GB1323007A - Walls of combustion chambers - Google Patents
Walls of combustion chambersInfo
- Publication number
- GB1323007A GB1323007A GB1723071A GB1723071A GB1323007A GB 1323007 A GB1323007 A GB 1323007A GB 1723071 A GB1723071 A GB 1723071A GB 1723071 A GB1723071 A GB 1723071A GB 1323007 A GB1323007 A GB 1323007A
- Authority
- GB
- United Kingdom
- Prior art keywords
- holes
- junction
- flame tube
- flanges
- gas turbine
- 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
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
- F23R3/06—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)
- Measuring Oxygen Concentration In Cells (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7020243A FR2093115A5 (pt) | 1970-06-02 | 1970-06-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1323007A true GB1323007A (en) | 1973-07-11 |
Family
ID=9056558
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1723071A Expired GB1323007A (en) | 1970-06-02 | 1971-05-26 | Walls of combustion chambers |
Country Status (4)
Country | Link |
---|---|
US (1) | US3735589A (pt) |
DE (1) | DE2126648C3 (pt) |
FR (1) | FR2093115A5 (pt) |
GB (1) | GB1323007A (pt) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2441342A (en) * | 2006-09-01 | 2008-03-05 | Rolls Royce Plc | Wall Elements for Gas Turbine Engine Components |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA980584A (en) * | 1972-11-10 | 1975-12-30 | Edward E. Ekstedt | Double walled impingement cooled combustor |
US3899881A (en) * | 1974-02-04 | 1975-08-19 | Gen Motors Corp | Combustion apparatus with secondary air to vaporization chamber and concurrent variance of secondary air and dilution air in a reverse sense |
FR2312654A1 (fr) * | 1975-05-28 | 1976-12-24 | Snecma | Perfectionnements aux chambres de combustion pour moteurs a turbine a gaz |
US4233123A (en) * | 1978-12-18 | 1980-11-11 | General Motors Corporation | Method for making an air cooled combustor |
FR2450349A1 (fr) * | 1979-03-01 | 1980-09-26 | Snecma | Perfectionnement au refroidissement des parois de chambres de combustion par pellicule d'air |
US5481867A (en) * | 1988-05-31 | 1996-01-09 | United Technologies Corporation | Combustor |
US6101814A (en) * | 1999-04-15 | 2000-08-15 | United Technologies Corporation | Low emissions can combustor with dilution hole arrangement for a turbine engine |
US6260359B1 (en) * | 1999-11-01 | 2001-07-17 | General Electric Company | Offset dilution combustor liner |
US6606861B2 (en) | 2001-02-26 | 2003-08-19 | United Technologies Corporation | Low emissions combustor for a gas turbine engine |
GB2460403B (en) * | 2008-05-28 | 2010-11-17 | Rolls Royce Plc | Combustor Wall with Improved Cooling |
US8171740B2 (en) * | 2009-02-27 | 2012-05-08 | Honeywell International Inc. | Annular rich-quench-lean gas turbine combustors with plunged holes |
US8141365B2 (en) * | 2009-02-27 | 2012-03-27 | Honeywell International Inc. | Plunged hole arrangement for annular rich-quench-lean gas turbine combustors |
US20170059159A1 (en) * | 2015-08-25 | 2017-03-02 | Rolls-Royce Corporation | Cmc combustor shell with integral chutes |
DE102016201452A1 (de) * | 2016-02-01 | 2017-08-03 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit Wandkonturierung |
WO2021118567A1 (en) * | 2019-12-12 | 2021-06-17 | Siemens Energy Global GmbH & Co. KG | Combustor liner in gas turbine engine |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447482A (en) * | 1945-04-25 | 1948-08-24 | Westinghouse Electric Corp | Turbine apparatus |
US2657531A (en) * | 1948-01-22 | 1953-11-03 | Gen Electric | Wall cooling arrangement for combustion devices |
GB700017A (en) * | 1951-03-05 | 1953-11-25 | Lucas Industries Ltd | Combustion chambers for prime movers |
BE535905A (pt) * | 1954-02-23 | |||
US3046742A (en) * | 1959-01-05 | 1962-07-31 | Gen Motors Corp | Combustion apparatus |
FR1520428A (fr) * | 1966-12-08 | 1968-04-12 | Snecma | Elément de paroi d'une chambre de combustion |
US3490230A (en) * | 1968-03-22 | 1970-01-20 | Us Navy | Combustion air control shutter |
-
1970
- 1970-06-02 FR FR7020243A patent/FR2093115A5/fr not_active Expired
-
1971
- 1971-05-26 GB GB1723071A patent/GB1323007A/en not_active Expired
- 1971-05-28 DE DE2126648A patent/DE2126648C3/de not_active Expired
- 1971-06-01 US US00148715A patent/US3735589A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2441342A (en) * | 2006-09-01 | 2008-03-05 | Rolls Royce Plc | Wall Elements for Gas Turbine Engine Components |
GB2441342B (en) * | 2006-09-01 | 2009-03-18 | Rolls Royce Plc | Wall elements with apertures for gas turbine engine components |
Also Published As
Publication number | Publication date |
---|---|
FR2093115A5 (pt) | 1972-01-28 |
DE2126648A1 (de) | 1971-12-09 |
DE2126648C3 (de) | 1978-12-21 |
US3735589A (en) | 1973-05-29 |
DE2126648B2 (de) | 1978-05-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |