Composites tooling speeds fabrication - Energy, labor cost cut sharply
Abstract
The hot-layup-tooling technique providing significant cost reduction in the fabrication of helicopter components is discussed. The operational characteristics of the process are described, as are experiments evaluating advantages over oven curing. A summary of cost savings attributable to the technique is presented, and future plans calling for development of a single step cure are mentioned.
- Publication:
-
ManTech Journal
- Pub Date:
- 1978
- Bibcode:
- 1978MaTeJ...3...15H
- Keywords:
-
- Aircraft Production Costs;
- Aircraft Structures;
- Composite Materials;
- Tooling;
- Aircraft Construction Materials;
- Cost Reduction;
- Fabrication;
- Kevlar (Trademark);
- Military Helicopters;
- Engineering (General)