GB600228A - Improvements relating to gas turbine power plants - Google Patents
Improvements relating to gas turbine power plantsInfo
- Publication number
- GB600228A GB600228A GB2774845A GB2774845A GB600228A GB 600228 A GB600228 A GB 600228A GB 2774845 A GB2774845 A GB 2774845A GB 2774845 A GB2774845 A GB 2774845A GB 600228 A GB600228 A GB 600228A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- generator
- base
- main base
- pressure 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
- 239000007789 gas Substances 0.000 abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
600,228. Propelling ships. BRITISH THOMSON-HOUSTON CO., Ltd., and FORSLING, B. E. G. Oct. 22, 1945, No. 27748. [Class 114] [Also in Group XXVI] A gas turbine power plant for installation in a ship or other confined space comprises a low pressure turbine 3 driving a co-axial available power output device such as a generator 2 mounted on a main base 1 and a high pressure turbine 6 driving a co-axial working fluid compressor 7 mounted on a sub-base 5 which is mounted on and is removable from the main base 1. The air from the compressor 7 is heated in a heat exchanger 9 by the exhaust gases of the turbine 3 before passing to the combustion chambers 10. An exciter for the generator 2 driven by the turbine 6 may be mounted on the sub-base 5 and used for starting the plant and for supplying power to the auxiliary pumps which, with the fuel and oil tanks, may be mounted in the main base beneath the generator 2 and low pressure turbine 3. The air released from a pressure relief valve 13 passes through a pipe 14 to the exhaust 15. Specification 599,775, [Group) XXVI], is referred to.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB600228A true GB600228A (en) | 1948-04-02 |
Family
ID=1740742
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2774845A Expired GB600228A (en) | 1945-10-22 | Improvements relating to gas turbine power plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB600228A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2939282A (en) * | 1954-04-07 | 1960-06-07 | Studebaker Packard Corp | Intake and exhaust ducting for gas turbine engine |
-
1945
- 1945-10-22 GB GB2774845A patent/GB600228A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2939282A (en) * | 1954-04-07 | 1960-06-07 | Studebaker Packard Corp | Intake and exhaust ducting for gas turbine engine |
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