GB600471A - Improvements in or relating to the production of aviation gasoline - Google Patents
Improvements in or relating to the production of aviation gasolineInfo
- Publication number
- GB600471A GB600471A GB123145A GB123145A GB600471A GB 600471 A GB600471 A GB 600471A GB 123145 A GB123145 A GB 123145A GB 123145 A GB123145 A GB 123145A GB 600471 A GB600471 A GB 600471A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fraction
- benzene
- boiling
- fractionated
- products
- 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
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 abstract 30
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 abstract 21
- 238000009835 boiling Methods 0.000 abstract 12
- 125000003118 aryl group Chemical group 0.000 abstract 8
- RWGFKTVRMDUZSP-UHFFFAOYSA-N cumene Chemical compound CC(C)C1=CC=CC=C1 RWGFKTVRMDUZSP-UHFFFAOYSA-N 0.000 abstract 6
- 229930195733 hydrocarbon Natural products 0.000 abstract 6
- 150000002430 hydrocarbons Chemical class 0.000 abstract 6
- 239000004215 Carbon black (E152) Substances 0.000 abstract 4
- UFWIBTONFRDIAS-UHFFFAOYSA-N Naphthalene Chemical compound C1=CC=CC2=CC=CC=C21 UFWIBTONFRDIAS-UHFFFAOYSA-N 0.000 abstract 4
- 150000001336 alkenes Chemical class 0.000 abstract 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 abstract 4
- 239000007789 gas Substances 0.000 abstract 4
- 238000004227 thermal cracking Methods 0.000 abstract 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 4
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 abstract 2
- QQONPFPTGQHPMA-UHFFFAOYSA-N Propene Chemical compound CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 abstract 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 abstract 2
- 239000002253 acid Substances 0.000 abstract 2
- 239000003054 catalyst Substances 0.000 abstract 2
- 239000004927 clay Substances 0.000 abstract 2
- 239000000470 constituent Substances 0.000 abstract 2
- 238000005336 cracking Methods 0.000 abstract 2
- 150000001925 cycloalkenes Chemical class 0.000 abstract 2
- 150000001993 dienes Chemical class 0.000 abstract 2
- 239000003085 diluting agent Substances 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 2
- 238000002156 mixing Methods 0.000 abstract 2
- 239000000203 mixture Substances 0.000 abstract 2
- 229910000476 molybdenum oxide Inorganic materials 0.000 abstract 2
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 abstract 2
- 239000003208 petroleum Substances 0.000 abstract 2
- 239000000843 powder Substances 0.000 abstract 2
- 239000002904 solvent Substances 0.000 abstract 2
- 239000001117 sulphuric acid Substances 0.000 abstract 2
- 235000011149 sulphuric acid Nutrition 0.000 abstract 2
- 150000003568 thioethers Chemical class 0.000 abstract 2
- 239000008096 xylene Substances 0.000 abstract 2
- 150000003738 xylenes Chemical class 0.000 abstract 2
- 229910000147 aluminium phosphate Inorganic materials 0.000 abstract 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10G—CRACKING HYDROCARBON OILS; PRODUCTION OF LIQUID HYDROCARBON MIXTURES, e.g. BY DESTRUCTIVE HYDROGENATION, OLIGOMERISATION, POLYMERISATION; RECOVERY OF HYDROCARBON OILS FROM OIL-SHALE, OIL-SAND, OR GASES; REFINING MIXTURES MAINLY CONSISTING OF HYDROCARBONS; REFORMING OF NAPHTHA; MINERAL WAXES
- C10G59/00—Treatment of naphtha by two or more reforming processes only or by at least one reforming process and at least one process which does not substantially change the boiling range of the naphtha
- C10G59/02—Treatment of naphtha by two or more reforming processes only or by at least one reforming process and at least one process which does not substantially change the boiling range of the naphtha plural serial stages only
- C10G59/04—Treatment of naphtha by two or more reforming processes only or by at least one reforming process and at least one process which does not substantially change the boiling range of the naphtha plural serial stages only including at least one catalytic and at least one non-catalytic reforming step
Landscapes
- Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
Abstract
A petroleum fraction is catalytically cracked or a naphtha catalytically reformed, an aromatic-rich fraction boiling within the range 200-500 DEG F. is separated, thermally cracked at at least 1200 DEG F. for a time from a few seconds to a fraction of a second, and an aromatic fraction of aviation gasoline boiling range is recovered from the products. The thermal cracking converts non-aromatics to lower boiling products, and higher boiling aromatics to benzene and toluene. The product may be acid treated to remove olefinic constituents and, if desired, fractionated to separate benzene and toluene or excess benzene may be alkylated to cumene. A high boiling feedstock such as gas oil or refined crude, may be catalytically cracked at about 800-1050 DEG F. using silica-alumina or other catalyst in a stationary or moving bed or as suspended powder. The products are fractionated to obtain a light fraction boiling up to about 200-225 DEG F. which may be worked up to a gasoline, and a fraction preferably of B.R. about 200-350 DEG F. which contains 50-80 per cent aromatics. This fraction, preferably with a diluent such as steam or hydrocarbon gases, for example steam equivalent to 80 mol. per cent of the mixture, is heated at 1200-1600 DEG F. and then quenched with water to 600-1000 DEG F. Hydrocarbons and water are condensed and the hydrocarbon layer fractionated to give a light fraction from which olefins and diolefins may be recovered, a heavy naphtha which may be used as a solvent or motor fuel or treated to recover naphthalene if present in the feed to the cracking step, and an intermediate aromatic fraction containing benzene, toluene and xylenes, for example a 145-350 DEG F. cut. This is freed from olefins with sulphuric acid, clay or fuller's earth and yields an aviation gasoline blending stock. The temperature in the thermal cracking stage should be at least equal to 1332-107.6 log. S + 10S-1,45, where S is the contact time in seconds. Alternatively, a naphtha, preferably a virgin naphtha of B.R. about 300-400 DEG F. containing more than 40 per cent naphthenes and cyclo-olefins, may be hydroformed at 850-1100 DEG F. using Group 6 oxides or sulphides, preferably molybdenum oxide on alumina, and the products fractionated as before, an intermediate fraction of B.R. 250-350 DEG or 450 DEG F. being thermally cracked, preferably with steam, quenched, and the desired aromatic fraction recovered.ALSO:A petroleum fraction is catalytically cracked or a naphtha catalytically reformed, an aromatic-rich fraction boiling within the range 200-500 DEG F. is separated, thermally cracked at at least 1200 DEG F. for a time from a few seconds to a fraction of a second, and an aromatic fraction of aviation gasoline boiling range is recovered from the products. The thermal cracking converts non-aromatics to lower boiling products, and higher boiling aromatics to benzene and toluene. The product may be acid treated to remove olefinic constituents and, if desired, fractionated to separate benzene and toluene or excess benzene may be alkylated to cumene. A high boiling feedstock such as gas oil or refined crude may be catalytically cracked at about 800-1050 DEG F. using silica-alumina or other catalyst in a stationary or moving bed or as suspended powder. The products are fractionated to obtain a light fraction boiling up to about 200-225 DEG F. which may be worked up to a gasoline, and a fraction preferably of B.R. about 200-350 DEG F. which contains 50-80 per cent aromatics. This fraction, preferably with a diluent such as steam or hydrocarbon gases, for example steam equivalent to 80 mol. per cent of the mixture, is heated at 1200-1600 and then quenched with water to 600-1000 DEG F. Hydrocarbons and water are condensed and the hydrocarbon layer fractionated to give a light fraction from which olefins and diolefins may be recovered, a heavy naphtha which may be used as a solvent or motor fuel or treated to recover naphthalene if present in the feed to the cracking step, and an intermediate aromatic fraction containing benzene, toluene, and xylenes, for example a 145-350 DEG F. cut. This is freed from olefins with sulphuric acid, clay or fuller's earth and yields an aviation gasoline blending stock. The temperature ( DEG F.) in the thermal cracking stage should be at least equal to 1332-107.6 log S+10S-1,45, where S is the contact time in seconds. Alternatively, a naphtha, preferably a virgin naphtha of B.R. about 300-400 DEG F. containing more than 40 per cent of naphthenes and cyclo-olefins, may be hydroformed at 850-110 DEG F. using Group 6 oxides or sulphides, preferably molybdenum oxide on alumina, and the products fractionated as before, an intermediate fraction of B.R. 250-350 DEG or 450 DEG F. being thermally cracked, preferably with steam, quenched and the desired aromatic fraction recovered. It may be fractionated to recover benzene and toluene or benzene in excess of specifications for aviation gasolene may be alkylated with propene and phosphoric acid at 400-500 DEG F. and 600 p.s.i. to yield cumene.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB600471A true GB600471A (en) | 1948-04-09 |
Family
ID=1626727
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB123145A Expired GB600471A (en) | 1945-01-15 | Improvements in or relating to the production of aviation gasoline |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB600471A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE969795C (en) * | 1952-11-03 | 1958-07-17 | Bataafsche Petroleum | Process for the production of gasoline with an octane number in the range from 90 to 100 from directly distilled gasoline by reforming |
| EP1365004A1 (en) * | 2002-05-23 | 2003-11-26 | ATOFINA Research | Production of olefins |
-
1945
- 1945-01-15 GB GB123145A patent/GB600471A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE969795C (en) * | 1952-11-03 | 1958-07-17 | Bataafsche Petroleum | Process for the production of gasoline with an octane number in the range from 90 to 100 from directly distilled gasoline by reforming |
| EP1365004A1 (en) * | 2002-05-23 | 2003-11-26 | ATOFINA Research | Production of olefins |
| WO2003099964A1 (en) * | 2002-05-23 | 2003-12-04 | Total Petrochemicals Research Feluy | Production of olefins |
| EP2267101A3 (en) * | 2002-05-23 | 2011-03-02 | Total Petrochemicals Research Feluy | Production of olefins |
| US8071833B2 (en) | 2002-05-23 | 2011-12-06 | Total Petrochemicals Research Feluy | Production of olefins |
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