14841 - Aero Engine Design and Analysis 2 Modulübersicht

Module Number: 14841
Module Title:Aero Engine Design and Analysis 2
  Flugtriebwerkskonstruktion und -analyse 2
Department: Faculty 3 - Mechanical Engineering, Electrical and Energy Systems
Responsible Staff Member:
  • Prof. Dr.-Ing. Höschler, Klaus
Language of Teaching / Examination:English
Duration:1 semester
Frequency of Offer: Every winter semester
Credits: 6
Learning Outcome:

By the conclusion of the module, students will have acquired the ability to comprehend the structure and building of core engine designs, encompassing turbines and exhaust chambers. They will be proficient in assessing innovative designs within the core engine domain and capable of autonomously suggesting and implementing well-justified modifications to conventional designs. The autonomous cultivation of application-oriented and research-focused knowledge serves as an additional aspect of the competencies gained in this module.

In general, the students will learn:

  • How an aero engine works
  • Different types of aero engines
  • Introduction to major system, subsystems and components
  • Design and analysis challenges
  • Impact of new technologies (digital, electrification,..)
  • Technology and innovation management
  • Real world applications
  • How a large enterprise works and new working practices
  • Career progression and expectations
Contents:

Turbines

  • Aerodynamics
  • Mechanical Design including Lifing
  • Special topics

Whole Engine Modelling (2)

  • Mechanical Design including Lifing
  • FBO, Design Challenges
  • Power Gear Box

Digital

  • Simulation & Modelling
  • Digital Twins
  • DevOps

Excursion & Innovation Management

Recommended Prerequisites:

Ideally successful completion of

  • 13802 Core Engine Design 1 or
  • 14840 Aero Engine Design and Analysis 1, and
  • basics knowledge on thermodynamics and turbomachinery
Mandatory Prerequisites:No successful completion of module 13803 Core Engine Design 2
Forms of Teaching and Proportion:
  • Lecture / 2 Hours per Week per Semester
  • Self organised studies / 150 Hours
Teaching Materials and Literature:
  • Lecture notes
  • Aircraft Engine Design, Third Edition, eISBN: 978-1-62410-650-7
  • Jet Engines: Fundamentals of Theory, Design and Operation, ISBN: 0760304599
Module Examination:Final Module Examination (MAP)
Assessment Mode for Module Examination:
  • Written examination, 120 minutes
Evaluation of Module Examination:Performance Verification – graded
Limited Number of Participants:None
Part of the Study Programme:
  • Master (research-oriented) / Hybrid Electric Propulsion Technology / PO 2024
  • Master (research-oriented) / Hybrid Electric Propulsion Technology /
  • Master (research-oriented) / Maschinenbau / PO 2023
  • Master (research-oriented) - Reduced Semester / Maschinenbau / PO 2023
  • Master (research-oriented) - Co-Op Programme with Practical Place / Maschinenbau - dual / PO 2023
Remarks:
  • Lectures start in winter semester 2026/27.
  • This module is previously offered as Core Engine Design 2.
Module Components:

Lecture and exam

 
Components to be offered in the Current Semester:
  • no assignment