Turbofan

Summary

The turbofan or fanjet is a type of airbreathing jet engine that is widely used in aircraft propulsion. The word "turbofan" is a portmanteau of "turbine" and "fan": the turbo portion refers to a gas turbine engine which achieves mechanical energy from combustion, and the fan, a ducted fan that uses the mechanical energy from the gas turbine to force air rearwards. Thus, whereas all the air taken in by a turbojet passes through the combustion chamber and turbines, in a turbofan some of that air bypasses these components. A turbofan thus can be thought of as a turbojet being used to drive a ducted fan, with both of these contributing to the thrust. The ratio of the mass-flow of air bypassing the engine core to the mass-flow of air passing through the core is referred to as the bypass ratio. The engine produces thrust through a combination of these two portions working together; engines that use more jet thrust relative to fan thrust are known as low-bypass turbofans, conversely those

Official source

https://en.wikipedia.org/wiki/Turbofan

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Related publications (1)

Experimental and Numerical Investigation of a Small-Scale Steam Turbine

Diya Achi

This paper focuses on a small-scale radial steam turbine which is part of a fan-turbine unit (FTU) realizing the anode off-gas recirculation of a Solid Oxide Fuel Cell (SOFC). Due to the small size of the turbine (15mm diameter), it is not possible to determine its power by directly measuring the torque. Therefore, the performance parameters are evaluated using thermodynamics. However, heat transfers within the FTU have a non-negligible impact on the evaluation of the turbine power and total-to-total isentropic efficiency. New temperature and pressure measurements were thus conducted to refine the experimental results and the numerical model. The analysis of the experimental and numerical results highlights the significant influence of heat transfers, and provides a range for the turbine power and total-to-total isentropic efficiency, which are on the order of 34W and 39%, respectively. Furthermore, a heat investigation was carried out on the FTU in order to localise and determine the heat losses to the environment by using a simplified model. Through investigation, the primary source of heat loss was located at the turbine outlet.

2020

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