HOT CYCLE ROTOR SYSTEM FABRICATION EFFORT
Abstract
The method of fabrication of the rotor, test machines and fabrication jigs and fixtures for the Hot Cycle Rotor System are presented. The design utilizes components, fabrication and assembly methods, and processes well established in the aircraft industry. In particular, the blade is composed of many identical small parts which are fabricated on existing high production machinery. Thus the design lends itself to fabrication of service craft at an early date and with minimum effort and cost.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1962
- Accession Number
- AD0290214
Entities
People
- J. T. Doyle