DE3770823D1 - Einrichtung zur regulierung des verbrennungsluftdurchsatzes in gasturbinenbrennkammern. - Google Patents

Einrichtung zur regulierung des verbrennungsluftdurchsatzes in gasturbinenbrennkammern.

Info

Publication number
DE3770823D1
DE3770823D1 DE8787115259T DE3770823T DE3770823D1 DE 3770823 D1 DE3770823 D1 DE 3770823D1 DE 8787115259 T DE8787115259 T DE 8787115259T DE 3770823 T DE3770823 T DE 3770823T DE 3770823 D1 DE3770823 D1 DE 3770823D1
Authority
DE
Germany
Prior art keywords
regulating
air flow
gas turbine
combustion air
combustion chambers
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE8787115259T
Other languages
English (en)
Inventor
Nobuyuki Iizuka
Katsukuni Hisano
Katsuo Wada
Fumiyuki Hirose
Osamu Arai
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Application granted granted Critical
Publication of DE3770823D1 publication Critical patent/DE3770823D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/18—Mechanical movements
    • Y10T74/18888—Reciprocating to or from oscillating
    • Y10T74/1892—Lever and slide
    • Y10T74/18968—Flexible connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
DE8787115259T 1987-10-19 1987-10-19 Einrichtung zur regulierung des verbrennungsluftdurchsatzes in gasturbinenbrennkammern. Expired - Lifetime DE3770823D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP87115259A EP0312620B1 (de) 1987-10-19 1987-10-19 Einrichtung zur Regulierung des Verbrennungsluftdurchsatzes in Gasturbinenbrennkammern

Publications (1)

Publication Number Publication Date
DE3770823D1 true DE3770823D1 (de) 1991-07-18

Family

ID=8197368

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787115259T Expired - Lifetime DE3770823D1 (de) 1987-10-19 1987-10-19 Einrichtung zur regulierung des verbrennungsluftdurchsatzes in gasturbinenbrennkammern.

Country Status (3)

Country Link
US (1) US4829764A (de)
EP (1) EP0312620B1 (de)
DE (1) DE3770823D1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5628182A (en) * 1993-07-07 1997-05-13 Mowill; R. Jan Star combustor with dilution ports in can portions
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
JP3706443B2 (ja) * 1996-09-24 2005-10-12 三菱重工業株式会社 アニュラ型ガスタービン燃焼器
US6925809B2 (en) 1999-02-26 2005-08-09 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
AU4607201A (en) * 1999-10-20 2001-04-30 Hitachi Limited Gas turbine combustor, pre-mixer for gas turbine combustors, and premixing method for gas turbine combustors
WO2001040713A1 (en) 1999-12-03 2001-06-07 Mowill Rolf Jan Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor
US20020104316A1 (en) * 2000-11-03 2002-08-08 Capstone Turbine Corporation Ultra low emissions gas turbine cycle using variable combustion primary zone airflow control
JP2003194338A (ja) 2001-12-14 2003-07-09 R Jan Mowill 可変出口形状を有するガスタービンエンジン用燃料／空気プレミキサ及び出口速度の制御方法
US6761033B2 (en) * 2002-07-18 2004-07-13 Hitachi, Ltd. Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low NOx combustion
GB201200237D0 (en) * 2012-01-09 2012-02-22 Rolls Royce Plc A combustor for a gas turbine engine
RU2595287C1 (ru) * 2015-04-09 2016-08-27 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" (КНИТУ-КАИ) Камера сгорания газотурбинного двигателя с регулируемым распределением воздуха

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR850434A (de) * 1938-03-24 1939-12-16
US2655787A (en) * 1949-11-21 1953-10-20 United Aircraft Corp Gas turbine combustion chamber with variable area primary air inlet
US2706913A (en) * 1953-06-01 1955-04-26 Trossi Domenico Mechanical movement for converting translatory motion into rotary motion, and vice versa, especially for precision instruments
US3958416A (en) * 1974-12-12 1976-05-25 General Motors Corporation Combustion apparatus
US3930368A (en) * 1974-12-12 1976-01-06 General Motors Corporation Combustion liner air valve
FR2472082A1 (fr) * 1979-12-19 1981-06-26 France Etat Perfectionnements apportes aux moteurs a combustion interne suralimentes, notamment aux moteurs diesel
US4419707A (en) * 1981-03-12 1983-12-06 Teletype Corporation Flexible band positioning device for a read/write head
US4497170A (en) * 1982-07-22 1985-02-05 The Garrett Corporation Actuation system for a variable geometry combustor
US4545196A (en) * 1982-07-22 1985-10-08 The Garrett Corporation Variable geometry combustor apparatus
US4525030A (en) * 1982-08-26 1985-06-25 General Scanning Inc. Positioner for optical element
US4523737A (en) * 1983-03-21 1985-06-18 Honeywell Inc. Sleeve valve actuator means
JPS60240833A (ja) * 1984-05-15 1985-11-29 Hitachi Ltd ガスタ−ビン燃焼方法及びガスタ−ビン燃焼器
JPS61195214A (ja) * 1985-02-22 1986-08-29 Hitachi Ltd ガスタ−ビン燃焼器の空気流量調整機構
JPH0663646B2 (ja) * 1985-10-11 1994-08-22 株式会社日立製作所 ガスタ−ビン用燃焼器

Also Published As

Publication number Publication date
US4829764A (en) 1989-05-16
EP0312620A1 (de) 1989-04-26
EP0312620B1 (de) 1991-06-12

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