GB617242A - Improvements in or relating to heat and power generating plant - Google Patents
Improvements in or relating to heat and power generating plantInfo
- Publication number
- GB617242A GB617242A GB19617/45A GB1961745A GB617242A GB 617242 A GB617242 A GB 617242A GB 19617/45 A GB19617/45 A GB 19617/45A GB 1961745 A GB1961745 A GB 1961745A GB 617242 A GB617242 A GB 617242A
- Authority
- GB
- United Kingdom
- Prior art keywords
- heater
- heat
- turbine
- air
- compressor
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/05—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
- F02C1/06—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy using reheated exhaust gas
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- High Energy & Nuclear Physics (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
617,242. Gas turbine plant. MASCHINENFABRIK OERLIKON. July 31, 1945, No. 19617. Convention date, Aug. 10, 1944. [Class 110 (iii)] The gases from a furnace first give up a portion of their heat to a liquid heater without generating a vapour and are then further cooled by utilizing them to transfer heat to a gas heater in which a gas compressed in a compressor is heated and then performs work in a gas turbine. The gases from the furnace 61 pass through a hot water heater 65 to two heaters L2 and L1 in which air from a compressor K is heated before passing to a turbine M which drives a generator N and the compressor K. The exhaust of the turbine is divided. Part passes to the furnace 61 as combustion air and the remainder passes through the heater L1 to pre-heat the air supplied by the compressor K. The air and combustion gas from the heater L1 together with the air supplied to the furnace as combustion air may be used to pre-heat the water before it passes to the heater 65 in heatexchangers B1, B2 and B3. The hot water from the heater 65 may be used in the heater H1 of the heat consumer H. The residual heat in the air leaving the heat-exchanger B1 may be utilized in the heater H3 of the consumer H. The heat obtained from cooling the compressor K and that obtained from a heat pump P, Q, R and S may be used in the heaters H2 and H4 of the heat consumer H. The temperature of the gases passing to the heater L2 may be controlled by passing some of the hot gases from the furnace through a passage 650 to a mixing chamber 80. Some of the gases passing through the heater L2 may be reheated by extracting them from the heater and mixing them with some of the hot gases taken from the passage 650 in a chamber 652. The turbine M may be controlled by byepassing a portion of the air in the air turbine circuit around some of the stages of the turbine; speed regulation of the compressor and of some of the turbine stages may also be provided. Specification 569,441 is referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH617242X | 1944-08-10 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB617242A true GB617242A (en) | 1949-02-03 |
Family
ID=4523844
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB19617/45A Expired GB617242A (en) | 1944-08-10 | 1945-07-31 | Improvements in or relating to heat and power generating plant |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB617242A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110906775A (en) * | 2019-10-30 | 2020-03-24 | 鞍钢股份有限公司 | Waste heat utilization system and method suitable for fluctuating thermal load |
-
1945
- 1945-07-31 GB GB19617/45A patent/GB617242A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110906775A (en) * | 2019-10-30 | 2020-03-24 | 鞍钢股份有限公司 | Waste heat utilization system and method suitable for fluctuating thermal load |
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