Grafted polymer drag-reducing agents, grafted polymer fuel additives and production methods therefor
The invention includes a method of reducing drag in a pipeline and/or improving the combustion efficiency of a fuel burning device by adding a grafted polymer to a hydrocarbon product. The invention also includes a method of improving the combustion efficiency of a gasoline engine by adding a grafted polymer to fuel and combusting the fuel within the gasoline engine, the grafted polymer having a viscoelastic effect in gasoline in the gasoline engine to generally correspond to a duration of the intake stroke/compression stroke/fuel burn sequence in a gasoline engine.
1. A method of improving the combustion efficiency of a fuel burning device, the method comprising:
introducing a liquid hydrocarbon product and a grafted polymer to a fuel burning device, the hydrocarbon product and grafted polymer having been transported through a pipeline prior to introduction to the fuel burning device, wherein the grafted polymer is dispersed in the hydrocarbon product and has a polymeric backbone and grafted branches extending from the backbone; the grafted polymer further having a structure that unzips upon thermal degradation; and
combusting the hydrocarbon product and the grafted polymer in the fuel burning device, the grafted polymer increasing the combustion efficiency of the fuel burning device.
2. The method of claim 1 , wherein the hydrocarbon product is crude.
3. The method of claim 1 , wherein the hydrocarbon product is a finished fuel.
4. The method of claim 1 , wherein the grafted polymer is synthesized by grafting polymer branches on preformed polymers.
5. The method of claim 1 , wherein the grafted polymer is synthesized by cryogrinding a polymer backbone at cryogenic temperatures and reacting the cryoground polymer backbone with a monomer or second polymer.
6. The method of claim 5 , wherein the polymer backbone is an elastomer which degrades thermally by unzipping.
7. The method of claim 5 , wherein the polymer backbone is PIB.
8. The method of claim 5 , wherein the monomer is selected from the group consisting of methyl methacrylate, isobutylene, ethyl methacrylate, 2-hydroxyethyl methacrylate, styrene, and alpha methylstyrene.
9. The method of claim 1 , wherein the fuel burning device is selected from the group consisting of internal combustion engines, furnaces, and boilers.
10. The method of claim 1 , wherein the hydrocarbon product includes an aviation turbine fuel.
11. A method of reducing drag in a pipeline, the method comprising:
providing a grafted polymer having a polymeric backbone and grafted branches extending from the backbone, the grafted polymer further having a structure that unzips upon thermal degradation;
introducing the grafted polymer in a liquid hydrocarbon product pipeline, such that the grafted polymer is dispersed in the liquid hydrocarbon product; and
transporting the hydrocarbon product and the grafted polymer in the pipeline, the grafted polymer reducing the drag in the pipeline.
12. The method of claim 11 , wherein the hydrocarbon product is crude.
13. The method of claim 11 , wherein the hydrocarbon product is a finished fuel.
14. The method of claim 11 , wherein the grafted polymer is synthesized by grafting polymer branches on preformed polymers.
15. The method of claim 11 , wherein the grafted polymer is synthesized by cryogrinding a polymer backbone at cryogenic temperatures and reacting the cryoground polymer backbone with a monomer or second polymer.
16. The method of claim 15 , wherein the polymer backbone is an elastomer which degrades thermally by unzipping.
17. The method of claim 15 , wherein the polymer backbone is PIB.
18. The method of claim 15 , wherein the monomer is selected from the group consisting of methyl methacrylate, isobutylene, ethyl methacrylate, 2-hydroxyethyl methacrylate, styrene, and alpha methylstyrene.
19. The method of claim 11 , further including combusting the hydrocarbon product and the grafted polymer in a fuel burning device, wherein the fuel burning device is selected from the group consisting of internal combustion engines, furnaces, and boilers.
20. The method of claim 11 , wherein the hydrocarbon product includes an aviation turbine fuel.