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Book: Corrosion: Materials
Series: ASM Handbook
Volume: 13B
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v13b.a0003969
EISBN: 978-1-62708-183-2
... illustrated. corrosion damage corrosion mechanisms corrosion of metals and alloys corrosion resistant material AS IS APPARENT from Volumes 13A and 13B of the ASM Handbooks, all materials will corrode given certain circumstances, conditions, and time. Although much is understood about...
Abstract
This article is a pictorial guide to forms of corrosion that draws attention to common pitfalls or situations that have caused premature corrosion, sometimes with expensive consequences. The examples used are not exhaustive; they highlight the necessity to fully examine materials, conditions, and specific circumstances that together can reduce the anticipated service life of a component or plant. The color images in this article are categorized according to the type of corrosion following the general order that is adopted in Volume 13A of ASM Handbook. The first table of the article provides a categorization of the forms of corrosion. It also provides a reference to articles or sections of articles in Volume 13A that detail the particular corrosion form or mechanism. The second table is a guide listing the figures in this article by material and by the corrosion form or mechanism illustrated.
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Corrosion damage of a T-45 aircraft access panel. Corrosion initiates at an...
Available to PurchasePublished: 01 January 2006
Fig. 15 Corrosion damage of a T-45 aircraft access panel. Corrosion initiates at and beneath electromagnetic interference (EMI) fingers (removed) needed to control the EMI. Courtesy of J. Benfer, Naval Air Depot—Jacksonville
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Extensive pitting corrosion damage of an aluminum lower longeron from a EA-...
Available to PurchasePublished: 01 January 2006
Fig. 7 Extensive pitting corrosion damage of an aluminum lower longeron from a EA-6B aircraft requiring removal and replacement with newly manufactured item. Courtesy of J. Benfer, Naval Air Depot—Jacksonville
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Fretting corrosion damage on the internal walls of aluminum electrical wire...
Available to PurchasePublished: 01 January 2006
Fig. 10 Fretting corrosion damage on the internal walls of aluminum electrical wire conduit installed within the wing of an EA-6B aircraft. Courtesy of J. Benfer, Naval Air Depot—Jacksonville
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Fasteners that appear solid at the ends may have hidden corrosion damage, s...
Available to PurchasePublished: 01 January 2006
Fig. 1 Fasteners that appear solid at the ends may have hidden corrosion damage, such as the wasp-waisting of bilge fastenings.
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in Failure of Boilers and Related Equipment
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
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Micrograph showing banded ferrite-pearlite structure and corrosion damage a...
Available to Purchase
in Failure of Boilers and Related Equipment
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 62 Micrograph showing banded ferrite-pearlite structure and corrosion damage at outer edge of the failed tube. Original magnification: 200×
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in Corrosion and Remaining Life Assessment
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
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in Corrosion and Remaining Life Assessment
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
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in Corrosion and Remaining Life Assessment
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
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Published: 01 January 2001
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Published: 01 January 2001
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Examples of engine component surface damage. (a) Evidence of hot corrosion ...
Available to PurchasePublished: 01 January 2006
Fig. 8 Examples of engine component surface damage. (a) Evidence of hot corrosion damage on the pressure side of a MAR-M-246 turbine blade. (b) Metallographic section across the airfoil of the MAR-M-246 blade, showing evidence of hot corrosion damage penetrating the leading edge (B) right
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Detail of damage by galvanic corrosion of an iron staff in contact with a c...
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in Corrosion of Metal Artifacts Displayed in Outdoor Environments
> Corrosion: Environments and Industries
Published: 01 January 2006
Fig. 2 Detail of damage by galvanic corrosion of an iron staff in contact with a cast bronze hand on a statue of Mercury (date 1962) located in Kingston, Ontario. Courtesy of Pierre Roberge, Royal Military College of Canada. Photograph 2003
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Fleet damage rate under (a) an effective and (b) an ineffective corrosion-c...
Available to PurchasePublished: 01 January 2006
Fig. 29 Fleet damage rate under (a) an effective and (b) an ineffective corrosion-control program
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Detail of damage by galvanic corrosion of an iron staff in contact with a c...
Available to PurchasePublished: 01 January 2006
Fig. 19 Detail of damage by galvanic corrosion of an iron staff in contact with a cast bronze hand on a statue of Mercury (date 1962) located in Kingston, Ontario. Courtesy of Pierre Roberge. Photograph 2003. See the article “Corrosion of Metal Artifacts Displayed in Outdoor Environments
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Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004127
EISBN: 978-1-62708-184-9
... provides information on the inspections steps, corrosion-control issues, and corrosion-prevention strategies for naval aircraft. It contains a table that lists typical locations of corrosion on the aircraft. The article also provides examples of aircraft corrosion damage. aluminum corrosion control...
Abstract
This article describes the influences of the operational environments of U.S. Navy aircraft during corrosion-control process. The most widely used materials in airframe structures and components, such as aluminum, steel, titanium, and magnesium alloy systems, are reviewed. The article provides information on the inspections steps, corrosion-control issues, and corrosion-prevention strategies for naval aircraft. It contains a table that lists typical locations of corrosion on the aircraft. The article also provides examples of aircraft corrosion damage.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002387
EISBN: 978-1-62708-193-1
... Abstract This article focuses on the subject of proactive or predictive maintenance with particular emphasis on the control and prediction of corrosion damage for life extension and failure prevention. It discusses creep life assessment from the perspective of creep-rupture properties...
Abstract
This article focuses on the subject of proactive or predictive maintenance with particular emphasis on the control and prediction of corrosion damage for life extension and failure prevention. It discusses creep life assessment from the perspective of creep-rupture properties and creepcrack growth. Practical methods based on replication and parametric approaches are also discussed.
Book Chapter
Corrosion Monitoring Using Microwave and Guided Wave Nondestructive Evaluation
Available to PurchaseSeries: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003658
EISBN: 978-1-62708-182-5
... Abstract Microwave and guided wave (GW) nondestructive evaluation (NDE) techniques are capable of detecting corrosion damage, cracks, and other defect types in inaccessible areas. This article describes the operation principles of the techniques and provides information on hidden corrosion...
Abstract
Microwave and guided wave (GW) nondestructive evaluation (NDE) techniques are capable of detecting corrosion damage, cracks, and other defect types in inaccessible areas. This article describes the operation principles of the techniques and provides information on hidden corrosion detection and the applications of microwave NDE devices and GW ultrasonic NDE devices.
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
... 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...
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.
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