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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
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：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
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：US20230383205A1
公开(公告)日：2023-11-30
申请号：US18246738
申请日：2021-10-19
Applicant: SHELL OIL COMPANY
Inventor： Hanane Belmokaddem BENNIS , Timothy Michael SHEA
CPC classification number: C10L1/223 , C10L1/1691 , C10L1/1608 , C10L2270/04 , C10L2200/043 , C10L2230/22
Abstract: An unleaded aviation fuel composition meets the requirements of the ASTM D910 specification. Furthermore, the unleaded aviation fuel compositions of the present invention exhibit reduced bladder delamination, improved materials compatibility such as reduced elastomer swelling and reduced paint staining, and improved engine endurance.
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4.发明申请公开(公告)号：US20160169790A1
公开(公告)日：2016-06-16
申请号：US14963284
申请日：2015-12-09
Applicant: SHELL OIL COMPANY
Inventor： Hanane Belmokaddem BENNIS , Timothy Michael SHEA , Michael Lane BAKER
CPC classification number: G01N17/006 , G01N11/00 , G01N17/002 , G01N17/046 , G01N33/28 , G01N33/2829
Abstract: A tester, systems and method for testing hydrocarbons are provided. The tester includes a test module supporting the component thereabout. The test module is operatively connectable to a fluid source to receive the hydrocarbon therefrom. A recirculation circuit is operatively connectable to the fluid circuit about the test module to recirculate the hydrocarbon thereabout whereby the hydrocarbon is passed over at least a portion of the component. The method involves passing the hydrocarbon over at least a portion of a plurality of the components, recirculating the hydrocarbon over the portion of each of the components, and performing a material test on each of the components.
Abstract translation: 提供了一种用于测试碳氢化合物的测试仪，系统和方法。 测试仪包括一个支持该组件的测试模块。 测试模块可操作地连接到流体源以从其接收烃。 循环回路可操作地连接到围绕测试模块的流体回路，以使烃在其周围再循环，由此烃通过部件的至少一部分。 该方法包括使烃超过多个组分的至少一部分，将烃再循环到每个组分的部分上，并对每个组分进行材料试验。
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Patent Agency Ranking
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℃。
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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
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：US20240076568A1
公开(公告)日：2024-03-07
申请号：US18262830
申请日：2022-02-23
Applicant: SHELL OIL COMPANY
Inventor： Hanane Belmokaddem BENNIS , Timothy Michael SHEA
CPC classification number: C10L1/223 , C10L1/06 , C10L1/1608 , C10L1/1824 , C10L1/1852 , C10L10/10 , C10L2200/0423 , C10L2270/04 , C10L2300/40
Abstract: An unleaded aviation fuel composition with improved octane properties has 20-35 vol. % toluene having a MON of at least 107; 2-10 vol. % aniline; from above 30 to 55 vol % of at least one alkylate or alkylate blend comprising isoparaffins 4-9 carbon atoms, 3-20 vol % C5 isoparaffins, 3-15 vol % C7 isoparaffins, and 60-90 vol % C8 isoparaffins, and less than 1 vol % C10+, based on the alkylate or alkylate blend; at least 8 vol % isopentane, 0.1-10 vol %, straight chain alkyl acetate; and 0.1-10 vol % branched chain alcohol having 4-8 carbon atoms, provided that the branched chain does not contain any t-butyl groups. The volume ratio of straight chain alkyl acetate to branched chain alcohol is in the range of 3:1 to 1:3 and the fuel composition contains less than 1 vol % of C8 aromatics.
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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
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：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
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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