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Development of the JT15D-1 Turbofan Engine
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English
Abstract
The UACL JT15D-1 engine is a 2200 lb thrust turbofan engine of the high bypass ratio type, the first small engine of the type to be certified and placed in production. The engine is briefly described, and the scope of development testing and resources applied is reviewed. A selection of major development problems is covered, and future developments are indicated.
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Authors
Topic
Citation
Cook, D., "Development of the JT15D-1 Turbofan Engine," SAE Technical Paper 720352, 1972, https://doi.org/10.4271/720352.Also In
References
- Beauregard J. P. “The Development of Small Gas Turbine Engines at UACL.” Canadian Aeronautics & Space Institute Jrl. October 1971
- Wrong C. G. “An Introduction to The JT15D Engine.” ASME Paper 69-GT-119
- Grabe W. Vanslyke G. K. “Icing Tests on the JT15D Turbofan Engine.” Proceedings of the Tenth National Conference on Environmental Effects of Aircraft and Propulsion Systems May 1971 Trenton, N.J.