公开(公告)号：EP2474598A1

公开(公告)日：2012-07-11

申请号：EP10812043.7

申请日：2010-08-30

申请人： JX Nippon Oil & Energy Corporation

发明人： KOYAMA Akira

IPC分类号： C10L1/04 ,  C10G3/00 ,  C10G45/62 ,  C10G45/64

CPC分类号： C10G3/50 ,  B01J21/12 ,  B01J23/38 ,  B01J23/42 ,  B01J23/70 ,  B01J27/19 ,  B01J29/064 ,  B01J35/023 ,  B01J37/0009 ,  B01J37/0201 ,  C10G3/46 ,  C10G3/48 ,  C10G3/49 ,  C10G45/02 ,  C10G45/58 ,  C10G65/043 ,  C10G2300/1014 ,  C10G2300/1018 ,  C10G2300/1033 ,  C10G2300/202 ,  C10G2300/301 ,  C10G2300/308 ,  C10G2300/4018 ,  C10G2300/80 ,  C10G2400/08 ,  C10L1/04 ,  C10L1/19 ,  C10L1/2235 ,  C10L1/2283 ,  C10L2200/0407 ,  C10L2200/043 ,  C10L2230/22 ,  C10L2270/04 ,  Y02P30/10 ,  Y02P30/20

摘要： To provide an aviation fuel oil composition which has excellent life cycle characteristics and achieves excellent specific fuel consumption. The aviation fuel oil composition according to the present invention includes: a first base which is a fraction having a boiling range of 140 to 280°C obtained through a step of hydrotreating a first feedstock containing a sulfur-containing hydrocarbon compound and an oxygen-containing hydrocarbon compound derived from an animal or vegetable oil and fat or a second feedstock which is an oil blend of the first feedstock and a petroleum-based base obtained by refining a crude oil; and a second base which is a fraction having a boiling range of 140 to 280°C obtained from a heavy oil cracking apparatus.

摘要翻译： 提供具有优异的生命周期特性并实现优异的比燃料消耗的航空燃料油组合物。 根据本发明的航空燃料油组合物包括：通过加氢处理含有含硫烃化合物和含氧烃的第一原料的步骤获得的沸点范围为140〜280℃的馏分的第一碱 来自动物或植物油和脂肪的烃化合物或第二原料，其是通过精制原油获得的第一原料和石油基碱的油混合物; 和由重油裂化装置得到的沸点范围为140〜280℃的馏分的第二碱。

公开(公告)号：EP2474596A1

公开(公告)日：2012-07-11

申请号：EP10812048.6

申请日：2010-08-30

申请人： JX Nippon Oil & Energy Corporation

发明人： HAYASAKA Kazuaki ,  ONO Hideki ,  KOYAMA Akira ,  IKI Hideshi

IPC分类号： C10G65/04 ,  B01J27/198 ,  B01J29/76 ,  C10G3/00 ,  C10G45/08 ,  C10G45/64 ,  C10G47/12 ,  C10L1/04

CPC分类号： B01J29/7484 ,  B01J23/85 ,  B01J23/883 ,  B01J29/7461 ,  B01J29/7492 ,  B01J29/85 ,  C10G3/46 ,  C10G3/49 ,  C10G3/50 ,  C10G45/64 ,  C10G2300/1014 ,  C10G2300/1018 ,  C10G2300/202 ,  C10G2400/08 ,  C10L1/04 ,  Y02P30/20

摘要： 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 6A 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.

摘要翻译： 一种用于在航空燃料油基材的制造方法，包括：由通过使原料的方法包括：从动物或植物油和脂肪得到接触与含氧烃化合物进行加氢处理的原料获得的第一产生的油的第一步骤 其中有脱氢和氢化功能和哪些第一双功能催化剂包括周期表第6A族的在无定形固体酸性物质的金属，第8族的金属，和氢，在存在; 并且通过使第一生成油接触到其中有脱氢和氢化功能和哪一个第二双功能催化剂加氢异构化生成的第一油获得第二生成油，包括航空燃料油基材的第二步骤包括该组的金属 在存在元素周期表和结晶固体酸性物质，氢气8。