GB619232A - Improvements in or relating to gas turbine plants - Google Patents
Improvements in or relating to gas turbine plantsInfo
- Publication number
- GB619232A GB619232A GB1888946A GB1888946A GB619232A GB 619232 A GB619232 A GB 619232A GB 1888946 A GB1888946 A GB 1888946A GB 1888946 A GB1888946 A GB 1888946A GB 619232 A GB619232 A GB 619232A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- shaft
- air
- compressor
- combustion chambers
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
619,232. Gas turbines. LOMBARD, A. A. June 24, 1946, Nos. 18889 and 29570. [Class 110 (iii)] In a gas turbine plant of the type having an air compressor driven through a shaft by a gas turbine arranged coaxially with the shaft and compressor, and in which the combustion system comprises a number of flame tubes and at least one air casing, the combustion chambers or flame tubes are arranged with their axes skewed relative to the shaft axis so that they lie in a helical manner around the shaft. The said axes are preferably rectilinear, but may be of helical form. Air from a two-stage centrifugal compressor leaves a diffuser chamber 20 through stub pipes 26 in a substantially tangential direction and flows through helically disposed combustion chambers 21 to a gas turbine 14. Individual combustion chambers may be replaced by an annular air-casing housing helically disposed flame tubes, and the compressor may then be of the axial-flow type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1888946A GB619232A (en) | 1946-06-24 | 1946-06-24 | Improvements in or relating to gas turbine plants |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1888946A GB619232A (en) | 1946-06-24 | 1946-06-24 | Improvements in or relating to gas turbine plants |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB619232A true GB619232A (en) | 1949-03-07 |
Family
ID=10120161
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1888946A Expired GB619232A (en) | 1946-06-24 | 1946-06-24 | Improvements in or relating to gas turbine plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB619232A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2888803A (en) * | 1954-08-30 | 1959-06-02 | Pon Lemuel | Intermittent combustion turbine engine |
| US4081957A (en) * | 1976-05-03 | 1978-04-04 | United Technologies Corporation | Premixed combustor |
| CN105953266A (en) * | 2016-05-04 | 2016-09-21 | 中国科学院工程热物理研究所 | Oblique flow combustion chamber structure |
-
1946
- 1946-06-24 GB GB1888946A patent/GB619232A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2888803A (en) * | 1954-08-30 | 1959-06-02 | Pon Lemuel | Intermittent combustion turbine engine |
| US4081957A (en) * | 1976-05-03 | 1978-04-04 | United Technologies Corporation | Premixed combustor |
| CN105953266A (en) * | 2016-05-04 | 2016-09-21 | 中国科学院工程热物理研究所 | Oblique flow combustion chamber structure |
| CN105953266B (en) * | 2016-05-04 | 2018-08-10 | 中国科学院工程热物理研究所 | A kind of oblique flow chamber structure |
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