Prof. Dr.-Ing. Konrad Vogeler

Konrad Vogeler © Michael Kretzschmar

Seniorprofessor

Name

Prof. Dr.-Ing. Konrad Vogeler

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Organization Name

Professur für Turbomaschinen und Flugantriebe

Professur für Turbomaschinen und Flugantriebe

Address work

Visiting address:

Zeuner-Bau, Raum 157 George-Bähr-Straße 3c

01069 Dresden

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work Tel.

Curriculum vitae

Date of Birth: 1949
Citizenship: German

Experiences

  • 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

Career

(beginning to end of)

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

Selected memberships, committee and expert activities

2005 - 2008 Planning Group AG Turbo
2006 - 2014 Review Board 401 DFG
2005 - heute Reviewer activities DFG Normalverf., SFB, Transregios,
BMWi LuFo, BMBWF (Austr.) Sp Sc,
2002 - heute Technology consulting, design reviews, staff training:
Siemens (Orlando FL, Charlotte NC, Mühlheim, Berlin), MAN (Oberhausen), FTT (Wildau, Jupiter FL), Hirschvogel Automotive

Publications until 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,
K.Vogeler 

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,
H.E.Gallus

 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,
Diss. RWTH Aachen 7/84

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,
K.Vogeler 

 Das Gasturbinenkraftwerk Riyadh 8 - unter schweizerischer Gesamtleitung gebaut Schweizer Journal, 3/86

S.Abassi,
A.Bölcs,
A.Cargill,
T.Fransson,
A.Suddhoo,
K.Vogeler

 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

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Last modified: May 18, 2022