Stationary Gas Turbines

The goal of this course is to teach the fundamentals of aerodynamic and mechanical design of thermal turbomachinery. After studying the Joule-Brayton thermodynamic process, the design of the major components of a heavy-duty gas turbine – compressor, combustion chamber, turbine, rotor, casing, and generator - are discussed with regard to aerodynamics, thermodynamics, and mechanical resilience. In addition to base-load operation, the importance of considering part-load and transient operation, e.g. startup and shutdown, in the design process is emphasized. The students are taught to realize that a turbomachine and its respective components are part of a complex system with often-conflicting design goals.

Recommended for 7th semester

Goal

  • Fundamentals of aerodynamic and mechanical design of thermal turbomachinery.
  • Analysis of Joule-Brayton thermodynamic process.
  • Importance of considering part-load and transient operation.
  • Design goals of turbomachinery and its components.

Recommended Previous Knowledge

  • Turbomachinery I
  • Heat transfer I
  • Fluid mechanics

Recommended Literature

  • Lecture script

Type of Examination

  • written exam

COURSE ENROLLMENT AND MATERIALSCOURSE ENROLLMENT AND MATERIALS

Further information about this module can be found via the Online Course Catalogue and Stud.IP. In addition, you must also register your attendance at this course via Stud.IP.


Lecturer

Prof. Dr.-Ing. Jörg Seume
Executive Director
Address
An der Universität 1
30823 Garbsen
Building
Room
315
Prof. Dr.-Ing. Jörg Seume
Executive Director
Address
An der Universität 1
30823 Garbsen
Building
Room
315

Tutor

Kirez - Foto Kirez - Foto
Oğuz Kirez, M.Sc.
Research Staff
Address
An der Universität 1
30823 Garbsen
Building
Room
311
Kirez - Foto Kirez - Foto
Oğuz Kirez, M.Sc.
Research Staff
Address
An der Universität 1
30823 Garbsen
Building
Room
311