (b) Microbiologically induced corrosion on fuel tank access door. (c) Bushing assembly. (d) Galvanic corrosion under aluminum-nickel bronze bushing, seen with bushing removed. See the article “Corrosion in Commercial Aviation
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Forms of corrosion in aircraft. (a) Exfoliation corrosion. (b) Microbiologi...
Available to PurchasePublished: 01 January 2006
Fig. 2 Forms of corrosion in aircraft. (a) Exfoliation corrosion. (b) Microbiologically induced corrosion on fuel tank access door. (c) (d) Galvanic corrosion under aluminum-nickel bronze bushing
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Image
Detection of galvanic exfoliation corrosion in aluminum wing skins. (a) Sch...
Available to PurchasePublished: 01 August 2018
Fig. 52 Detection of galvanic exfoliation corrosion in aluminum wing skins. (a) Schematic showing source and growth of galvanic exfoliation corrosion. (b) Eddy current impedance responses for exfoliation corrosion around fastener holes in wing skins. (c) Schematic illustrating use of circle
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Exfoliation corrosion in an alloy 7178-T651 plate exposed to a seacoast env...
Available to PurchasePublished: 01 December 1998
Fig. 2 Exfoliation corrosion in an alloy 7178-T651 plate exposed to a seacoast environment. Cross section of the plate shows how exfoliation develops by corrosion along boundaries of thin, elongated grains.
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Image
Exfoliation corrosion of an aluminum T-45 cockpit kick plate angle resultin...
Available to PurchasePublished: 01 January 2006
Fig. 11 Exfoliation corrosion of an aluminum T-45 cockpit kick plate angle resulting from water intrusion within cockpit areas. Courtesy of J. Benfer, Naval Air Depot, Jacksonville. See the article “U.S. Navy Aircraft Corrosion” in this Volume.
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Published: 15 June 2019
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Exfoliation corrosion in an alloy 7178-T651 plate exposed to a seacoast env...
Available to PurchasePublished: 15 June 2019
Fig. 16 Exfoliation corrosion in an alloy 7178-T651 plate exposed to a seacoast environment. Cross section of the plate shows how exfoliation develops by corrosion along boundaries of thin, elongated grains.
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Image
Exfoliation corrosion in an alloy 7178-T651 plate exposed to a seacoast env...
Available to PurchasePublished: 01 January 2005
Fig. 17 Exfoliation corrosion in an alloy 7178-T651 plate exposed to a seacoast environment. Cross section of the plate shows how exfoliation develops by corrosion along boundaries of thin, elongated grains
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Exfoliation corrosion resistance of alloy 7055-T765 (ASTM rating EB) is muc...
Available to PurchasePublished: 01 January 2006
Fig. 11 Exfoliation corrosion resistance of alloy 7055-T765 (ASTM rating EB) is much superior to that for 7075-T65 (ASTM rating ED)
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Published: 01 January 2006
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Internal exfoliation corrosion of a barostatic release unit associated with...
Available to PurchasePublished: 01 January 2006
Fig. 8 Internal exfoliation corrosion of a barostatic release unit associated with an F-14 ejection seat. Courtesy of J. Benfer, Naval Air Depot—Jacksonville
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Exfoliation corrosion of a integral fuel tank on a P-3 aircraft resulting f...
Available to PurchasePublished: 01 January 2006
Fig. 9 Exfoliation corrosion of a integral fuel tank on a P-3 aircraft resulting from long-term exposure to moisture, salts, and fuel-system icing inhibitors. Courtesy of J. Benfer, Naval Air Depot—Jacksonville
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Image
Exfoliation corrosion of an aluminum T-45 cockpit kick plate angle resultin...
Available to PurchasePublished: 01 January 2006
Fig. 18 Exfoliation corrosion of an aluminum T-45 cockpit kick plate angle resulting from water intrusion within cockpit areas. Courtesy of J. Benfer, Naval Air Depot—Jacksonville
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Image
Exfoliation corrosion around a fastener hole in a 7049-T73 aluminum alloy l...
Available to PurchasePublished: 01 January 2006
Fig. 3 Exfoliation corrosion around a fastener hole in a 7049-T73 aluminum alloy longeron. Radial arrows indicate measurements taken to assess damage.
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Book Chapter
Military Aircraft Corrosion Fatigue
Available to PurchaseSeries: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004128
EISBN: 978-1-62708-184-9
... inspection intervals, and perform repair and maintenance of aircraft in service. It illustrates the types of corrosive attack observed in aircraft structures, including uniform, galvanic, pitting, filiform, fretting, intergranular, exfoliation corrosion, and stress-corrosion cracking. The article discusses...
Abstract
Corrosion, fatigue, and their synergistic interactions are among the principal causes of damage to aircraft structures. This article describes aircraft corrosion fatigue assessment in the context of different approaches used to manage aircraft structural integrity, schedule aircraft inspection intervals, and perform repair and maintenance of aircraft in service. It illustrates the types of corrosive attack observed in aircraft structures, including uniform, galvanic, pitting, filiform, fretting, intergranular, exfoliation corrosion, and stress-corrosion cracking. The article discusses geometric parameters such as pit dimensions, surface roughness, loss of metal thickness, and volume increase due to pillowing to quantitatively characterize the types of corrosion. It also explains the two most common fatigue life assessment methods used in the military aerospace industry: fatigue crack initiation and crack growth analysis.
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004169
EISBN: 978-1-62708-184-9
... Abstract This article describes the commonly observed forms of airplane corrosion, namely: general corrosion, exfoliation corrosion, pitting corrosion, microbiologically induced corrosion, galvanic corrosion, filiform corrosion, crevice corrosion, stress-corrosion cracking, and fretting...
Abstract
This article describes the commonly observed forms of airplane corrosion, namely: general corrosion, exfoliation corrosion, pitting corrosion, microbiologically induced corrosion, galvanic corrosion, filiform corrosion, crevice corrosion, stress-corrosion cracking, and fretting. It discusses the factors influencing airplane corrosion from the manufacturing perspective: design, manufacturing, and service-related factors. The article explains the collection of corrosion data and provides an overview of the implementation and evolution of airline corrosion prevention and control programs and directions being considered in the design for corrosion prevention of airplanes.
Book: Corrosion: Materials
Series: ASM Handbook
Volume: 13B
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v13b.a0003815
EISBN: 978-1-62708-183-2
... Abstract This article focuses on the various forms of corrosion that occur in the passive range of aluminum and its alloys. It discusses pitting corrosion, galvanic corrosion, deposition corrosion, intergranular corrosion, stress-corrosion cracking, exfoliation corrosion, corrosion fatigue...
Abstract
This article focuses on the various forms of corrosion that occur in the passive range of aluminum and its alloys. It discusses pitting corrosion, galvanic corrosion, deposition corrosion, intergranular corrosion, stress-corrosion cracking, exfoliation corrosion, corrosion fatigue, erosion-corrosion, atmospheric corrosion, filiform corrosion, and corrosion in water and soils. The article describes the effects of composition, microstructure, stress-intensity factor, and nonmetallic building materials on the corrosion behavior of aluminum and its alloys. It also provides information on the corrosion resistance of anodized aluminum in contact with foods, pharmaceuticals, and chemicals.
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003646
EISBN: 978-1-62708-182-5
... Abstract This article discusses the applications and use of salt spray (fog) testing used to test the resistance of aluminum alloys to exfoliation corrosion. There are two basic types of salt-spray/fog corrosion tests: static condition tests and cyclic condition tests. The article provides...
Abstract
This article discusses the applications and use of salt spray (fog) testing used to test the resistance of aluminum alloys to exfoliation corrosion. There are two basic types of salt-spray/fog corrosion tests: static condition tests and cyclic condition tests. The article provides a discussion of these tests and indicates the significant differences in each type test used in the combination of weathering and corrosion testing procedures. It also provides information on the test specimen preparation for spray (fog) corrosion tests. Industry specific standards for test specimen procedures often reference the ASTM standards as a basis. The article includes various ASTM standards that describe several cleaning procedures used prior to testing. It describes the major components of a corrosion test chamber.
Book Chapter
Corrosion Resistance of Aluminum and Aluminum Alloys
Available to PurchaseSeries: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003130
EISBN: 978-1-62708-199-3
... and aluminum alloys, including pitting corrosion, intergranular corrosion, exfoliation corrosion, galvanic corrosion, stray-current corrosion, deposition corrosion, crevice corrosion, filiform corrosion, stress-corrosion cracking, corrosion fatigue, and hydrogen embrittlement. The article also presents a short...
Abstract
This article discusses the corrosion resistance of aluminum and aluminum alloys in various environments, such as in natural atmospheres, fresh waters, seawater, and soils, and when exposed to chemicals and their solutions and foods. It describes the forms of corrosion of aluminum and aluminum alloys, including pitting corrosion, intergranular corrosion, exfoliation corrosion, galvanic corrosion, stray-current corrosion, deposition corrosion, crevice corrosion, filiform corrosion, stress-corrosion cracking, corrosion fatigue, and hydrogen embrittlement. The article also presents a short note on aluminum clad products and corrosion at joints.
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