US20070044374A1

US20070044374A1 - Aviation fuel cold flow additives and compositions

Info

Publication number: US20070044374A1
Application number: US11/438,816
Authority: US
Inventors: Fang Deng; William Carey; Zen-Yu Chang; Sherif Eldin; Alan Goliaszewski
Original assignee: General Electric Co
Current assignee: General Electric Co
Priority date: 2003-06-12
Filing date: 2006-05-23
Publication date: 2007-03-01
Also published as: AR044683A1; TW200516137A; WO2005001005A1; US20040250468A1

Abstract

Aviation fuel, such as jet fuel, blends and methods for improving cold flow properties of such fuels at extremely low temperatures are disclosed. Cold flow properties of, for example, JP-8 jet fuel are improved by addition to the fuel of an oil-soluble, polar nitrogen-containing compound. Demonstratable cold flow improvement of such fuels at temperatures of about −53° C. and lower is shown.

Description

CROSS REFERENCE TO RELATED APPLICATION

This application is a continuation of U.S. patent application Ser. No. 10/459,842 filed Jun. 12, 2003 and claims the benefit of the filing date of the aforesaid application under 35 USC §120.

FIELD OF THE INVENTION

The invention pertains to jet fuel blends and methods in which a cold flow enhancement agent is added to the jet fuel to improve fuel flow rates and flow characteristics at low fuel temperatures.

BACKGROUND OF THE INVENTION

It is important that aviation fuel exhibits a freeze point that is sufficiently low to allow adequate fuel flow through fuel system lines and filters to the engine. It is known that fuel temperature decreases as flight time increases and that longer duration flights typically require lower freezing point fuels than do shorter duration flights.
Additionally, high altitude flights, such as those conducted under military operational conditions, also require lower freezing point fuels than do lower altitude conventional flights. Quite obviously then, there is a need to provide freeze point depressant/cold flow enhancement aids for aviation fuels, particularly for jet fuels, which will allow for sufficient fuel flow to desired combustion locations at the extremely low fuel temperatures encountered at high altitude and long duration flights. Publications WO 01/32811 A1 and WO 01/62874 A2 discuss details of aviation fuels and the need for lowered freeze point fuel blends.
One such means of enhancing the cold flow properties of wax containing hydrocarbon fluids is via use of polymeric pour point depressant additives. For example, use of poly[(meth)acrylates] as a pour point depressant for hydrocarbon lubricating oil is taught by U.S. Pat. Nos. 5,312,884 and 5,368,761. Additionally, the use of poly[α-olefins] to improve the cold flow properties of gas oil is taught by El-Gamal et al., J. of Polym. Sci. 61, pp. 1265-1272 (1966). The use of a low molecular weight highly branched polymer of normal α-olefin to improve the cold flow properties of residual fuel oil is taught in U.S. Pat. No. 4,022,590.
The use of nitrogen compounds, such as amides, amine salts, and ammonium salts of carboxylic acids or anhydrides, or sulpho anhydrides, as an adjuvant to polymeric pour point additives in middle distillate fuels is also known to those skilled in the art. These compounds act as wax crystal modifiers and/or anti-agglomeration agents to provide enhanced cold flow properties relative to the polymeric pour point additive as a stand-alone treatment. For example, see U.S. Pat. Nos. 3,982,909; 4,211,534; and 5,516,443; and EP Application Nos. 0 261 959 A2; 0 261 957 A2; and 0 272 889 A2.
WO 01/62874 A2 teaches the use of various chemical additives, including certain copolymers of vinyl acetate and ethylene, to lower the freeze point of aviation fuels. It is further taught that certain classes of pour point additives known to those skilled in the art for treating middle distillates, such as heating oils and diesel fuels, are not necessarily effective in the treatment of aviation fuel and actually may be detrimental.

SUMMARY OF THE INVENTION

The invention is directed to a method of improving the cold flow rate of jet fuel. The method includes adding to the jet fuel an effective amount of the purpose of a cold flow rate enhancement agent (CFREA) having an oil-soluble, polar, nitrogen-containing compound. In one aspect, from 1-7,500 mg of CFREA is added to 1 liter of the jet fuel.
The present invention and its advantages over the prior art will become apparent upon reading the following detailed description and the appended claims with reference to the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

The above mentioned and other features of this invention will become more apparent and the invention itself will be better understood by reference to the following description of embodiments of the invention taken in conjunction with the accompanying drawings, wherein:
FIG. 1 is a viscosity curve illustrating the effect additives have upon the viscosity of the aviation fuel according to one embodiment of the invention.
Corresponding reference characters indicate corresponding parts throughout the views of the drawings.

DESCRIPTION OF THE INVENTION

Methods for improving the cold flow rate of aviation fuels, and jet fuels in particular are provided wherein the jet fuel is blended with a cold flow rate enhancement agent (CFREA). The CFREA is an oil-soluble, polar, nitrogen-containing compound.
The oil-soluble, polar nitrogen-containing compounds are set forth in U.S. Pat. No. 4,211,534 (Feldman) incorporated by reference herein. Basically, as stated in the '534 specification, these compounds are oil-soluble amine salts and/or amides that are generally formed by reaction of at least one molar proportion of hydrocarbyl acid having 1-4 carboxyl groups or their anhydrides, with a hydrocarbyl substituted primary, secondary, and/or tertiary amine.
In the case of the polycarboxylic acids, or anhydrides, all of the acid groups may be converted to amine salts or amides, or part of the acid groups may be left unreacted.
The term “hydrocarbyl” as defined in U.S. Pat. No. 4,211,534 includes groups that may be branched or straight chain, saturated or unsaturated, aliphatic, cycloaliphatic, aryl, alkaryl, substituted derivatives thereof and the like. Typically, these hydrocarbyl groups will consist from about 4-24 carbon atoms, more preferably 10-20 carbon atoms. In general, the resultant compound should contain sufficient hydrocarbyl content so as to be soluble in the fuel matrix.
Exemplary hydrocarbyl substituted acids and anhydrides include, but are not limited to, hexanoic acid, lauric acid, palmitic acid, steric acid, behenic acids, benzoic acids, 1,2,4,5-benzenetetracarboxylic dianhydride, 1,2-cyclohexanedicarboxylic anhydride, ethylenediaminetetraacetic dianhydride, salicylic acid, succinic acid, succinic anhydride, alkenyl succinic anhydrides, polyisobutenyl succinic anhydrides (PIBSA), phthalic acids, phthalic anhydride, naphthenic acids, naphthenic anhydrides, and the like. Particularly preferred is phthalic anhydride.
The hydrocarbyl substituted amines may be primary, secondary, or tertiary; preferably primary or secondary.
Exemplary hydrocarbyl substituted primary amines include, but are not limited to, coco amine, tallow amine, hydrogenated fatty primary amine, 2-ethylhexylamine, n-dodecyl amine, C_12-14or C_16-22tertiary alkyl primary amines from Rohm and Haas Company marketed under the trade name Primene®, mixtures thereof and the like. Particularly preferred is the C_16-22tertiary alkyl primary amine marketed by Rohm and Haas Company under the trade name Primene® JM-T.
Exemplary hydrocarbyl substituted secondary amines include, but are not limited to, dicocoalkylamine, didecylamine, dioctadecylamine, ditallowamine, dihydrogenated tallowalkylamine, mixtures thereof and the like. Particularly preferred is dihydrogenated tallowalkylamine which is commercially available from Akzo Nobel Corporation under the trade name Armeen® 2HT.
As would be understood by one skilled in the art in view of the present disclosure, it is intended that the aforementioned examples do not in any way limit the description of the nitrogen-containing compounds. Furthermore, it is to be understood that ester analogs derived from a hydrocarbyl alcohol, and hydrocarbyl sulfo acid analogs such as those derived from o-sulphobenzoic acid or its anhydride, are also within the purview of the present invention.
An especially preferred group of polar nitrogen-containing compounds are mixed amine salt/amides derived from reaction of hydrocarbyl acid (having two or more carboxyl groups) or its anhydrides as set forth above with a hydrocarbyl secondary amine. The resulting intermediate amide acid is then neutralized with a primary amine.
Generally, the preferred group of polar nitrogen containing compounds can be represented by the formula

wherein Z is a divalent organic radical, and R₁, R₂and R₃are independently chosen from C₁₀-C₄₀hydrocarbyl groups. The hydrocarbyl groups include straight or branched chain, saturated or unsaturated aliphatic, cycloaliphatic, aryl or alkylaryl moieties. These hydrocarbyl groups may contain other groups or atoms such as hydroxy groups, carbonyl groups, ester groups, oxygen, sulfur, or chlorine groups. As stated above, the hydrocarbyl groups may be on the order of C₁₀-C₄₀with the range of C₁₄-C₂₄even more preferred. The R₁, R₂, and R₃groupings can also represent mixtures of different hydrocarbyl groups. Preferably, R₃≠R₁or R₂.
The resulting compound should contain sufficient hydrocarbon content to be oil-soluble.
The preferred oil-soluble, polar nitrogen-containing compound is prepared by initial reaction of a hydrocarbyl acid or its anhydride and a secondary amine, such as the Armeen® 2HT. Then, the resulting mixed amine salt/amide is neutralized with a primary amine such as the commercially available Primene® JM-T product. Approximately equimolar amounts of the reactants are used, resulting in a mixed substituted amide/amine salt.
The most preferred polar nitrogen containing compound is an oil-soluble mixed amide/amine salt formed via reaction of equimolar amounts of phthalic anhydride with the secondary amine, Armeen® 2HT. The product of this reaction is then further reacted with an equimolar amount of the primary amine, Primene® JM-T to form benzoic acid, 2-[(bis(hydrogenated tallow alkyl)amino)carbonyl]-C₁₆-C₂₂tert-alkyl amine salt having the structural formula:

wherein R₁and R₂are mixtures of C₁₆and C₁₈hydrocarbons from the commercially available tallowamine product, and R₃is a mixture of C_18-22hydrocarbons from the commercially available Primene® JM-T product.
The CFREAs of the present invention should be added to an aviation fuel, for which improved cold flow performance is desired, in an amount effective for the purpose. In the preferred embodiment of the invention, the aviation fuel is selected from Jet Fuel A, Jet Fuel A-1, Jet Fuel B, JP-4, JP-8, and JP-8+100. Most preferably the jet fuel is a JP-8 based fuel such as neat JP-8 or the formulated JP-8+100.
Jet Fuel A and Jet Fuel A-1 are kerosene-type fuels with Jet Fuel B being a “wide cut” fuel. Jet A is used for many domestic commercial flights in the U.S. Most preferably, the CFREAs of the invention are used to increase the cold flow characteristics of military jet fuels such as JP-5, JPTS, JP-7, JP-8, and JP-8+100. JP-5 is currently used by the U.S. Navy with JP-8 and JP-8+100 used by the Air Force.

These fuel types are described in the following Table 1.

TABLE 1


U.S. Military Jet Fuel

	Year		Freeze
	Intro-		Point	Flash
Fuel	duced	Type	° C. Max	Point	Comments

JP-5	1952	kerosene	−46	60
JPTS	1956	kerosene	−53	43	High thermal stability
JP-7	1960	kerosene	−43	60
JP-8	1979	kerosene	−47	38	U.S. Air Force
JP-8 +	1998	kerosene	−47	38	U.S. Air Force
100					contains additives
					for improved thermal
					stability

JP = jet propulsion
Source: Chevron “Aviation Fuels” Technical Review.

On a 100% actives basis, the CFREA is preferably added to the jet fuel in an amount of about 1-7,500 mg/L of the jet fuel. More preferably, the CFREA is added in an amount of between about 200-5,000 mg/L, most preferably about 4,000 mg/L. The jet fuel/CFREA blend is capable of improving the cold flow rate of jet fuel, specifically, JP-8 based jet fuel, at fuel temperatures on the order of about −53° C. and below. Experimental results have indicated that the CFREAs when blended with JP-8 based jet fuel in accordance with the invention improve cold flow rates of the fuel so that they are, as measured in accordance with Table 2 and the test system described, on the order of about 0.60 (g/s) and greater at fuel temperatures of about −53° C. and lower.
The CFREAs of the invention can be employed in combination with conventional fuel additives such as dispersants, antioxidants, and metal deactivators. Such additives are known to those skilled in the art, for example see U.S. Pat. Nos. 5,596,130 and 5,614,081.
The invention will be described further in conjunction with the following examples that are included for illustrative purposes only and should not be construed to limit the invention.

EXAMPLE 1

Preparation of Benzoic acid, 2-[(bis(hydrogenated tallow alkyl)amino)carbonyl]-C₁₆-C₂₂tert-alkyl amine salt

To a four-necked reaction flask equipped with a mechanical overhead stirrer, thermocouple, reflux condenser, nitrogen sparge tube, addition port with septum and a heating mantle was added phthalic anhydride (99%, 5.0 g, 0.03342 mole) and Armeen® 2HT (17.0 g, 0.03342 mole amine). The resulting wax mixture was then heated to 90° C. under nitrogen with mixing and held for four hours. Primene® JM-T (10.9 g, 0.03342 mole amine) was then added to the reactor at 90° C. over an eight-minute period, after which the batch was maintained at 90° C. for an additional four hours before cooling to room temperature to yield a wax like material. This was then diluted in Aromatic 100 to yield a 25 wt % solution of the nitrogen-containing compound.

EXAMPLE 2

This preparation was a scaleup of Example 1 (basis: phthalic anhydride, 99%, 344.74 g, 2.30 mole) except the hold times after the Armeen® 2HT and Primene® JM-T additions were decreased to one-hour each.

Cold Flow Additive Testing

JP-8 jet fuel was then treated with a known amount of additive solution and subjected to cold flow testing. Cold flow tests were conducted utilizing a Cold Additive Screening Test (CAST) and low temperature viscometer apparatus.
In general, the CAST apparatus consists of two 500 ml flasks, one at atmospheric pressure and one sealed, connected via a ¼″ Teflon tube. A known amount of fuel is charged to the flask at atmospheric pressure, and the apparatus is cooled to the desired test temperature in an environmental chamber. Once cooled to the desired temperature vacuum (2″ Hg) is applied to the sealed flask. The effectiveness of an additive is determine by measuring the time it takes for the fuel to flow to the sealed flask, and the amount of fuel remaining in the atmospheric flask after the fuel flow ceases.

Screening results of the additives of the present invention in the CAST apparatus are provided in Table 2 below. At approximately −53° C. the untreated fuel has solidified and exhibited 100% holdup and essentially no fuel flow. Addition of the additives of the present invention to the fuel dramatically improved the cold flow properties at approximately −53° C. as evidenced by a substantial decrease in hold up and increase in fuel flow.

TABLE 2


CAST Testing Results

	Conc.	Fuel Temp	Holdup	Flow Rate
Additive 1	(mg/L)*	(° C.)	(%)	(g/s)

None	N/A	−53.5	100	N/A
Example 1	8000	−52.7	10	1.34
Example 1	16000	−53.3	9	0.93
Example 2	12000	−57.8	25	0.47
Example 2	12000	−55.1	7	0.85
Example 2	14000	−57.0	13	0.83
Example 2	14000	−55.2	10	1.06
Example 2	16000	−57.1	8	0.82
Example 2	16000	−55.2	8	0.93

Low temperature viscosity studies of the treated fuel were carried out using a scanning Brookfield Viscometer in the temperature range of −5° C. to −60° C. as described by S. Zabarnick and M. Vangsness, Petroleum Chemistry Preprints 2002, 47(3), pp. 243-246 (2002). The results of this testing are given in Table 2. The knee temperature is defined as the temperature at which a rapid viscosity increase occurs due to crystal formation. It is desirable to have the “knee temperature” for a treated fuel to be shifted to a lower temperature relative to the neat fuel. It is also highly desirable to minimize the rate of viscosity increase as the fuel is cooled below the knee temperature.
Table 3 summarizes the results for the low temperature viscosity studies. The letter designation corresponds to the viscosity curve for that treatment in the companion graph presented in FIG. 1. It can be seen from the data presented that the additives of the present invention lower the knee temperature of the fuel. Additionally, as shown in FIG. 1, addition of the additives of the invention significantly reduces the rate of viscosity increase. The effect is pronounced to the extent that at higher additive levels there was no obvious knee temperature (curve “C” of FIG. 1).

TABLE 3

Low Temperature Viscosity Results-Knee

Temperature in JP-8 Fuel

Letter Additive 1 Conc. (mg/L)* Knee Temp (° C.)

A None N/A −52.0

B Example 2 12000 −55.2

C Example 2 16000 None Observed
While the specification above has been drafted to include the best mode of practicing the invention as required by the patent statutes, the invention is not to be limited to that best mode or to other specific embodiments set forth in the specification. The breadth of the invention is to be measured only by the literal and equivalents constructions applied to the appended claims.

Claims

1. Method of improving the cold flow rate of jet fuel comprising adding to said jet fuel an effective amount of the purpose of a cold flow rate enhancement agent (CFREA) comprising an oil-soluble, polar, nitrogen-containing compound.

2. Method as recited in claim 1 comprising adding from a 1-7,500 mg of said CFREA to said jet fuel, based upon 1 liter of said jet fuel.

3. Method as recited in claim 1 wherein said jet fuel is a JP-8 based jet fuel.

4. Method as recited in claim 1 wherein said oil-soluble, polar nitrogen compound comprises an amine salt or amide.

5. Method as recited in claim 4, wherein said oil-soluble, polar nitrogen compound comprises a reaction product formed from reaction of a hydrocarbyl acid having two or more carboxyl groups or anhydride thereof, and a hydrocarbyl secondary amine followed by neutralization of the resulting product with a hydrocarbyl primary amine.

6. Method as recited in claim 1 wherein said oil-soluble, polar nitrogen compound is benzoic acid, 2-[(bis(hydrogenated tallow alkyl)amino)carbonyl]-C₁₆-C₂₂tert-alkyl amine salt.

7. Method as recited in claim 2 wherein said oil-soluble, polar nitrogen-containing compound is represented by the formula

wherein Z is a divalent organic radical, and R₁, R₂, and R₃are independently chosen from C₁₀-C₄₀hydrocarbyl groups.

8. Method as recited in claim 2 wherein said oil-soluble, polar, nitrogen-containing compound is formed from a reaction of a hydrocarbyl acid having from about 1 to about 4 carboxyl groups or anhydrides thereof with a hydrocarbyl substituted primary, secondary, or tertiary amine.

9. Method as recited in claim 8 wherein said hydrocarbyl acid or anhydride and hydrocarbyl substituted primary, secondary, and tertiary amines each have from about 4 to about 24 carbon atoms.

10. Method as recited in claim 9 wherein said hydrocarbyl acid or anhydride and hydrocarbyl substituted primary, secondary, and tertiary amines each have from about 10-24 carbon atoms.

11. Method as recited in claim 3 wherein said JP-8 jet fuel is subjected to temperatures of −53.0° C. and lower.