gas turbine design

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Bids
4
Avg Bid (INR)
3075
Project Budget (INR)
₹1500 - ₹2000

Project Description:
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
2.Aerodynamic calculation of mid passage turbine stage/stages,
velocity triangles, selection of blade profiles, solidity, number of blades, stage efficiency etc
3.Selection of materials and bearings.
4.Layout 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 required:
Aerospace Engineering, Engineering, Mechanical Engineering
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toto88 India
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