Gas Turbine Engine Compressor Blade Design in Siemens NX
Gas Turbine Engine Compressor Blade Design in Siemens NX, available at $54.99, has an average rating of 3.85, with 36 lectures, based on 16 reviews, and has 93 subscribers.
You will learn about Industrial Gas Turbine Engine Compressor Blade Drawing Study Gas Turbine Engine Compressor 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 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 or Anyone with an interest to learn about aerospace applications of CAD software. 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 or Anyone with an interest to learn about aerospace applications of CAD software.
Enroll now: Gas Turbine Engine Compressor Blade Design in Siemens NX
Summary
Title: Gas Turbine Engine Compressor Blade Design in Siemens NX
Price: $54.99
Average Rating: 3.85
Number of Lectures: 36
Number of Published Lectures: 36
Number of Curriculum Items: 36
Number of Published Curriculum Objects: 36
Original Price: $199.99
Quality Status: approved
Status: Live
What You Will Learn
- Industrial Gas Turbine Engine Compressor Blade Drawing Study
- Gas Turbine Engine Compressor 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
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
- Anyone with an interest to learn about aerospace applications of CAD software.
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
- Anyone with an interest to learn about aerospace applications of CAD software.
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 airflow 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 power plant of an aircraft that 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.
In this course; we have the right content covered which will give you ample knowledge of blades.
At the beginning of this course ; you will be given a fundamental orientation on a Gas turbine engine. After that we shall discuss about the importance of the Blades in the Gas turbine engines’ operation and power generation.
Further, we will start an Industrial Project on the 5th stage blade of the Gas Turbine Engine Compressor Module of an Aero Engine.
All the knowledge that you will get in this course is purely industrial based and this will upgrade your knowledge level to match with the Gas Turbine industry professionals.
Course Curriculum
Chapter 1: Introduction to the course
Lecture 1: Introduction
Chapter 2: Introduction to Gas Turbine Engine
Lecture 1: What is a Gas Turbine Engine and its Use
Lecture 2: Gas Turbine Engine Power generation mechanism
Lecture 3: Role of Blades in the Gas Turbine
Chapter 3: Aerofoils
Lecture 1: Introduction to Aerofoils
Lecture 2: Aerofoil Geometry
Lecture 3: Drawing Aerofoil from given data
Chapter 4: 5th Stage Compressor Rotor Blade of an Aero Engine
Lecture 1: Introduction to Project
Lecture 2: Preparing 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: Development of the Axial Dovetail Root
Lecture 9: Finishing Touches to the Model
Chapter 5: 3rd Stage Compressor Rotor Blade of an Aero Engine
Lecture 1: Introduction to Project
Lecture 2: Preparing 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: Radial Dovetail Root drawing study
Lecture 9: Sketching Root Cross section
Lecture 10: Modelling Radial Dovetail Root
Lecture 11: Appling Finishing Touches to the Model
Chapter 6: Impeller of an Aircraft Turbo Starter Unit
Lecture 1: Introduction to Project
Lecture 2: Preparing Aerofoil data
Lecture 3: Importing Aerofoil Sections
Lecture 4: Creating Blade body
Lecture 5: Developing the Main body
Lecture 6: Generating all the blades
Lecture 7: Trimming the blades
Lecture 8: Giving Contour to the blades
Lecture 9: Generating the keyway slot
Instructors
-
Roy Academy
Learn from the industrial mentors -
S N S Roy
Engineering Consultant and Corporate Trainer
Rating Distribution
- 1 stars: 1 votes
- 2 stars: 1 votes
- 3 stars: 2 votes
- 4 stars: 5 votes
- 5 stars: 7 votes
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