BE539609A - - Google Patents
Info
- Publication number
- BE539609A BE539609A BE539609DA BE539609A BE 539609 A BE539609 A BE 539609A BE 539609D A BE539609D A BE 539609DA BE 539609 A BE539609 A BE 539609A
- Authority
- BE
- Belgium
- Prior art keywords
- turbine
- compressor
- installation
- motor
- gas
- Prior art date
Links
- 238000009434 installation Methods 0.000 claims description 7
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 238000011084 recovery Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 description 15
- 238000001914 filtration Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000000746 purification Methods 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000003638 reducing agent Substances 0.000 description 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
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
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)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE539609A true BE539609A (de) |
Family
ID=169261
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE539609D BE539609A (de) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE539609A (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1141138B (de) * | 1960-03-26 | 1962-12-13 | Ludwig Huber Dr Ing | Brennkraft-Turbinenanlage, insbesondere Heizvorrichtung, mit einem Schwingrohrbrenner |
-
0
- BE BE539609D patent/BE539609A/fr unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1141138B (de) * | 1960-03-26 | 1962-12-13 | Ludwig Huber Dr Ing | Brennkraft-Turbinenanlage, insbesondere Heizvorrichtung, mit einem Schwingrohrbrenner |
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