Numerical investigation of vortex reducer flows in the high pressure compressor of modern aeroengines

D Peitsch, M Stein, S Hein… - Turbo Expo …, 2002 - asmedigitalcollection.asme.org
… the main components of gas turbines. Programmes for the high pressure turbine and for the
combustion chamber. have been set up. The high pressure compressor has been identified …

Experimental analysis of varied vortex reducer configurations for the internal air system of jet engine gas turbines

A Gu¨ nther, W Uffrecht, E Kaiser… - Turbo Expo …, 2008 - asmedigitalcollection.asme.org
… be taken from an earlier compressor stage. The air … turbine blades causes high pressure
losses in the cavities between the compressor and turbine discs due to side friction and vortex

The experimental investigations of centripetal air bleed with tubed vortex reducer for secondary air system in gas turbine

X Chen, Y Feng, L Wu - Turbo Expo: Power for Land …, 2014 - asmedigitalcollection.asme.org
… In a modern gas turbine, the air bled through High Pressure Compressor (HPC) rotor drums
… cool the High Pressure Turbine (HPT). The centripetal air flow creates a strong vortex, which …

Numerical analysis of industrial gas turbine secondary air systems employing vortex reducers

T Sibilli, GH Cho, F Kholi… - Turbo Expo …, 2018 - asmedigitalcollection.asme.org
… This is called a freevortex, characterized by a high pressure … The full gas turbine SAS model
for this engine application, … the co-rotating compressor disks and the vortex reducer. The disk …

Secondary air systems in aeroengines employing vortex reducers

D Negulescu, M Pfitzner - Turbo Expo …, 2001 - asmedigitalcollection.asme.org
… during the design of a gas turbine. Both types of … The rig features two compressor discs where
the vortex reducers are … achieved in the region of high pressure ratios on the upper branch …

Numerical study on varied vortex reducer configurations for the flow path optimization in compressor cavities

X Du, H Zhu, Z Zhang - Turbo Expo: Power for Land …, 2011 - asmedigitalcollection.asme.org
high pressure losses and limit the cooling flow rate. The present work investigates the fluid
flow for twelve kinds of vortex reducer … engine gas turbines two different kinds of vortex reducer

Experimental investigation of pressure losses in a co-rotating cavity with radial inflow employing tubed vortex reducers with varied nozzles

Z Liang, X Luo, Y Feng, G Xu - Experimental Thermal and Fluid Science, 2015 - Elsevier
… from the compressor platform to cool down the turbine discs but … For the present study of
air-cooling for a gas turbine, Ro is used … < 4.5 × 10 4 ), high pressure drop happens, where the …

Experimental study on a hybrid vortex reducer system in reducing the pressure drop in a rotating cavity with radial inflow

S Wei, J Mao, J Yan, X Han, Z Tu, R Tian - Experimental Thermal and Fluid …, 2020 - Elsevier
… The gas supply system provides dry and stable air to the test section. The compressor
pumps the airflow into the air resource, and the air passes through the drying device, which …

Numerical analysis of secondary airflow in a rotating cavity of a gasturbine at high operating points with vortex reducer implementation

A Mucci, FK Kholi, T Sibilli, JK Min, MY Ha… - Heat and Mass Transfer, 2021 - Springer
… “free-vortex”, and produces a high pressure drop across the … co-rotating compressor disks
and the vortex reducer. The disk … the oblong channel in the vortex reducer. For the case of the …

[HTML][HTML] Torque and energy recovery of a compressor disk cavity in gas turbine engines

W Shen, S Wang, F Huang, M Wang - Case Studies in Thermal Engineering, 2024 - Elsevier
… of a compressor disk cavity with tubed vortex reducer (TVR) to improve the secondary air
system performance of gas turbine … In gas turbine engines, a high-pressure turbine provides …