公开(公告)号：US20150113862A1

公开(公告)日：2015-04-30

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

IPC: C10L1/223 ,  C10L1/16 ,  C10L1/19

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。

公开(公告)号：US20150175920A1

公开(公告)日：2015-06-25

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: C10L10/10 ,  C10L10/14 ,  C10L1/16 ,  C10L1/22 ,  C10L1/18

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。

公开(公告)号：US20150159106A1

公开(公告)日：2015-06-11

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

IPC: C10L10/10 ,  C10L1/10

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℃。

公开(公告)号：US20150175921A1

公开(公告)日：2015-06-25

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: C10L10/10 ,  C10L10/14 ,  C10L1/22 ,  C10L1/18 ,  C10L1/16

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。

公开(公告)号：US20150113861A1

公开(公告)日：2015-04-30

申请号：US14340911

申请日：2014-07-25

Applicant: SHELL OIL COMPANY

Inventor： Timothy Michael SHEA ,  Trevor James DAVIES ,  Michael Clifford MACKNAY

IPC: C10L10/10 ,  C10L10/14

CPC classification number: C10L10/10 ,  C10L1/02 ,  C10L1/10 ,  C10L1/16 ,  C10L1/1608 ,  C10L1/1616 ,  C10L1/19 ,  C10L1/223 ,  C10L10/14 ,  C10L2200/0259 ,  C10L2200/0423 ,  C10L2270/023 ,  C10L2270/04 ,  C10L2300/40

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 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 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 最终沸点小于210℃，调节燃烧热为43.5MJ / kg，蒸汽压在38至49kPa范围内，凝固点小于-58℃。

公开(公告)号：US20150113866A1

公开(公告)日：2015-04-30

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

IPC: C10L10/10

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℃。

公开(公告)号：US20150113865A1

公开(公告)日：2015-04-30

申请号：US14340731

申请日：2014-07-25

Applicant: SHELL OIL COMPANY

Inventor： Timothy Michael SHEA ,  Michael Clifford MACKNAY ,  Hanane Belmokaddem BENNIS

IPC: C10L1/223 ,  C10L1/182

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。