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公开(公告)号:US09120991B2
公开(公告)日:2015-09-01
申请号:US14340669
申请日:2014-07-25
Applicant: SHELL OIL COMPANY
Inventor: Timothy Michael Shea , Trevor James Davies , Michael Clifford Macknay , Hanane Belmokaddem Bennis
CPC classification number: C10L1/223 , C10L1/10 , C10L1/1608 , C10L1/1616 , C10L1/19 , C10L2200/0423 , C10L2300/40
Abstract: High octane unleaded aviation fuel compositions having a CHN content of at least 97.2 wt %, less than 2.8 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 210° 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.
Abstract translation: 高辛烷值无铅航空燃料组合物,其CHN含量为至少97.2重量%,小于2.8重量%的氧含量,T 10为至多75℃,T40为至少75℃,T 50为至多 105℃,T90至多135℃,最终沸点低于210℃,调节燃烧热至少43.5MJ / kg,蒸气压在38至49的范围内 提供kPa。
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公开(公告)号:US09127225B2
公开(公告)日:2015-09-08
申请号:US14340731
申请日:2014-07-25
Applicant: SHELL OIL COMPANY
CPC classification number: C10L1/223 , C10L1/10 , C10L1/1608 , C10L1/1616 , C10L1/1824 , C10L2200/0423 , C10L2300/40
Abstract: High octane unleaded aviation fuel composition having high aromatics content and CHN content of at least 97.8 wt %, 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.
Abstract translation: 高辛烷值无铅航空燃料组合物具有高芳烃含量和CHN含量至少为97.8重量%,少于2.2重量%的氧含量,T 10为至多75℃,T40为至少75℃,T50 至多105℃,T90至多135℃,最终沸点低于190℃,调节后的燃烧热至少为43.5MJ / kg,蒸汽压在 提供38至49kPa。
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公开(公告)号:US09388358B2
公开(公告)日:2016-07-12
申请号:US14340882
申请日:2014-07-25
Applicant: SHELL OIL COMPANY
Inventor: Timothy Michael Shea , Trevor James Davies , Michael Clifford Macknay , Hanane Belmokaddem Bennis
IPC: C10L1/16 , C10L1/223 , C10L1/182 , C10L10/10 , C10L1/02 , C10L1/00 , C10L1/18 , C10L1/22 , C10L10/14 , C10L1/19
CPC classification number: C10L10/10 , C10L1/00 , C10L1/02 , C10L1/16 , C10L1/1608 , C10L1/18 , C10L1/19 , C10L1/22 , C10L1/223 , C10L10/14 , C10L2200/0259 , C10L2200/0415 , C10L2230/22 , C10L2270/023 , C10L2270/04
Abstract: High octane unleaded aviation gasoline having low aromatics content and 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 and a freezing point of less than −58° C. is provided.
Abstract translation: 具有低芳烃含量的高辛烷值无铅航空汽油和至多75℃的T10,至少75℃的T40,至多105℃的T50,至多135℃的T90,至多135℃的T90 最终沸点低于190℃,调节至少43.5MJ / kg的燃烧热,38至49kPa范围内的蒸气压和小于-58℃的凝固点。
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公开(公告)号:US09388357B2
公开(公告)日:2016-07-12
申请号:US14340860
申请日:2014-07-25
Applicant: SHELL OIL COMPANY
Inventor: Timothy Michael Shea , Trevor James Davies , Michael Clifford Macknay , Hanane Belmokaddem Bennis
CPC classification number: C10L10/10 , C10L1/00 , C10L1/1824 , C10L1/223 , C10L2200/0259 , C10L2200/0407 , C10L2200/0415 , C10L2200/0423 , C10L2230/22 , C10L2270/023 , C10L2270/04
Abstract: High octane unleaded aviation fuel compositions having high aromatics content and a CHN content of at least 98 wt %, less than 2 wt % of oxygen content, an adjusted heat of combustion of at least 43.5 MJ/kg, a vapor pressure in the range of 38 to 49 kPa, freezing point is less than −58° C. is provided.
Abstract translation: 高辛烷值无铅航空燃料组合物,其芳烃含量高,CHN含量至少为98重量%,氧含量小于2重量%,调节后的燃烧热为43.5兆焦耳/公斤,蒸气压在 38至49kPa,凝固点小于-58℃。
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公开(公告)号:US09388356B2
公开(公告)日:2016-07-12
申请号:US14340830
申请日:2014-07-25
Applicant: SHELL OIL COMPANY
Inventor: Timothy Michael Shea , Trevor James Davies , Michael Clifford Macknay , Hanane Belmokaddem Bennis
IPC: C10L1/16 , C10L1/182 , C10L1/223 , C10L1/19 , C10L10/10 , C10L1/10 , C10L1/02 , C10L1/18 , C10L1/22 , C10L10/14
CPC classification number: C10L10/10 , C10L1/02 , C10L1/10 , C10L1/16 , C10L1/1608 , C10L1/1616 , C10L1/18 , C10L1/1824 , C10L1/22 , C10L1/223 , C10L10/14 , C10L2200/0259 , C10L2200/0423 , C10L2270/04 , C10L2300/40
Abstract: High octane unleaded aviation fuel compositions having high aromatics content and CHN content of at least 98 wt %, less than 2 wt % of oxygen content, 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.
Abstract translation: 高辛烷值无铅航空燃料组合物,其芳族化合物含量高,CHN含量至少为98重量%,氧含量小于2重量%,调节后的燃烧热为43.5兆焦耳/公斤,蒸气压为38 至49 kPa。
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公开(公告)号:US09035114B1
公开(公告)日:2015-05-19
申请号:US14340793
申请日:2014-07-25
Applicant: SHELL OIL COMPANY
Inventor: Timothy Michael Shea , Trevor James Davies , Michael Clifford MacKnay , Hanane Belmokaddem Bennis
CPC classification number: C10L10/10 , C10L1/10 , C10L1/1608 , C10L1/1616 , C10L1/19 , C10L1/223 , C10L2200/0259 , C10L2200/0423 , C10L2270/04 , C10L2300/40
Abstract: High octane unleaded aviation fuel compositions having high aromatics content and a CHN content of at least 97.2 wt %, less than 2.8 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, freezing point is less than −58° C. is provided.
Abstract translation: 高辛烷值无铅航空燃料组合物具有高芳烃含量和CHN含量至少为97.2重量%,小于2.8重量%氧含量,T10至多75℃,T40至少为75℃, T50最多为105℃,T90为135℃以下,最终沸点低于190℃,调节后的燃烧热为43.5MJ / kg,蒸气压在该范围内 为38〜49kPa,凝固点小于-58℃。
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