Module number: 11351
Offered every summer semester
Credit Points: 6
written/oral exam at the end of the semester which must be passed with a minimum grade of 4.0
The students will learn about the specification, the design realisation and the validation process of those components which are required to integrate a jet engine 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 engine to aircraft interface.
Requirements, functioning and design of a nacelle (intake, cowl doors, nozzle), thrust reverser, engine build 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 engine integration