IT1185959B - Combustore per turbina a gas raffreddato mediante separazione ad urto con raffreddamento a velo fluido interno - Google Patents

Combustore per turbina a gas raffreddato mediante separazione ad urto con raffreddamento a velo fluido interno

Info

Publication number
IT1185959B
IT1185959B IT22315/85A IT2231585A IT1185959B IT 1185959 B IT1185959 B IT 1185959B IT 22315/85 A IT22315/85 A IT 22315/85A IT 2231585 A IT2231585 A IT 2231585A IT 1185959 B IT1185959 B IT 1185959B
Authority
IT
Italy
Prior art keywords
sail
combustor
cooling
gas turbine
internal fluid
Prior art date
Application number
IT22315/85A
Other languages
English (en)
Italian (it)
Other versions
IT8522315A0 (it
Inventor
Edward Wayne Tobery
Ronald Joseph Kuznar
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of IT8522315A0 publication Critical patent/IT8522315A0/it
Application granted granted Critical
Publication of IT1185959B publication Critical patent/IT1185959B/it

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/045Air inlet arrangements using pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00Casings; Linings; Walls
    • F23M5/08Cooling thereof; Tube walls
    • F23M5/085Cooling thereof; Tube walls using air or other gas as the cooling medium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • F23R3/08Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Spray-Type Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT22315/85A 1984-10-04 1985-09-30 Combustore per turbina a gas raffreddato mediante separazione ad urto con raffreddamento a velo fluido interno IT1185959B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US65755484A 1984-10-04 1984-10-04

Publications (2)

Publication Number Publication Date
IT8522315A0 IT8522315A0 (it) 1985-09-30
IT1185959B true IT1185959B (it) 1987-11-18

Family

ID=24637675

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22315/85A IT1185959B (it) 1984-10-04 1985-09-30 Combustore per turbina a gas raffreddato mediante separazione ad urto con raffreddamento a velo fluido interno

Country Status (6)

Country Link
EP (1) EP0178820A1 (en])
JP (1) JPS6186519A (en])
KR (1) KR860003469A (en])
CN (1) CN85107191A (en])
IT (1) IT1185959B (en])
MX (1) MX161443A (en])

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19547703C2 (de) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Brennkammer, insbesondere Ringbrennkammer, für Gasturbinentriebwerke
GB9919981D0 (en) * 1999-08-24 1999-10-27 Rolls Royce Plc Combustion apparatus
KR100395643B1 (ko) * 2000-10-04 2003-08-21 한국기계연구원 가스터빈 연소기
US7975487B2 (en) 2006-09-21 2011-07-12 Solar Turbines Inc. Combustor assembly for gas turbine engine
US8448443B2 (en) * 2007-10-11 2013-05-28 General Electric Company Combustion liner thimble insert and related method
JP2011102669A (ja) 2009-11-10 2011-05-26 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器及びガスタービン
KR20150074155A (ko) 2012-10-24 2015-07-01 알스톰 테크놀러지 리미티드 희석 가스 혼합기를 가진 연속 연소
US8707673B1 (en) * 2013-01-04 2014-04-29 General Electric Company Articulated transition duct in turbomachine
EP2989389B1 (en) * 2013-04-25 2018-08-01 Ansaldo Energia Switzerland AG Sequential combustion with dilution gas
EP3037726B1 (en) * 2014-12-22 2018-09-26 Ansaldo Energia Switzerland AG Separate feedings of cooling and dilution air
FR3037107B1 (fr) * 2015-06-03 2019-11-15 Safran Aircraft Engines Paroi annulaire de chambre de combustion a refroidissement optimise
CN105042640B (zh) * 2015-08-11 2018-05-08 南京航空航天大学 航空发动机燃烧室火焰筒的冷却结构
CN109642472B (zh) * 2016-08-30 2021-07-06 西门子股份公司 用于燃气轮机的冲击冷却特征
CN110185554B (zh) * 2019-03-08 2021-09-10 西北工业大学 一种用于喷气发动机矢量喷管的双层壁冷却结构
CN110107914A (zh) * 2019-04-10 2019-08-09 南京航空航天大学 一种基于三角形截面导流板(环)的冲击-气膜冷却结构
CN113464283B (zh) * 2021-08-10 2022-10-21 南京航空航天大学 一种旋转爆震发动机复合主动冷却结构及旋转爆震发动机
CN113739208B (zh) * 2021-09-09 2022-08-26 成都中科翼能科技有限公司 一种用于低污染燃气轮机的混合冷却火焰筒

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3369363A (en) * 1966-01-19 1968-02-20 Gen Electric Integral spacing rings for annular combustion chambers
US4109459A (en) * 1974-07-19 1978-08-29 General Electric Company Double walled impingement cooled combustor
GB2095816B (en) * 1981-03-27 1984-12-12 Westinghouse Electric Corp Gas turbine combustor

Also Published As

Publication number Publication date
EP0178820A1 (en) 1986-04-23
MX161443A (es) 1990-09-27
IT8522315A0 (it) 1985-09-30
JPH0317045B2 (en]) 1991-03-07
CN85107191A (zh) 1986-09-24
KR860003469A (ko) 1986-05-26
JPS6186519A (ja) 1986-05-02

Similar Documents

Publication Publication Date Title
IT1185959B (it) Combustore per turbina a gas raffreddato mediante separazione ad urto con raffreddamento a velo fluido interno
GB2097479B (en) Cooled vane for a gas turbine engine
GB2163218B (en) Cooled vane or blade for a gas turbine engine
GB2053367B (en) Cooled shroud for a gas turbine engine
IT7926656A0 (it) Turbina raffreddata ad aria per motore a turbina a gas.
BR8200239A (pt) Conjunto de refrigeracao de camisa de veneziana de um combustor para motor de turbina a gas
DE3261740D1 (en) Stage of a gas turbine jet engine with air cooling means for the turbine rotor disc
GB2108202B (en) Air cooling systems for gas turbine engines
IT8619527A1 (it) Turbomotore a gas con migliorato rendimento termico
IT1108741B (it) Sistemi di raffreddamento per motori a turbina a gas
GB2155413B (en) A mechanism for improving flow conditions at air inlets for gas turbine engines installed in aircraft
IT1098088B (it) Raffreddatore dell'aria di raffreddamento per motore a gas a turboventilatore
FR2592092B1 (fr) Turbine a aubes refroidies notamment pour moteur a turbine a gaz
NO900803L (no) Kjoelte blader for en gassturbinmotor
IT1178620B (it) Complesso di combustione per motore a turbina a gas
IT1133988B (it) Paletta raffreddata per traspirazione,per un motore a turbina a gas
IL62556A (en) Combustor liner construction for gas turbine engines
IL62557A0 (en) Combustor liner construction for gas turbine engines
DE3675690D1 (de) Prallkuehlung fuer einen turbineneinlasskanal.
FR2422036B1 (fr) Dispositif de refroidissement des elements mobiles d'un moteur a turbine a gaz
EP0266297A3 (en) Cooling air manifold for a gas turbine engine
IT8124388A0 (it) Struttura di carcassa per motore di turbina a gas.
IT7821869A0 (it) Paletta di rotore raffreddata per motore a turbina a gas.
IT1163366B (it) Prediffusore per motori a turbina a gas
IT8022967A0 (it) Stantuffo di compensazione e guarnizione di tenuta per motore a turbina a gas.

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970926