Sealing technology is a key feature to improve efficiency of steam turbines for both new power stations and modernization projects. One of the most powerful sealing alternatives for reducing parasitic leakages in the blade path of a turbine as well as in shaft sealing areas is the use of brush seals, which are also widely used in gas turbines and turbo compressors. The advantage of brush seals over other sealing concepts is based on the narrow gap that is formed between the brush seal bristle tips and the mating rotor surface together with its radial adaptivity. While the narrow gap between the bristle tips and the rotor leads to a strongly decreased flow through the seal compared with conventional turbomachinery seals, it is important to be aware of the tight gap that can be bridged by relative motion between the rotor and the brush seal, leading to a contact of the bristles and the rotor surface. Besides abrasive wear occurrence, the friction between the bristles and the rotor leads to heat generation which can be detrimental to turbine operation due to thermal effects, leading to rotor bending connected to increasing shaft vibrations. In order to investigate the frictional heat generation of brush seals, different investigation concepts have been introduced through the past years. To broaden the knowledge about frictional heat generation and to make it applicable for steam turbine applications, a new testing setup was designed for the steam test rig of the Institute of Jet Propulsion and Turbomachinery - TU Braunschweig, Germany, enabling temperature measurements in the rotor body under stationary and transient operation in steam by using rotor-integrated thermocouples. Within this paper, the development of the instrumented new rotor design and all relevant parts of the new testing setup is shown along with the testing ability by means of the validation of the test rig concept and the achieved measurement accuracy. First results prove that the new system can be used to investigate frictional heat generation of brush seals under conditions relevant for steam turbine shaft seals.
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ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
June 13–17, 2016
Seoul, South Korea
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4978-1
PROCEEDINGS PAPER
Brush Seal Frictional Heat Generation: Test Rig Design and Validation Under Steam Environment
J. Friedrichs,
J. Friedrichs
TU Braunschweig, Braunschweig, Germany
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J. Flegler
J. Flegler
Siemens AG, Mülheim a. d. Ruhr, Germany
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M. Raben
TU Braunschweig, Braunschweig, Germany
J. Friedrichs
TU Braunschweig, Braunschweig, Germany
J. Flegler
Siemens AG, Mülheim a. d. Ruhr, Germany
Paper No:
GT2016-56951, V05AT15A017; 12 pages
Published Online:
September 20, 2016
Citation
Raben, M, Friedrichs, J, & Flegler, J. "Brush Seal Frictional Heat Generation: Test Rig Design and Validation Under Steam Environment." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 5A: Heat Transfer. Seoul, South Korea. June 13–17, 2016. V05AT15A017. ASME. https://doi.org/10.1115/GT2016-56951
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