GB631547A - Improvements relating to plants in which solid material is subjected to heating and cooling - Google Patents
Improvements relating to plants in which solid material is subjected to heating and coolingInfo
- Publication number
- GB631547A GB631547A GB26676/47A GB2667647A GB631547A GB 631547 A GB631547 A GB 631547A GB 26676/47 A GB26676/47 A GB 26676/47A GB 2667647 A GB2667647 A GB 2667647A GB 631547 A GB631547 A GB 631547A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- exchanger
- atmosphere
- compressor
- combustion
- 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
- 238000001816 cooling Methods 0.000 title abstract 3
- 238000010438 heat treatment Methods 0.000 title abstract 2
- 239000011343 solid material Substances 0.000 title abstract 2
- 239000007789 gas Substances 0.000 abstract 5
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 239000000567 combustion gas Substances 0.000 abstract 2
- 239000000463 material Substances 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 239000002826 coolant Substances 0.000 abstract 1
- 239000000112 cooling gas Substances 0.000 abstract 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10B—DESTRUCTIVE DISTILLATION OF CARBONACEOUS MATERIALS FOR PRODUCTION OF GAS, COKE, TAR, OR SIMILAR MATERIALS
- C10B39/00—Cooling or quenching coke
- C10B39/02—Dry cooling outside the oven
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Materials Engineering (AREA)
- High Energy & Nuclear Physics (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
631,547. Cooling material discharged from furnaces. SULZER FRERES SOC. ANON. Oct. 3, 1947, No. 26676. Convention date, Oct. 4, 1946. [Class 51 (ii)] [Also in Group XXVI] A plant in which a heated solid material is cooled by causing a gaseous cooling medium to pass through the material subsequently giving up at least a part of the heat so acquired to drive a gas turbine comprises in the form shown in Fig. 1 a chamber 1 into which cold air is injected through a pipe 6 and becoming heated enters a gas turbine 10, connected to the shaft of which is a compressor 18 and electric generator 21, the residue of heat being extracted in a steam boiler 12 and a cooler 14 the cooled gas finally entering a compressor 18 which recirculates it through the pipe 6 into the cooling chamber 1. Fig. 2 shows a modification in which the cooling gas gives up its heat in an exchanger 22 and boiler 24 before returning to the chamber the air for the turbine being taken from the atmosphere by compressor 28, preheated in exchanger 29 and then passing in succession through the exchanger 22, turbine 30, preheater 29, and steam boiler 24 then being either discharged to the atmosphere through pipe 31 or returned to the compressor via a cooler. In another arrangement the working medium of the turbine does not enter a preheater but after passing through exchanger 22 enters a combustion chamber where it is burnt with a combustion gas introduced by means of a compressor driven by the gas turbine, the combustion-products after passage through the turbine being discharged into the atmosphere through boiler 24 and pipe 31. In a further example the combustion gas is not mixed with the working medium but heats it by heat exchange the combustion-products being discharged into the atmosphere through a steam superheater, the boiler 24 and pipe 31. In another modification the working medium after leaving exchanger 22 is burnt in a combustion chamber before entering in succession a high pressure and a low pressure turbine the medium then passing to the atmosphere through a recuperator. Air is drawn from the atmosphere by means of a compressor driven by the low pressure turbine, is cooled, then passes into another compressor driven by the high pressure turbine before entering the exchanger 22 via the recuperator. Fig. 7 shows a further embodiment in which the working medium is compressed by low and high pressure compressors 65 and 66 a part being preheated in exchanger. 22 and another part in recuperator 68. After uniting the medium is again split one part being burnt with gas in a combustion chamber 76 thereby heating an exchanger'71 the combustion-products passing to high pressure and low pressure turbines 80 and 81 in series before being discharged into the atmosphere and the other part flowing through the exchanger 71, turbine 73 driving the compressors 65 and 66, and the recuperator 68 so returning to the low and high pressure compressors. The high pressure turbine 80 drives the make-up compressor 83 whilst the low pressure turbine 81 drives an electric generator 21.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH631547X | 1946-10-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB631547A true GB631547A (en) | 1949-11-04 |
Family
ID=4524776
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB26676/47A Expired GB631547A (en) | 1946-10-04 | 1947-10-03 | Improvements relating to plants in which solid material is subjected to heating and cooling |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB631547A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102985665A (en) * | 2010-07-02 | 2013-03-20 | 埃克森美孚上游研究公司 | Low emission triple-cycle power generation systems and methods |
-
1947
- 1947-10-03 GB GB26676/47A patent/GB631547A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102985665A (en) * | 2010-07-02 | 2013-03-20 | 埃克森美孚上游研究公司 | Low emission triple-cycle power generation systems and methods |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2633707A (en) | Compound plant for producing mechanical power and heating steam with gas and steam turbines | |
US2428136A (en) | Combustion gas and waste heat steam turbine | |
US2404938A (en) | Gas turbine plant | |
GB811393A (en) | Improvements in and relating to gas turbine plants | |
US2341490A (en) | Gas turbine plant | |
GB619114A (en) | Improvements relating to gas turbine plant | |
US2392623A (en) | Gas-turbine plant | |
GB631547A (en) | Improvements relating to plants in which solid material is subjected to heating and cooling | |
GB413697A (en) | Improvements in and relating to gas turbine plant | |
GB604028A (en) | Improvements in or relating to thermal power plants | |
GB569441A (en) | Improvements in or relating to combustion plant | |
GB716274A (en) | Improvements in or relating to recuperative heat exchangers | |
GB711271A (en) | Improvements in or relating to waste heat recovery installations | |
GB1104075A (en) | Method of combustion of high-sulphur ash fuels at thermal power stations | |
JPS5490846A (en) | Cool and hot wind generating apparatus | |
GB656102A (en) | Improvements relating to combined gas and steam turbine systems | |
GB619312A (en) | Improvements relating to gas turbine plant | |
GB604392A (en) | Improvements in or relating to a power plant | |
SU88643A1 (en) | Mode of operation of thermal power plants | |
GB645265A (en) | Improvements in gas turbine plant for producing simultaneously driving energy and heat at moderate temperature | |
GB587449A (en) | Improvements in motive power installations having a generator for hot gas under pressure | |
GB675971A (en) | Improvements in or relating to thermodynamic power plant | |
GB621954A (en) | Improvements in or relating to thermal power plant | |
GB191402511A (en) | Gas Turbines. | |
GB607311A (en) | Improvements in or relating to gas turbine power plants |