Refinement of Casting Techniques for Small Air-Cooled, Turbine Blades. Phase 1
Abstract
T700 stage-two turbine blade was redesigned to permit application of advanced coring practices to investment cast turbine blades. The redesign resulted in a more producible turbine blade and reduced the overall cost of the blade. The design history, manufacturing steps, qualification procedures, engine test results and cost analysis are discussed for the radial-hole cooled turbine blade.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1977
- Accession Number
- ADA038561
Entities
People
- G. S. Irons
Organizations
- General Electric