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Composite Structures-Technical Breakthrough for Helicopter Rotor Blades Boeing Vertol Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Douglas, L. L., author.
Conference Name:
Aerospace Engineering and Manufacturing Meeting (1975-11-17 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1975
Summary:
In this decade we are witnessing the transition from all metal to all composite helicopter rotor blades. One such helicopter is already in full scale production. A driving factor is structural reliability and guarantee against catastrophic failure. Low crack propagation rate and the nature of failures in composite structures are the characteristics which make this quality product superior to metal structures for rotor blades. The ability to economically tailor blades aerodynamically and dynamically offer important advances in performance, flying qualities, low stress levels, and low vibratory forces
Notes:
Vendor supplied data
Publisher Number:
751108
Access Restriction:
Restricted for use by site license

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