Computational Modal Analysis of a Low Pressure Turbine blade of Different Materials

 Low pressure turbine is the last turbine stage in a gas turbine engine. As per research, LPT is quite heavy and is even up to one third of the total weight of the engine. A lighter and stiffer material is required to decrease the weight of the stage for better performance of the engine. 

2025-06-28 16:30:53 - Adil Khan

Project Title

Computational Modal Analysis of a Low Pressure Turbine blade of Different Materials

Project Area of Specialization Mechanical EngineeringProject Summary

 Low pressure turbine is the last turbine stage in a gas turbine engine. As per research, LPT is quite heavy and is even up to one third of the total weight of the engine. A lighter and stiffer material is required to decrease the weight of the stage for better performance of the engine. 
In this project, modal analysis of the specified low pressure turbine blade is done computationally, by comparing nickel base and titanium base materials.

Project Objectives Project Implementation Method Benefits of the Project Technical Details of Final Deliverable Final Deliverable of the Project Hardware SystemCore Industry OthersOther IndustriesCore Technology OthersOther TechnologiesSustainable Development Goals Responsible Consumption and ProductionRequired Resources
Item Name Type No. of Units Per Unit Cost (in Rs) Total (in Rs)
Total in (Rs) 0
N/A Miscellaneous 000

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