Composite Hub/Metal Blade Compressor Rotor.
Abstract
The objective of this program was to design and fabricate a low cost compressor rotor for a small jet engine.The rotor hub and blade keepers were compression molded with graphite epoxy. Each pair of metallic blades was held in the hub by a keeper. All keepers were locked in the hub with circumferential windings. Feasibility of fabrication was demonstrated in this program.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1978
- Accession Number
- ADA301687
Entities
People
- Sam Yao