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Design of Jet Engine Rotors for Long Life Pratt and Whitney Aircraft, Div. United Aircraft Corporation

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Sattar, S. A., author.
Conference Name:
National Air Transportation Meeting (1975-05-06 : Hartford, Connecticut, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1975
Summary:
Jet engine rotors are the most highly stressed large volumes of material in the engine. They possess millions of inch pounds of kinetic energy at normal speeds. Considerable care in design and analysis must be taken to ensure that the parts do not fail over the full life cycle of the engine. In this paper, major design criteria are identified and discussed, with special emphasis on the long-life aspects of disk design methodology. The role of fracture mechanics is discussed as it applies to intrinsic material defects as well as the residual life of the part after crack initiation. Future trends, including the impact of powder metallurgy on design, and retirement of disks for cause are discussed
Notes:
Vendor supplied data
Publisher Number:
750619
Access Restriction:
Restricted for use by site license

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