Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines

C Koupper - 2015 - theses.hal.science
Nowadays, engines powering modern and large commercial or military aircraft essentially
rely on gas turbine technologies. Since the first prototypes built in the 40's, the efficiency and …

Experimental test rig for combustor-turbine interaction research and test results analysis

H Yin, S Liu, Y Feng, M Li… - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
Lean premixed combustion technology has been adopted widely for heavy duty gas turbine
application. At the combustor inlet section, the basic burner arrangement is multiple-swirl …

Defining a Testbed for the US Turbine Industry: The National Experimental Turbine (NExT)

KA Thole, M Barringer, RA Berdanier… - AIAA Propulsion and …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3489. vid The importance of
continued advancements in gas turbine technology for power generation, aviation, and oil …

Investigation of Unsteady Flow Phenomena in First Vane Caused by Combustor Flow With Swirl

S Jacobi, C Mazzoni, K Chana… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
The flow at the combustor turbine interface of power generation gas turbines with can
combustors is characterized by high and non-uniform turbulence levels, lengthscales and …

Development and application of a concentration probe for mixing flows tracking in turbomachinery applications

G Babazzi, T Bacci, A Picchi… - Journal of …, 2022 - asmedigitalcollection.asme.org
Modern gas turbines present important temperature distortions in the core-engine flowpath,
mainly in the form of hot and cold streaks imputed to combustor burners and components …

A discussion on removal mechanisms in grinding polycrystalline diamond

F Schindler, R Brocker, F Klocke… - Journal of …, 2016 - asmedigitalcollection.asme.org
Polycrystalline diamond (PCD) grinding takes an important role in the field of tool
manufacture. Regardless, there is still lack of process knowledge about the occurring …

Thermal investigation of integrated combustor vane concept under engine-realistic conditions

S Jacobi, B Rosic - Journal of Turbomachinery, 2017 - asmedigitalcollection.asme.org
This paper presents a thermal investigation of the integrated combustor vane concept for
power generation gas turbines with individual can combustors. This concept has the …

Development and aerothermal investigation of integrated combustor vane concept

S Jacobi, B Rosic - Journal of Turbomachinery, 2016 - asmedigitalcollection.asme.org
This paper presents the development and aerothermal investigation of the integrated
combustor vane concept for power generation gas turbines with individual can combustors …

Research on the swirling flow effect of the combustor–turbine interaction on vane film cooling

S Liu, H Yin - … in Materials Sciences, Energy Technology and …, 2017 - api.taylorfrancis.com
Lean premixed combustion technology has been adopted widely for heavy-duty gas turbine
application. At the combustor inlet section, the basic burner arrangement is multiple-swirl …