CORROSION OF AIRCRAFT LANDING GEAR STEELS

Authors
Citation
Eu. Lee et J. Waldman, CORROSION OF AIRCRAFT LANDING GEAR STEELS, Naval engineers journal, 106(6), 1994, pp. 77-83
Citations number
NO
Categorie Soggetti
Engineering, Marine",Oceanografhy
Journal title
ISSN journal
00281425
Volume
106
Issue
6
Year of publication
1994
Pages
77 - 83
Database
ISI
SICI code
0028-1425(1994)106:6<77:COALGS>2.0.ZU;2-E
Abstract
Carrier-based aircraft landing gear demands a tough, corrosion-resista nt material. Because of its high tensile strength, 300M steel was acce pted as the standard material for aircraft landing gear. However, its corrosion resistance and fracture toughness are low, and is ill-suited for advanced aircraft landing gear. A newly developed nickel-cobalt a lloy steel, named ''AerMet 100,'' has an outstanding combination of hi gh fracture toughness and high tensile strength. Since its mechanical properties surpass those of the 300M steel, it has great potential for application to aircraft landing gear and other fracture critical comp onents. However, its corrosion behavior was not fully understood. This study was initiated to characterize the corrosion behavior. The chara cterization effort included clarification of stress corrosion cracking , immersion corrosion, salt spray corrosion, and humidity corrosion of AerMet 100 steel. For comparison, an identical study was concurrently performed for 300M steel. The results indicate that AerMet 100 steel is superior to 300M steel with respect to corrosion resistance as well as mechanical properties.