| 摘要 |
Disclosed is an aviation fuel oil composition that contains: a first base, which is a distillate fraction having a boiling range of 140-280˚C, and which is obtained via a process wherein a first raw material oil that contains a sulfur-containing hydrocarbon compound and an oxygen-containing hydrocarbon compound derived from an animal/plant oil or fat, or alternatively a second raw material oil that is a mixture of the first raw material oil and a petroleum base obtained by refining crude oil is subjected to a hydrogenation treatment; and a second base, which is a distillate fraction having a boiling range of 140-280˚C, and which is obtained from a heavy oil cracking apparatus. |
