Aviation fuel composition

US9528058B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9528058-B2
Application numberUS-201514588663-A
CountryUS
Kind codeB2
Filing dateJan 2, 2015
Priority dateJan 3, 2014
Publication dateDec 27, 2016
Grant dateDec 27, 2016

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  1. Title

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  2. Abstract

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  5. First independent claim

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present invention relates to an aviation fuel composition comprising an energy providing component that includes 70 to 99.9 vol. % of a hydrocarbon mixture, and 0.1 to 30 vol. % of an alcohol component selected from the group consisting of one or more Guerbet alcohols, having a number or mean value of number of carbon atoms, respectively, of equal to or less than 12, and optionally one or more aviation fuel additives. The invention further relates to a method for manufacturing the aviation fuel composition.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of combusting an aviation fuel composition, the method comprising the steps of providing a liquid phase hydrocarbon mixture selected from the group consisting of jet fuels, the liquid phase hydrocarbon mixture optionally containing one or more additives, providing an alcohol component selected from the group consisting of one or more Guerbet alcohols, having a number or mean number of carbon atoms, respectively, of equal to or less than 12, mixing the liquid phase hydrocarbon mixture with the alcohol component in a ratio within the range of from 99.9/0.1 to 70/30 with respect to vol. % to form an aviation fuel mixture, wherein the liquid phase hydrocarbon mixture and the alcohol component make up 100% of the aviation fuel mixture, and combusting the aviation fuel mixture resulting from the mixing. 2. A method consisting of: adding an alcohol component selected from the group consisting of one or more Guerbet alcohols, having a number or mean value of number of carbon atoms, respectively, of equal to or less than 12, in an amount of from 0.1 to 30 vol. %, as an energy providing component, to an aviation fuel composition comprising a hydrocarbon mixture selected from the group consisting of jet fuels with optional aviation fuel additives, in an amount of from 70 to 99.9 vol %, to form a Guerbet alcohol and hydrocarbon fuel mixture, wherein the hydrocarbon mixture has an electrical conductivity, and the Guerbert alcohol and hydrocarbon fuel mixture has a greater electrical conductivity than the conductivity of the hydrocarbon mixture; and combusting the Guerbet alcohol and hydrocarbon fuel mixture, as-is, to produce emissions having a lower amount of harmful exhaust gases than emissions resulting from combusting the hydrocarbon mixture alone. 3. The method of claim 2 , wherein the Guerbet alcohol and hydrocarbon fuel mixture comprises i) 80 to 95 vol. % of the hydrocarbon mixture, and ii) 5 to 20 vol. % of the one or more Guerbet alcohols. 4. The method of claim 2 , wherein the Guerbet alcohol and hydrocarbon fuel mixture comprises i) 85 to 95 vol. % of the hydrocarbon mixture, and ii) 5 to 15 vol. % of the one or more Guerbet alcohols. 5. The method of claim 2 , wherein the energy providing component Guerbet alcohol and hydrocarbon fuel mixture comprises i) 98 to 99.9 vol. % of the hydrocarbon mixture, and ii) 0.1 to 2 vol. % of the one or more Guerbet alcohols. 6. The method of claim 2 , wherein the hydrocarbon mixture comprises a kerosene-type fuel. 7. The method of claim 6 , wherein said hydrocarbon mixture is Jet Fuel A, Jet Fuel A-1, or a combination thereof. 8. The method of claim 2 , further comprising obtaining the one or more Guerbert alcohols, at least in part from renewable resources. 9. The method of claim 2 , wherein the one or more Guerbet alcohols are selected from the group consisting of 2-Methyl-1-Pentanol, 2-Ethyl-1-hexanol, and 2-Propyl-1-heptanol. 10. The method of claim 2 , wherein the one or more Guerbet alcohols is 2-Ethyl-1-hexanol. 11. The method of claim 2 , wherein the one or more Guerbet alcohols is a mixture of Guerbet alcohols, comprising two or more Guerbet alcohols having carbon atom numbers of 5, 6, 7, 8, 9, or 10. 12. The method of claim 2 , wherein the aviation fuel composition comprises one or more aviation fuel additives selected from the group consisting of anti-icing agents, antioxidants, corrosion inhibitors, lubricity improvers, metal deactivators, static dissipators, electrical conductivity additives, biocides, thermal stability improvers, or a mixture thereof. 13. A method comprising adding an alcohol component selected from the group consisting of one or more Guerbet alcohols, having a number or mean value of number of carbon atoms, respectively, of equal to or less than 12, in an amount of from 0.1 to 30 vol. %, to an aviation fuel composition comprising a hydrocarbon mixture selected from the group of jet fuels, in an amount of from 70 to 99.9 vol % to improve electrical conductivity of and to reduce emission of harmful exhaust gases of combustion of, the aviation fuel composition.

Assignees

Inventors

Classifications

  • for reducing smoke development · CPC title

  • Mixing, stirring of fuel components · CPC title

  • C10L1/1824Primary

    mono-hydroxy · CPC title

  • Renewables or materials of biological origin · CPC title

  • for turbines, planes, power generation · CPC title

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What does patent US9528058B2 cover?
The present invention relates to an aviation fuel composition comprising an energy providing component that includes 70 to 99.9 vol. % of a hydrocarbon mixture, and 0.1 to 30 vol. % of an alcohol component selected from the group consisting of one or more Guerbet alcohols, having a number or mean value of number of carbon atoms, respectively, of equal to or less than 12, and optionally one or m…
Who is the assignee on this patent?
Arkema France, Process Design Center BV, OBR Spólka Akcyjna
What technology area does this patent fall under?
Primary CPC classification C10L1/1824. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Dec 27 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).