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Featured researches published by Daniel Gloss.


ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition | 2011

Experimental Investigation of Geometrical Parameters on the Pressure Recovery of Low Pressure Steam Turbine Exhaust Hoods

Conrad Finzel; Markus Schatz; Michael Casey; Daniel Gloss

The three-dimensional inhomogeneous flow in the exhaust hoods of low pressure steam turbines is a major cause of losses and the design of low-loss exhaust hoods remains a challenge, particularly in retrofit units. This paper examines the sensitivity of certain geometrical exhaust hood parameters on the pressure recovery of the whole exhaust system of low pressure steam turbines. The experimental investigations are carried out in a scaled exhaust system test rig operating at full-scale Mach numbers and near design flow conditions. The measurements for all exhaust hood configurations have been performed on two axial-radial diffuser geometries at two different load points, which represent the outflow in the design point of a last stage rotor with and without shrouds. The flow measurements make use of pneumatic probes and wall pressure taps. The influence of the exhaust hood area, the flow area in the horizontal joint plane and the location of the steam inlet are examined. The sensitivity of the pressure recovery on these parameters is evaluated. The flow area in the horizontal joint plane is identified as the most sensitive geometrical parameter in the exhaust hood of low pressure steam turbines.Copyright


International Journal of Turbomachinery, Propulsion and Power | 2016

Impact of the Exhaust Geometry on Flow Losses in a High-Pressure Steam Turbine

Christian Musch; Simon Hecker; Daniel Gloss; Ruben Steinhoff


Archive | 2013

Method for detecting a crack in rotor blades in the operation of a turboengine

Heinrich Stüer; Frank Deister; Ingo Förster; Daniel Gloss; Christian Musch; Frank Truckenmüller


Archive | 2013

Method for laying out a steam filter and steam valve with the steam filter

Susanne Gollerthan; Christian Böhme; Frank Deister; Manuel Ettler; Daniel Gloss; Volker Guck; Marco Schwarze; Hannes Teuber; Carsten Thiemann


Archive | 2013

Method for temperature balance in a steam turbine

Daniel Gloss; Frank Deister; Ingo Förster; Christian Musch; Heinrich Stüer; Frank Truckenmüller


Archive | 2012

METHOD FOR A TEMPERATURE COMPENSATION IN A STEAM TURBINE

Frank Deister; Ingo Förster; Daniel Gloss; Christian Musch; Heinrich Stüer; Frank Truckenmüller


Archive | 2012

INTERNALLY COOLABLE COMPONENT FOR A GAS TURBINE WITH AT LEAST ONE COOLING DUCT

Marcel Eifel; Daniel Gloss; Andreas Heselhaus; Stephan Klumpp; Marco Link; Uwe Sieber; Stefan Völker; Michael Wagner


Archive | 2012

Cooling rib system for a cooling passage of a turbine blade

Marcel Eifel; Daniel Gloss; Andreas Heselhaus; Stephan Klumpp; Marco Link; Uwe Sieber; Stefan Völker; Michael Wagner


Archive | 2011

Internally cooled component for a gas turbine with at least one cooling channel

Marcel Eifel; Daniel Gloss; Andreas Heselhaus; Stephan Klumpp; Marco Link; Uwe Sieber; Stefan Völker; Michael Wagner


Archive | 2011

Cooling fin system for a cooling channel and turbine blade

Marcel Eifel; Daniel Gloss; Andreas Heselhaus; Stephan Klumpp; Marco Link; Uwe Sieber; Stefan Völker; Michael Wagner

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