BE748070A - Structure de parois et trous de combustion pour une turbine a gaz - Google Patents

Structure de parois et trous de combustion pour une turbine a gaz

Info

Publication number: BE748070A
Authority: BE; Belgium
Prior art keywords: gas turbine; wall structure; combustion holes; combustion; holes
Prior art date: 1969-04-02

Application number

Other languages

English (en)

French (fr)

Inventor

R W Batt

A Kurti

P Goldberg

I Segalman

Original Assignee

United Aircraft 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.)

1969-04-02

Filing date

1970-03-27

Publication date

1970-08-31

1970-03-27 Application filed by United Aircraft Corp filed Critical United Aircraft Corp

1970-08-31 Publication of BE748070A publication Critical patent/BE748070A/xx

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
- F23R3/06—Arrangement of apertures along the flame tube
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
- 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
- F23R3/06—Arrangement of apertures along the flame tube
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)

BE748070D 1969-04-02 1970-03-27 Structure de parois et trous de combustion pour une turbine a gaz BE748070A (fr)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US81274869A	1969-04-02	1969-04-02

Publications (1)

Publication Number	Publication Date
BE748070A true BE748070A (fr)	1970-08-31

Family

ID=25210507

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BE748070D BE748070A (fr)	1969-04-02	1970-03-27	Structure de parois et trous de combustion pour une turbine a gaz

Country Status (9)

Country	Link
US (1)	US3545202A (xx)
BE (1)	BE748070A (xx)
CH (1)	CH514069A (xx)
DE (1)	DE2012949B2 (xx)
FR (1)	FR2042279A5 (xx)
GB (1)	GB1247144A (xx)
IL (1)	IL33996A (xx)
NL (1)	NL7004574A (xx)
SE (1)	SE355635B (xx)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB1271084A (en) *	1968-05-13	1972-04-19	T C Borrie Ltd	Improvements in or relating to cartridge-operated hand tools
US3706203A (en) *	1970-10-30	1972-12-19	United Aircraft Corp	Wall structure for a gas turbine engine
US3702058A (en) *	1971-01-13	1972-11-07	Westinghouse Electric Corp	Double wall combustion chamber
US3844116A (en) *	1972-09-06	1974-10-29	Avco Corp	Duct wall and reverse flow combustor incorporating same
US3934408A (en) *	1974-04-01	1976-01-27	General Motors Corporation	Ceramic combustion liner
US3981142A (en) *	1974-04-01	1976-09-21	General Motors Corporation	Ceramic combustion liner
FR2340453A1 (fr) *	1976-02-06	1977-09-02	Snecma	Corps de chambre de combustion, notamment pour turboreacteurs
US4073137A (en) *	1976-06-02	1978-02-14	United Technologies Corporation	Convectively cooled flameholder for premixed burner
US4132066A (en) *	1977-09-23	1979-01-02	United Technologies Corporation	Combustor liner for gas turbine engine
CH633347A5 (de) *	1978-08-03	1982-11-30	Bbc Brown Boveri & Cie	Gasturbine.
US4333216A (en) *	1981-03-23	1982-06-08	United Technologies Corporation	Method for manufacturing a sandwich panel structure
US4488869A (en) *	1982-07-06	1984-12-18	Coen Company, Inc.	High efficiency, low NOX emitting, staged combustion burner
US4619604A (en) *	1983-06-30	1986-10-28	Carrier Corporation	Flame radiator structure
GB8424525D0 (en) *	1984-09-28	1984-11-07	Leyland Vehicles	Variable transmission
DE3535443C1 (de) *	1985-10-04	1986-11-20	MTU Motoren- und Turbinen-Union München GmbH, 8000 München	Brennkammer fuer ein Gasturbinentriebwerk,insbesondere Ringbrennkammer,mit mindestes einer Luftzufuhrbuchse
FR2599821B1 (fr) *	1986-06-04	1988-09-02	Snecma	Chambre de combustion pour turbomachines a orifices de melange assurant le positionnement de la paroi chaude sur la paroi froide
US20090235668A1 (en) *	2008-03-18	2009-09-24	General Electric Company	Insulator bushing for combustion liner
US8387397B2 (en) *	2009-01-27	2013-03-05	General Electric Company	Flow conditioner for use in gas turbine component in which combustion occurs
US9062884B2 (en) *	2011-05-26	2015-06-23	Honeywell International Inc.	Combustors with quench inserts
US9360215B2 (en)	2012-04-02	2016-06-07	United Technologies Corporation	Combustor having a beveled grommet
DE102012022259A1 (de) *	2012-11-13	2014-05-28	Rolls-Royce Deutschland Ltd & Co Kg	Brennkammerschindel einer Gasturbine sowie Verfahren zu deren Herstellung
US9328663B2 (en)	2013-05-30	2016-05-03	General Electric Company	Gas turbine engine and method of operating thereof
US9366184B2 (en)	2013-06-18	2016-06-14	General Electric Company	Gas turbine engine and method of operating thereof
WO2015030927A1 (en) *	2013-08-30	2015-03-05	United Technologies Corporation	Contoured dilution passages for a gas turbine engine combustor
US9810430B2 (en)	2013-12-23	2017-11-07	United Technologies Corporation	Conjoined grommet assembly for a combustor
US10386070B2 (en)	2013-12-23	2019-08-20	United Technologies Corporation	Multi-streamed dilution hole configuration for a gas turbine engine
EP2927595B1 (en) *	2014-04-02	2019-11-13	United Technologies Corporation	Grommet assembly and method of design
FR3022613B1 (fr) *	2014-06-24	2019-04-19	Safran Helicopter Engines	Bossage pour chambre de combustion.
US9851105B2 (en) *	2014-07-03	2017-12-26	United Technologies Corporation	Self-cooled orifice structure
CN105318356A (zh) *	2014-07-21	2016-02-10	北京航天动力研究所	一种大深宽比变截面换热通道
DE102015225107A1 (de) *	2015-12-14	2017-06-14	Rolls-Royce Deutschland Ltd & Co Kg	Gasturbinenbrennkammer mit Schindelbefestigung mittels Rastelementen
US20180283695A1 (en) *	2017-04-03	2018-10-04	United Technologies Corporation	Combustion panel grommet
US10495001B2 (en)	2017-06-15	2019-12-03	General Electric Company	Combustion section heat transfer system for a propulsion system
US11022308B2 (en) *	2018-05-31	2021-06-01	Honeywell International Inc.	Double wall combustors with strain isolated inserts
US10808930B2 (en) *	2018-06-28	2020-10-20	Raytheon Technologies Corporation	Combustor shell attachment
US11371701B1 (en)	2021-02-03	2022-06-28	General Electric Company	Combustor for a gas turbine engine
US11560837B2 (en) *	2021-04-19	2023-01-24	General Electric Company	Combustor dilution hole
US11774098B2 (en)	2021-06-07	2023-10-03	General Electric Company	Combustor for a gas turbine engine
US12146660B2 (en)	2021-06-07	2024-11-19	General Electric Company	Combustor for a gas turbine engine
US11885495B2 (en)	2021-06-07	2024-01-30	General Electric Company	Combustor for a gas turbine engine including a liner having a looped feature
US11959643B2 (en)	2021-06-07	2024-04-16	General Electric Company	Combustor for a gas turbine engine
US12152777B2 (en)	2021-06-07	2024-11-26	General Electric Company	Combustor for a gas turbine engine
US12085283B2 (en)	2021-06-07	2024-09-10	General Electric Company	Combustor for a gas turbine engine
US12060995B1 (en) *	2023-03-22	2024-08-13	General Electric Company	Turbine engine combustor with a dilution passage

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CH255541A (de) *	1947-05-12	1948-06-30	Bbc Brown Boveri & Cie	Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen.
US2672728A (en) *	1951-05-23	1954-03-23	Westinghouse Electric Corp	Reinforced combustion chamber construction
BE535497A (xx) *	1954-02-26
US3038309A (en) *	1959-07-21	1962-06-12	Gen Electric	Cooling liner for jet engine afterburner
US3407596A (en) *	1967-03-15	1968-10-29	Navy Usa	Prevaporizing burner can

1969
- 1969-04-02 US US812748A patent/US3545202A/en not_active Expired - Lifetime
1970
- 1970-03-03 IL IL33996A patent/IL33996A/xx unknown
- 1970-03-05 GB GB00595/70A patent/GB1247144A/en not_active Expired
- 1970-03-18 DE DE19702012949 patent/DE2012949B2/de not_active Withdrawn
- 1970-03-18 CH CH412870A patent/CH514069A/de not_active IP Right Cessation
- 1970-03-25 SE SE04102/70A patent/SE355635B/xx unknown
- 1970-03-26 FR FR7011545A patent/FR2042279A5/fr not_active Expired
- 1970-03-27 BE BE748070D patent/BE748070A/xx unknown
- 1970-04-01 NL NL7004574A patent/NL7004574A/xx unknown

Also Published As

Publication number	Publication date
GB1247144A (en)	1971-09-22
US3545202A (en)	1970-12-08
DE2012949A1 (de)	1970-10-08
CH514069A (de)	1971-10-15
DE2012949B2 (de)	1971-09-09
IL33996A (en)	1972-12-29
IL33996A0 (en)	1971-06-23
NL7004574A (xx)	1970-10-06
FR2042279A5 (xx)	1971-02-05
SE355635B (xx)	1973-04-30

Publication	Publication Date	Title
BE748070A (fr)	1970-08-31	Structure de parois et trous de combustion pour une turbine a gaz
CH541066A (fr)	1973-08-31	Turbine à gaz
BE746282A (fr)	1970-07-31	Moteurs a turbine a gaz perfectionnes
BE744919A (fr)	1970-07-01	Moteurs a turbine a gaz perfectionnes
CH502517A (fr)	1971-01-31	Installation motrice à turbine à gaz
CH437385A (fr)	1967-06-15	Paroi thermo-isolante
CH496166A (it)	1970-09-15	Turbina a gas
CH520267A (fr)	1972-03-15	Turbine à gaz
AT307821B (de)	1973-06-12	Gasturbine
CH525384A (fr)	1972-07-15	Turbine à gaz
BE750574A (fr)	1970-11-19	Bruleur pour combustibles gazeux
CH534300A (fr)	1973-02-28	Turbine à gaz
BE748072A (fr)	1970-08-31	Structure de parois pour une turbine a gaz
FR1530850A (fr)	1968-06-28	Installation de turbine à gaz ouverte
CH512670A (de)	1971-09-15	Heissgasmotor
AT295719B (de)	1972-01-10	Gasbrenner
FR1498522A (fr)	1967-10-20	Installation de filtrage de gaz
BE763641A (fr)	1971-08-02	Bruleur pour combustibles gazeux
BE762822A (fr)	1971-08-11	Grilloir a gaz
FR1524810A (fr)	1968-05-10	Turbine à gaz
BE772436A (fr)	1972-03-10	Eclateur declenche dans un gaz
FR1484643A (fr)	1967-09-20	Turbine à gaz
FR1537390A (fr)	1968-08-23	Dispositif de démarrage à turbine à vapeur dans une installation de turbine à gaz
CH498380A (de)	1970-10-31	Gasströmungsmesser
FR1484133A (fr)	1967-06-09	Installation à turbine à gaz