Accession Number:

ADA301687

Title:

Composite Hub/Metal Blade Compressor Rotor.

Descriptive Note:

Contract rept.,

Corporate Author:

FIBER SCIENCE INC GARDENA CA

Personal Author(s):

Report Date:

1978-01-01

Pagination or Media Count:

35.0

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.

Subject Categories:

  • Laminates and Composite Materials
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE