GB993412A - Improvements in or relating to the manufacture of sulphur dioxide - Google Patents
Improvements in or relating to the manufacture of sulphur dioxideInfo
- Publication number
- GB993412A GB993412A GB25647/61A GB2564761A GB993412A GB 993412 A GB993412 A GB 993412A GB 25647/61 A GB25647/61 A GB 25647/61A GB 2564761 A GB2564761 A GB 2564761A GB 993412 A GB993412 A GB 993412A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sulphur dioxide
- sulphur
- turbine
- combustion chamber
- 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
Classifications
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B17/00—Sulfur; Compounds thereof
- C01B17/48—Sulfur dioxide; Sulfurous acid
- C01B17/50—Preparation of sulfur dioxide
- C01B17/58—Recovery of sulfur dioxide from acid tar or the like or from any waste sulfuric acid
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B17/00—Sulfur; Compounds thereof
- C01B17/48—Sulfur dioxide; Sulfurous acid
- C01B17/50—Preparation of sulfur dioxide
- C01B17/54—Preparation of sulfur dioxide by burning elemental sulfur
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P20/00—Technologies relating to chemical industry
- Y02P20/10—Process efficiency
- Y02P20/129—Energy recovery, e.g. by cogeneration, H2recovery or pressure recovery turbines
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
A gas turbine is driven by sulphur dioxide produced in the combustion chamber of the turbine, the sulphur dioxide thereby being cooled. The sulphur dioxide may be produced by burning sulphur, pyrites or "waste sludge" (a viscous acid material resulting from the purification of petroleum and lubricating oils by treatment with sulphuric acid). In the combustion of pyrites, a dust separator is inserted between the combustion chamber and the turbine. The walls of the combustion chamber may be maintained at 300 DEG C. by heat-exchange with molten sulphur to be burnt. The sulphur dioxide may be further cooled by passage from the gas turbine through a waste heat boiler. Alternatively or in addition, further cooling may be effected by passing the sulphur dioxide through a heat-exchanger for preheating the oxygen-containing gas for the combustion. The sulphur dioxide may then be catalytically converted into sulphuric acid directly or via the production of sulphur trioxide. Prior compression of the oxygen-containing gas may be effected in an axial, centrifugal or displacement type compressor. The compressor may have two stages. The gas turbine may be of the axial or radial flow type and may have four stages. Corrosion vulnerable surfaces may be of high chromium steel, nickel-chromium-cobalt alloy, or aluminium.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25647/61A GB993412A (en) | 1961-07-19 | 1961-07-19 | Improvements in or relating to the manufacture of sulphur dioxide |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25647/61A GB993412A (en) | 1961-07-19 | 1961-07-19 | Improvements in or relating to the manufacture of sulphur dioxide |
Publications (1)
Publication Number | Publication Date |
---|---|
GB993412A true GB993412A (en) | 1965-05-26 |
Family
ID=10231069
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25647/61A Expired GB993412A (en) | 1961-07-19 | 1961-07-19 | Improvements in or relating to the manufacture of sulphur dioxide |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB993412A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2257426A1 (en) * | 1972-11-23 | 1974-06-20 | Uhde Gmbh Friedrich | METHOD AND DEVICE FOR GENERATING GASES WITH SO DEEP TWO CONDITIONS |
US4010246A (en) * | 1974-10-12 | 1977-03-01 | Hoechst Aktiengesellschaft | Process for preparing sulfur dioxide |
US5503821A (en) * | 1990-03-23 | 1996-04-02 | Monsanto Company | Methods for recovering high grade process energy from a contact sulfuric acid process |
EP1329592A1 (en) * | 2002-01-18 | 2003-07-23 | Siemens Aktiengesellschaft | Turbine with at least four stages and utilisation of a turbine blade with reduced mass |
-
1961
- 1961-07-19 GB GB25647/61A patent/GB993412A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2257426A1 (en) * | 1972-11-23 | 1974-06-20 | Uhde Gmbh Friedrich | METHOD AND DEVICE FOR GENERATING GASES WITH SO DEEP TWO CONDITIONS |
US4010246A (en) * | 1974-10-12 | 1977-03-01 | Hoechst Aktiengesellschaft | Process for preparing sulfur dioxide |
US5503821A (en) * | 1990-03-23 | 1996-04-02 | Monsanto Company | Methods for recovering high grade process energy from a contact sulfuric acid process |
EP1329592A1 (en) * | 2002-01-18 | 2003-07-23 | Siemens Aktiengesellschaft | Turbine with at least four stages and utilisation of a turbine blade with reduced mass |
WO2003060292A1 (en) * | 2002-01-18 | 2003-07-24 | Siemens Aktiengesellschaft | Turbine comprising at least four stages and use of a turbine blade with a reduced mass |
US7229254B2 (en) | 2002-01-18 | 2007-06-12 | Siemens Aktiengesellschaft | Turbine blade with a reduced mass |
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