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Introduction to the Course
Introduction to the Course
Introduction to Gas Turbine Engine
What is a Gas Turbine Engine and its Use
Gas Turbine Engine Power generation mechanism
Role of Blades in the Gas Turbine
Aerofoils
Introduction to Aerofoils
Aerofoil Geometry
Drawing Aerofoil from given data
Project-1: 5th Stage Compressor Rotor Blade of an Aero Engine
Introduction to Project
Preparing Aerofoil data
Sketching Aerofoil Section I-I
Sketching Aerofoil Section II-II
Sketching Aerofoil Section III-III
Sketching Aerofoil Section IV-IV
Sketching Aerofoil Section V-V
Development of the Axial Dovetail Root
Finishing Touches to the Model
Project-2: 3rd Stage Compressor Rotor Blade of an Aero Engine
Introduction to Project
Preparing Aerofoil data
Sketching Aerofoil Section I-I
Sketching Aerofoil Section II-II
Sketching Aerofoil Section III-III
Sketching Aerofoil Section IV-IV
Sketching Aerofoil Section V-V
Radial Dovetail Root drawing study
Sketching Root Cross section
Modelling Radial Dovetail Root
Appling Finishing Touches to the Model
Project-3: 2nd Stage Turbine Blade of an Aero Engine
Introduction to Project
Preparing Aerofoil data
Sketching Aerofoil Section I-I
Sketching Aerofoil Section II-II
Sketching Aerofoil Section III-III
Sketching Aerofoil Section IV-IV
Sketching Aerofoil Section V-V
Sketching the Fir tree cross-section of root
Finishing the Root
Labyrinth of Shroud
Finalising Shroud
Appling Finishing touches to the model
Project-4: 4th Stage Turbine Blade of an Aero Engine
Introduction to Project
Preparing Aerofoil data
Sketching Aerofoil Section I-I
Sketching Aerofoil Section II-II
Sketching Aerofoil Section III-III
Sketching Aerofoil Section IV-IV
Sketching Aerofoil Section V-V
Generating Fir tree Root
Developing Root Platform
Generating Scallop of Root
Applying Finishing touches to the root
Sketching Cooling Channel Sec-GG
Sketching Cooling Channel Sec-UU
Sketching Cooling Channel Sec-WW
Sketching Cooling Channel Sec-RR
Sketching Cooling Channel Sec-SS
Sketching Cooling Channel Sec-TT
Creating Cooling Pin Holes
Project-5: Impeller of an Aircraft Turbo Starter Unit
Introduction to Project
Preparing Aerofoil data
Importing Aerofoil Sections
Creating Blade body
Developing the Main body
Generating all the blades
Trimming the blades
Giving Contour to the blades
Generating the keyway slot
Conclusion and Goodbye Message.
Preview - Gas Turbine Engine Blade Design using Siemens NX
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