JPS6149136A
Expired / Lapsed
JP
⏱️ 0.0 years remaining
Operation control method of gas turbine
Assignee: Mitsubishi Heavy Industries Ltd
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Filing: 1984-08-16
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Granted: —
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Expires: 2004-08-16
Abstract
Abstract PURPOSE:To reduce the concentration of NOX in exhaust gas, by setting a proportion of pilot fuel to 25-50% when the operation only supplying pilot fuel is transferred to the operation supplying the pilot fuel mixing in main fuel. CONSTITUTION:A gas turbine provides the first fuel nozzle 2 supplying pilot fuel and the second fuel nozzle 5 supplying main fuel to a combustor 1. The turbine, when its operation is transferred from a 30-60% load only supplying pilot fuel to a 100% load, sets a proportion of the pilot fuel to mixed fuel to 25-50%. In this way, concentration of NOX in exhaust gas of the gas turbine can be reduced.
Inventors
- 👤 Shigemi Bandai
- 👤 重実 萬代
- 👤 Nobuo Sato
- 👤 佐藤 亘男
- 👤 Ichiro Fukue
- 👤 福江 一郎
- 👤 Kuniaki Aoyama
- 👤 邦明 青山
Bibliographic Details
Application Number
—
Jurisdiction
JP
Data Source
google_patents
Last Synchronized
2026-10-27 23:16
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/32; F02C9/34
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References Cited (Backward Citations)
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