JP2008291842A - ガスタービンの燃焼室の圧力ダイナミックスを制御しかつそのライフサイクルを推定する方法 - Google Patents
ガスタービンの燃焼室の圧力ダイナミックスを制御しかつそのライフサイクルを推定する方法 Download PDFInfo
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- JP2008291842A JP2008291842A JP2008132584A JP2008132584A JP2008291842A JP 2008291842 A JP2008291842 A JP 2008291842A JP 2008132584 A JP2008132584 A JP 2008132584A JP 2008132584 A JP2008132584 A JP 2008132584A JP 2008291842 A JP2008291842 A JP 2008291842A
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- combustion chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N3/00—Regulating air supply or draught
- F23N3/002—Regulating air supply or draught using electronic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N5/00—Systems for controlling combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2225/00—Measuring
- F23N2225/04—Measuring pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2241/00—Applications
- F23N2241/20—Gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N5/00—Systems for controlling combustion
- F23N5/16—Systems for controlling combustion using noise-sensitive detectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00013—Reducing thermo-acoustic vibrations by active means
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Control Of Turbines (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Valve Device For Special Equipments (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
【解決手段】本方法は、タービンの燃焼室(14)に対応して配置した1つ又はそれ以上のプローブ(30)によって、該燃焼室(14)内の圧力振動の振幅及び該圧力振動の持続時間又はサイクルを測定する段階と、燃焼室(14)を形成した特定の材料、所定の燃焼周波数、並びに測定した圧力振動の振幅及びサイクル値についてのWohler曲線を作成することによって、該燃焼室(14)の疲労条件下における挙動を評価する段階と、タービンの疲労条件下で機能した間における燃焼室(14)への累積損傷(D)をPalmgren−Miner仮説によって測定する段階と、測定した累積損傷値(D)が超過した場合に、タービンの防護措置を実施する段階とを含む。
【選択図】 図1
Description
F(x):=6.651・exp(−1.583・10−6・x)+1.839
を得ることができる。
y=6.651・exp(1.583・106・x)+1.839solve,x→(631711.93935565382186)・ln(.15035333032626672681・y−.27649977447000451060)
g(y):=(631711.93935565382186)・ln(.15035333032626672681・y−.27649977447000451060)、
を算出することが必要である。
12 入口ダクト
14 燃焼室
16 供給ダクト
18 ダクト
20 タービン
22 発電機
24 シャフト
26 シャフト
28 出口ダクト
30 プローブ
Claims (4)
- 入口ダクト(12)を通してその中に導入された空気を加圧することができる少なくとも1つの圧縮機(10)と、前記加圧空気を供給ダクト(16)から流入した気体燃料と混合する少なくとも1つの燃焼室(14)と、前記燃焼室(14)から流入した気体のエネルギーを1つ又はそれ以上の作業機械(22)を作動させるために利用可能な仕事エネルギーに変換することができる少なくとも1つのタービン(20)とを含む形式のガスタービンにおける燃焼を制御する方法であって、
前記燃焼室(14)に対応して配置した1つ又はそれ以上のプローブ(30)によって、該燃焼室(14)内の圧力振動の振幅及び前記圧力振動の持続時間又はサイクルを測定する段階と、
前記燃焼室(14)を形成した特定の材料、所定の燃焼周波数、並びに前記測定圧力振動の振幅及びサイクル値についてのヴェーラー曲線を作成することによって、該燃焼室(14)の疲労条件下における挙動を評価する段階と、
前記タービンの疲労条件下で機能した間における前記燃焼室(14)への累積損傷(D)を下記に定義したパルムグレン−マイナー則
D=累積損傷
k=振幅レベル数
Ni=前記Wohler曲線から導き出したi番目レベルの振幅において破損に達するのに必要なサイクル数
ni=i番目レベルの振幅において経過したサイクル数、
によって測定する段階と、
前記測定した累積損傷値(D)が超過した場合に、前記タービンの防護措置を行う段階と、
を含む方法。 - 前記測定したサイクル値及び振幅値を、指数回帰f(x)で近似させる段階をさらに含む、請求項1記載の方法。
- 前記サイクル数(Ni)を決定するために前記指数回帰f(x)の逆関数g(x)を算出する段階をさらに含む、請求項2記載の方法。
- 前記防護措置を行う段階が、前記タービンを拡散火炎動作条件下に置く段階と、前記燃焼室(14)内の圧力振動を減少させる段階とを含む、請求項1記載の方法。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT001048A ITMI20071048A1 (it) | 2007-05-23 | 2007-05-23 | Metodo per il controllo delle dinamiche di pressione e per la stima del ciclo di vita della camera di combustione di una turbina a gas |
ITMI2007A001048 | 2007-05-23 |
Publications (2)
Publication Number | Publication Date |
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JP2008291842A true JP2008291842A (ja) | 2008-12-04 |
JP5290625B2 JP5290625B2 (ja) | 2013-09-18 |
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JP2008132584A Expired - Fee Related JP5290625B2 (ja) | 2007-05-23 | 2008-05-21 | ガスタービンの燃焼室の圧力ダイナミックスを制御しかつそのライフサイクルを推定する方法 |
Country Status (8)
Country | Link |
---|---|
US (1) | US8868313B2 (ja) |
EP (1) | EP1995519B1 (ja) |
JP (1) | JP5290625B2 (ja) |
KR (1) | KR101457696B1 (ja) |
CN (1) | CN101311510B (ja) |
CA (1) | CA2630953C (ja) |
IT (1) | ITMI20071048A1 (ja) |
RU (1) | RU2465519C2 (ja) |
Cited By (2)
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JP2012233480A (ja) * | 2011-05-05 | 2012-11-29 | Alstom Technology Ltd | ガスタービン機関を高い動的プロセス値に対して保護する方法及び前記方法を行うためのガスタービン機関 |
JP2015529768A (ja) * | 2012-08-30 | 2015-10-08 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | ガスタービンとその運転監視方法および監視装置 |
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US8924506B2 (en) | 2000-12-27 | 2014-12-30 | Bradium Technologies Llc | Optimized image delivery over limited bandwidth communication channels |
US8370046B2 (en) * | 2010-02-11 | 2013-02-05 | General Electric Company | System and method for monitoring a gas turbine |
US8437880B2 (en) * | 2010-05-17 | 2013-05-07 | General Electric Company | System and method for enhancement of power generation facilities |
CN105973597B (zh) * | 2016-05-27 | 2019-04-09 | 北京交通大学 | 列车轴箱轴承寿命的试验预测方法 |
US11016117B2 (en) | 2018-08-31 | 2021-05-25 | Honeywell International Inc. | Air data probe replacement determination system |
US11422153B2 (en) | 2020-01-24 | 2022-08-23 | Honeywell International Inc. | Air data probe replacement determination system |
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- 2008-05-21 JP JP2008132584A patent/JP5290625B2/ja not_active Expired - Fee Related
- 2008-05-21 EP EP08156638.2A patent/EP1995519B1/en active Active
- 2008-05-22 RU RU2008120462/06A patent/RU2465519C2/ru active
- 2008-05-22 KR KR1020080047721A patent/KR101457696B1/ko active IP Right Grant
- 2008-05-23 CN CN2008101091074A patent/CN101311510B/zh not_active Expired - Fee Related
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Also Published As
Publication number | Publication date |
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CA2630953A1 (en) | 2008-11-23 |
KR20080103446A (ko) | 2008-11-27 |
KR101457696B1 (ko) | 2014-11-03 |
JP5290625B2 (ja) | 2013-09-18 |
RU2465519C2 (ru) | 2012-10-27 |
ITMI20071048A1 (it) | 2008-11-24 |
EP1995519A2 (en) | 2008-11-26 |
EP1995519B1 (en) | 2020-04-08 |
CN101311510A (zh) | 2008-11-26 |
CN101311510B (zh) | 2013-06-19 |
RU2008120462A (ru) | 2009-11-27 |
US20080294322A1 (en) | 2008-11-27 |
CA2630953C (en) | 2015-07-21 |
EP1995519A3 (en) | 2017-07-26 |
US8868313B2 (en) | 2014-10-21 |
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