Composite Structures-Technical Breakthrough for Helicopter Rotor Blades

751108

02/01/1975

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/751108
Pages
17
Citation
Douglas, L., and Stratton, W., "Composite Structures-Technical Breakthrough for Helicopter Rotor Blades," SAE Technical Paper 751108, 1975, https://doi.org/10.4271/751108.
Additional Details
Publisher
Published
Feb 1, 1975
Product Code
751108
Content Type
Technical Paper
Language
English