FR2194881A1 - - Google Patents
Info
- Publication number
- FR2194881A1 FR2194881A1 FR7327466A FR7327466A FR2194881A1 FR 2194881 A1 FR2194881 A1 FR 2194881A1 FR 7327466 A FR7327466 A FR 7327466A FR 7327466 A FR7327466 A FR 7327466A FR 2194881 A1 FR2194881 A1 FR 2194881A1
- Authority
- FR
- France
- 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.)
- Granted
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
- F23R3/002—Wall structures
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/20—Heat transfer, e.g. cooling
- F05B2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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)
- Spray-Type Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US27727372A | 1972-08-02 | 1972-08-02 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2194881A1 true FR2194881A1 (en) | 1974-03-01 |
FR2194881B1 FR2194881B1 (en) | 1977-05-13 |
Family
ID=23060145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7327466A Expired FR2194881B1 (en) | 1972-08-02 | 1973-07-26 |
Country Status (8)
Country | Link |
---|---|
JP (1) | JPS4980411A (en) |
BE (1) | BE801615A (en) |
CA (1) | CA994115A (en) |
DE (1) | DE2338210A1 (en) |
FR (1) | FR2194881B1 (en) |
IL (1) | IL42390A0 (en) |
IT (1) | IT992653B (en) |
NL (1) | NL7310008A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2653410A1 (en) * | 1975-11-29 | 1977-06-08 | Rolls Royce 1971 Ltd | COMBUSTION CHAMBER FOR A GAS TURBINE JET ENGINE |
FR2334824A1 (en) * | 1975-12-11 | 1977-07-08 | Gen Electric | PERFECTED COMBUSTION CHAMBER |
FR2531748A1 (en) * | 1982-08-16 | 1984-02-17 | Gen Electric | DOUBLE FUNCTION COOLING AIR COMBUSTION SHIRT |
FR2585770A1 (en) * | 1985-08-02 | 1987-02-06 | Snecma | EXPANDED BOWL INJECTION DEVICE FOR TURBOMACHINE COMBUSTION CHAMBER |
FR2610701A1 (en) * | 1987-02-06 | 1988-08-12 | Gen Electric | COOLING CHAMBER COOLING STRUCTURE FOR A TURBOJET ENGINE |
FR2614973A1 (en) * | 1987-05-06 | 1988-11-10 | Rolls Royce Plc | COMBUSTION CHAMBER |
FR2624954A1 (en) * | 1987-12-18 | 1989-06-23 | Rolls Royce Plc | COMBUSTION CHAMBER STRUCTURE FOR A GAS TURBINE ENGINE |
FR2673705A1 (en) * | 1991-03-06 | 1992-09-11 | Snecma | Combustion chamber of a turbine engine equipped with an anti-coking device for the bottom of said chamber |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2312654A1 (en) * | 1975-05-28 | 1976-12-24 | Snecma | COMBUSTION CHAMBERS IMPROVEMENTS FOR GAS TURBINE ENGINES |
JPS6115418Y2 (en) * | 1977-09-12 | 1986-05-13 | ||
JPS58175372U (en) * | 1982-05-17 | 1983-11-24 | 三菱重工業株式会社 | Impingement jet cooling surface |
US4584834A (en) * | 1982-07-06 | 1986-04-29 | General Electric Company | Gas turbine engine carburetor |
US4566280A (en) * | 1983-03-23 | 1986-01-28 | Burr Donald N | Gas turbine engine combustor splash ring construction |
JPH0660740B2 (en) * | 1985-04-05 | 1994-08-10 | 工業技術院長 | Gas turbine combustor |
JPS6281864U (en) * | 1985-11-07 | 1987-05-25 | ||
CA1306873C (en) * | 1987-04-27 | 1992-09-01 | Jack R. Taylor | Low coke fuel injector for a gas turbine engine |
US5012645A (en) * | 1987-08-03 | 1991-05-07 | United Technologies Corporation | Combustor liner construction for gas turbine engine |
US4843825A (en) * | 1988-05-16 | 1989-07-04 | United Technologies Corporation | Combustor dome heat shield |
GB2221979B (en) * | 1988-08-17 | 1992-03-25 | Rolls Royce Plc | A combustion chamber for a gas turbine engine |
US5307637A (en) * | 1992-07-09 | 1994-05-03 | General Electric Company | Angled multi-hole film cooled single wall combustor dome plate |
DE4444961A1 (en) * | 1994-12-16 | 1996-06-20 | Mtu Muenchen Gmbh | Device for cooling in particular the rear wall of the flame tube of a combustion chamber for gas turbine engines |
FR2733582B1 (en) * | 1995-04-26 | 1997-06-06 | Snecma | COMBUSTION CHAMBER COMPRISING VARIABLE AXIAL AND TANGENTIAL TILT MULTIPERFORATION |
DE19727407A1 (en) * | 1997-06-27 | 1999-01-07 | Siemens Ag | Gas-turbine combustion chamber heat shield with cooling arrangement |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1052060A (en) * | 1900-01-01 | |||
US2510645A (en) * | 1946-10-26 | 1950-06-06 | Gen Electric | Air nozzle and porting for combustion chamber liners |
GB932513A (en) * | 1961-01-11 | 1963-07-31 | Rolls Royce | Gas turbine engine combustion chamber |
FR1510755A (en) * | 1966-02-21 | 1968-01-19 | Bristol Siddeley Engines Ltd | Liquid fuel combustion chamber, for engines incorporating a gas turbine |
FR1532361A (en) * | 1967-04-25 | 1968-07-12 | Snecma | Vaporization and gyration combustion chamber |
FR2045362A5 (en) * | 1969-04-17 | 1971-02-26 | Gen Electric |
-
1973
- 1973-05-30 IL IL42390A patent/IL42390A0/en unknown
- 1973-06-28 BE BE132863A patent/BE801615A/en unknown
- 1973-07-03 CA CA175,419A patent/CA994115A/en not_active Expired
- 1973-07-18 NL NL7310008A patent/NL7310008A/xx unknown
- 1973-07-19 IT IT26767/73A patent/IT992653B/en active
- 1973-07-26 FR FR7327466A patent/FR2194881B1/fr not_active Expired
- 1973-07-27 DE DE19732338210 patent/DE2338210A1/en active Pending
- 1973-08-02 JP JP48086422A patent/JPS4980411A/ja active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1052060A (en) * | 1900-01-01 | |||
US2510645A (en) * | 1946-10-26 | 1950-06-06 | Gen Electric | Air nozzle and porting for combustion chamber liners |
GB932513A (en) * | 1961-01-11 | 1963-07-31 | Rolls Royce | Gas turbine engine combustion chamber |
FR1510755A (en) * | 1966-02-21 | 1968-01-19 | Bristol Siddeley Engines Ltd | Liquid fuel combustion chamber, for engines incorporating a gas turbine |
FR1532361A (en) * | 1967-04-25 | 1968-07-12 | Snecma | Vaporization and gyration combustion chamber |
FR2045362A5 (en) * | 1969-04-17 | 1971-02-26 | Gen Electric |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2653410A1 (en) * | 1975-11-29 | 1977-06-08 | Rolls Royce 1971 Ltd | COMBUSTION CHAMBER FOR A GAS TURBINE JET ENGINE |
FR2333126A1 (en) * | 1975-11-29 | 1977-06-24 | Rolls Royce | GAS TURBINE ENGINE COMBUSTION CHAMBER REFRIGERATION DEVICE |
FR2334824A1 (en) * | 1975-12-11 | 1977-07-08 | Gen Electric | PERFECTED COMBUSTION CHAMBER |
FR2531748A1 (en) * | 1982-08-16 | 1984-02-17 | Gen Electric | DOUBLE FUNCTION COOLING AIR COMBUSTION SHIRT |
FR2585770A1 (en) * | 1985-08-02 | 1987-02-06 | Snecma | EXPANDED BOWL INJECTION DEVICE FOR TURBOMACHINE COMBUSTION CHAMBER |
EP0214003A1 (en) * | 1985-08-02 | 1987-03-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Fuel injection nozzle with an enlarged screen for the combustion chamber of a gas turbine |
US4766722A (en) * | 1985-08-02 | 1988-08-30 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) | Enlarged bowl member for a turbojet engine combustion chamber |
FR2610701A1 (en) * | 1987-02-06 | 1988-08-12 | Gen Electric | COOLING CHAMBER COOLING STRUCTURE FOR A TURBOJET ENGINE |
FR2614973A1 (en) * | 1987-05-06 | 1988-11-10 | Rolls Royce Plc | COMBUSTION CHAMBER |
FR2624954A1 (en) * | 1987-12-18 | 1989-06-23 | Rolls Royce Plc | COMBUSTION CHAMBER STRUCTURE FOR A GAS TURBINE ENGINE |
FR2673705A1 (en) * | 1991-03-06 | 1992-09-11 | Snecma | Combustion chamber of a turbine engine equipped with an anti-coking device for the bottom of said chamber |
Also Published As
Publication number | Publication date |
---|---|
FR2194881B1 (en) | 1977-05-13 |
IL42390A0 (en) | 1973-07-30 |
CA994115A (en) | 1976-08-03 |
JPS4980411A (en) | 1974-08-02 |
DE2338210A1 (en) | 1974-02-14 |
BE801615A (en) | 1973-10-15 |
IT992653B (en) | 1975-09-30 |
NL7310008A (en) | 1974-02-05 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |