IP Library Granted Patent US 9,283,552
Granted Patent B2
US 9,283,552 · App. 13/391,727 · Granted Mar 15, 2016

Method for producing aviation fuel oil base and aviation fuel oil composition

Inventors: Kazuaki Hayasaka (Tokyo, JP); Hideki Ono (Tokyo, JP); Akira Koyama (Tokyo, JP); Hideshi Iki (Tokyo, JP)
Assignee: JX NIPPON OIL & ENERGY CORPORATION
B01J29/7484B01J23/883B01J29/7461B01J29/7492C10G3/46C10G3/49C10G3/50C10G45/64C10L1/04B01J23/85B01J29/85C10G2300/1014C10G2300/1018C10G2300/202C10G2400/08
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Quick Facts
Patent No.
US 9,283,552
App. No.
13/391,727
Granted
Mar 15, 2016
Kind
B2
Abstract

A method for producing an aviation fuel oil base, including: a first step of obtaining a first generated oil by hydrotreating a feedstock by bringing a feedstock which includes an oxygen-containing hydrocarbon compound derived from an animal or vegetable oils and fat into contact with a first dual functional catalyst which has dehydrogenation and hydrogenation functions and which includes a metal of group 6B of the periodic table, a metal of group 8, and an amorphous solid acidic substance, in the presence of hydrogen; and a second step of obtaining a second generated oil including an aviation fuel oil base by hydroisomerizing the first generated oil by bringing the first generated oil into contact with a second dual functional catalyst which has dehydrogenation and hydrogenation functions and which includes a metal of the group 8 of the periodic table and a crystalline solid acidic substance, in the presence of hydrogen.

Claims (20)

1. A method for producing an aviation fuel oil base, comprising:

first obtaining a first generated oil by hydrotreating a feedstock which contains an oxygen-containing hydrocarbon compound derived from an animal or vegetable oils and fat by bringing the feedstock into contact with a first dual functional catalyst which has dehydrogenation and hydrogenation functions and which comprises a metal of group 6B of the periodic table, a metal of group 8, and an amorphous solid acidic substance, in the presence of hydrogen, wherein the feedstock contains 1 to 100 mass ppm in terms of sulfur atoms of a sulfur-containing hydrocarbon compound, and wherein the sulfur content included in the first generated oil is 10 mass ppm or less; and

then obtaining a second generated oil comprising an aviation fuel oil base by hydroisomerizing the first generated oil by bringing the first generated oil into contact with a second dual functional catalyst which has dehydrogenation and hydrogenation functions and which comprises a metal of group 8 of the periodic table and a crystalline solid acidic substance, in the presence of hydrogen;

wherein the cracking ratio is no greater than 20 mass % when obtaining the second generated oil by hydroisomerizing the first oil.

2. The method for producing an aviation fuel oil base according to claim 1 , wherein the metal of group 6B of the periodic table in the first dual functional catalyst is molybdenum and/or tungsten, and

the metal of group 8 of the periodic table in the first dual functional catalyst is cobalt and/or nickel, and

wherein the method comprises sulfiding the first dual functional catalyst, before the bringing the feedstock into contact with a first dual functional catalyst.

3. The method for producing an aviation fuel oil base according to claim 1 , wherein the crystalline solid acidic substance in the second dual functional catalyst is a crystalline substance comprising at least one crystal selected from the group consisting of a one-dimensional, 10-member ring aluminosilicate having an MEL structure, a TON structure, an MTT structure, and an MRE structure, and a silicoaluminophosphate having an AEL structure.

4. The method for producing an aviation fuel oil base according to claim 1 , wherein

the crystalline solid acidic substance in the second dual functional catalyst comprises a one-dimensional, 10-member ring aluminosilicate and/or a silicoaluminophosphate, and

a total content of the one-dimensional, 10-member ring aluminosilicate and the silicoaluminophosphate is 65 to 85 mass %.

5. The method for producing an aviation fuel oil base according to claim 3 , wherein the one-dimensional, 10-member ring aluminosilicate comprises at least one selected from the group consisting of ZSM-11, ZSM-22, ZSM-23, and ZSM-48, and

the silicoaluminophosphate comprises at least one selected from the group consisting of SAPO-11 and SAPO-34.

6. The method for producing an aviation fuel oil base according to claim 1 , wherein a hydroisomerization ratio exceeds 90 mass %.

7. An aviation fuel oil composition, containing a first aviation fuel oil base obtained by the method for producing an aviation fuel oil base according to claim 1 and a second aviation fuel oil base produced from a petroleum-based feedstock, wherein

a content of the first aviation fuel oil base is 5 to 50 mass % and a content of the second aviation fuel oil base is 50 to 95 mass %.

8. The method for producing an aviation fuel oil base according to claim 4 , wherein the one-dimensional, 10-member ring aluminosilicate comprises at least one selected from the group consisting of ZSM-11, ZSM-22, ZSM-23, and ZSM-48, and

the silicoaluminophosphate comprises at least one selected from the group consisting of SAPO-11 and SAPO-34.

9. An aviation fuel oil composition, containing a first aviation fuel oil base obtained by the method for producing an aviation fuel oil base according to claim 1 and a second aviation fuel oil base produced from a petroleum-based feedstock, wherein

a content of the first aviation fuel oil base is 5 to 50 mass % and a content of the second aviation fuel oil base is 50 to 95 mass %.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 4, 2012
From: HAYASAKA, KAZUAKI; ONO, HIDEKI; KOYAMA, AKIRA; IKI, HIDESHI
To: JX NIPPON OIL & ENERGY CORPORATION
Reel/Frame 028157/0546 →
Priority Claims (1)
JP 2009-200918 · Aug 31, 2009 · national
Continuity (1)
Related Publication 20120216449A1 · Aug 30, 2012