EVOLUTION OF THE CAST INTERNALLY COOLED GAS TURBINE AIRFOIL

610436

01/01/1961

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
Preformed soluble ceramic cores are used in investment castings to provide monolithic cast airfoils having a hollow internal geometry which permits the maximum heat transfer for air cooling. The castings have superior endurance life, greater reproducibility than a fabricated airfoil, and can be manufactured economically.
This paper is a description of the development of cast hollow turbine airfoils with various internal configurations which have been tested on full-scale engines. The limited testing confirms that the product will provide the designer with unlimited latitude and control of the heat transfer characteristics in turbine airfoil applications.
Metallurgical investigation has shown the castings to be sound, and inspection methods for close quality control are described.
Meta TagsDetails
DOI
https://doi.org/10.4271/610436
Pages
16
Citation
McCORMICK, H., and REED, J., "EVOLUTION OF THE CAST INTERNALLY COOLED GAS TURBINE AIRFOIL," SAE Technical Paper 610436, 1961, https://doi.org/10.4271/610436.
Additional Details
Publisher
Published
Jan 1, 1961
Product Code
610436
Content Type
Technical Paper
Language
English