RU97108034A - METHOD FOR PRODUCING AVIATION GASOLINE - Google Patents

METHOD FOR PRODUCING AVIATION GASOLINE

Info

Publication number
RU97108034A
RU97108034A RU97108034/04A RU97108034A RU97108034A RU 97108034 A RU97108034 A RU 97108034A RU 97108034/04 A RU97108034/04 A RU 97108034/04A RU 97108034 A RU97108034 A RU 97108034A RU 97108034 A RU97108034 A RU 97108034A
Authority
RU
Russia
Prior art keywords
aviation gasoline
fraction
producing aviation
hydrodearomatization
reformate
Prior art date
Application number
RU97108034/04A
Other languages
Russian (ru)
Other versions
RU2120467C1 (en
Inventor
К.Г. Абдульминев
А.Ф. Ахметов
Original Assignee
Уфимский государственный нефтяной технический университет
Filing date
Publication date
Application filed by Уфимский государственный нефтяной технический университет filed Critical Уфимский государственный нефтяной технический университет
Priority to RU97108034A priority Critical patent/RU2120467C1/en
Priority claimed from RU97108034A external-priority patent/RU2120467C1/en
Application granted granted Critical
Publication of RU2120467C1 publication Critical patent/RU2120467C1/en
Publication of RU97108034A publication Critical patent/RU97108034A/en

Links

Claims (3)

1. Способ получения авиационного бензина путем каталитического риформинга прямогонного бензина с получением риформата, выделением из риформата головной и остаточной фракций, направлением головной фракции на гидродеароматимзацию в присутствии платинсодержащего катализатора при повышенной температуре и давлении до 5 МПа, и объемной скорости подачи сырья 1-5 ч-1, отличающийся тем, что из риформата выделяют головную фракцию НК-90oC, среднюю фракцию 90-140oC и остаточную фракцию 140-KKoC, а продукт гидродеароматизации смешивают с средней фракцией 90-140oC.1. A method of producing aviation gasoline by catalytic reforming of straight-run gasoline to obtain reformate, separation of the head and residual fractions from the reformate, directing the head fraction to hydrodearomatization in the presence of a platinum-containing catalyst at an elevated temperature and pressure of up to 5 MPa, and a bulk feed rate of 1-5 hours -1 , characterized in that the head fraction NK-90 o C, the middle fraction 90-140 o C and the residual fraction 140-KK o C are isolated from the reformate, and the hydrodearomatization product is mixed with the middle fraction 90-140 o C. 2. Способ получения авиационного бензина по п.1, отличающийся тем, что в качестве платинсодержащего катализатора используют алюмоплатиновый катализатор АП-64. 2. The method of producing aviation gasoline according to claim 1, characterized in that the aluminum-platinum catalyst AP-64 is used as a platinum-containing catalyst. 3. Способ получения авиационного бензина по пп.1 и 2, отличающийся тем, что гидродеароматизацию проводят при 200-450oC.3. The method of producing aviation gasoline according to claims 1 and 2, characterized in that the hydrodearomatization is carried out at 200-450 o C.
RU97108034A 1997-05-13 1997-05-13 Method of producing aircraft motor gasoline RU2120467C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97108034A RU2120467C1 (en) 1997-05-13 1997-05-13 Method of producing aircraft motor gasoline

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97108034A RU2120467C1 (en) 1997-05-13 1997-05-13 Method of producing aircraft motor gasoline

Publications (2)

Publication Number Publication Date
RU2120467C1 RU2120467C1 (en) 1998-10-20
RU97108034A true RU97108034A (en) 1999-03-10

Family

ID=20193020

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97108034A RU2120467C1 (en) 1997-05-13 1997-05-13 Method of producing aircraft motor gasoline

Country Status (1)

Country Link
RU (1) RU2120467C1 (en)

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