Patent Grant
11020933
As crude oil prices soar, energy efficiency in the transportation sector has become especially important. Accordingly, there a very high demand for modern engines and drive trains to improve fuel economy and energy efficiency by reducing frictional losses at various contact interfaces. The present invention may have the benefit of improving fuel economy and energy efficiency by reducing friction between engine components under various operating conditions.
One aspect of this invention relates to incorporating surface texture designs onto engine component surfaces, which may significantly reduce frictional losses for high-contact pressure regions. Previously, surface texturing had only been used commercially in applications involving two flat surfaces or two conformal surfaces. Specific applications with such surfaces have included, for example, water pump seals in automobiles and seals in pumps. Those applications generally involve high speed, low-load operating conditions.
The basic principles of surface texture designs as reflected in
(Regime I) hydrodynamic lubrication regime (“HD”) (high-speed and low-load) —the effects of textured surfaces are a) enhanced hydrodynamic lubrication with dimples or grooves; b) cavitational pressure lift mechanism under certain conditions; and c) reverse flow induced by dimples or grooves.
(Regime II) elastohydrodynamic lubrication regime (“EHL”) (increasing load from HD regime) —a) not all dimple sizes and shapes would reduce friction (they actually increase friction if not implemented properly). The dimples have to induce squeezed film lubrication (wedge effect) or partial kinetic hydrostatic lift lubrication mechanism to effect friction reduction. Therefore, the angle of the dimple edge with respect to horizontal plane, bottom shape, dimple spacing in both x and y directions are important, and potential cavitation lift could also be one of the mechanisms to effect friction reduction.
(Regime III) boundary lubrication regime (much lower speed and higher load, so the two sliding surfaces touch one another) —the dimples operating in this regime require hydrostatic pressure to be generated by the trapped lubricant to enable the onset of hydrodynamic film lubrication mechanism.
There have traditionally been two common recognitions in the texturing community based on experimental results: 1) only one of the two sliding surfaces should be textured; 2) texture only works in conformal contacting surfaces (such as journal beatings, seals, but will not work on curved surface sliding against another curve surface). The present invention circumvents these two restrictions by selecting the shape and sizing the dimples smaller than the contact width to function properly under these conditions.
Additionally, significant technical barriers for introducing textures to engines have previously existed relating to the lack of low-cost fabrication techniques, which could allow for the application of textures over large areas of surface including, for example, large automotive and diesel engine components, which are made of tool steel or bearing steel, sometimes with additional surface treatment to enhance durability. Accordingly, another aspect of this invention relates to the surface texture fabrication procedure. Conventional microlithography uses rigid masks (typically glass or Mylar) (usually at several millimeter dimensions) and is not capable of fabricating textures on curved surfaces due to the need for a UV exposure processing step. Alternative techniques such as embossing, nanomechanical scratching, nanoprinting, and laser ablation techniques 1) are very expensive; 2) are time consuming; 3) potentially damage the surface resulting in fatigue strength degradation; and 4) are not capable of fabricating complex mixed shape feature patterns in one processing step. Therefore, one of the crucial barriers to the potential widespread application of surface texturing to engine components has been the lack of large area flexible masks that are capable of wrapping around large automotive and diesel engine components for lithography and electrochemical etching.
Another aspect of this invention attempts to resolve the wear problem of textured surface running in occasional boundary lubrication regime by adding a tough thin protective diamond dike-carbon film (“DLC”), specially formulated and processed to have unique combination of physical, chemical, and nanomechanical properties for this application. DLC films can have many variations and traditional DLC films that have been tested do not work under this application. DLC films generally have lower reactivity towards traditional lubricants (containing typical phosphorus antiwear additives such as zine dialkyl dithiophosphate or trecreyl phosphates). According to an embodiment of this invention, a bonded chemical film contains chemistry that reacts with the DLC film so that the DLC film carries its own lubricant chemistry to make the combination highly durable. At the same time, DLC with bonded chemical films demonstrate highly effective friction reduction in engine components and make the surface textures long lasting. This aspect of the invention can also be used to protect surfaces of non-automotive components as well.
DLC, as used herein, is a generic term describing a class of compositions. There can be thousands of diamond-like carbon films with differing and varying properties and thicknesses, processing techniques (different gaseous atmospheres during deposition), and differing degrees of “filtering” of raw materials vapors and particles. The properties of the DLC film depend strongly on processing methods, processing conditions, the gases used in the sputtering process, and the thickness of the film. DLC films include nanocrystalline diamond particles dispersed in an amorphous carbon matrix. The number of diamond particles in a particular DLC film can be measured using Laser Raman Spectroscopy, as SP3 peak, or any other suitable method. The graphitic matrix is represented by the SP2 peak. The term SP3/SP2 reflects the hardness and toughness of the film. Not all DLC films can protect textured surfaces. An embodiment of this invention relates to a DLC film that can be used to protect textured surfaces.
The present invention relates to techniques for lowering friction between moving surfaces of, for example, in an internal combustion engine. The present invention generally is directed to reducing friction between parts of an internal combustion engine by introducing texture modifications in the surfaces that come in contact with each other. In a preferred embodiment, these surfaces are engine piston rings, cylinder liners, and their respective pins and bearings. In one embodiment, the surface textures are depressions of specific sizes, shapes, and arrangements. In another embodiment, the surface textures can be of different sized textural shapes that vary depending on the engine operational load and speed.
In one aspect of the invention, a texture pattern is implemented that reduces friction as components move from low-load, high-speed conditions to high-load, low-speed conditions. In this aspect of the invention, dimples act as a wedge, which effectively lifts the surface and causes a decrease in viscous shearing and a corresponding reduction in friction.
Another aspect of the invention relates to surface texture design with the mixture of different surface features shapes and sizes. This type of mixed shape texturing combines textures designed for low-load, high-speed operating conditions and the textures that are designed for high-load, low-speed operations. This type of texture arrangement may be referred to as a multiscale texture. By using elliptical-shaped (typically smaller and deeper dimples), and circular-shaped dimples (typically large size and shallower) the result is enhanced friction reduction for an engine component experiencing variable loads and speeds in its operation (such as a ring liner, cam lifter, etc.). This arrangement may allow for the reduction of friction in engine components during operation when the component experiencing various load and speed ranges.
Another aspect of the invention relates to the surface texture fabrication technique. Such technique may use acid (or alkaline) resistant flexible (soft) large area masks on large area steel engine components with curved surfaces, for example, internal combustion engine piston rings and cylinder liners, cams, lifters, rollers, roller pins, etc. In one embodiment of the invention, the surface textural features and associated pattern are created on the large size of elastomeric polymer film (soft mask) with dimension accuracy. In another embodiment, the patterned soft mask is applied onto a large surface (flat or curved including cylindrical rollers surfaces) to be followed by electrochemical etching to imprint the textures onto the steel engine component.
In one aspect of this invention, a pattern may be created on a soft plastic mask. Starting out with a clean silicon wafer, a self-assembled monolayer (“SAM”) of hydrophobic molecules (to prevent sticking) are deposited on the wafer; this is followed by placing a pure silver (Ag) film on top of SAM. A photolithographic process is used to produce the desired texture pattern on the silver film. The patterned silver film is then coated with a hydrophilic SAM layer. On top of the SAM layer, a poly dimethylsiloxane (“PDMS”) film is deposited using spin-coating. After baking, the patterned PDMS, i.e., the soft mask, is peeled off from the Si surface.
In another aspect of this invention, the soft mask may be directly applied onto the engine components. The size of the soft mask is only limited by the size of the silicon wafer available (for example, and without limitation, a six-inch, 12-inch, or 18 inch-diameter silicon wafer may be used). The soft mask is very flexible with a typical thickness in the range of 0.1-1.0 mm. The texture pattern on this soft mask may be precisely transferred onto the components without the limitation of size and curvature. The surface textures can then be etched into the surface using conventional electrochemical etching techniques. The technique of using large size of patterned soft mask overcomes the technical barriers in applying surface texture to engine components.
Another aspect of the present invention relates to surface layers for protecting surface texture from wear and reducing friction between moving surfaces, such as in an internal combustion engine component. This aspect of the invention is directed to protecting the surface textures by introducing thin film or coatings under high-load, low-speed conditions where wear may damage the textures. In one embodiment, the protective layers include wear resistant coating. In another embodiment, the protective layers include bonded chemical film on top of the wear resistant coating to provide long term durability of the textured surface.
In another embodiment of the invention, the engine or machine components are first textured to have small dimples on their surface. The dimples are then coated with a DLC layer. In another embodiment of this invention, the DLC layer is further coated with a reactive chemistry with the DLC layer. (DLC is inert and hence does not react with most antiwear chemistries, such as zinc dialky dithiophosphates or Trecyl phosphates, the two most dominant antiwear additives on the market today). This reactive layer will protect the DLC film and synergistically reduce the friction further.
In another embodiment of this invention, to provide additional impact resistance, common in engine operation or in other applications, after the introduction of the reactive chemistry bonded to the engine component surface, an inert molecule is introduced to the surface by dip coating, such as alkylcyclopentanes, which does not bond with DLC surface. This is to be followed by creating a polymer canopy on top of the mixed molecular assembly. An alkmonomer layer is spin-coated on top of the molecular assembly and UV radiated to form a polymer layer on the surface. This helps to prevent the evaporation of the reactive chemistry and encapsulate the inert molecule underneath, providing a visco-elastic layer. This also helps to achieve enhanced durability and reactivity of the DLC coating with the friction reducing anti-wear additives in the lubricant. This process effectively makes the film become part of the surface structure, and, therefore, it will not be leached out by the lubricant used in the engine or machine, and can function independently.
The surface texturing in accordance present invention may utilize textural patterns on a surface of various shapes, sizes, depth, arrangements, and areal density. The various shapes may include, but are not limited to, circles, ellipses, triangles, parallelograms, and grooves of various depth, edge angles, and several orientation angles with respect to the sliding directions. The size of dimples (depressions) may range from few microns up to hundreds of microns. In some applications, it is advantageous to fabricate multi-scale dimples or profusions to achieve friction reduction in large components such as marine diesel engines. The typical depth of depression may be in the range of 1-8 microns. Larger depressions provide enhanced hydrodynamic lubrication at high speed. This permits the large surface features to operate effectively under high speed. Small depressions provide extra lift due to the squeeze of lubricant trapped in the depression. This permits the small surface features to operate effectively under low speed and high load conditions. The areal density of large size dimples may be in the range of 15% to 25%. The areas density of small size depressions may be in the range of 5% to 10%. The arrangement of these different depressions may be arranged in an alternating pattern. However, any suitable arrangement of depressions of the same, similar, or different sizes may be used.
As an example of an embodiment of one aspect of the invention, texturing may be applied to a piston ring segment in a typical top piston ring slides over a cross-hatched cylinder liner. The cross hatch marks may be of the same order of magnitude in size and shape to dimples with the cross hatch angle of from 17° to 27° with respect to the horizontal plane of the engine cylinder, and the intersecting angle between the cross-hatching marks may be about 35° to 55°. The height of the cross-hatching lines may be about 3 to 10 μm. This may allow the dimples on the ring surface to work with another “textured” surface.
In an exploratory study, two separate individual patterns were incorporated onto a surface at the same time: one large surface texture pattern at or below two microns deep; one elliptical dimple pattern above two microns deep. In this study, the presence of both dimple patterns actually enhanced one and other as the combined pattern achieved much lower friction coefficients under both low loads and high loads over a wide speed range.
In another study, deep small dimples were fabricated inside of large dimples. As an initial design, a mixed pattern was used, i.e., dual textures of small deep dimples and large shallow dimples with built-in small deep dimples inside large shallow dimples (multiscale texture). This was followed by a totally integrated design (large shallow dimples with small deep dimples inside).
The resulting compound textures were evaluated using the test conditions shown in Table 1, where the test conditions for pin-on-disk and four ball testers are tabulated.
(157 MPa)
(314 MPa)
(470 MPa)
Examples of various surface texture designs are shown in
These surface texture patterns were evaluated in low-load, high-speed conditions (run on the pin-on-disk tester), and high-load, low-speed conditions (run on the four ball tester). The experimental results are shown in
In a study for a diesel engine piston ring-cylinder liner application, two different shapes of dimples were incorporated onto a surface to form a pattern: circular-shaped and elliptical-shaped dimples were arranged in an array such that alternating of circle and ellipse with defined areal density. The presence of both dimple shapes and sizes actually enhances one and other. The combined pattern achieves much lower friction coefficients under both low speed and high speed over a wide load range.
Testing on the effect of surface texturing has also been performed using Cameron-Plint reciprocating test rig. The cylinder liner sample is a segment of production cylinder, such that the liner surface consists of cross-hatching lines. The cross-hatched lines are a form of surface texture commonly used in industrial applications. The width of the liner segment is 12 mm and its length is 58 mm. The piston ring segment slides against the liner segment with a stroke length of 12.4 mm. Based on the geometry of testing setup, the apparent contact pressure is in the range of 0.8-6.7 MPa. The equivalent average linear sliding speed ranges from 0.05 m/s to 0.6 m/s for the reciprocating frequencies of 2-24 Hz. White oil (ISO 32 grade equivalent) with 2% Tricresylphosphate (TCP) and 1% antioxidant was used as the testing lubricant. This simple treatment prevented rapid degradation of lubricant without affecting the friction characteristics. For a selected frequency, a step loading procedure was used to apply loads from 30 N to 240 N with increments of 30 N. The test was run for five minutes for each load step, and the average frictional force was recorded. This procedure was repeated for frequencies from 2 Hz to 24 Hz in increments of 2 Hz. The test conditions are listed in Table 2.
One set of the testing results is illustrated in
The Cameron-Flint reciprocating testing was carried out for textured piston ring specimens at room temperature using the test procedure described above. The un-textured piston ring was also tested at room temperature as baseline for comparison purpose.
As an example of testing performed on an embodiment of the present invention, in a diesel engine piston ring-cylinder liner application, two different shapes of dimples have been incorporated onto a surface to form a pattern: circular-shape and elliptical-shaped dimples were arranged in an array such that alternating of circle and ellipse with defined areal density.
The Cameron-Plint reciprocating testing was carried out for textured piston ring specimens at room temperature using the test procedure described above. The un-textured piston ring was also tested at room temperature as baseline for comparison purpose.
These texture pattern designs are shown in
The testing results at frequencies of 24 Hz are shown in
The surface texturing described herein may be applied by variety of methods; however, as discussed above, the prior art methods have a number of drawbacks. Accordingly, the present invention may use a patterned elastomeric polymer film (soft mask) to create texture patterns to be etched onto real engine component parts made of steel. In one embodiment, this invention relates to a method, or procedure of creating patterns onto the soft mask. In another embodiment, the soft mask may be directly applied onto the engine component to create patterns via electrochemical etching. The engine component may have a rough, wavy, or curved surface of hundreds of millimeters in size. Electrochemical etching may be used to create textures (arrays of micrometer sized dimples of various geometry, shape, and pattern) on the engine component surface.
Soft lithography techniques have been developed to deposit organic molecular assemblies on clean flat surfaces, such as silicon wafer surface for the construction of micro devices (MEMS or NEMS) for sense, compute, and actuate purposes. However, no known techniques have been developed for making masks for large area texturing and on relative “rough” surfaces such as production engine parts, which have high surface roughness and waviness. Engine parts materials also have very complex surface materials composition, such as multi-layer surface layer comprising of metals, ceramic powders, and eutectic multiphase materials. Hence, making photoresist (polymeric material) adhere to the surface, depositing self assembled molecules, and controlling the bonding of organic molecules to such surfaces are extremely difficult. On rough surfaces, the roughness itself produces varying surface energy levels and defect sites; as a result, depositing uniform molecular layers may not be feasible, making a uniform organic layer (photo-resist deposition) for proper UV exposure time for photolithographic purpose difficult. All these barriers make such soft masks fabrication for electrochemical etching of steel parts unavailable until now.
With reference to
Since the PDMS mask can conform to irregular surfaces, the technique, in theory, can be applied to curve surfaces. However, soft lithography has not been applied to large area lithography or used in subsequent etching. Engine components require sixes of hundreds of millimeters and require subsequent UV lithography and chemical etching steps. Also PDMS material is transparent to ultraviolet light; therefore, the PDMS mask cannot be used for UV lithography and etching steps.
In accordance with this invention, photo-lithography may be combined with a thin film deposition technique, and soft-lithography to transfer micro-patterns from a Si wafer coated with Ag film onto a soft transparent PDMS film. To separate the PDMS film from the silicon substrate, a self-assembled monolayer (“SAM”) has to be deposited on the film to ensure that the film can be peeled off easily.
The fabricated PDMS soft mask may then be used to fabricate texture patterns on the steel surface. Optical images of a PDMS mask with textures and texture feature on a PDMS mask after the deposition of Ag film are shown in
In an exemplary embodiment, the technique may be performed using a six-inch silicon wafer.
In another exemplary embodiment, the soft mask technique and electrochemical etching process may be performed on an engine component, i.e., piston ring surface. In an exemplary embodiment, a soft mask can be fabricated according to the procedures discussed above. The detailed steps are described as follows:
The hydrophobicity of the modified surface with the first SAM film was confirmed with a 120° water contact angle (FTA32 goniometer). The hydrophilicy of the modified surface with the second SAM film was also confirmed with a water contact angle of 12°.
The PDMS soft mask can then be used to fabricate surface texture patterns on engine piston ring surfaces. The piston ring sample may be cleaned by steps with ethanol, acetone, and DI water, and then dried with nitrogen. A positive photoresist film may then be applied on the cleaned surface by spin-coating process. The PDMS soft mask may then be used to cover the photoresist coated surface and exposed to the UV light to transfer the surface texture pattern onto the photoresist film. The PDMS soft mask may then removed from the surface after the UV exposure. After developing, the surface texture may be fabricated by electrochemical etching process. TEM images of textured piston ring surfaces are shown in
In another aspect of this invention, a thin film layer, such as a DLC coating, may be applied to the textured surfaces of engine or machine components. There are several parameters to consider for such a thin film: (1) the nature and composition of the film; (2) the thickness of the film; (3) the adhesion characteristics of the film to the substrate; (4) the hardness of the film in relation to the substrate; and (5) the compatibility of the film with lubricant chemistry.
Adding a film to a complicated textured surface may alter the dimension and shape of the textured dimple. This may further alter the friction reduction ability of the textures. If the thickness of the film is too thin, then the durability may be compromised. The nature and composition of the film control the adhesion characteristics of the film to the substrate. It also requires the thin films to have the ability to conform to the textured surface with minimum residual stresses. There are no known films capable of meeting all these requirements.
To determine the sufficiency of different films, testing was performed as follows. A collection of high hardness wear resistant films were deposited on textured surfaces, these include chromium nitride, titanium nitride, carbides, and diamond-like-carbon films. The film thickness ranges from 90 nm to 200 nm thick. A test procedure was developed to test the degree of surface texture protection and the durability of the film. The four ball tester is used and the testing condition is tabulated in Table 1.
The failure observed for thin films typically takes the form of delamination at the edge of the dimple (201) as shown in
In view of the results of such thin film testing, a DLC film was identified as a preferred material to serve as a protection layer applied to textured surface. An example of an embodiment of the DLC film in accordance with this aspect of the present invention was tested. The film thickness ranged from 90 nm to 250 nm and was deposited using a closed field unbalanced magnetron sputtering ion plating system. An interlayer was engineered to increase adhesion between the steel substrate (for example, 52100 steel) and the DLC film. The configuration of the coating targets were Cr with 4.0 A current and C with 3.0 A current. The deposition rates were 20.0 nm/min for Cr adhesive interlayer, 16.8 nm/min for CrC graded layer, and 10.1 nm/min for pure DLC top layer. The bias voltage varied from −60 V to −40 V during pure DLC deposition.
The DLC coating morphology and adhesion testing result is shown in
In another embodiment of this invention, modifications may be made to the DLC layer that may be applied between moving surfaces of an internal combustion engine over the textured layer. The technique described herein allows for the DLC film to bring its own lubricants into the application it serves. While the internal combustion engine application is specifically discussed, those of ordinary skill in the art would recognize that the film discussed herein may be similarly applied to moving parts in other applications, including, for example, biomedical devices, telescopes, and gears. Traditionally, carbon has been very difficult to lubricate, since it is essentially inert. In the techniques described herein, a process of molecular engineering films to obtain that lubrication is described.
The process is first described generally, followed by more specific examples below. DLC contains a carbon surface and is generally inert. Since only about 30% of the DLC surface is typically considered active, a first molecule is applied to the surface that reacts with that 30% of the carbon on the surface. Next, a second molecule is added by a coating technique, which essentially floats on the surface. Then to prevent the material from evaporating, a polymeric monomer layer is added by a spray deposition technique on top of the combination. Once the polymeric monomer is sprayed, it is activated by UV radiation. The polymeric monomer then becomes polymerized and essentially forms a tent or canopy on top of the surface. An effective thickness of the surface layer is approximately 20 Angstroms. Moreover, 12-18 GPa has been found to be an effective DLC hardness range for the application discussed.
Different type of molecules may be used as contemplated by this invention. For example, for applications such as friction reduction, a hydrocarbon with an alcohol functional group may be used as the first molecule. Then an inert functional molecule, such as Benzene, may be used as the second molecule. Then polystyrene film may be then applied as the polymeric monomer layer on top.
With this coating, the DLC surface now acts in a manner like that of a bumper. Traditional DLC film is hard, but it is also brittle. With this technique contemplated by this aspect of the present invention, the new layer essentially acts like rubber, and the DLC becomes much more robust and useful. Benefits of the combination include the reduction of friction when it is used on surfaces of, for example, engine components as well as, for example, corrosion protection and rust prevention.
A more graphitic DLC film with a 150 nm thickness and 12 GPa nanohardness, contemplated by the present invention, was also tested by the following procedure. DLC coated aluminum based disks (i.e., magnetic hard disks for information storage technology) were used for chemical deposition, encapsulation, and thickness measurement, and were tested for friction on a pin-on-disk tester. The chemical compounds were deposited on DLC coated hard disks using a dip-coating technique. Solutions of 0.5% to 2.0% by weight of various compounds were prepared in cyclohexane or hexane. The solutions were mixed for a minimum of 10 minutes in an ultrasonic bath prior to dip coating to ensure a complete solubilization of the compounds. Deposition was carried out in a dipcoater using a dip speed of 40 to 60 mm/min. The resulting films were then annealed at 165° F. for 10 minutes under argon atmosphere to bind the molecules to the DLC surface while avoiding oxidation. After annealing, the films were washed with 10 ml of cyclohexane or hexane, to remove any molecules that were not chemically bound on the surface. The film was then covered with a thin layer of polymeric monomers and then UV irradiated to encapsulate the chemical film underneath.
The friction properties of both the encapsulated films and not encapsulated films were tested with the pin-on-disk machine using a step-loading procedure. The load was varied from 1 N to 25 N, and the speed was varied from 0.015 m/s to 0.20 m/s to cover the hydrodynamic and boundary lubrication regimes. To extend the load range of the test, two diameters of the pin (balls) were used (1.5 mm and 6.125 mm). A step loading test was used to evaluate the deposited film. At each sliding speed, eight different loads were applied and the steady state friction for that film was recorded. The testing results are illustrated in
The durability of the encapsulated and not encapsulated films was tested using a ball-on-three flats geometry of a four ball tester. The testing procedure may be described as follows:
Stage I: Minicycle step loading sequence:
First cycle: started at 1.15 m/s linear speed (3000 rpm), increased loads front 5, 10, 15, 20, 25, 30 Kg per every 3 minutes (or longer until a steady state friction trace is obtained). The typical time was 3 minutes for each load.
Second cycle: lowered the speed from 1.15 m/s to 0.96 m/s (2500 rpm) and repeated the loading from 5 Kg to 30 Kg steps.
For a total cycle, the speed changed from 1.15 m/s, 0.96 m/s, 0.77 m/s, 0.57 m/s, 0.38 m/s, to 0.19 m/s in an increasingly severe test condition. Minicycle 7 and 8 will basically repeat the condition of cycle 1 and 2.
Stage II: Durability test (time to failure test sequence):
To clearly separate the various chemistries and textures, a time to failure test sequence was used. After the eight mini-cycles of testing, if no failure was observed, then the test started at 1.15 m/s speed and 2 kg load for 3 minutes, the load was increased to 5, 10, 20 Kg. At that time, the test continued for one hour until failure. If no failure was observed, the load was increased to 30 kg for an hour, then 40 kg for an hour.
Following the above mentioned test procedure, if no failure was observed, the sample was subjected to stage II durability test as illustrated in
The testing results of Stage I for a specific combination of chemistry and textures are summarized in
The testing results of Stage II durability test for various bonded chemical films are shown in
In a specific embodiment, the method for enhancing the DLC film may include the following steps: (a) coating the DLC film with a mixture of reactive chemicals specific to DLC surface such as long chain alcohols, olyel alcohols, glycols, polyglycols of various chain lengths; the film is allowed to anneal at moderate temperatures (70° C. to 160° C. depending on the chemical species) for a period of time (5 to 30 minutes depending on specific molecular structure); (b) solvent washing after annealing to remove any unreacted molecules; (c) adding alkylcyclopentanes or other inert molecules to the surface by dipcoating to fill the unreacted space on the surface; (d) adding polymeric monomers to the top of the surface using spin coating or other means; and (e) radiating the layer of polymeric monomers with UV light of suitable wavelength and time duration to encapsulate the molecular assembly underneath.
Other molecules that may be used separately or in combination with alcohols are Amine O, thiocarbamates, esters, and polyesters, copper oleates, and sulfur leates. Under typical conditions, about 20% to 40% of the DLC surface will be covered with a monolayer or more of these molecules after washing with appropriate solvents. The polymeric monomer may be comprised of polystyrene or polypropylene or other polymer blends suitable for UV irradiation induced polymerization.
The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
This application is a divisional of U.S. patent application Ser. No. 14/000,857, which is the 371 U.S. national phase of International Application no. PCT/US2012/025949, filed Feb. 21, 2012, which claims priority to provisional U.S. application Nos. 61/445,503 and 61/445,507, both filed on Feb. 22, 2011. The entire disclosures of all such applications are incorporated herein by reference.
This invention was made with government support under Department of Energy Prime Contract No. DOE/NETL DE-AC26-04NT41817-520.01.04 via Subcontract No RDS 41817M3459 awarded to George Washington University from Research and Development Solutions, LLC. The government has certain rights in the invention.
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| Number | Date | Country | |
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| 20190193372 A1 | Jun 2019 | US |
| Number | Date | Country | |
|---|---|---|---|
| 61445507 | Feb 2011 | US | |
| 61445503 | Feb 2011 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 14000857 | US | |
| Child | 16290648 | US |
