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REDUCING THE DEMAND OF COOLANT AT THE SIDEWALL OF A HIGH PRESSURE TURBINE CASCADE BY MEANS OF SLOT WIDTH MODULATION

Woopen, Michael and Dannhauer, Axel and Gieß, Peter-Anton (2012) REDUCING THE DEMAND OF COOLANT AT THE SIDEWALL OF A HIGH PRESSURE TURBINE CASCADE BY MEANS OF SLOT WIDTH MODULATION. ASME, Turbo Expo 2012, 11. - 15. Juni 2012, Kopenhagen, Dänemark.

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Abstract

Within the framework of the German research project AGTurbo the influence of slot flows associated with cooling configurations were investigated experimentally. One interesting result of this work was the severe enhancement of the horse shoe vortex by the coolant dependent on the slot’s position and the ejected mass. Based on these results, further promising film cooling configurations with slot ejection were investigated numerically. Setting up the numerical studies was a challenging task since a very detailed model of the slot, the supply cavity, and the supply tubes had to be generated. Tests proved that smallest deviations against the experiment resulted in completely different flow structures. Nevertheless, the secondary flow structure as well as the aerodynamic parameters could be modeled excellently. According to the velocity field in front of a plane turbine cascade, higher wall pressure arises upstream of the leading edge region of the blades while the pressure drops to a minimum in the center of the passage. To avoid excessive ejection of coolant in the low pressure region the reduction of the local slot area is an appropriate method to decrease the slot mass flow in this particular area. An iterative method is introduced considering the desired mass flow rate and the prevailing total pressure in order to calculate the slot area and to avoid reverse flow. The variation of the film cooling effectiveness indicates a very uniform distribution of cooling air behind the slot which persists within the passage.

Item URL in elib:https://elib.dlr.de/76986/
Document Type:Conference or Workshop Item (Paper)
Title:REDUCING THE DEMAND OF COOLANT AT THE SIDEWALL OF A HIGH PRESSURE TURBINE CASCADE BY MEANS OF SLOT WIDTH MODULATION
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Woopen, MichaelDLR, AT-TU, jetzt RWTH AachenUNSPECIFIED
Dannhauer, AxelDLR, AT-TUUNSPECIFIED
Gieß, Peter-AntonDLR, AT-TUUNSPECIFIED
Date:June 2012
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:high pressure turbine, endwall cooling concepts, heat transfer, film cooling effectiveness, computational fluid dynamics
Event Title:ASME, Turbo Expo 2012
Event Location:Kopenhagen, Dänemark
Event Type:international Conference
Event Dates:11. - 15. Juni 2012
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Deposited By: Giess, Dr.-Ing. Peter-Anton
Deposited On:13 Aug 2012 16:25
Last Modified:13 Aug 2012 16:25

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