Numerical simulation of the flow pulsations origin in cascades of the rear blade rows in a gas turbine axial compressor using low calorific fuel

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23210%2F08%3A00500469" target="_blank" >RIV/49777513:23210/08:00500469 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Numerical simulation of the flow pulsations origin in cascades of the rear blade rows in a gas turbine axial compressor using low calorific fuel

Original language description

Fatigue failure of the last three stator rows vanes (S17, EGV1 and EGV2) in the seventeen stage gas turbine axial compressor occurred in the power plant where low calorific fuel, syngas, was used. Causes of this dangerous phenomenon were flow pulsationswith the frequency of 380 to 400 Hz that were found by the experimental investigation of the duty gas turbine. Mechanism of the flow unsteadiness origin was studied with the help of flow simulations in 2D stator cascade system. Three numerical experiments were carried out.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

JL - Fatigue and fracture mechanics

OECD FORD branch

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Project

<a href="/en/project/1M06059" target="_blank" >1M06059: Advanced Technologies and Systems for Power Engineering</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2008

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

Proceedings of the 2008 ASME turbo expo 2008

ISBN

978-0-7918-4316-1

ISSN

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e-ISSN

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Number of pages

13

Pages from-to

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Publisher name

ASME

Place of publication

New York

Event location

Berlín

Event date

Jun 13, 2008

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

000262646900046