FR1095756A - Chambre de combustion de moteur - Google Patents
Chambre de combustion de moteurInfo
- Publication number
- FR1095756A FR1095756A FR1095756DA FR1095756A FR 1095756 A FR1095756 A FR 1095756A FR 1095756D A FR1095756D A FR 1095756DA FR 1095756 A FR1095756 A FR 1095756A
- Authority
- FR
- France
- Prior art keywords
- combustion chamber
- engine combustion
- engine
- chamber
- combustion
- 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
- F23R3/10—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
-
- 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
- F23R3/045—Air inlet arrangements using pipes
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1463/53A GB736823A (en) | 1953-01-19 | 1953-01-19 | Engine combustion chambers |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1095756A true FR1095756A (fr) | 1955-06-06 |
Family
ID=9722419
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1095756D Expired FR1095756A (fr) | 1953-01-19 | 1954-03-16 | Chambre de combustion de moteur |
Country Status (4)
Country | Link |
---|---|
US (1) | US2807139A (de) |
DE (1) | DE961672C (de) |
FR (1) | FR1095756A (de) |
GB (1) | GB736823A (de) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB980363A (en) * | 1961-12-04 | 1965-01-13 | Jan Jerie | Improvements in or relating to gas turbines |
US4301657A (en) * | 1978-05-04 | 1981-11-24 | Caterpillar Tractor Co. | Gas turbine combustion chamber |
DE4242650A1 (de) * | 1992-12-17 | 1994-06-23 | Asea Brown Boveri | Gasturbinenbrennkammer |
GB9407029D0 (en) * | 1994-04-08 | 1994-06-08 | Rolls Royce Plc | Gas turbine engine combustion apparatus |
FR2748088B1 (fr) * | 1996-04-24 | 1998-05-29 | Snecma | Optimisation du melange de gaz brules dans une chambre de combustion annulaire |
US20090090110A1 (en) * | 2007-10-04 | 2009-04-09 | Honeywell International, Inc. | Faceted dome assemblies for gas turbine engine combustors |
US8141365B2 (en) * | 2009-02-27 | 2012-03-27 | Honeywell International Inc. | Plunged hole arrangement for annular rich-quench-lean gas turbine combustors |
US8171740B2 (en) * | 2009-02-27 | 2012-05-08 | Honeywell International Inc. | Annular rich-quench-lean gas turbine combustors with plunged holes |
GB2589885A (en) * | 2019-12-11 | 2021-06-16 | Rolls Royce Plc | Combustor |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB583211A (en) * | 1940-01-24 | 1946-12-12 | Anglo Saxon Petroleum Co | Improved process and apparatus for the continuous generation of gases by reaction between air and liquid or pulverulent combustible material |
GB578764A (en) * | 1942-09-08 | 1946-07-11 | Rover Co Ltd | Improvements relating to combustion chambers for internal combustion turbines |
GB595831A (en) * | 1944-03-16 | 1947-12-18 | Power Jets Ltd | Improvements relating to combustion apparatus |
BE468999A (de) * | 1944-11-28 | |||
US2517015A (en) * | 1945-05-16 | 1950-08-01 | Bendix Aviat Corp | Combustion chamber with shielded fuel nozzle |
US2531810A (en) * | 1946-06-05 | 1950-11-28 | Kellogg M W Co | Air inlet arrangement for combustion chamber flame tubes |
US2488911A (en) * | 1946-11-09 | 1949-11-22 | Surface Combustion Corp | Combustion apparatus for use with turbines |
US2541171A (en) * | 1947-01-25 | 1951-02-13 | Kellogg M W Co | Air inlet structure for combustion chambers |
NL74196C (de) * | 1947-08-11 | |||
US2607193A (en) * | 1947-10-25 | 1952-08-19 | Curtiss Wright Corp | Annular combustion chamber with multiple notched fuel nozzles |
US2671314A (en) * | 1950-01-26 | 1954-03-09 | Socony Vacuum Oil Co Inc | Gas turbine and method of operation therefor |
FR1025198A (fr) * | 1950-09-27 | 1953-04-13 | Chambre à combustion continue et ondes explosives | |
GB715909A (en) * | 1952-02-01 | 1954-09-22 | Rolls Royce | Improvements in or relating to combustion equipment of gas-turbine engines |
FR1052475A (fr) * | 1952-03-15 | 1954-01-25 | Snecma | Chambres de combustion convenant en particulier aux turbines à gaz |
-
1953
- 1953-01-19 GB GB1463/53A patent/GB736823A/en not_active Expired
-
1954
- 1954-03-08 US US414741A patent/US2807139A/en not_active Expired - Lifetime
- 1954-03-11 DE DEL18237A patent/DE961672C/de not_active Expired
- 1954-03-16 FR FR1095756D patent/FR1095756A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE961672C (de) | 1957-04-11 |
GB736823A (en) | 1955-09-14 |
US2807139A (en) | 1957-09-24 |
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