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Second stage rotor blade

  • Added: 03.07.2014
  • Size: 6 MB
  • Downloads: 2
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Description

Course design for turbines Two-stage power turbine for gas turbine

Project's Content

icon
icon
icon blades.bak
icon blades.dwg
icon task.jpg
icon расчет_цикла_ГТУ.xmcd
icon треугольники скоростей.bak
icon Чертеж1.bak
icon Чертеж1_ready.bak
icon Чертеж1_ready.dwg
icon Чертеж1_ready_recover.bak
icon Чертеж1_recover.bak
icon
icon comp.bak
icon MFC46D.tmp
icon прочность.bak
icon прочность.dwg
icon прочность.xmcd
icon
icon 7. Список литературы (35).doc
icon comp.dwg
icon Mathcad - расчет_цикла_ГТУ.pdf
icon task.jpg
icon Оглавлени1.doc
icon титульный лист.doc
icon Чертеж1_ready.frw

Additional information

Contents

1. Source Data ______________________________________________________

2. Calculation of the optimum degree of pressure increase in the compressor _____________

3. Calculates the parameters for the selected pressure increase ______________

4. Calculation of turbine stages ______________________________________________

5. Profiling of second stage blades _________________________________

6. Calculation of second stage rotor blade strength _______________________

List of literature used ____________________________________________

Drawings content

icon blades.dwg

blades.dwg

icon Чертеж1_ready.dwg

Чертеж1_ready.dwg

icon прочность.dwg

прочность.dwg

icon comp.dwg

comp.dwg

icon Mathcad - расчет_цикла_ГТУ.pdf

icon Чертеж1_ready.frw

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