UTC Combustor and Turbine Aerothermal Interaction
Rolls-Royce University Technology Centre (UTC)
The Rolls-Royce University Technology Centre at TU Darmstadt was founded to investigate the aerodynamic and thermal interaction between combustion chamber and turbine. In a strategic partnership between science and industry, we develop new technologies for aircraft engines that will meet future economic and ecological goals.
The Rolls-Royce University Technology Centre (UTC) was established in 2006, and has since achieved valuable results in the field of the environmental performance of aero-engines. The UTC thus serves one of the core objectives of the aviation industry, which is striving to achieve stringent environmental targets by 2050 (Flightpath 2050) as part of the industry-wide research alliance ACARE (Advisory Council for Aeronautics Research in Europe).
The ambitious ACARE targets of reducing nitrogen oxides by 90 % per passenger kilometer, CO2 emissions by 75 %, and noise by 65 % are only possible through fundamental revisions in the combustion process. It is essential to take technical changes in the combustion chamber into account when designing turbines, because the temperature at the turbine inlet already exceeds the melting temperatures of the materials used. Sophisticated cooling mechanisms ensure safe turbine operation at these temperatures and enable high efficiencies and low CO2 emissions in modern aircraft engines.
This is the development environment in which the research center at the TU Darmstadt operates, where researchers are investigating new combustion technologies and their modeling on the one hand, and their effects on the turbine on the other.
At TU Darmstadt, scientists from three institutes contribute to the research in aero-engines with the industry partner Rolls-Royce Deutschland.
The UTC is directed by Prof. Heinz-Peter Schiffer (Institute of Gas Turbines and Aerospace Propulsion, (opens in new tab)). Additionally, the heads of institute Prof. Christian Hasse (Institute of Simulation of reactive Thermo-Fluid Systems, GLR (opens in new tab)) and Prof. Andreas Dreizler (Institute of Reactive Flows and Diagnostics, STFS (opens in new tab)) and their teams contribute to the success of the cooperation. RSM
Together, the institutes provide significant knowledge in the areas of experimental measurements and investigations of combustion processes (RSM) and the compressor and turbine stage (GLR), as well as numerical counterparts for combustion modeling (STFS) and fluid flow simulations of compressor and turbine (GLR).
40th International Symposium on Combustion in Milan
August 01, 2024
The Combustion Institute’s 40th International Symposium – Emphasizing Energy Transition was held in Milan, Italy, from July 21 to July 26. Throughout the week, researchers from around the world presented their work and provided insights into the future of combustion technologies.
Annual Combustion and Turbines UTC Review
June 10, 2024
This year's Annual Combustion and Turbines UTC Review was held at the RRD site in Dahlewitz. The event provided an excellent platform for teams to exchange insights into recent work across various RRD partner locations.
4 successful Ph.D. defenses in 7 seven days
February 28, 2024
Update regarding ASME Turbo Expo 2023 in Boston
December 01, 2023
STFS researchers Hanna Reinhardt and Philipp Koob presented recent findings of our aero-engines group at the ASME Turbo Expo 2023 in Boston.
Symposium on Thermoacoustics in Combustion (SoTiC) in Zurich
October 25, 2023
The STFS aero-engine thermoacoustics team Cetin Alanyalioglu and Hanna Reinhardt travelled to Zurich in September 2023 to network with the scientific acoustics community and to present the resent advances in processing of thermoacoustic data sets and hybrid, high-fidelity LES-CAA coupling.