公开(公告)号：US20230028449A1

公开(公告)日：2023-01-26

申请号：US17786230

申请日：2020-12-28

Applicant: SHELL OIL COMPANY

Inventor： Anton HUNT ,  Cynthia Natalie GINESTRA ,  Joanna Margaret BAULDREAY ,  Paul Franciscus BOGERS ,  Elise Marie MINER

IPC: C06B47/12 ,  C06D5/08

Abstract: The present disclosure relates to a rocket propellant composition comprising (a) a liquid oxygen; and (b) a hydrocarbon mixture comprising: (i) a hydrogen content from about 14.0 mass % to about 16.0 mass %, by mass of the hydrocarbon mixture; (ii) a kinematic viscosity of from about 5 mm2/s to about 8 mm2/s at a temperature ranging from about −35° C. to about −33° C.; and (iii) a sulfur content of from about 0 ppm to about 0.1 ppm, by mass of 0 the hydrocarbon mixture.

公开(公告)号：US20180230393A1

公开(公告)日：2018-08-16

申请号：US15385994

申请日：2016-12-21

Applicant: SHELL OIL COMPANY

Inventor： Joanna Margaret BAULDREAY ,  Brice Nathaniel DALLY ,  Gregory HEMIGHAUS ,  Cynthia Natalie GINESTRA ,  Anton HUNT

IPC: C10L1/16 ,  C10L10/02 ,  C10L1/04

CPC classification number: C10L1/1691 ,  C10L1/04 ,  C10L10/02 ,  C10L10/06 ,  C10L2200/043 ,  C10L2270/04

Abstract: By blending a quantity of synthetic cyclo-paraffinic kerosene fuel blending component comprising at least 99.5 mass % of carbon and hydrogen content and at least 50 mass % of cyclo-paraffin into kerosene base fuel, kerosene based-propulsion fuels can be upgraded to higher quality kerosene based-propulsion fuels such as jet fuel or rocket fuel to meet certain specification and/or increase volumetric energy content of the propulsion fuel.

公开(公告)号：US20180230392A1

公开(公告)日：2018-08-16

申请号：US15385982

申请日：2016-12-21

Applicant: SHELL OIL COMPANY

Inventor： Cynthia Natalie GINESTRA ,  Brice Nathaniel DALLY ,  Joanna Margaret BAULDREAY ,  Gregory HEMIGHAUS

IPC: C10L1/16 ,  C10L10/02 ,  C10L10/06 ,  C10L1/04

CPC classification number: C10L1/1691 ,  C10G2300/1051 ,  C10G2300/1081 ,  C10L1/04 ,  C10L10/02 ,  C10L10/06 ,  C10L2200/043 ,  C10L2270/04

Abstract: By blending a quantity of synthetic cyclo-paraffinic kerosene fuel blending component comprising at least 99.5 mass % of carbon and hydrogen content and at least 50 mass % of cyclo-paraffin into kerosene base fuel, kerosene based-propulsion fuels can be upgraded to higher quality kerosene based-propulsion fuels such as jet fuel or rocket fuel to meet certain specification and/or increase volumetric energy content of the propulsion fuel.

公开(公告)号：US20170175019A1

公开(公告)日：2017-06-22

申请号：US15386023

申请日：2016-12-21

Applicant: SHELL OIL COMPANY

Inventor： Cynthia Natalie GINESTRA ,  Brice Nathaniel DALLY ,  Joanna Margaret BAULDREAY ,  Gregory HEMIGHAUS

IPC: C10L1/04 ,  F02C3/24 ,  F02K7/00

CPC classification number: C10L1/04 ,  C10L2200/043 ,  C10L2270/04 ,  C10L2290/24 ,  F02C3/24 ,  F02K7/00 ,  F05D2220/323

Abstract: By blending a quantity of synthetic cyclo-paraffinic kerosene fuel blending component comprising at least 99.5 mass % of carbon and hydrogen content and at least 50 mass % of cyclo-paraffin into kerosene base fuel, kerosene based-propulsion fuels can be upgraded to higher quality kerosene based-propulsion fuels such as jet fuel or rocket fuel to meet certain specification and/or increase volumetric energy content of the propulsion fuel.

公开(公告)号：US20160326448A1

公开(公告)日：2016-11-10

申请号：US15144855

申请日：2016-05-03

Applicant: SHELL OIL COMPANY

Inventor： Joanna Margaret BAULDREAY ,  Cynthia Natalie GINESTRA ,  Gregory HEMIGHAUS ,  Brice Nathaniel DALLY ,  Paul George BLOMMEL

IPC: C10L10/02 ,  F02C7/30 ,  F02C9/40 ,  C10L1/04

CPC classification number: C10L10/02 ,  C10L1/04 ,  C10L2200/043 ,  C10L2270/04 ,  C10L2290/24 ,  F02C7/30 ,  F02C9/40 ,  F05D2220/323 ,  F05D2300/70

Abstract: Reduced emissions in a jet fuel having aromatics content can be achieved by incorporating a quantity of an aromatic kerosene fuel blending component, preferably a bio-derived synthetic aromatic kerosene, comprising at least 90 wt. % of aromatics, less than 10 wt. % of indanes and tetralins and less than 1 wt. % of naphthalene into a jet fuel in a manner to meet the aromatic content specification for jet fuels. A jet fuel having aromatics content having reduced number-based nvPM emissions compared to equivalent total aromatics content petroleum-derived kerosene jet fuel is obtained.

Abstract translation: 具有芳族化合物含量的喷气燃料中的排放减少可以通过加入一定量的芳香族煤油燃料调和组分（优选生物衍生的合成芳香族煤油）来实现，该组合物包含至少90wt。 ％的芳族化合物，小于10wt。 ％的茚满和四氢化萘并且小于1wt。 ％的萘以符合喷气燃料的芳族化合物含量的方式进入喷气燃料。 获得了与等效的总芳族化合物含量相比，具有芳烃含量降低的基于数量的nvPM排放的喷气燃料与石油衍生的煤油喷射燃料。