GB1089467A - Improvements in or relating to gas turbines - Google Patents
Improvements in or relating to gas turbinesInfo
- Publication number
- GB1089467A GB1089467A GB2094865A GB2094865A GB1089467A GB 1089467 A GB1089467 A GB 1089467A GB 2094865 A GB2094865 A GB 2094865A GB 2094865 A GB2094865 A GB 2094865A GB 1089467 A GB1089467 A GB 1089467A
- Authority
- GB
- United Kingdom
- Prior art keywords
- segments
- suspended
- gas turbine
- flame tube
- axial
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
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
- 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
- F05B2260/202—Heat transfer, e.g. cooling by film cooling
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)
Abstract
1,089,467. Gas turbine combustion chambers. PRVNI BRNENSKA STROJIRNA, ZAVODY KLEMENTA GOTTWALDA, NARODNI PODNIK. May 18, 1965 [May 21, 1964], No. 20948/65. Heading F1L. A gas turbine combustion chamber comprises an intermediate casing 2 suspended by supports 3 from an outer casing 1 and a flame tube formed by segments 5 suspended from the intermediate casing and overlapping both axially and circumferentially in spaced relationship so that cooling air enters the flame tube through the axial and tangential passages so formed. Ribs (10, 11), Fig. 4 (not shown), space the segments 5 apart at the circumferential and axial overlaps.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CS291664 | 1964-05-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1089467A true GB1089467A (en) | 1967-11-01 |
Family
ID=5367680
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2094865A Expired GB1089467A (en) | 1964-05-21 | 1965-05-18 | Improvements in or relating to gas turbines |
Country Status (5)
| Country | Link |
|---|---|
| AT (1) | AT257279B (en) |
| CH (1) | CH428324A (en) |
| DE (1) | DE1291554B (en) |
| FR (1) | FR1435410A (en) |
| GB (1) | GB1089467A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2418867A1 (en) * | 1978-03-01 | 1979-09-28 | Gen Electric | LOW CALORIFIC GAS COMBUSTION CHAMBER |
| FR2479900A1 (en) * | 1980-04-02 | 1981-10-09 | United Technologies Corp | INTERIOR TRIM OF COMBUSTION CHAMBER |
| GB2160964A (en) * | 1984-06-25 | 1986-01-02 | Gen Electric | Combustion chamber construction |
| US5259182A (en) * | 1989-12-22 | 1993-11-09 | Hitachi, Ltd. | Combustion apparatus and combustion method therein |
| US9335048B2 (en) | 2014-03-11 | 2016-05-10 | Rolls-Royce Deutschland Ltd & Co Kg | Combustion chamber of a gas turbine |
| US9506653B2 (en) | 2014-03-11 | 2016-11-29 | Rolls-Royce Deutschland Ltd & Co Kg | Combustion chamber of a gas turbine |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2087065B (en) * | 1980-11-08 | 1984-11-07 | Rolls Royce | Wall structure for a combustion chamber |
| US4628694A (en) * | 1983-12-19 | 1986-12-16 | General Electric Company | Fabricated liner article and method |
| FR2567250A1 (en) * | 1984-07-06 | 1986-01-10 | Gen Electric | Combustion chamber for a gas turbine engine |
| DE3535442A1 (en) * | 1985-10-04 | 1987-04-09 | Mtu Muenchen Gmbh | RING COMBUSTION CHAMBER FOR GAS TURBINE ENGINES |
| US4928479A (en) * | 1987-12-28 | 1990-05-29 | Sundstrand Corporation | Annular combustor with tangential cooling air injection |
| US4920742A (en) * | 1988-05-31 | 1990-05-01 | General Electric Company | Heat shield for gas turbine engine frame |
| FR2646880A1 (en) * | 1989-05-11 | 1990-11-16 | Snecma | THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR |
| DE10233805B4 (en) * | 2002-07-25 | 2013-08-22 | Alstom Technology Ltd. | Annular combustion chamber for a gas turbine |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH255541A (en) * | 1947-05-12 | 1948-06-30 | Bbc Brown Boveri & Cie | Cooled metal combustion chamber for generating heating and propellant gases. |
| BE490776A (en) * | 1948-10-26 | |||
| GB700004A (en) * | 1949-12-12 | 1953-11-25 | Babcock & Wilcox Ltd | Improvements in or relating to combustion apparatus |
-
1965
- 1965-05-14 CH CH676965A patent/CH428324A/en unknown
- 1965-05-17 DE DE1965P0036817 patent/DE1291554B/en active Pending
- 1965-05-18 GB GB2094865A patent/GB1089467A/en not_active Expired
- 1965-05-20 AT AT459965A patent/AT257279B/en active
- 1965-05-21 FR FR17972A patent/FR1435410A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2418867A1 (en) * | 1978-03-01 | 1979-09-28 | Gen Electric | LOW CALORIFIC GAS COMBUSTION CHAMBER |
| FR2479900A1 (en) * | 1980-04-02 | 1981-10-09 | United Technologies Corp | INTERIOR TRIM OF COMBUSTION CHAMBER |
| US4414816A (en) * | 1980-04-02 | 1983-11-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Combustor liner construction |
| GB2160964A (en) * | 1984-06-25 | 1986-01-02 | Gen Electric | Combustion chamber construction |
| US5259182A (en) * | 1989-12-22 | 1993-11-09 | Hitachi, Ltd. | Combustion apparatus and combustion method therein |
| US9335048B2 (en) | 2014-03-11 | 2016-05-10 | Rolls-Royce Deutschland Ltd & Co Kg | Combustion chamber of a gas turbine |
| US9506653B2 (en) | 2014-03-11 | 2016-11-29 | Rolls-Royce Deutschland Ltd & Co Kg | Combustion chamber of a gas turbine |
Also Published As
| Publication number | Publication date |
|---|---|
| FR1435410A (en) | 1966-04-15 |
| CH428324A (en) | 1967-01-15 |
| AT257279B (en) | 1967-09-25 |
| DE1291554B (en) | 1969-03-27 |
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