13804 - Engine Integration Modulübersicht

Module Number: 13804
Module Title:Engine Integration
  Triebwerksintegration
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:The students will learn about the specification, the design realisation and the validation process of those components which are required to integrate a propulsion system into an aircraft. Furthermore, the required engineering processes to attain this task are provided. The students will therefore be prepared for the work at the interface between propulsion system and aircraft.
Contents:Requirements, functioning and design of a nacelle (intake, cowl doors, nozzle), thrust reverser, engine build-up unit and mounts, assembly, maintenance, noise reduction, fire protection, development- and validation process, interface management, legal requirements and means of compliance, cost and cost reduction, future aircraft concepts and their propulsion integration.
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:None
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 Engine Integration
Components to be offered in the Current Semester:
  • no assignment