The gas-dynamic calcualation of the axial turbine stage - методичка по прочим предметам

 

Тезисы:

  • The gas-dynamic calculation of THE axial turbine stage.
  • These two rows of airfoils form a turbine stage.
  • To produce the driving torque , the turbine unit may consist of one or several stages.
  • Three stage turbine unite assembly is shown in fig.1.
  • All of these parameters are chosen for the first turbine stage of the designed engine.
  • Main geometrical dimensions of the turbine stage.
  • Full gas pressure and stagnated gas temperature at the entry to the turbine stage.
  • Turbine stage work.
  • The useful torque, created by turbine is transmitted to compressor by turbine shaft.
  • Stage scheme, sections designation and diametrical dimensions are shown in figure 3.

 

 

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