US5024055A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Device for detecting combustion conditions in combustors
Assignee: Hitachi Ltd
•
Filing: 1989-08-04
•
Granted: 1991-06-18
•
Expires: 2009-08-04
Abstract
Abstract A device 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 plurality of sensors for measuring concentration of unburnt component in the combustion gas, which is disposed on the downstream side of the gas turbine, a unit for obtaining a distribution pattern of the measured concentration and for investigating the obtained 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
2026-11-03 01:11
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: 12
Claim 1
Independent Claim
81 words
A device for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus including said combustors and a gas turbine driven by combustion gas from said combustors, said device comprising: means disposed on a downstream side of said gas turbine for measuring a concentration of at least one unburnt component in said combustion gas; means for obtaining a distribution pattern of said measured concentration; and means for examining said obtained distribution pattern to detect combustion conditions in said combustors.
Claim 2
Independent Claim
81 words
A device for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus including said combustors and a gas turbine driven by combustion gas from said combustors, said device comprising: means disposed on a downstream side of said gas turbine for measuring a concentration of at least one unburnt component in said combustion gas; means for obtaining a distribution pattern of said measured concentration; and means for examining said obtained distribution pattern to detect combustion conditions in said combustors.
Claim 3
Dependent Claim
26 words
A detecting device according to claim 1, wherein said measuring means includes a plurality of sensors equal to or greater than a number of said combustors.
Claim 4
Dependent Claim
110 words
A detecting device according to claim 1, for detecting combustion conditions in a plurality of combustors in a gas-turbine apparatus including said combustors and a gas turbine apparatus including said combustors and a gas turbine driven by combustion gas from said combustors, said device comprising; means disposed on a downstream side of said gas turbine for measuring a concentration of at least one unburnt component in the combustion gas; means for obtaining a distribution pattern of said measured concentration; and means for investigating said obtained distribution pattern to detect combustion conditions in said combustors, said means for investigating compares said distribution pattern of said measured concentration with prestored distribution patterns.
Claim 5
Dependent Claim
32 words
A detecting device according to claim 3, wherein said means for investigating includes memory means for storing distribution patterns, and comparator means for comparing said distribution pattern stored in said memory means.
Claim 6
Dependent Claim
18 words
A detecting device according to claim 2, wherein said plurality of sensors are arranged equiangularly on one circle.
Claim 7
Dependent Claim
111 words
A control device for controlling combustion in a plurality of combustors in a gas-turbine apparatus including said combustors and a gas turbine driven by combustion gas from said combustors, said device comprising: means disposed on a downstream side of said gas turbine for measuring a concentration of at least one unburnt component in said combustion gas; means for obtaining a distribution pattern of said measured concentration of said at least one unburnt component; means for examining said distribution pattern to detect conditions in said combustors; and means for adjusting flow rates of air and/or of fuel to be fed to the respective combustors on the basis of said detected combustion conditions.
Claim 8
Dependent Claim
111 words
A control device for controlling combustion in a plurality of combustors in a gas-turbine apparatus including said combustors and a gas turbine driven by combustion gas from said combustors, said device comprising: means disposed on a downstream side of said gas turbine for measuring a concentration of at least one unburnt component in said combustion gas; means for obtaining a distribution pattern of said measured concentration of said at least one unburnt component; means for examining said distribution pattern to detect conditions in said combustors; and means for adjusting flow rates of air and/or of fuel to be fed to the respective combustors on the basis of said detected combustion conditions.
Claim 9
Dependent Claim
29 words
A control device according to claim 6, wherein said measuring means is disposed in a position in which said combustion gas from said combustors flow at an increased speed.
Claim 10
Dependent Claim
56 words
A control device according to claim 6, 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 said flow rate adjusting means adjusts flow rates of air and/or of fuel to be fed to the respective second stage combustion chamber.
Claim 11
Dependent Claim
24 words
A detecting device according to claim 3, wherein said combustion conditions include at least one of a misfiring or abnormal combustion or said combustors.
Claim 12
Dependent Claim
37 words
A control device according to claim 6, wherein said measuring means is disposed in a position in which a flow direction of said combustion gas from said combustors is changed and the flow speed thereof is increased.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-06-17 | 1994-12-17 | 1995-06-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-06-17 | 1998-12-17 | 1999-06-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-06-17 | 2002-12-17 | 2003-06-18 | $7700.00 | Window Closed / Lapsed |