Overview
The course covers a broad range of topics from general compressors layouts to a detailed approach to flow paths aerodynamic design. The extensive theoretical part is supported by multiple examples and exercises that bring a real practical understanding of the learned topics.
The scope includes:
- Axial Compressor Basics
- Compressor Aerodynamic Design
- Off-Design Performances Prediction
- Profiling and 3D Blade Design
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The goal of this training course is to enrich engineering education of attendees by providing them with a comprehensive set of information on axial compressor design and operation.
Today’s tendency to minimize energy consumption coupled with the growing demand for environmentally-friendly technologies emphasize the necessity of implementation of new, cost-effective engineering solutions. The Axial Compressor Fundamentals course is designed to help mechanical and aerospace engineers keep up to date with the ever-developing industry and continually increase the efficiency of turbomachinery to meet the evolving needs of their customers.
Who Should Attend
- Engineers involved in design and maintenance of axial compressors for different applications, such as gas turbines for power generation, aircraft engines and various industrial applications.
- Design and developments engineers involved in the turbomachinery design and optimization process who are looking for ways to improve the design and operation.
- Engineering and turbomachinery scholars seeking to gain a deep insight into the axial compressor basics, including compressors gas dynamics, thermodynamics and structural analysis.
- Mechanical and aerospace engineering professors who want to supplement their teaching program with a detailed, industry-focused overview of axial compressors to prepare students for their future engineering careers.
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Examples of Course Schedule and Contents
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Day 1*
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1. Axial Compressor Basics
- Classification of compressors
- Gas dynamics
- Gas turbine cycles
- Compressor principles of operation
- Compressor stage elements
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2. Compressor Aerodynamic Design
- Compressor stage design
- Multistage compressor
- Losses in stage; Deviation angle
- Endwall boundary layer effects
- Transonic compressor stages
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Day 2
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3. Off-Design Performances Prediction
- Performances prediction methods
- Stall and Surge
- Compressor and turbine matching
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4. Profiling and 3D Blade Design
- Compressor Blade profiles
- 2D and 3D flow in channel
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The tools used: scientific calculator, AxSTREAM
*Please note that the course schedule is not fixed and could be customized following the specific attendees’ requirements and needs.
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Locations and Dates for 2012
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