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    Energy efficient engine: Turbine intermediate case and low-pressure turbine component test hardware detailed design report (1982)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A four stage, low pressure turbine component has been designed to power the fan and low pressure compressor system in the Energy Efficient Engine. Designs for a turbine intermediate case and an exit guide vane assembly also have been established. The components incorporate numerous technology features to enhance efficiency, durability, and performance retention. These designs reflect a positive step towards improving engine fuel efficiency on a component level. The aerodynamic and thermal/mechanical designs of the intermediate case and low pressure turbine components are presented and described. An overview of the predicted performance of the various component designs is given.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-167973 , NAS 1.26:167973 , PWA-5594-191
    Format: application/pdf
    Location Call Number Expected Availability
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