Prof. Dr.-Ing. Konrad Vogeler
© Michael Kretzschmar
Seniorprofessor
NameProf. Dr.-Ing. Konrad Vogeler
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Professur für Turbomaschinen und Flugantriebe
Besuchsadresse:
Zeuner-Bau, Raum 157 George-Bähr-Straße 3c
01069 Dresden
Persönliche Daten
Geburtsjahr: 1949
Staatsangehörigkeit: deutsch
Erfahrungen
- Design of high temperature Gasturbines
- Numerical Fluid Mechanics
- Aerodynamics
- Heat Transfer
- Cooling Technology
- Performance analysis
- Secondary Air and Sealing Systems
- Lifetime assessment of Gas Turbine Blades
- Design and Manufacturing of Gas Turbine Blades
- High temperature materials and coatings
- Failure analysis
Beruflicher Werdegang
| 4/70-9/77 | study of aeronautical engineering at Technische Hochschule Aachen (RWTH Aachen) Diploma in Mechanical Engineering at RWTH Aachen, Dipl.-Ing |
| 10/77 - 9/78 | Research Associate at Aeronautics Department of Naval Postgraduate School; Monterey, CA (USA) start of doctoral research work on theoretical investigation of flutter of compressor blades in supersonic flow supervisor: Prof. M. Platzer |
| 10/78 - 12/78 | traveling the US |
| 1/79 - 3/83 | research scientist at Institute for Jet Propulsion and Turbomachines RWTH Aachen Experimental and theoretical investigation of the aeroelastic behaviour of compressor blades in supersonic flow thesis advisor: Prof.H. Gallus and Prof.M. Platzer (NPGS Monterey) |
| 7/84 | Ph.D. at RWTH Aachen; Dr.-Ing. |
| 5/83 | BBC Brown Boveri AG, Baden / Switzerland since 1/ 88 ABB Asea Brown Boveri AG / Switzerland since 1/ 90 ABB Kraftwerke AG / Switzerland ( since 2000 Alstom Power Generation / Switzerland) |
| 5/83 - 12/87 | Development Engineer: Design of gas turbine blades aerodynamics, aeroelastic problems, cooling system, life cycle |
| 1/88 - 2/95 | Team Leader Turbine: Turbine Design, Aerodynamics, Cooling System, Life Cycle of Bladings, Power, Efficiency, Design Specification; Planning and Evaluation of Operating Tests at Turbines; Analysis of Blade Failures; Technology Development with |
| 3/89 - 4/91 | Head of Aero-Thermodynamic of the development project for the IGT GT11N2: turbine development; performance parameters of the GT- thermal block, blade aerodynamics, cooling systems, life cycle, secondary air system |
| 5/91 - 2/97 | Head of Turbine development in the project for the IGT GT24 / GT26: LP-Turbine, aerodynamics, cooling system, materials, life cycle power and efficiency, secondary air system, planning and evaluation prototype tests of the turbine, design of the turbine blades, development of the manufacturing process for the turbine blades: cooperation with manufacturers (Howmet, PCC e.a.) costs and schedules |
| 2/97 - 1/99 | Deputy Head of dept. "Integrated Turbine Development": post development and service support of all ABB IG-Turbines (GT24 / GT26, GT11N2, GT13E2, GT8C2) concepts for future turbines; aerodynamics, cooling system, material, life cycle, power and efficiency, secondary air system, planning and evaluation of turbine tests, design turbine blades, manufacturing support for turbine blades: cooperation with manufacturers (USA, UK, F, CH, D) (Quality, schedules, cost) |
| since 1.2.99 | Professor of Turbomachinery and Jet Propulsion at Technische Universität Dresden (C4-professorship) Teaching and research projects |
Ausgewählte Mitgliedschaften, Gremien- und Gutachtertätigkeiten
| 2005 - 2008 | Planungsgruppe AG Turbo |
| 2006 - 2014 | Fachkollegium 401 DFG |
| 2005 - heute |
Gutachtertätigkeit DFG Normalverf., SFB, Transregios, |
| 2002 - heute |
Technologieberatung, Design Reviews, Mitarbeiterausbildung: |
Veröffentlichungen bis 1/99
|
K.Vogeler |
A Method of Characteristic Approach to the Problem of Supersonic Flow Past Oscillating Cascades with Finite Blade Thickness, Naval Postgraduate School, Monterey, CA USA Rep. No. NPS67-78-912; 10/78 |
|
K.Vogeler |
A Method of Characteristic Solution for a Finite Oscillating Supersonic Cascade with Thickness Effects Proc. Symposium on Aeroelasticity in Turbomachines Lausanne (CH), 9/80, Editor P.Suter |
|
H.E.Gallus, |
Berechnung und Messung der Druckverteilung an oszillierenden Schaufelprofilen in zweidimensionaler Überschallströmung Mitt.d. Inst.f. Strahlantriebe der RWTH Aachen 6/81 No. 81-04 |
|
K.Vogeler, |
Bestimmung der Flatterstabilität von Schaufeln in einem Gitter bei Überschallströmung VDI Tagung, VDI-Ber. Nr.487, 1983 |
|
K.Vogeler |
Gitter mit harmonisch schwingenden Schaufeln in Überschallströmung, |
|
K.Vogeler |
The Unsteady Pressure Distribution on Parabolic Profiles in a Finite Cascade Oscillating in Supersonic Flow Proc. IUTAM Symposium on Unsteady Aerodynamics of Turbomachines and Propellers Cambridge (UK), 9/84, Editor D.Whitehead |
|
P.Felix, |
Das Gasturbinenkraftwerk Riyadh 8 - unter schweizerischer Gesamtleitung gebaut Schweizer Journal, 3/86 |
|
S.Abassi, |
Analysis of time-dependent model cascade turbine data and predictions in the transonic flow regions Proc. 6th International Conference on Aeroelasticity in Turbomachines and Propellers Notre Dame University, South Bend (USA), 9/91; Editor H.Atassi |
|
K.Vogeler |
The Potential of Sequential Combustion for High Bypass Jet Engines ASME Turbo Expo 1998, Stockholm; ASME 98-GT-311 |