GB730126A - Improvements in or relating to gas turbine installations - Google Patents
Improvements in or relating to gas turbine installationsInfo
- Publication number
- GB730126A GB730126A GB15275/53A GB1527553A GB730126A GB 730126 A GB730126 A GB 730126A GB 15275/53 A GB15275/53 A GB 15275/53A GB 1527553 A GB1527553 A GB 1527553A GB 730126 A GB730126 A GB 730126A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- turbine
- air
- valve
- separate
- 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
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
Abstract
730,126. Gas turbine plant. MASCHINENFABRIK AUGSBURG-NURNBERG AKT.- GES. June 1, 1953 [June 3, 1952], No. 15275/53. Class 110(3). In a gas turbinecompressor installation adapted to supply compressed air to a consumer network operating at a higher pressure than the turbine, the final compression of the air for the network is effected in a separate compressor the delivery pressure of which is independent of the speed of the apparatus. The turbine 4 drives a compressor 1 which supplies air to the combustion chamber 3 through a heat exchanger 2 and feeds a separate compressor 6, driven through gearing 5 via an intercooler 7. The compressor 6 delivers air to the network 9 through a non- return valve 8, and is fitted with a by pass connection 11 provided with a valve which can be opened for no-load operation. A temperature-sensitive device 12 gradually opens the valve 10 and limits the fuel supply in the event of a prolonged excessive temperature. A turbine driving a generator may be arranged in parallel with the turbine 4. A modification employs a series arrangement of two turbines driving two compressors, the separate compressor being driven directly by the second turbine which also drives a generator. The separate compressor is fed from the first compressor or from a tapping on the second compressor.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE730126X | 1952-06-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB730126A true GB730126A (en) | 1955-05-18 |
Family
ID=6636230
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB15275/53A Expired GB730126A (en) | 1952-06-03 | 1953-06-01 | Improvements in or relating to gas turbine installations |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB730126A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5586429A (en) * | 1994-12-19 | 1996-12-24 | Northern Research & Engineering Corporation | Brayton cycle industrial air compressor |
-
1953
- 1953-06-01 GB GB15275/53A patent/GB730126A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5586429A (en) * | 1994-12-19 | 1996-12-24 | Northern Research & Engineering Corporation | Brayton cycle industrial air compressor |
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