A test device for premixed gas turbine combustion oscillations [electronic resource]
Saved in:
| Online Access: |
Online Access |
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| Format: | Government Document Electronic eBook |
| Language: | English |
| Published: |
Washington, D.C. : Oak Ridge, Tenn. :
United States. Department of Energy. ; distributed by the Office of Scientific and Technical Information, U.S. Department of Energy,
1996.
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| Subjects: |
| Abstract: | This paper discusses the design and operation of a test combustor suitable for studying combustion oscillations caused by a commercial-scale gas turbine fuel nozzle. Aside from the need to be conducted at elevated pressures and temperatures, it is desirable for the experimental device to be flexible in its geometry so as to provide an acoustic environment representative of the commercial device. The combustor design, capabilities, and relevant instrumentation for such a device are presented, along with initial operating experience and preliminary data that suggests the importance of nozzle reference velocity and air temperature. |
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| Item Description: | Published through SciTech Connect. 09/01/1996. "doe/metc/c--96/7245" " conf-9603196--1" "DE96013549" "NONE" Advanced turbin system (ATS) combustion workshop, Lake Arrowhead, CA (United States), 19-22 Mar 1996. Gemmen, R.S.; Yip, M.J.; Richards, G.A. USDOE Morgantown Energy Technology Center, WV (United States) |
| Physical Description: | 21 p. : digital, PDF file. |