Advanced Gas Turbine Engine Blade Design using CATIA

Advanced Gas Turbine Engine Blade Design using CATIA, available at $39.99, has an average rating of 4.5, with 33 lectures, based on 1 reviews, and has 33 subscribers.

You will learn about Industrial Gas Turbine Engine – Turbine Blade Drawing Study Gas Turbine Engine – Turbine Blade 3D Solid Modeling in CATIA Understanding the basics of aerofoil through real industrial drawings Application of CATIA in Aerospace Industry This course is ideal for individuals who are Engineers, Hobbyist and anyone with a zeal to learn fundamentals of Blade Design for aerospace applications or Students and individuals looking to upgrade their Resume by including an Industrial Project It is particularly useful for Engineers, Hobbyist and anyone with a zeal to learn fundamentals of Blade Design for aerospace applications or Students and individuals looking to upgrade their Resume by including an Industrial Project.

Enroll now: Advanced Gas Turbine Engine Blade Design using CATIA

Summary

Title: Advanced Gas Turbine Engine Blade Design using CATIA

Price: $39.99

Average Rating: 4.5

Number of Lectures: 33

Number of Published Lectures: 33

Number of Curriculum Items: 33

Number of Published Curriculum Objects: 33

Original Price: $199.99

Quality Status: approved

Status: Live

What You Will Learn

Industrial Gas Turbine Engine – Turbine Blade Drawing Study
Gas Turbine Engine – Turbine Blade 3D Solid Modeling in CATIA
Understanding the basics of aerofoil through real industrial drawings
Application of CATIA in Aerospace Industry

Who Should Attend

Engineers, Hobbyist and anyone with a zeal to learn fundamentals of Blade Design for aerospace applications
Students and individuals looking to upgrade their Resume by including an Industrial Project

Target Audiences

Engineers, Hobbyist and anyone with a zeal to learn fundamentals of Blade Design for aerospace applications
Students and individuals looking to upgrade their Resume by including an Industrial Project

The power generation in a gas turbine engine mainly depends upon the amount of air it can suck from the atmosphere and how efficiently the air flow through the engine to finally get utilised in the turbine and exhaust section.

All these depend on the 1000’s of blades that are used inside the gas turbine engine. Blades are the most critical and abused part inside the gas turbine engine which is the powerplant of an aircraft which gives it the ability to propel ahead.

The gas turbine engine’s application is limitless as it has great power to weight ratio. It is used for powering aeroplanes, helicopters, ships, trains, power plants, pumps, gas compressors, tanks etc.

And behind each successful gas turbine is a set of highly sophisticated and precise blades. Particularly Turbine blades.
Turbine blades are subjected to very high fatigue load and Temperature over 1000 deg.C during its operation inside the engine. Due to this fact they come with Firtree root, Shroud and root with labyrinth for sealing the air and internal cooling channels.

In this course; we have the right content covered which will give you ample knowledge on Turbine blades.

There are 2 Projects included in this Course:

2nd Stage Turbine Blade of an Aero Engine
4th Stage Turbine Blade of an Aero Engine

The first project contains a Firtree root and a Shroud with labyrinth.

The Second project is on a Turbine blade having Firtree root with labyrinth as root platform and Internal cooling channels for Cooling the blade during operation.

In both Projects you will experience the Turbine blade industrial drawing and the process for studying those drawings.

All the knowledge that you will get in this course is purely industrial based and this will upgrade you knowledge level to match with the Gas Turbine industry professionals.

So STOP Thinking; Take free lectures and Join Today.

Course Curriculum

Chapter 1: Introduction

Lecture 1: Introduction

Chapter 2: 2nd Stage Turbine Blade of an Aero Engine

Lecture 1: Introduction to Project

Lecture 2: Preparing and Importing Aerofoil data

Lecture 3: Sketching Aerofoil Section I-I

Lecture 4: Sketching Aerofoil Section II-II

Lecture 5: Sketching Aerofoil Section III-III

Lecture 6: Sketching Aerofoil Section IV-IV

Lecture 7: Sketching Aerofoil Section V-V

Lecture 8: Fir Tree Root drawing study

Lecture 9: Sketching the Fir tree cross-section of root

Lecture 10: Finishing the Root

Lecture 11: Labyrinth of Shroud

Lecture 12: Finalising Shroud

Lecture 13: Appling Finishing touches to the model

Chapter 3: 7- 4th Stage Turbine Blade of an Aero Engine

Lecture 1: Introduction to Project

Lecture 2: Preparing and Importing the Aerofoil data

Lecture 3: Sketching Aerofoil Section I-I

Lecture 4: Sketching Aerofoil Section II-II

Lecture 5: Sketching Aerofoil Section III-III

Lecture 6: Sketching Aerofoil Section IV-IV

Lecture 7: Sketching Aerofoil Section V-V

Lecture 8: Generating Fir tree Root

Lecture 9: Developing Root Platform

Lecture 10: Generating Scallop of Root

Lecture 11: Appling Finishing touches to the root

Lecture 12: Sketching Cooling Channel View-GG

Lecture 13: Sketching Cooling Channel Sec-UU

Lecture 14: Sketching Cooling Channel Sec-WW

Lecture 15: Sketching Cooling Channel Sec-RR

Lecture 16: Sketching Cooling Channel Sec-SS

Lecture 17: Sketching Cooling Channel Sec-TT

Lecture 18: Creating Cooling Channels

Lecture 19: Creating Cooling Pin Holes

Instructors

Roy Academy
Learn from the industrial mentors
S N S Roy
Engineering Consultant and Corporate Trainer

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