CH500438A - Brennkammer, insbesondere für Gasturbinentriebwerke - Google Patents

Brennkammer, insbesondere für Gasturbinentriebwerke

Info

Publication number: CH500438A
Authority: CH; Switzerland
Prior art keywords: combustion chamber; gas turbine; turbine engines; engines; combustion
Prior art date: 1968-10-16

Application number

CH1530369A

Other languages

English (en)

Inventor

John Faitani Joseph

Waclaw Jr Mieczkowski William

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.)

1968-10-16

Filing date

1969-10-13

Publication date

1970-12-15

1969-10-13 Application filed by United Aircraft Corp filed Critical United Aircraft Corp

1970-12-15 Publication of CH500438A publication Critical patent/CH500438A/de

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
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
- 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)

CH1530369A 1968-10-16 1969-10-13 Brennkammer, insbesondere für Gasturbinentriebwerke CH500438A (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US76795368A	1968-10-16	1968-10-16

Publications (1)

Publication Number	Publication Date
CH500438A true CH500438A (de)	1970-12-15

Family

ID=25081076

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CH1530369A CH500438A (de)	1968-10-16	1969-10-13	Brennkammer, insbesondere für Gasturbinentriebwerke

Country Status (9)

Country	Link
US (1)	US3498055A (de)
BE (1)	BE740301A (de)
BR (1)	BR6913369D0 (de)
CH (1)	CH500438A (de)
DE (1)	DE1951198C3 (de)
FR (1)	FR2020807A1 (de)
GB (1)	GB1252194A (de)
IL (1)	IL33166A (de)
NL (1)	NL6915585A (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE1934700B2 (de) *	1969-07-09	1972-01-05	Mtu Muenchen Gmbh	Brennstoffduese fuer gasturbinentriebwerke
US3630024A (en) *	1970-02-02	1971-12-28	Gen Electric	Air swirler for gas turbine combustor
USRE30160E (en) *	1970-03-04	1979-11-27	United Technologies Corporation	Smoke reduction combustion chamber
US3643430A (en) *	1970-03-04	1972-02-22	United Aircraft Corp	Smoke reduction combustion chamber
US3656298A (en) *	1970-11-27	1972-04-18	Gen Motors Corp	Combustion apparatus
US3741483A (en) *	1971-12-10	1973-06-26	Mitsubishi Heavy Ind Ltd	Combustion air supply arrangement for gas turbines
US3916619A (en) *	1972-10-30	1975-11-04	Hitachi Ltd	Burning method for gas turbine combustor and a construction thereof
JPS5342897B2 (de) *	1972-11-09	1978-11-15
GB1429677A (en) *	1973-03-20	1976-03-24	Rolls Royce	Gas turbine engine combustion equipment
US3901446A (en) *	1974-05-09	1975-08-26	Us Air Force	Induced vortex swirler
US4155220A (en) *	1977-01-21	1979-05-22	Westinghouse Electric Corp.	Combustion apparatus for a gas turbine engine
US4151713A (en) *	1977-03-15	1979-05-01	United Technologies Corporation	Burner for gas turbine engine
FR2426157B1 (fr) *	1978-05-20	1985-07-26	Rolls Royce	Chambre de combustion de moteur a turbine a gaz a prise annulaire d'air refrigerant
GB2099978A (en) *	1981-05-11	1982-12-15	Rolls Royce	Gas turbine engine combustor
US5297385A (en) *	1988-05-31	1994-03-29	United Technologies Corporation	Combustor
FR2673705A1 (fr) *	1991-03-06	1992-09-11	Snecma	Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.
EP1263355B1 (de)	2000-02-14	2005-04-27	Potencia Medical AG	Hydraulisches gerät zur behandlung von harninkontinenz
DE102006041955A1 (de) *	2006-08-30	2008-03-20	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Verfahren zur Steuerung der Verbrennung in einer Brennkammer und Brennkammervorrichtung
US9181812B1 (en) *	2009-05-05	2015-11-10	Majed Toqan	Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines
US9027350B2 (en) *	2009-12-30	2015-05-12	Rolls-Royce Corporation	Gas turbine engine having dome panel assembly with bifurcated swirler flow
US9599343B2 (en) *	2012-11-28	2017-03-21	General Electric Company	Fuel nozzle for use in a turbine engine and method of assembly
US9228747B2 (en) *	2013-03-12	2016-01-05	Pratt & Whitney Canada Corp.	Combustor for gas turbine engine
USD911402S1 (en) *	2019-07-18	2021-02-23	Illinois Tool Works Inc.	Chamber
US11885497B2 (en) *	2019-07-19	2024-01-30	Pratt & Whitney Canada Corp.	Fuel nozzle with slot for cooling
US11933498B2 (en)	2020-10-13	2024-03-19	Venture Aerospace, Llc	Aerospace structure methods of manufacturing

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2560207A (en) *	1948-02-04	1951-07-10	Wright Aeronautical Corp	Annular combustion chamber with circumferentially spaced double air-swirl burners
US2700416A (en) *	1949-06-30	1955-01-25	Rolls Royce	Fuel injection means for gas-turbine engines and combustion equipment used therewith
US2982099A (en) *	1956-10-09	1961-05-02	Rolls Royce	Fuel injection arrangement in combustion equipment for gas turbine engines
US3134229A (en) *	1961-10-02	1964-05-26	Gen Electric	Combustion chamber

1968
- 1968-10-16 US US767953A patent/US3498055A/en not_active Expired - Lifetime
1969
- 1969-10-08 GB GB1252194D patent/GB1252194A/en not_active Expired
- 1969-10-10 DE DE1951198A patent/DE1951198C3/de not_active Expired
- 1969-10-12 IL IL33166A patent/IL33166A/xx unknown
- 1969-10-13 CH CH1530369A patent/CH500438A/de not_active IP Right Cessation
- 1969-10-13 FR FR6935057A patent/FR2020807A1/fr not_active Withdrawn
- 1969-10-15 NL NL6915585A patent/NL6915585A/xx unknown
- 1969-10-15 BE BE740301D patent/BE740301A/xx unknown
- 1969-10-16 BR BR213369/69A patent/BR6913369D0/pt unknown

Also Published As

Publication number	Publication date
FR2020807A1 (de)	1970-07-17
BE740301A (de)	1970-03-16
DE1951198C3 (de)	1973-12-06
US3498055A (en)	1970-03-03
BR6913369D0 (pt)	1973-06-26
DE1951198B2 (de)	1973-05-17
GB1252194A (de)	1971-11-03
NL6915585A (de)	1970-04-20
DE1951198A1 (de)	1970-05-14
IL33166A (en)	1973-08-29
IL33166A0 (en)	1970-03-22

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Legal Events

Date	Code	Title	Description
1974-05-15	PL	Patent ceased