• Keine Ergebnisse gefunden

INSTITUT FÜR LUFTFAHRTANTRIEBE UNIVERSITÄT STUTTGART

N/A
N/A
Protected

Academic year: 2022

Aktie "INSTITUT FÜR LUFTFAHRTANTRIEBE UNIVERSITÄT STUTTGART"

Copied!
1
0
0

Wird geladen.... (Jetzt Volltext ansehen)

Volltext

(1)

INSTITUT FÜR LUFTFAHRTANTRIEBE UNIVERSITÄT STUTTGART

Prof. Dr.-Ing. S. Staudacher

Pfaffenwaldring 6 D-70569 Stuttgart

Telefon (0711) 685 63520 Telefax (0711) 685 63505

Bachelorarbeit für

Herrn/Frau cand. aer. N.N

Development of a Performance Model of an Avco Lycoming ALF 502 Engine

Work description:

Predicting the gradual engine deterioration is one of the keys to optimize aircraft rotations and maintenance schedules resulting in lowering the operating costs of an aircraft. Gradual deterio- ration is highly dependent upon environmental conditions and power setting. In the past, only single snapshots of flights where provided. Hence, large portions of the mission were unknown, making the development of predictive engine deterioration models close to impossible. New en- gines provide continuously recorded data giving the possibility to analyse the complete flight mis- sion.

The NASA released a dataset of commercial flights where in-flight data are recorded continuously.

Unfortunately, the provided measurements are insufficient for a throughout analysis of engine deterioration. A hybrid Ansatz including a thermodynamic engine model synthesizing the missing measurements would help to develop a deterioration prediction model.

Within the scope of this bachelor thesis, an existing thermodynamic model of an Avco Lycoming ALF 502 engine is to be improved in the power synthesis software NPSS. It means a preliminary research to understand the main engine parameters and familiarization with NPSS must be first carried out. Once the performance model of the engine is completed, the creation of an interface that enables the user to run the model easily and rapidly needs to be developed. The final presen- tation and thesis could be written either in English or German.

Work schedule:

- Literature research

- Familiarisation with the existing NPSS model and understand what could/must be im- proved

- Creation of the interface of the engine model

- Elaboration of the results and preparation of the final presentation

Prerequisites:

- Knowledge gained during Luftfahrtantriebe und Turbomaschinen - Programming skills in C, Matlab/Python

- Minimum 102 LP (credits) required

Betreuer: Stefano Scarso, M.Sc stefano.scarso@ila.uni-stuttgart.de +49 (0)711 685-63696

Referenzen

ÄHNLICHE DOKUMENTE

A host of researchers in the last 15 years [8] have suggested another way to explain software architectures: Instead of pre- senting an architectural model as a

One snow season (2017/2018) with an extreme event was chosen and the time series of the three winter months of air temperature, topsoil temperature and liquid precipitation

The concept of Gross National Happiness (GNH) represents an original and highly significant initiative and the Government has been diligent in finding ways to apply this policy

Aus einem bereits existierenden Datenmodell zum Vorentwurf von Verdichtern und einem Entwurf einer geometrischen Fan-Modellierung soll unter Beibehal- tung der Methodik ein

Am Höhenprüfstand der Universität Stuttgart werden moderne Flugtriebwerke und deren Kompo- nenten unter realistischen Flugbedingungen erprobt.. Ein wichtiger Aspekt einer

Ziel dieser Masterarbeit ist der Aufbau einer Flugsimulation auf Basis eines Punktmassenmodells einer A321 zur Ermittlung der Umgebungsbedingungen und des

Die Spaltströmung und deren Wechselwirkung mit der Passagenströmung führen zu sehr komplexen Strömungsphänomenen mit einer erheblichen Bedeutung für die Turbomaschine. Die

Damit die Luftfahrt noch ressourceneffizienter wird, baut man Strukturen deutlich leichter, wodurch sie schwingungsanfälliger werden.. Um die Festigkeit gegenüber