Lear Fan Propulsion System

800609

4/1/1980

Authors
Abstract
Content
An aircraft propulsion system for Mach .6 flight is being developed which utilizes two turboshaft engines driving a pusher propeller through driveshafts and a combining gearbox. This system will provide greater operational safety as well as improved aircraft efficiency. This report describes design features, installation considerations, and operational characteristics of the system, and reviews methods of system analysis.
Meta TagsDetails
DOI
https://doi.org/10.4271/800609
Citation
Cooney, D., "Lear Fan Propulsion System," Turbine Powered Executive Aircraft Meeting, Scottsdale, Arizona, United States, April 9, 1980, https://doi.org/10.4271/800609.
Additional Details
Publisher
Published
4/1/1980
Product Code
800609
Content Type
Technical Paper
Language
English