IT1018959B - Perfezionamento nelle disposizioni di raffreddamento delle camere di combustione di motori a turbina a gas - Google Patents

Perfezionamento nelle disposizioni di raffreddamento delle camere di combustione di motori a turbina a gas

Info

Publication number
IT1018959B
IT1018959B IT52592/74A IT5259274A IT1018959B IT 1018959 B IT1018959 B IT 1018959B IT 52592/74 A IT52592/74 A IT 52592/74A IT 5259274 A IT5259274 A IT 5259274A IT 1018959 B IT1018959 B IT 1018959B
Authority
IT
Italy
Prior art keywords
improvement
gas turbine
combustion chambers
turbine engines
cooling arrangements
Prior art date
Application number
IT52592/74A
Other languages
English (en)
Italian (it)
Original Assignee
Rolls Royce 1971 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 Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT1018959B publication Critical patent/IT1018959B/it

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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • 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
    • F23R3/002—Wall structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
IT52592/74A 1973-08-16 1974-08-13 Perfezionamento nelle disposizioni di raffreddamento delle camere di combustione di motori a turbina a gas IT1018959B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3881273A GB1438379A (en) 1973-08-16 1973-08-16 Cooling arrangement for duct walls

Publications (1)

Publication Number Publication Date
IT1018959B true IT1018959B (it) 1977-10-20

Family

ID=10405835

Family Applications (1)

Application Number Title Priority Date Filing Date
IT52592/74A IT1018959B (it) 1973-08-16 1974-08-13 Perfezionamento nelle disposizioni di raffreddamento delle camere di combustione di motori a turbina a gas

Country Status (6)

Country Link
US (1) US3898797A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS5088417A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2438845C3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2241055A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1438379A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT1018959B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
US4200149A (en) * 1976-12-06 1980-04-29 Murray Pechner Heat exchanger with fluid turbulator
DE2839627C2 (de) * 1977-09-13 1983-11-03 Hitachi, Ltd., Tokyo Gasbrenner
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
JPH0660740B2 (ja) * 1985-04-05 1994-08-10 工業技術院長 ガスタービンの燃焼器
US5329772A (en) * 1992-12-09 1994-07-19 General Electric Company Cast slot-cooled single nozzle combustion liner cap
US6018950A (en) * 1997-06-13 2000-02-01 Siemens Westinghouse Power Corporation Combustion turbine modular cooling panel
US6155056A (en) * 1998-06-04 2000-12-05 Pratt & Whitney Canada Corp. Cooling louver for annular gas turbine engine combustion chamber
US6408629B1 (en) * 2000-10-03 2002-06-25 General Electric Company Combustor liner having preferentially angled cooling holes
US6672067B2 (en) * 2002-02-27 2004-01-06 General Electric Company Corrugated cowl for combustor of a gas turbine engine and method for configuring same
US6711900B1 (en) * 2003-02-04 2004-03-30 Pratt & Whitney Canada Corp. Combustor liner V-band design
CN100419214C (zh) * 2006-12-29 2008-09-17 清华大学深圳研究生院 单活塞式单组元液压自由活塞发动机
US7942006B2 (en) * 2007-03-26 2011-05-17 Honeywell International Inc. Combustors and combustion systems for gas turbine engines
FR2944584B1 (fr) * 2009-04-17 2014-08-22 Turbomeca Chambre de combustion avec deflecteur de refroidissement de fond de chambre brase.
FR2947035B1 (fr) * 2009-06-17 2011-07-15 Turbomeca Refroidissement de paroi de chambre de combustion de moteur a turbine a gaz
WO2015077755A1 (en) * 2013-11-25 2015-05-28 United Technologies Corporation Film cooled multi-walled structure with one or more indentations
US11608783B2 (en) 2020-11-04 2023-03-21 Delavan, Inc. Surface igniter cooling system
US11473505B2 (en) 2020-11-04 2022-10-18 Delavan Inc. Torch igniter cooling system
US11692488B2 (en) 2020-11-04 2023-07-04 Delavan Inc. Torch igniter cooling system
US11635027B2 (en) 2020-11-18 2023-04-25 Collins Engine Nozzles, Inc. Fuel systems for torch ignition devices
US11421602B2 (en) 2020-12-16 2022-08-23 Delavan Inc. Continuous ignition device exhaust manifold
US11635210B2 (en) 2020-12-17 2023-04-25 Collins Engine Nozzles, Inc. Conformal and flexible woven heat shields for gas turbine engine components
US11754289B2 (en) 2020-12-17 2023-09-12 Delavan, Inc. Axially oriented internally mounted continuous ignition device: removable nozzle
US11486309B2 (en) 2020-12-17 2022-11-01 Delavan Inc. Axially oriented internally mounted continuous ignition device: removable hot surface igniter
US20220195933A1 (en) * 2020-12-17 2022-06-23 Delavan Inc. Radially oriented internally mounted continuous ignition device
US12092333B2 (en) * 2020-12-17 2024-09-17 Collins Engine Nozzles, Inc. Radially oriented internally mounted continuous ignition device
US11209164B1 (en) 2020-12-18 2021-12-28 Delavan Inc. Fuel injector systems for torch igniters
US11680528B2 (en) 2020-12-18 2023-06-20 Delavan Inc. Internally-mounted torch igniters with removable igniter heads

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
GB1136543A (en) * 1966-02-21 1968-12-11 Rolls Royce Liquid fuel combustion apparatus for gas turbine engines
US3671171A (en) * 1970-11-27 1972-06-20 Avco Corp Annular combustors
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly

Also Published As

Publication number Publication date
US3898797A (en) 1975-08-12
DE2438845A1 (de) 1975-03-06
FR2241055A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1975-03-14
DE2438845C3 (de) 1981-01-29
JPS5088417A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1975-07-16
GB1438379A (en) 1976-06-03
DE2438845B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1980-05-14

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