Module Number:
| 13803
|
Module Title: | Core Engine Design 2 |
|
Kerntriebwerkskonstruktion 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 summer 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. |
Contents: | - Overall: purpose of construction, construction process and cooperation with other departments, legally aviation standards and certification requirements, general view on core engines
- Turbine: annulus determination, construction of blades, construction of rotors and static parts (casings and structures)
- Exhaust chambers: design of exhaust nozzles, types, variable area nozzles, construction aspects
|
Recommended Prerequisites: | None |
Mandatory Prerequisites: | None |
Forms of Teaching and Proportion: | -
Lecture
/ 2 Hours per Week per Semester
-
Exercise
/ 2 Hours per Week per Semester
-
Self organised studies
/ 120 Hours
|
Teaching Materials and Literature: | - 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: | - Oral examination, 60 minutes OR Written examination, 120 minutes
In the first lecture it will be announced, if he examination will be offered in written or oral form.
|
Evaluation of Module Examination: | Performance Verification – graded |
Limited Number of Participants: | 50 |
Part of the Study Programme: | -
Master (research-oriented) /
Hybrid Electric Propulsion Technology /
PO 2024
|
Remarks: | None |
Module Components: | VL+Ü+PRÜ Core Engine Design 2 |
Components to be offered in the Current Semester: | |