GB367130A - Improvements in gas turbines - Google Patents
Improvements in gas turbinesInfo
- Publication number
- GB367130A GB367130A GB186331A GB186331A GB367130A GB 367130 A GB367130 A GB 367130A GB 186331 A GB186331 A GB 186331A GB 186331 A GB186331 A GB 186331A GB 367130 A GB367130 A GB 367130A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gases
- rotary engine
- turbine
- compressor
- take place
- 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 6
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 238000007906 compression Methods 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 2
- 230000006835 compression Effects 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
-
- 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
- F02C6/006—Open cycle gas-turbine in which the working fluid is expanded to a pressure below the atmospheric pressure and then compressed to atmospheric pressure
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
367,130. Motor power plant. WALTER, H., 7, Hohenzollerndamm, Berlin. Jan. 20, 1931, No. 1863. [Class 110 (iii).] In a gas turbine plant in which hot gases, are expanded adiabaticallyf, g<1> to below atmospheric pressure partly in a turbine and partly in a rotary engine, the gases are cooled in an intercooler and then re-compressed adiabatically or polytropically to atmospheric pressure. Air is compressed by a primary compressor A, which is driven by a rotary engine C, and after combustion in a chamber B the gases are led to a turbine T, which drives a dynamo or other machine, and then complete the adiabatic expansion in the rotary engine C. After being cooled in one or more stages either at constant volume g<111>, g<11> or at constant pressure g<1>, g<11> the gases are compressed in a secondary compressor C<1> and part returned to the combustion chamber B after further compression in an auxiliary compressor A<2>. A quantity of fresh air for combustion is provided by the compressor A. The intercooling may be secured by a jet condenser or a surface condenser. The rotary engine may receive the gases before the turbine or the flow to the two engines may take place in parallel. The re-compression line may be an adiabatic gll, h or a polytrope g<11>, h<1>, Fig. 6, and cooling to an isothermal d, e take place at constant pressure along the line z. Cooling may take place at constant volume.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB186331A GB367130A (en) | 1931-01-20 | 1931-01-20 | Improvements in gas turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB186331A GB367130A (en) | 1931-01-20 | 1931-01-20 | Improvements in gas turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB367130A true GB367130A (en) | 1932-02-18 |
Family
ID=9729329
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB186331A Expired GB367130A (en) | 1931-01-20 | 1931-01-20 | Improvements in gas turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB367130A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2428830A (en) * | 1942-04-18 | 1947-10-14 | Turbo Engineering Corp | Regulation of combustion gas turbines arranged in series |
| US2461186A (en) * | 1942-02-20 | 1949-02-08 | Bbc Brown Boveri & Cie | Gas turbine installation |
| US2554593A (en) * | 1941-08-08 | 1951-05-29 | Rateau Soc | Apparatus, including gas turbines for the direct driving of vehicles |
| GB2140873A (en) * | 1983-06-03 | 1984-12-05 | Gen Electric | Closed-cycle gas turbine chemical processor |
| WO2018195622A1 (en) * | 2017-04-25 | 2018-11-01 | Associação Paranaense De Cultura - Apc | Binary-cycle turbine engine comprising three isothermal processes and four adiabatic processes and a method for controlling the thermodynamic cycle of the turbine engine |
-
1931
- 1931-01-20 GB GB186331A patent/GB367130A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2554593A (en) * | 1941-08-08 | 1951-05-29 | Rateau Soc | Apparatus, including gas turbines for the direct driving of vehicles |
| US2461186A (en) * | 1942-02-20 | 1949-02-08 | Bbc Brown Boveri & Cie | Gas turbine installation |
| US2428830A (en) * | 1942-04-18 | 1947-10-14 | Turbo Engineering Corp | Regulation of combustion gas turbines arranged in series |
| GB2140873A (en) * | 1983-06-03 | 1984-12-05 | Gen Electric | Closed-cycle gas turbine chemical processor |
| DE3419216A1 (en) * | 1983-06-03 | 1984-12-06 | General Electric Co., Schenectady, N.Y. | CHEMICAL PROCESSOR WITH CLOSED CIRCUIT |
| FR2546976A1 (en) * | 1983-06-03 | 1984-12-07 | Gen Electric | GAS TURBINE CHEMICAL TREATMENT FACILITY OPERATING IN CLOSED CYCLE |
| WO2018195622A1 (en) * | 2017-04-25 | 2018-11-01 | Associação Paranaense De Cultura - Apc | Binary-cycle turbine engine comprising three isothermal processes and four adiabatic processes and a method for controlling the thermodynamic cycle of the turbine engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2646663A (en) | Semiopen circuit gas-turbine engine | |
| GB484289A (en) | Improvements in and relating to internal combustion turbine plants | |
| GB764951A (en) | Method and apparatus for liquefying natural gas for shipment and storage | |
| GB367130A (en) | Improvements in gas turbines | |
| GB529786A (en) | Improvements in or relating to gas turbine installations | |
| GB1212511A (en) | Improvements in power generating plant | |
| GB1521265A (en) | Exhaust gas power extractor for internal combustion engin | |
| GB387264A (en) | Improvements in and relating to the regulation of the performance of gas turbines | |
| GB504263A (en) | Improvements in and to gas turbines | |
| GB651166A (en) | Improvements in or relating to gas turbine plant with semi-open circuit | |
| GB368317A (en) | Improvements in or relating to turbines | |
| GB390448A (en) | Improvements in or relating to gas turbine plants particularly for propulsion of ships | |
| GB433630A (en) | Improvements in or relating to the cycles of the working fluid in internal combustion engines and turbines | |
| GB645588A (en) | Improvements in or relating to gas turbine power plants | |
| GB566531A (en) | Improvements in power plant including an internal-combustion-operated motive-gas generator of the free-piston type | |
| GB716145A (en) | Improvements in aircraft jet propulsion engines including a ducted fan | |
| GB620492A (en) | Improvements in or relating to gas-turbine power plants | |
| GB400914A (en) | Systems for the utilisation of exhaust gas | |
| GB596305A (en) | Improvements in or relating to plant for providing hot compressed air | |
| GB813990A (en) | Improvements in gas turbines utilising the waste heat of internal combustion engines | |
| GB411787A (en) | Improvements in gas turbine plant | |
| GB851441A (en) | Improvements in air conditioning and/or air pressurising apparatus for aircraft | |
| GB392733A (en) | Improvements in refrigerating systems for the liquifaction of gases | |
| GB447855A (en) | Improvements in or relating to internal combustion engine plants with an exhaust gas turbine and compressors driven thereby | |
| GB451930A (en) | Improvements relating to a process and apparatus for producing compressed air for internal combustion engines and applicable to other purposes |