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Aerospace and Aircraft Coatings / Charles R. Hegedus, Stephen J. Spadafora, Anthony T. Eng, David F. Pulley, Donald J. Hirst.

Format:
Book
Author/Creator:
Spadafora, Stephen J., author.
Eng, Anthony T., author.
Hegedus, Charles R., author.
Hirst, Donald J., author.
Pulley, David F., author.
Contributor:
American Society for Testing and Materials
ASTM International.
Series:
Journal of ASTM International. Manual Series ; MNL12239M.
ASTM manual series ; MNL12239M
Language:
English
Subjects (All):
Aerospace industries--Costs.
Aerospace industries.
Industrial procurement.
Offset (Accounting).
Physical Description:
1 online resource (12 pages) : illustrations, figures, tables.
Volume 2012, Issue 17 (January 2012)
Other Title:
ASTM digital library.
Place of Publication:
West Conshohocken, Pa. : ASTM International, 2012.
System Details:
Mode of access: World Wide Web.
text file PDF
Summary:
ORGANIC COATINGS ARE PRIMARILY APPLIED TO aircraft for environmental protection and appearance. Reference [1] concludes, The rate controlling parameter for the corrosion of aircraft alloys, excluding the mechanical damage factor, is the degradation time of the protective coating system. This clearly indicates the importance of the coating system's durability and its ability to control corrosion and erosion. Relative to appearance, commercial aircraft benefit from the aesthetic characteristics of the coating system, while military aircraft rely on camouflage properties to minimize enemy detection and tracking during mission operations. To meet operational requirements, aircraft coating systems traditionally consist of a primer and a topcoat. Primers inhibit corrosion of the substrate and enhance adhesion of subsequent topcoats, while topcoats are applied for appearance and to enhance overall durability of the coating system. Self-priming topcoats, which perform as both primer and topcoat in a single coating, have recently been introduced [2,3]. In addition, specialty coatings are strategically applied to perform various functions such as protection against rain erosion, chafing, immersion in fuel, and high temperature. References [46] provide more detail on the formulation and properties of aircraft coatings. A number of factors affect the performance of aircraft coatings, including the substrate material, the aircraft's operational environment, and flight conditions. Aircraft structures and skins are manufactured from numerous metallic alloys and polymeric composites with a variety of pre-paint treatments, thus complicating the adhesion and corrosion inhibition characteristics of the coating system. Environmental conditions also can vary dramatically (arctic, tropical, marine, industrial, desert, et cetera). Skin temperatures during flight can range from 54 to 177C (65 to 350F) while ground conditions may be relatively benign or highly corrosive. Aircraft type and mission also play important roles in coating system performance. A commuter aircraft that hops from island to island in the tropics sees frequent pressurization and depressurization along with high temperature, humidity, and salt water. In contrast, a military tactical aircraft may fly far fewer hours but will experience extreme structural loads during flight conditions. These flight conditions place environmental and mechanical stresses on the aircraft coating system. Therefore, selection of appropriate test and evaluation procedures is an essential component for determining acceptable coatings for aircraft application [7].
Notes:
"ASTM Stock Number: MNL12239M".
Includes bibliographical references 18.
Electronic reproduction. W. Conshohocken, Pa. : ASTM International, 2012. Mode of access: World Wide Web. System requirements: Web browser. Access may be restricted to users at subscribing institutions.
Description based on publisher's website, viewed May 03, 2017.
ISBN:
9780803188914 (e-ISBN)
9780803170179
Access Restriction:
Restricted for use by site license.

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