发明名称 High octane unleaded aviation gasoline
摘要 <p>High octane unleaded aviation fuel composition having high aromatics content and CHN content of at least 97.8wt%, less than 2.2 wt% of oxygen content, a T10 of at most 75°C, T40 of at least 75° C, a T50 of at most 105° C, a T90 of at most 135°C, a final boiling point of less than 190°C, an adjusted heat of combustion of at least 43.5 MJ/kg, a vapor pressure in the range of 38 to 49 kPa is provided.</p>
申请公布号 GB201413250(D0) 申请公布日期 2014.09.10
申请号 GB20140013250 申请日期 2014.07.25
申请人 SHELL INTERNATIONALE RESEARCH MAATSCHAPPIJ B.V. 发明人
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