基本信息:
- 专利标题： AVIATION FUEL OIL COMPOSITION
- 专利标题（中）：航空燃油组合物
- 申请号：US13391891 申请日：2010-08-30
- 公开(公告)号：US20120198757A1 公开(公告)日：2012-08-09
- 发明人： Akira Koyama
- 申请人： Akira Koyama
- 申请人地址： JP Tokyo
- 专利权人： JX NIPPON OIL & ENERGY CORPORATION
- 当前专利权人： JX NIPPON OIL & ENERGY CORPORATION
- 当前专利权人地址： JP Tokyo
- 优先权： JP2009-200695 20090831
- 国际申请： PCT/JP2010/064700 WO 20100830
- 主分类号： C10L1/10
- IPC分类号： C10L1/10
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（中）：
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化合物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， 含有源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。