GB734231A - Operation of gas turbine equipment - Google Patents
Operation of gas turbine equipmentInfo
- Publication number
- GB734231A GB734231A GB1015653A GB1015653A GB734231A GB 734231 A GB734231 A GB 734231A GB 1015653 A GB1015653 A GB 1015653A GB 1015653 A GB1015653 A GB 1015653A GB 734231 A GB734231 A GB 734231A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sulphate
- gas turbine
- corrosion
- turbine equipment
- metal
- 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
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
- C10L1/00—Liquid carbonaceous fuels
- C10L1/10—Liquid carbonaceous fuels containing additives
- C10L1/14—Organic compounds
- C10L1/18—Organic compounds containing oxygen
-
- 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
- F02C7/30—Preventing corrosion or unwanted deposits in gas-swept spaces
Abstract
734,231. Preventing furnace corrosion. STANDARD OIL DEVELOPMENT CO. Feb. 23, 1954 [April 14, 1953], No. 10156/53. Class 51 (1). A process for reducing the corrosion of an oilfired gas turbine comprises burning the oil fuel together with a minor proportion of a metal sulphate which is unstable at 850‹ C. so that the sulphate decomposes and yields an oxide which reacts with vanadium pentoxide, the said metal sulphate being finely distributed throughout the combustion zone. Aluminium, zinc or tin sulphate may be used; the sulphate may be injected into the combustion chamber as an aqueous solution or as a slurry. Specification 705,176 is referred to.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1015653A GB734231A (en) | 1953-04-14 | 1953-04-14 | Operation of gas turbine equipment |
DEST8049A DE1008056B (en) | 1953-04-14 | 1954-04-13 | Process for the production of hot gases of low corrosivity from a heating oil containing sulfur and vanadium |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1015653A GB734231A (en) | 1953-04-14 | 1953-04-14 | Operation of gas turbine equipment |
Publications (1)
Publication Number | Publication Date |
---|---|
GB734231A true GB734231A (en) | 1955-07-27 |
Family
ID=9962565
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1015653A Expired GB734231A (en) | 1953-04-14 | 1953-04-14 | Operation of gas turbine equipment |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1008056B (en) |
GB (1) | GB734231A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3581491A (en) * | 1969-01-07 | 1971-06-01 | United Aircraft Corp | Prevention of hot corrosion in gas turbine engines |
EP2453120A4 (en) * | 2009-07-07 | 2016-04-20 | Mitsubishi Hitachi Power Sys | Operation control method for gas turbine and operation controller for gas turbine |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE497461A (en) * | 1949-08-10 |
-
1953
- 1953-04-14 GB GB1015653A patent/GB734231A/en not_active Expired
-
1954
- 1954-04-13 DE DEST8049A patent/DE1008056B/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3581491A (en) * | 1969-01-07 | 1971-06-01 | United Aircraft Corp | Prevention of hot corrosion in gas turbine engines |
EP2453120A4 (en) * | 2009-07-07 | 2016-04-20 | Mitsubishi Hitachi Power Sys | Operation control method for gas turbine and operation controller for gas turbine |
Also Published As
Publication number | Publication date |
---|---|
DE1008056B (en) | 1957-05-09 |
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