USRE34143E - Oilless internal combustion engine having gas phase lubrication - Google Patents
Oilless internal combustion engine having gas phase lubrication Download PDFInfo
- Publication number
- USRE34143E USRE34143E US07/756,258 US75625891A USRE34143E US RE34143 E USRE34143 E US RE34143E US 75625891 A US75625891 A US 75625891A US RE34143 E USRE34143 E US RE34143E
- Authority
- US
- United States
- Prior art keywords
- piston
- cylinder
- receptacle
- grooves
- annular
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M9/00—Lubrication means having pertinent characteristics not provided for in, or of interest apart from, groups F01M1/00 - F01M7/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0672—Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases or frames
- F02F7/0085—Materials for constructing engines or their parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16N—LUBRICATING
- F16N15/00—Lubrication with substances other than oil or grease; Lubrication characterised by the use of particular lubricants in particular apparatus or conditions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M1/00—Pressure lubrication
- F01M1/08—Lubricating systems characterised by the provision therein of lubricant jetting means
- F01M2001/083—Lubricating systems characterised by the provision therein of lubricant jetting means for lubricating cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/08—Ceramics; Oxides
- F05C2203/0865—Oxide ceramics
- F05C2203/0882—Carbon, e.g. graphite
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2253/00—Other material characteristics; Treatment of material
- F05C2253/16—Fibres
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- This invention relates to the art of engine lubrication and, more particularly, to oil-less lubrication for the piston-cylinder chamber.
- a low heat rejection engine particularly for a diesel engine, has the potential to provide significant improvement in fuel economy. Heat rejection can be reduced by eliminating liquid cooling normally incorporated in the block of a diesel engine and replacing all or a portion of the combustion chamber components with materials that can operate at uncooled combustion temperatures, such as ceramics. This is sometimes referred to as an adiabatic diesel engine.
- Still another object of this invention is to provide an oilless uncooled internal combustion engine that has improved gap control and reduced friction with considerably reduced gas blow-by.
- the invention is a gas phase lubrication system which operates effectively within an oilless engine.
- Such engine has a piston reciprocal within a cylinder and along an axis of such cylinder while providing an annular gap therebetween to receive combustion gas.
- gas phase lubrication system comprises: (a) an annular receptacle in at least one of the piston and cylinder; (b) an annular body of graphite carrying high temperature solid lubricant disposed in such receptacle, the body presenting a face projecting beyond the receptacle; (c) an elastomer material, retentive of elasticity at the maximum operating temperature to be experienced by the body, interposed between the body and receptacle to urge the body to close the gap under substantially all operating conditions of the engine; and (d) axially directed grooves in the body face sized to substantially trap cylinders of combustion gases therein by viscosity under low pressure gradients and to limit the passage of the combustion gases through such grooves or from such trapped gas cylinders
- the receptacles for receiving the annular solid lubricant may be (i) restricted to the lower region of the piston side wall as a shallow ring, which region will oppose the cylinder wall and experience a maximum operating temperature of 550° F., (ii) receptacles in the piston side wall extending substantially upward from adjacent the bottom of the piston to above the piston pin, as a sleeve, which region will oppose the cylinder wall having a maximum operating temperature of up to 800° F., (iii) shallow annular ring receptacles separated at two locations, one adjacent the top and one adjacent the bottom of the piston side wall, (iv) reversed in position from any of the above by positioning the receptacles in the cylinder wall rather than the piston side wall, and (v) include the addition of similar receptacles as in (i)-(iii) to the cylinder wall thereby providing complementary receptacles in both the cylinder wall and piston side wall.
- the chemistry for the elastomer and solid lubricant may be varied depending upon the maximum operating temperature to be experienced, and a coating of solid film lubricant with a reduced coefficient of friction may be disposed on the opposing cylinder wall or piston wall not containing the first receptacle.
- the grooves are sized (cross-section) to insure gas therewithin under low gradients as well as under high pressure gradients.
- Such grooves preferably have a radial depth of 0.003-0.005 inches and preferably are semicylindrical so that the width of such grooves will be in the range of 0.006-0.01 inches.
- the alignment of the grooves will make an angle with the cylinder axis of 2-5% to facilitate rotation of the trapped gas phase cylinder as the piston reciprocates.
- FIG. 1 is a partially sectional and partially schematic view of a four-stroke uncooled oilless engine within which the invention herein is incorporated;
- FIG. 2 is a thermal gradient map superimposed on each of the piston and cylinder wall
- FIG. 3 is an enlarged central sectional view of a piston and cylinder assembly presenting a first embodiment of this invention using a gas phase control restricted to the lower region of the piston side wall;
- FIG. 4 is an enlarged view of a portion of FIG. 3;
- FIG. 5 is an enlarged sectional view taken substantially along line 5--5 of FIG. 4;
- FIG. 6 is an enlarged sectional view taken along line 6--6 of FIG. 1;
- FIG. 7 is a graphical illustration plotting the coefficient of friction with time for various matched materials useful in an adiabatic engine
- FIG. 8 is a graphical illustration of time plotted against wear for the various combinations of materials used in FIG. 7;
- FIG. 9 is a graphical illustration of friction and wear under different conditions for a solid film lubricant coating of this invention against graphite;
- FIG. 10 is an enlarged schematic view of the piston and cylinder and gas phase control of FIG. 3 at top dead center and bottom dead center, both in the cold and the hot operating conditions;
- FIG. 11 is an enlarged central sectional view of a piston and cylinder representing a second embodiment of this invention.
- FIG. 12 is an enlarged sectional view taken substantially along a vertical radial plane of FIG. 5;
- FIG. 13 is a schematic view of the piston and cylinder arrangement of FIG. 11 showing the change in thermal expansion of such components from hot to cold;
- FIG. 14 is an enlarged central sectional view of still a third embodiment of this invention.
- FIG. 15 is an enlarged sectional view taken substantially along line 15--15 of FIG. 17;
- FIG. 16 is an enlarged central sectional view of a fourth embodiment of this invention.
- Uncooled is used herein to mean an engine that is devoid of conventional cooling such as a water jacket or fins for air cooling.
- the resulting higher operating temperatures can be projected to provide at least a 9% improvement in the indicated specific fuel consumption relative to a water cooled, base line engine at part load operating conditions (i.e., 1200 rpm at 38 psi BMEP). Since conventional oil lubrication cannot be used at the higher operating temperatures because such oils will pyrolyze, gas phase lubrication is used.
- Oil is also eliminated in the crankcase; without crankcase oil, a sealing system to separate the oil from the hot upper cylinder area, where coking can occur, is not required.
- Oilless ceramic roller bearings 17 and 16 for the crankshaft and connecting rod respectively eliminate this need for oil in the crankcase. With ceramic roller bearings for the valve train finger followers and camshaft (19 and 18), as well as suitable dry lubrication, the engine is further simplified eliminating the need for oil, the oil pump, oil filter and oil gallery drilling.
- oilless is used herein to mean devoid of conventional piston rings between the piston and cylinder wall that are designed to ride on a fluid film.
- Sintered silicon nitride was used as the material for the structural cylinder wall and piston.
- Sintered silicon nitride has coefficient of thermal expansion of about 3.6 ⁇ 10 6 /°C., a modulus of rupture of about 85 ksi which is stable up through the temperature range of 1600° F. and has a thermal conductivity which is about 50% of the value of cast iron.
- this invention provides a gas phase lubrication control for any material of which the piston and cylinder wall may be constructed. This comprises cooled engines as well as uncooled engines; it is to be recognized that the benefits of this invention will accrue to a greater degree with an uncooled engine.
- Gas phase lubrication between a piston and cylinder wall is dependent on maintaining a tight clearance or annular gap effective in triggering viscous drag to hold a gas phase film therein.
- it is very difficult to achieve and maintain a tight and uniform annular gap throughout all aspects of engine operation.
- the gas phase changes in viscosity and pressure during each of the strokes of the engine operation, and concentricity of the piston within the cylinder bore changes due to major and minor mechanical side thrust loads of the connecting rod which is articulating from side to side.
- FIGS. 3-8 illustrate a first embodiment of a gas phase blow-by control useful in an oilless engine.
- This invention recognizes that it is very difficult to design a consistently tight gap h between the piston 13 and cylinder wall 12 under all operating conditions. Instead, this invention closes the available annular gap h by use of an antifriction annular body 20 that is radially biased. As shown in FIG. 5, gas phase cylinders 21 are trapped in grooves 22 in the face 23 of such body 20 to act as bearings during reciprocation of the piston 13.
- this embodiment restricts the receptacle 24 for receiving the annular gap closing body 20 to the lower region 25 of the piston side wall 26, which region 25 will oppose the cylinder wall to experience a maximum operating temperature of about 550° F.
- the region 25 preferably extends from adjacent the bottom 26a of piston side wall to below but adjacent the piston pin opening 27.
- the annular receptacle or groove 22 may be dovetailed or under-cut in cross-sectional configuration to facilitate holding the annular body 20 therein. The undercut may form a negative angle of 5°-15° with the cylinder wall surface 26.
- the depth or radial extent of such receptacle is in the range of 2 mm to half the thickness of the piston wall, and may have an axial extent 25 which is in the range of 5-15 mm if used at only the bottom of the piston and 15-30 mm if used to hold a sleeve as in another embodiment.
- the body 20 is comprised of a graphite carrying, high temperature solid lubricant.
- a high temperature solid lubricant is used herein to mean a solid lubricant that has a coefficient of friction of 0.02-0.1 at 600° F.
- the body presents a face 23 which projects out of the receptacle 24 to tend to engage the opposed cylinder wall surface 28.
- Such solid lubricant is preferably a composite, by volume, of 40% graphite, 20% MoS 2 , and the remainder a thermally stable (does not decompose up to 375° C. or 700° F.) polymer such as polyarylsulfone; the solid lubricant may also be a metal matrix composite having about 40% graphite and the remainder aluminum or cast iron.
- Such metal matrix composites may be formed by power metallurgy or other suitable means to provide a porous material that can expose graphite for intermittent or supplementary lubrication purposes. Up to 13% of the graphite may be substituted with boron nitride.
- the solid lubricant may also include up to 10% copper and one of LiF, NaF and CaF, as a substitute for the MoS 2 .
- An elastomer material 30 is interposed between the body 20 and the receptacle or groove 24 to urge the body face 23 to close the gap h under all operating conditions of the engine.
- the cross-sectional configuration of the elastomer material may be similar to the shell of an automotive rubber tire which is U-shaped with curved lips 30a at the exposed extremity thereof.
- the elastomer material 30 must be effective to retain its elasticity up to a maximum operating temperature of about 550° F.
- Materials that are useful for this purpose may comprise silanes, such as Dow Corning Resin #95-077GA or Cilastic GA.
- the resins are compounded with glass fibers (such as Owens Corning #497 Fiber).
- the fibers are chopped to a short length (such as 1/4 inch) and coated with Dow Corning Primer Q36-061 diluted in trichloroethylene and dried for about 10 hours.
- the coated fibers are then mixed with the silane resin as well as with zinc oxide and some carbon black.
- the mixture is blended with a catalyst for about 15 minutes and then degassed for 3/4 to 1 hour and formed as an extruded material, preferably in the tire shell shape.
- Horizontal annular grooves 32 may be defined in the back of the body 20 to provide areas where the elastomer material 30 may interlock with the body and provide a firmer mating therebetween. Such horizontal annular grooves may have a depth of about 0.003-0.005 inches such as shown in FIG. 4.
- axially directed grooves 22 are defined in the outer face 23 of the body to trap gas phase cylinders 21 therein by viscosity when the grooves are under a low pressure gradient, and to limit passage of combustion gases through the grooves or from such gas cylinders under high pressure gradients to 1% or less of the cylinder gas flow charge volume.
- the gas cylinders function as rotating bearings to ride the piston during reciprocation.
- Low pressure gradient is used to mean a gradient of 4500 psi or less
- high pressure gradient is used herein to mean a gradient from 400 psi up to 1700-2000 psi.
- Grooves 22 are directed axially, but preferably deviate from perfect parallelism with piston or cylinder axis 33 by an angle of 2°-15°. It is desirable that the grooves overlap along a line-of-sight (looking along the surface of the piston parallel to its axis) due to the skewing and thus roll over the full interfacing surface of the cylinder wall. Such slight skewing facilitates the rolling of the gas phase cylinders 21 by viscous drag of the cylinder wall during piston reciprocation.
- the axially directed grooves 22 may have a depth of about 0.003-0.01 inches and are spaced apart a distance of about 3 mm; the total semiconductor cross-sectional volume of all the grooves should together provide the predetermined blow-by under a high pressure gradient that is limited to 1% or less of the gas charge volume.
- annular body which is limited to the bottom lower extent of the piston side wall or skirt, as shown in FIG. 3, the annular body will not be exposed to temperatures in excess of 550° F. during its normal operation in a four cycle engine. Therefore, the elastomer and body should maintain a closure tendency across the gap, and the graphite contained in type body and the rotating gas cylinders in the grooves 22 will provide sufficient antifriction lubrication therebetween.
- a solid film lubricant coating 35 (see FIG. 7) containing either BN or MoS 2 with graphite may be applied to the cylinder wall.
- the coating is comprised of about 40% by weight of high temperature thermoplastic resin such as polyarylsulfone, 40% graphite, and 20% of either MoS 2 or BN.
- a resin that is thermally stable up to about 700° F. is polymer 360, known as Astrel, manufactured by Minnesota Mining and Manufacturing Company. Such resin may be dissolved in dimethyl acetamide to make a syrupy paste to facilitate blending of other ingredients. After the cylinder wall surface is thoroughly cleaned to remove any oxidation, such wall may be grit blasted to increase porosity and thereby the reception of the coating. The blended mixture is spread over the cleansed and porous surface and dried at about 250°-300° F. for at least 15 minutes.
- This polymer based coating mixture will have a coefficient of friction which is 1/2 to 1/3 that of the metal matrix graphite-carrying composite of body 20.
- FIGS. 7, 8 and 9 a test using such coating against Si 3 N 4 was compared to uncoated Si 3 N 4 or graphite on Si 3 N 4 .
- FIG. 7 shows a plot 36 for coefficient of friction for a coated silicon nitride cylinder wall against which a graphite body is rubbed thereagainst; it had the lowest overall coefficient of friction compared to plots 37 for uncoated silicon nitride against silicon nitride and plot 38 for a graphite body against silicon nitride.
- FIG. 7 shows a plot 36 for coefficient of friction for a coated silicon nitride cylinder wall against which a graphite body is rubbed thereagainst; it had the lowest overall coefficient of friction compared to plots 37 for uncoated silicon nitride against silicon nitride and plot 38 for a
- the supporting surface may be provided with reservoirs 43 or grooves to capture or retain the solid film lubricant coating 44, much in the manner of porosity.
- These reservoirs may be grooves in the cylinder wall, which grooves are vertically oriented, spaced apart a distance of about 3 mm, and each may have a semicircular depth of about 0.003 inches.
- the gas phase control of this first embodiment functions to close the gap (shown as 0.06 mm) with cylinder 12 both at top dead center and bottom dead center for the piston 13 when the engine is cold (ambient conditions). This is illustrated in solid full line.
- the piston is illustrated with an exaggerated chamfer 46 and a piston diameter of about 80 mm.
- the chamfer increases the gap at the piston shoulder to 0.10 mm.
- the chamfer is needed to compensate for the mushrooming effect (see broken line 47 of the hot piston) that takes place at the crown of the piston due to exposure to the highest temperatures and thus the highest thermal growth.
- the cylinder wall 12 will also undergo a gradient of thermal growth with the greatest change in dimension at the top of the cylinder wall (see broken line 48 for the hot cylinder wall). Please note that if the piston top was not chamfered, its hot size would interfere with the cylinder wall during the bottom dead center position. With the chamfer the hot size of the piston crown will always stay separated (at 49). Thus, the control body 20 must only accommodate a change in gap from a radial distance of 50 when cold to a radial distance of 51 when the parts are hot, which may be a very slight change or may be very large, depending on design.
- an alternative embodiment incorporates a similar control body, but the modified annular body 53 is expanded to have an axial extent 54 from the bottom of the piston side wall to above the piston pin area, approximately three-quarters of the way up the side wall of the piston.
- Such control body forms a sleeve which will be exposed to a higher maximum operating temperature, as high as 880° F.
- the face of the body is coated with a solid film lubricant containing MoS 2 or BN and graphite as described earlier.
- the cylinder wall 12 should contain a coating 60 of such polymer/molybdenum disulfide/graphite mixture.
- Both coatings, on body face 55 and on the cylinder wall 12, should contain reservoir grooves 61 in the supporting substrate to assist in distributing the material at higher temperatures, as shown in FIG. 12.
- the grooves on the cylinder wall may be vertically oriented, spaced apart about a distance of 3 mm, while the grooves on the face of the solid lubricant body may be horizontal spiral grooves oriented to across the grooves in the cylinder wall during piston reciprocation and promote a mutual distribution of the solid film lubricant particularly at higher temperatures.
- This embodiment is best suited to an articulated piston where the piston crown is made separately from the piston skirt; it works well in either a four or two stroke engine.
- FIG. 13 illustrates how the sleeve type gas phase control will function.
- the body 20 is exaggerated to show how it extends up a more significant distance of the piston side wall.
- Elastomer material 30 is exposed to temperatures in excess of 700° F. at the top of the body and thus a refractory coating 67 may be deposited on the elastomer at such exposed areas 66.
- the body 20 must accommodate a wider fluctuation in the gap from cold to hot (i.e., from cold radial distance 63 to hot radial distance 64 and 65).
- FIGS. 14 and 15 provides for the control body to be in a receptacle disposed at 70, not only in the piston, but also at 71 on the cylinder wall.
- the control bodies each will have elastomers urging the two bodies together to close the gap between the piston and cylinder wall.
- One or the other of the mating control bodies may have blow-by grooves or both may have blow-by grooves. It is possible that the elastomer may be eliminated from the piston in this embodiment. This is useful because the cylinder wall runs considerably cooler than certain regions of the piston wall and such cylinder wall will be better able to protect the elastomer.
- FIG. 16 illustrates still another embodiment which employs shallow ring bodies 80 and 81, one adjacent the top of the piston and another adjacent the bottom of the piston side wall.
- Each annular body 80 and 81 employs the same type of elastomer and graphite-carrying solid lubricant body, as described in Embodiment One, to close the gaps 82 and 83 at the top and bottom of the piston, respectively.
- the net effect of separated bodies is to trap a gas film therebetween (across extent 84) to more effectively operate as a squeeze film and thereby insure antifriction characteristics therebetween.
- Both of the shallow control bodies will have axially directed blow-by grooves to facilitate the provision of rolling gas phase cylinders acting as bearings.
- This embodiment is particularly helpful in a four-stroke engine where any gas phase squeeze film may be particularly thin during the intake and exhaust strokes. This trapping of the gas phase between the annular control bodies facilitates the maintenance of such film during such strokes.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
Description
Claims (19)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/756,258 USRE34143E (en) | 1988-02-23 | 1991-09-06 | Oilless internal combustion engine having gas phase lubrication |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/159,615 US4872432A (en) | 1988-02-23 | 1988-02-23 | Oilless internal combustion engine having gas phase lubrication |
US07/756,258 USRE34143E (en) | 1988-02-23 | 1991-09-06 | Oilless internal combustion engine having gas phase lubrication |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US07/159,615 Reissue US4872432A (en) | 1988-02-23 | 1988-02-23 | Oilless internal combustion engine having gas phase lubrication |
Publications (1)
Publication Number | Publication Date |
---|---|
USRE34143E true USRE34143E (en) | 1992-12-15 |
Family
ID=26856123
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US07/756,258 Expired - Lifetime USRE34143E (en) | 1988-02-23 | 1991-09-06 | Oilless internal combustion engine having gas phase lubrication |
Country Status (1)
Country | Link |
---|---|
US (1) | USRE34143E (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1996004466A1 (en) * | 1994-07-22 | 1996-02-15 | Hannoosh James G | A two-cycle ceramic/metallic internal combustion engine |
DE19651069A1 (en) * | 1996-12-09 | 1997-04-30 | Lothar Strach | Oil-less uncooled adiabatic diesel engine |
US5934236A (en) * | 1992-11-12 | 1999-08-10 | Ford Global Technologies, Inc. | Low friction valve train |
WO2000050753A1 (en) * | 1999-02-22 | 2000-08-31 | Caterpillar Inc. | Free piston internal combustion engine with piston head having non-metallic bearing surface |
US6167856B1 (en) | 1992-11-12 | 2001-01-02 | Ford Global Technologies, Inc. | Low friction cam shaft |
US6581381B2 (en) * | 2001-11-15 | 2003-06-24 | Chang Sun Kim | Engine having adiabatic members in its combustion chambers, engine capable of reusing exhausted energy, and high pressure jet assembly having the engine |
US6951193B1 (en) | 2002-03-01 | 2005-10-04 | Draper Samuel D | Film-cooled internal combustion engine |
US20060000214A1 (en) * | 2004-05-26 | 2006-01-05 | Sri International | Compliant walled combustion devices |
US20060060164A1 (en) * | 2004-09-20 | 2006-03-23 | Gerfast Sten R | Internal combustion engine without oil |
US20060065228A1 (en) * | 2004-05-26 | 2006-03-30 | Sri International | Compliant walled combustion devices II |
US20060255047A1 (en) * | 2005-05-11 | 2006-11-16 | Mitsunori Gotou | Reinforcing structure of cylinder barrel |
US20100288252A1 (en) * | 2006-09-12 | 2010-11-18 | Marlon Moss | Non-Polluting Two-Stroke Engine with Air-Cooled Piston |
US20130319365A1 (en) * | 2012-05-30 | 2013-12-05 | GM Global Technology Operations LLC | Method for in-situ forming of low friction coatings on engine cylinder bores |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3890950A (en) * | 1973-10-02 | 1975-06-24 | Megatech Corp | Piston lubricating |
GB2050882A (en) * | 1979-06-12 | 1981-01-14 | Ford Motor Co | Method of treating a metal contact surface |
-
1991
- 1991-09-06 US US07/756,258 patent/USRE34143E/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3890950A (en) * | 1973-10-02 | 1975-06-24 | Megatech Corp | Piston lubricating |
GB2050882A (en) * | 1979-06-12 | 1981-01-14 | Ford Motor Co | Method of treating a metal contact surface |
Non-Patent Citations (2)
Title |
---|
"A Low Friction, Unlubricated Silicon Carbide Diesel Engine", SAE paper No. 830313, by Timoney et al. |
A Low Friction, Unlubricated Silicon Carbide Diesel Engine , SAE paper No. 830313, by Timoney et al. * |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5934236A (en) * | 1992-11-12 | 1999-08-10 | Ford Global Technologies, Inc. | Low friction valve train |
US6167856B1 (en) | 1992-11-12 | 2001-01-02 | Ford Global Technologies, Inc. | Low friction cam shaft |
WO1996004466A1 (en) * | 1994-07-22 | 1996-02-15 | Hannoosh James G | A two-cycle ceramic/metallic internal combustion engine |
US6050234A (en) | 1994-07-22 | 2000-04-18 | James G. Hannoosh | Two-cycle ceramic/metallic internal combustion engine |
DE19651069A1 (en) * | 1996-12-09 | 1997-04-30 | Lothar Strach | Oil-less uncooled adiabatic diesel engine |
DE19651069C2 (en) * | 1996-12-09 | 1998-09-10 | Lothar Strach | Oilless and uncooled diesel engine without piston rings with adiabatic operation |
WO2000050753A1 (en) * | 1999-02-22 | 2000-08-31 | Caterpillar Inc. | Free piston internal combustion engine with piston head having non-metallic bearing surface |
US6581381B2 (en) * | 2001-11-15 | 2003-06-24 | Chang Sun Kim | Engine having adiabatic members in its combustion chambers, engine capable of reusing exhausted energy, and high pressure jet assembly having the engine |
US6951193B1 (en) | 2002-03-01 | 2005-10-04 | Draper Samuel D | Film-cooled internal combustion engine |
US20080093849A1 (en) * | 2004-05-26 | 2008-04-24 | Sri International | Compliant walled combustion devices for producing mechanical and electrical energy |
US7485978B2 (en) | 2004-05-26 | 2009-02-03 | Sri International | Compliant walled combustion devices for producing mechanical and electrical energy |
US20060065228A1 (en) * | 2004-05-26 | 2006-03-30 | Sri International | Compliant walled combustion devices II |
US7895985B2 (en) | 2004-05-26 | 2011-03-01 | Sri International | Compliant walled combustion devices |
US7237524B2 (en) | 2004-05-26 | 2007-07-03 | Sri International | Compliant walled combustion devices |
US7240655B2 (en) | 2004-05-26 | 2007-07-10 | Sri International | Compliant walled combustion devices II |
US20060000214A1 (en) * | 2004-05-26 | 2006-01-05 | Sri International | Compliant walled combustion devices |
US20060060164A1 (en) * | 2004-09-20 | 2006-03-23 | Gerfast Sten R | Internal combustion engine without oil |
US7412956B2 (en) * | 2005-05-11 | 2008-08-19 | Kayaba Industry Co., Ltd. | Reinforcing structure of cylinder barrel |
US20060255047A1 (en) * | 2005-05-11 | 2006-11-16 | Mitsunori Gotou | Reinforcing structure of cylinder barrel |
US20100288252A1 (en) * | 2006-09-12 | 2010-11-18 | Marlon Moss | Non-Polluting Two-Stroke Engine with Air-Cooled Piston |
US7895978B2 (en) * | 2006-09-12 | 2011-03-01 | Soundstarts, Inc. | Non-polluting two-stroke engine with air-cooled piston |
US20130319365A1 (en) * | 2012-05-30 | 2013-12-05 | GM Global Technology Operations LLC | Method for in-situ forming of low friction coatings on engine cylinder bores |
US9133739B2 (en) * | 2012-05-30 | 2015-09-15 | GM Global Technology Operations LLC | Method for in-situ forming of low friction coatings on engine cylinder bores |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4872432A (en) | Oilless internal combustion engine having gas phase lubrication | |
AU616944B2 (en) | Uncooled oilless internal combustion engine having uniform gas squeeze film lubrication | |
USRE34143E (en) | Oilless internal combustion engine having gas phase lubrication | |
Nakada | Trends in engine technology and tribology | |
US5469777A (en) | Piston assembly having abradable coating | |
US5598763A (en) | Flutter free piston ring assembly | |
US5490445A (en) | Ultra low device volume piston system | |
US9562491B2 (en) | Carbon scraping ring with abradable coating | |
US5029562A (en) | Hybrid piston for high temperature engine | |
US5392692A (en) | Antiblow-by piston and seal construction for high temperature applications | |
US4598675A (en) | Components for internal combustion engines | |
Essig et al. | Diesel engine emissions reduction—the benefits of low oil consumption design | |
GB2287522A (en) | Making and using a piston ring assembly | |
US6289872B1 (en) | Rotating sleeve engine | |
Takiguchi et al. | Characteristics of friction and lubrication of two-ring piston | |
USRE34336E (en) | Uncooled oilless internal combustion engine having uniform gas squeeze film lubrication | |
McGeehan | A survey of the mechanical design factors affecting engine oil consumption | |
US6050234A (en) | Two-cycle ceramic/metallic internal combustion engine | |
JPH11294255A (en) | Internal combustion engine | |
FURUHAMA | Tribology on reciprocating internal combustion engines | |
JP3890857B2 (en) | Piston lubrication structure | |
Sreenath et al. | Experimental studies on the wear of engine components | |
Taylor | Engine friction lubricant sensitivities: a comparison of modern diesel and gasoline engines | |
GB2189005A (en) | Engines | |
US20060060164A1 (en) | Internal combustion engine without oil |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FPAY | Fee payment |
Year of fee payment: 4 |
|
FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
FPAY | Fee payment |
Year of fee payment: 8 |
|
AS | Assignment |
Owner name: MID-AMERICA COMMERCIALIZATION CORPORATION, A CORP. Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:FORD MOTOR COMPANY;REEL/FRAME:011369/0412 Effective date: 20001031 |
|
AS | Assignment |
Owner name: FORD GLOBAL TECHNOLOGIES, INC. A MICHIGAN CORPORAT Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:FORD MOTOR COMPANY, A DELAWARE CORPORATION;REEL/FRAME:011467/0001 Effective date: 19970301 |
|
FPAY | Fee payment |
Year of fee payment: 12 |
|
AS | Assignment |
Owner name: MID-AMERICA COMMERCIALIZATION, KANSAS Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNOR, PREVIOUSLY RECORDED AT REEL 011369 FRAME 0412;ASSIGNOR:FORD GLOBAL TECHNOLOGIES, INC.;REEL/FRAME:011783/0528 Effective date: 20001201 |
|
AS | Assignment |
Owner name: FORD GLOBAL TECHNOLOGIES, LLC, MICHIGAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:NATIONAL INSTITUTE FOR STRATEGIC TECHNOLOGY ACQUISITION AND COMMERCIALIZATION;REEL/FRAME:017480/0567 Effective date: 20060405 |
|
AS | Assignment |
Owner name: NATIONAL INSTITUTE FOR STRATEGIC TECHNOLOGY ACQUIS Free format text: CHANGE OF NAME;ASSIGNOR:MID-AMERICA COMMERCIALIZATION CORPORATION;REEL/FRAME:019955/0279 Effective date: 20040628 |
|
AS | Assignment |
Owner name: FORD MOTOR COMPANY, MICHIGAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:RAO, VEMULAPALLI DURGA NAGESWAR;WADE, WALLACE R.;REEL/FRAME:020105/0618 Effective date: 19880223 |
|
SULP | Surcharge for late payment |