Advanced Gas Turbine Engine Blade Design using Siemens NX

Published 06/2022
MP4 | Video: h264, 1280×720 | Audio: AAC, 44.1 KHz, 2 Ch
Genre: eLearning | Language: English + srt | Duration: 31 lectures (4h 37m) | Size: 3 GB

Learn Drawing study and 3D CAD modeling process of Gas Turbine Engine – Turbine Blades using 2 Live Industrial Projects

What you’ll learn
Industrial Gas Turbine Engine – Turbine Blade Drawing Study
Gas Turbine Engine- Turbine Blade 3D Solid Modeling in Siemens NX
Understanding the basics of aerofoil through real industrial drawings
Application of Siemens NX in Aerospace Industry
Learn from an Author who is an Industrial Expert and mentor with Over 45 years of Experience

Requirements
Computer loaded with Siemens NX
Knowledge of Basic tools of Siemens NX would be an advantage

Description
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.

Who this course is for
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
Anyone with an interest to learn about aerospace applications of CAD software.

Advanced Gas Turbine Engine Blade Design using Siemens NX

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