Cooling Modern Aero Engine Turbine Blades and Vanes

660053

2/1/1966

Authors
Abstract
Content
Part One reviews the application of turbine blade and vane cooling in current Rolls-Royce civil aero engines, together with some side effects on engine design and development.
Part Two presents a history of turbine blade and vane material improvement and of aircooling development as applied in these engines. Related problems affecting turbine blade and vane deterioration in engines are described, and an outline is given of a method of creep life determination in cooled blades.
Meta TagsDetails
DOI
https://doi.org/10.4271/660053
Citation
Hare, A., and Malley, H., "Cooling Modern Aero Engine Turbine Blades and Vanes," SAE Technical Paper 660053, 1966, https://doi.org/10.4271/660053.
Additional Details
Publisher
Published
2/1/1966
Product Code
660053
Content Type
Technical Paper
Language
English