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High Temperature Turbine Design Considerations
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1971 by SAE International in United States
Annotation ability available
The major technological developments which have made possible the trend towards higher temperatures in modern aircraft gas turbine engines are discussed. The relative importance of manufacturing processes, material developments, cooling techniques, analytical design procedures, rupture and cyclic life considerations, and aerodynamic and mechanical design improvements are discussed along with illustrative examples and technical data.
The need for a balanced design approach is stressed, and examples are given where trade-offs can be made. It is noted that the advances in aircraft engines during the last 10 years have been based on the evolution of sound engineering principles, extensive component and engine development, and careful consideration of the operational requirements rather than a tremendous breakthrough or revolutionary concept in any one area.
|Technical Paper||Trends in High Temperature Materials Technology for Advanced Aircraft Turbine Engines|
|Technical Paper||The Aviation Industries’ Use of Product Safety Standards|
|Aerospace Standard||Altitude Graphs Aircraft Reciprocating Engine Performance|
CitationSuciu, S., "High Temperature Turbine Design Considerations," SAE Technical Paper 710462, 1971, https://doi.org/10.4271/710462.
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