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US5107673A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for detecting combustion conditions in combustors

Assignee: Hitachi Ltd
•
Filing: 1991-04-30
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Granted: 1992-04-28
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Expires: 2011-04-30
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Abstract

Abstract A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes the combustors and a gas turbine driven by combustion gas from the combustors, comprises a step for measuring concentration of unburnt component in the combustion gas by means of a plurality of sensors disposed on the downstream side of the gas turbine, a step for obtaining a distribution pattern of the measured concentration, and a step for investigating the distribution pattern to detect combustion conditions in the combustors.

Inventors

  • 👤 Isao Sato
  • 👤 Seiichi Kirikami
  • 👤 Akira Shimura
  • 👤 Fumiyuki Hirose
  • 👤 Hiroshi Inose
  • 👤 Haruo Urushidani
  • 👤 Osamu Arai

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 08:38
CPC Classifications
F; F23; F23N; F23N5/00; F23N5/003; F05; F05D; F05D2270/00; F05D2270/01; F05D2270/08; F05D2270/083; F05D2270/0831; F23N2241/00; F23N2241/20

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 80 words
A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of: measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine; obtaining a distribution pattern of said measured concentration; and examining said distribution pattern to detect combustion conditions in said combustors.
Claim 2
Independent Claim 80 words
A method for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of: measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine; obtaining a distribution pattern of said measured concentration; and examining said distribution pattern to detect combustion conditions in said combustors.
Claim 3
Dependent Claim 17 words
A detecting method according to claim 1, wherein said steps are repeated over a predetermined time period.
Claim 4
Dependent Claim 33 words
A detecting method according to claim 1, wherein the step of measuring includes measuring the combustion gas at a position at which the combustion gas from the combustors flows at an increased speed.
Claim 5
Dependent Claim 34 words
A detecting method according to claim 1, wherein the step of examining includes storing the distribution pattern in a memory means, and comparing said distribution pattern with distribution patterns prestored in said memory means.
Claim 6
Dependent Claim 100 words
A control method for controlling combustion in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of: measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine; obtaining a distribution pattern of said measured concentration; examining said distribution pattern to detect combustion conditions in said combustors; and adjusting flow rates of air and/or fuel to be fed to the respective combustors in dependence upon detected combustion conditions.
Claim 7
Dependent Claim 100 words
A control method for controlling combustion in a plurality of combustors in a gas-turbine apparatus which includes a gas turbine driven by combustion gas from said combustors, said method comprising the steps of: measuring a concentration of at least one uncombusted component in said combustion gas by a plurality of sensors disposed on a downstream side of said gas turbine; obtaining a distribution pattern of said measured concentration; examining said distribution pattern to detect combustion conditions in said combustors; and adjusting flow rates of air and/or fuel to be fed to the respective combustors in dependence upon detected combustion conditions.
Claim 8
Dependent Claim 57 words
A control method for controlling combustion according to claim 5, wherein each of said combustors includes a first stage combustion chamber and a second stage combustion chamber disposed downstream of said first stage combustion chamber, and wherein the step of adjusting includes adjusting flow rates of air and/or fuel fed to the respective second stage combustion chambers.
Claim 9
Dependent Claim 37 words
A control method for controlling combustion according to claim 6, wherein the step of examining includes storing the distribution pattern in a memory means, and comparing said distribution pattern with distribution patterns prestored in said memory means.
Claim 10
Dependent Claim 36 words
A control method for controlling combustion according to claim 5, wherein the step of measuring includes measuring the combustion gas at a position at which the combustion gas from the combustors flows at an increased speed.
Claim 11
Dependent Claim 37 words
A control method for controlling combustion according to claim 5, wherein the step of examining includes storing the distribution pattern in a memory means, and comparing said distribution pattern with distribution patterns prestored in said memory means.

References Cited (Backward Citations)

JPS539911A Cited
JPS5741524A Cited
JPS61197726A Cited
US4731990A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-04-28 1995-10-28 1996-04-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-04-28 1999-10-28 2000-04-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-04-28 2003-10-28 2004-04-28 $7700.00 Window Closed / Lapsed

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