Hydrocarbon composition for use in compression-ignition engines
    1.
    发明授权
    Hydrocarbon composition for use in compression-ignition engines 有权
    用于压燃式发动机的烃组合物

    公开(公告)号:US08075761B2

    公开(公告)日:2011-12-13

    申请号:US11280508

    申请日:2005-11-15

    IPC分类号: C10L1/08

    CPC分类号: C10L1/08 Y10S208/95

    摘要: The invention provides a hydrocarbon composition for use in CI engines, said composition comprising a blend of hydrocarbons derived from a LTFT and from a HTFT process, said LTFT derived hydrocarbon being blended with said HTFT derived hydrocarbon in a volumetric ratio of from 1:20 to 20:1. The invention further provides a process for the production of the hydrocarbon composition and a the fuel composition including, in addition to the hydrocarbon composition, one or more component selected from the group including a crude oil derived diesel fuel, a crude oil derived naphtha, a lubricant or light cycle oil (LCO).

    摘要翻译: 本发明提供用于CI发动机的烃组合物,所述组合物包含衍生自LTFT和HTFT方法的烃的共混物,所述LTFT衍生的烃与所述HTFT衍生的烃以1:20至 20:1。 本发明还提供一种生产该烃组合物的方法和一种燃料组合物,该组合物除烃组合物外还包含一种或多种选自以下的组分:原油衍生的柴油,原油衍生的石脑油, 润滑剂或轻质循环油(LCO)。

    Hydrocarbon composition for use in compression-lgnition engines
    2.
    发明申请
    Hydrocarbon composition for use in compression-lgnition engines 有权
    用于压缩发动机的烃组合物

    公开(公告)号:US20060122442A1

    公开(公告)日:2006-06-08

    申请号:US11280508

    申请日:2005-11-15

    IPC分类号: C10L1/16

    CPC分类号: C10L1/08 Y10S208/95

    摘要: The invention provides a hydrocarbon composition for use in CI engines, said composition comprising a blend of hydrocarbons derived from a LTFT and from a HTFT process, said LTFT derived hydrocarbon being blended with said HTFT derived hydrocarbon in a volumetric ratio of from 1:20 to 20:1. The invention further provides a process for the production of the hydrocarbon composition and a the fuel composition including, in addition to the hydrocarbon composition, one or more component selected from the group including a crude oil derived diesel fuel, a crude oil derived naphtha, a lubricant or light cycle oil (LCO).

    摘要翻译: 本发明提供用于CI发动机的烃组合物,所述组合物包含衍生自LTFT和HTFT方法的烃的共混物,所述LTFT衍生的烃与所述HTFT衍生的烃以1:20至 20:1。 本发明还提供一种生产该烃组合物的方法和一种燃料组合物,该组合物除烃组合物外还包含一种或多种选自以下的组分:原油衍生的柴油,原油衍生的石脑油, 润滑剂或轻质循环油(LCO)。

    PROCESS FOR THE PRODUCTION OF COMPRESSION IGNITION ENGINE, GAS TURBINE, AND FUEL CELL FUEL AND COMPRESSION IGNITION ENGINE, GAS TURBINE, AND FUEL CELL FUEL BY SAID PROCESS
    4.
    发明申请
    PROCESS FOR THE PRODUCTION OF COMPRESSION IGNITION ENGINE, GAS TURBINE, AND FUEL CELL FUEL AND COMPRESSION IGNITION ENGINE, GAS TURBINE, AND FUEL CELL FUEL BY SAID PROCESS 审中-公开
    压缩点火发动机,燃气轮机和燃料电池燃料和压缩点火发动机,燃气涡轮机和燃料电池燃料的生产过程

    公开(公告)号:US20080076949A1

    公开(公告)日:2008-03-27

    申请号:US11945161

    申请日:2007-11-26

    IPC分类号: C10L1/16

    CPC分类号: C10L1/08 C10G2/30 F02B1/12

    摘要: The invention provides a Fischer-Tropsch derived compression ignition engine, gas turbine, and fuel cell fuel which is interchangeably useable in compression ignition engines, gas turbines, and fuel cells, said fuel selected from a substantially C5 to C9 cut, a substantially C5 to C9 cut blended with a substantially C9 to C14 cut, a substantially C5 to C9 cut blended with a substantially C9 to C14 cut and a substantially C14 to C22 cut, and a substantially C5 to C9 cut blended with a substantially C14 to C22 cut. The invention extends to a process for preparing said fuel and the use of such a fuel in a CI engine, and HCCI engine, a turbine, and/or a fuel cell.

    摘要翻译: 本发明提供了一种费 - 托衍生的压燃式发动机,燃气轮机和燃料电池燃料,其可在压燃式发动机,燃气轮机和燃料电池中互换使用,所述燃料选自基本上为C5至C9的切割,基本为C5至 C9切割与基本上C9至C14切割混合,基本上C5至C9切割与基本上C9至C14切割并基本上C14至C22切割混合,并且基本上C 5至C 9切割与基本上C14至C22切割共混。 本发明延伸到制备所述燃料的方法和在CI发动机,HCCI发动机,涡轮机和/或燃料电池中使用这种燃料。

    Low sulphur diesel fuel and aviation turbine fuel
    5.
    发明授权
    Low sulphur diesel fuel and aviation turbine fuel 有权
    低硫柴油和航空涡轮燃料

    公开(公告)号:US08183419B2

    公开(公告)日:2012-05-22

    申请号:US12132590

    申请日:2008-06-03

    IPC分类号: C10L1/10

    摘要: A process for the production of a synthetic low sulphur diesel fuel and a low soot emission aviation fuel is disclosed. The process includes fractionation of a Low Temperature Fischer-Tropsch feedstock into a light kerosene fraction and a heavier diesel fraction in a volumetric ratio of at least 1:2 to form the light kerosene fraction having a smoke point greater than 50 mm, a freezing point of below −47° C., a BOCLE lubricity wear scar less than 0.85 mm, and an anti-oxidant additiveless thermal stability tube deposit rating at 260° C. of less than 1 useable as a low soot emission aviation fuel and/or an aviation fuel blend stock, and the heavier diesel fraction having CFPP according to IP309 of below −5° C., a density@20° C. of at least 0.78 kg/l, and a viscosity@40° C. of above 2 cSt useable as a synthetic low sulphur diesel fuel and/or a diesel fuel blend stock.

    摘要翻译: 公开了生产合成低硫柴油燃料和低烟灰排放航空燃料的方法。 该方法包括将低温费 - 托原料分馏成轻质煤油馏分和至少1:2的体积比的较重柴油馏分以形成烟点大于50毫米的轻煤油馏分,凝固点 低于-47℃,BOCLE润滑性磨损痕迹小于0.85mm,并且在260℃下的抗氧化剂无添加剂热稳定性管沉积物评级小于1,可用作低烟灰发射航空燃料和/或 航空燃料混合料,以及具有低于-5℃的IP309的CFPP的较重的柴油馏分,至少0.78kg / l的20℃的密度和高于2cC的40℃的粘度 可用作合成低硫柴油和/或柴油混合原料。

    LOW SULPHUR DIESEL FUEL AND AVIATION TURBINE FUEL
    7.
    发明申请
    LOW SULPHUR DIESEL FUEL AND AVIATION TURBINE FUEL 有权
    低硫柴油燃料和航空涡轮燃料

    公开(公告)号:US20090013590A1

    公开(公告)日:2009-01-15

    申请号:US12132590

    申请日:2008-06-03

    IPC分类号: C10L1/18

    摘要: A process for the production of a synthetic low sulphur diesel fuel and a low soot emission aviation fuel is disclosed. The process includes fractionation of a Low Temperature Fischer-Tropsch feedstock into a light kerosene fraction and a heavier diesel fraction in a volumetric ratio of at least 1:2 to form the light kerosene fraction having a smoke point greater than 50 mm, a freezing point of below −47° C., a BOCLE lubricity wear scar less than 0.85 mm, and an anti-oxidant additiveless thermal stability tube deposit rating at 260° C. of less than 1 useable as a low soot emission aviation fuel and/or an aviation fuel blend stock, and the heavier diesel fraction having CFPP according to IP309 of below −5° C., a density@20° C. of at least 0.78 kg/l, and a viscosity@40° C. of above 2 cSt useable as a synthetic low sulphur diesel fuel and/or a diesel fuel blend stock.

    摘要翻译: 公开了生产合成低硫柴油燃料和低烟灰排放航空燃料的方法。 该方法包括将低温费 - 托原料分馏成轻质煤油馏分和至少1:2的体积比的较重柴油馏分以形成烟点大于50毫米的轻煤油馏分,凝固点 低于-47℃,BOCLE润滑性磨损痕迹小于0.85mm,并且在260℃下的抗氧化剂无添加剂热稳定性管沉积物评级小于1,可用作低烟灰发射航空燃料和/或 航空燃料混合料,以及具有低于-5℃的IP309的CFPP的较重的柴油馏分,至少0.78kg / l的20℃的密度和高于2cC的40℃的粘度 可用作合成低硫柴油和/或柴油混合原料。

    Process for the production of compression ignition engine, gas turbine, and fuel cell fuel and compression ignition engine, gas turbine, and fuel cell fuel by said process
    8.
    发明申请
    Process for the production of compression ignition engine, gas turbine, and fuel cell fuel and compression ignition engine, gas turbine, and fuel cell fuel by said process 审中-公开
    通过所述方法生产压燃式发动机,燃气轮机和燃料电池燃料和压燃式发动机,燃气轮机和燃料电池燃料的方法

    公开(公告)号:US20060243640A1

    公开(公告)日:2006-11-02

    申请号:US11406016

    申请日:2006-04-18

    IPC分类号: C10L1/04 C07C27/06

    CPC分类号: C10L1/04 C10L1/06

    摘要: The invention provides a Fischer-Tropsch derived compression ignition engine, gas turbine, and fuel cell fuel which is interchangeably useable in compression ignition engines, gas turbines, and fuel cells, said fuel selected from a substantially C5 to C9 cut, a substantially C5 to C9 cut blended with a substantially C9 to C14 cut, a substantially C5 to C9 cut blended with a substantially C9 to C14 cut and a substantially C14 to C22 cut, and a substantially C5 to C9 cut blended with a substantially C14 to C22 cut. The invention extends to a process for preparing said fuel and the use of such a fuel in a CI engine, and HCCI engine, a turbine, and/or a fuel cell.

    摘要翻译: 本发明提供了一种费 - 托衍生的压燃式发动机,燃气轮机和燃料电池燃料,其可在压燃式发动机,燃气轮机和燃料电池中互换使用,所述燃料选自基本上为C5至C9的切割,基本为C5至 C9切割与基本上C9至C14切割混合,基本上C5至C9切割与基本上C9至C14切割并基本上C14至C22切割混合,并且基本上C 5至C 9切割与基本上C14至C22切割共混。 本发明延伸到制备所述燃料的方法和在CI发动机,HCCI发动机,涡轮机和/或燃料电池中使用这种燃料。

    Low sulphur diesel fuel and aviation turbine fuel
    10.
    发明授权
    Low sulphur diesel fuel and aviation turbine fuel 有权
    低硫柴油和航空涡轮燃料

    公开(公告)号:US07390397B2

    公开(公告)日:2008-06-24

    申请号:US11256285

    申请日:2005-10-19

    IPC分类号: B01D3/14

    摘要: A process for the production of a synthetic low sulphur diesel fuel and a low soot emission aviation fuel is disclosed. The process includes fractionation of a Low Temperature Fischer-Tropsch feedstock into a light kerosene fraction and a heaver diesel fraction in a volumetric ratio of at least 1:2 to form the light kerosene fraction having a smoke point greater than 50 mm, a freezing point of below −47° C., a BOCLE lubricity wear scar less than 0.85 mm, and an anti-oxidant additiveless thermal stability tube deposit rating at 260° C. of less than 1 useable as a low soot emission aviation fuel and/or an aviation fuel blend stock, and the heavier diesel fraction having CFPP according to IP309 of below −5° C., a density@20° C. of at least 0.78 kg/l, and a viscosity@40° C. of above 2 cSt useable as a synthetic low sulphur diesel fuel and/or a diesel fuel blend stock.

    摘要翻译: 公开了生产合成低硫柴油燃料和低烟灰排放航空燃料的方法。 该方法包括将低温费 - 托原料分馏成轻质煤油馏分和至少1:2的体积比的海弗柴油馏分以形成烟点大于50毫米的轻煤油馏分,凝固点 低于-47℃,BOCLE润滑性磨损痕迹小于0.85mm,并且在260℃下的抗氧化剂无添加剂热稳定性管沉积物评级小于1,可用作低烟灰发射航空燃料和/或 航空燃料混合料,以及具有低于-5℃的IP309的CFPP的较重的柴油馏分,至少0.78kg / l的20℃的密度和高于2cC的40℃的粘度 可用作合成低硫柴油和/或柴油混合原料。