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Turboshaft

Aerospace Engineering

A turboshaft engine is a form of gas turbine engine optimized to produce shaft horsepower rather than jet thrust. In concept it is very similar to a turbojet, but with additional turbine stages that extract more energy from the exhaust and convert it into output shaft power instead of thrust. It is even more similar to a turboprop, with only minor differences between the two, and a single engine design is often sold in both turboshaft and turboprop forms. This description is adapted from Wikipedia contributors under CC BY-SA 4.0; changes were made. https://creativecommons.org/licenses/by-sa/4.0/

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Source Turboshaft (Wikipedia)
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Turboshaft (Wikipedia)
  • Lead section
    A turboshaft engine is a form of gas turbine that is optimized to produce shaft horsepower rather than jet thrust.
  • In Group: Gas Turbine Aircraft Engines, lead: form of gas turbine optimized to produce shaft horsepower rather than jet thrust
  • In Field: Aerospace Engineering, Introduction
    A turboshaft engine is a form of gas turbine that is optimized to produce shaft horsepower rather than jet thrust.
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