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Improved Steel for Landing Gear Design McDonnell Aircraft Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Macy, William W., author.
Conference Name:
Aerospace Technology Conference & Exposition (1989-09-25 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1989
Summary:
An improved high-strength, high-toughness steel has been developed which shows considerable promise for landing gear applications. Previous materials provided high strength or high toughness, but not both. The improved material is a modified chemistry of AF1410 steel with increased carbon and an altered heat treat process. Tensile ultimate strengths (Ftu) of over 260 ksi (1.79 GPa) have been achieved while maintaining plane strain fracture toughness (Klc) in excess of 100 ksh/inch (110 MPam). In addition, the material has low sensitivity to environmental factors such as hydrogen embrittlement and stress corrosion cracking
Notes:
Vendor supplied data
Publisher Number:
892335
Access Restriction:
Restricted for use by site license

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