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gas turbine design

Design a gas turbine with a given inlet turbine temperature, net shaft power and shaft RPM. The design report must include the following:

1. Calculation and selection of Thermodynamic Cycle with Justification

[url removed, login to view] calculation of mid passage turbine stage/stages,

velocity triangles, selection of blade profiles, solidity, number of blades, stage efficiency etc

[url removed, login to view] of materials and bearings.

[url removed, login to view] sketch with proper tolerances and clearances

My

TURBINE INLET TEMPERATURE=1700 DEGREES FAHRENHEIT

SHAFT POWER (H.P) = 5,000

RPM=7200

REPORT:

I. INTRODUCTION

Indicating usefulness, applications and other criteria you have considered in planning your project

II. DESIGN

2.1 selection and calculation of thermodynamic cycle

2.2 selection of initial parameters for design

2.3 preliminary aerodynamics calculations and development of

computer program

2.4 Selection of blade profile, number of blades, and key

dimensions

2.5 Refinements standardization of design and final design

III. MATERIAL SELECTION

IV. LAYOUT SKETCH

V. Recommendations for improvement

Skills: Aerospace Engineering, Engineering, Mechanical Engineering

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