US20080017164A1 - Piston-pin bearing lubrication system and method for a two sroke internal combustion engine - Google Patents
Piston-pin bearing lubrication system and method for a two sroke internal combustion engine Download PDFInfo
- Publication number
- US20080017164A1 US20080017164A1 US11/818,660 US81866007A US2008017164A1 US 20080017164 A1 US20080017164 A1 US 20080017164A1 US 81866007 A US81866007 A US 81866007A US 2008017164 A1 US2008017164 A1 US 2008017164A1
- Authority
- US
- United States
- Prior art keywords
- pump
- connecting rod
- piston
- oil
- stroke cycle
- 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.)
- Abandoned
Links
- 238000000034 method Methods 0.000 title claims abstract description 16
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 10
- 238000005461 lubrication Methods 0.000 title abstract description 16
- 239000010687 lubricating oil Substances 0.000 claims abstract description 29
- 239000003921 oil Substances 0.000 claims description 62
- 230000001133 acceleration Effects 0.000 claims description 7
- 230000001050 lubricating effect Effects 0.000 claims description 7
- 238000004891 communication Methods 0.000 claims description 6
- 238000006243 chemical reaction Methods 0.000 claims description 5
- 238000002347 injection Methods 0.000 claims description 4
- 239000007924 injection Substances 0.000 claims description 4
- 238000000926 separation method Methods 0.000 claims description 4
- 238000013459 approach Methods 0.000 description 7
- 238000007906 compression Methods 0.000 description 5
- 239000010705 motor oil Substances 0.000 description 5
- 230000006835 compression Effects 0.000 description 4
- 238000005086 pumping Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 2
- 239000012141 concentrate Substances 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003534 oscillatory effect Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
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
- F01M1/00—Pressure lubrication
- F01M1/02—Pressure lubrication using lubricating pumps
-
- 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
- F01M1/06—Lubricating systems characterised by the provision therein of crankshafts or connecting rods with lubricant passageways, e.g. bores
-
- 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
- F01M1/02—Pressure lubrication using lubricating pumps
- F01M2001/0207—Pressure lubrication using lubricating pumps characterised by the type of pump
-
- 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
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/02—Arrangements of lubricant conduits
- F01M2011/025—Arrangements of lubricant conduits for lubricating gudgeon pins
-
- 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
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B19/00—Machines or pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B1/00 - F04B17/00
- F04B19/20—Other positive-displacement pumps
- F04B19/22—Other positive-displacement pumps of reciprocating-piston type
Definitions
- This invention is related to the field of internal combustion engines and more specifically to a lubrication system and method that supplies lubricating oil to the piston-pin bearings of two-cycle engines.
- Some conventional internal combustion engines are configured to provide lubricating oil to piston-pin bearings by pumping the oil into the small gap surrounding much of the circumference of the pin.
- one portion of the pin is in constant contact with the journal surface of the connecting rod during the entire stroke cycle of the engine. That portion is difficult to lubricate and is subject to wear.
- lubricating oil is pumped through passages in the crankshaft and connecting rods to the piston pins.
- the present invention provides several improvements to the piston-pin lubricating system of two-cycle engines. Several embodiments are shown which utilize an inertia pump in a connecting rod to overcome the forces and inject the proper amount of oil between the normally abutting bearing surfaces of the piston-pin and connecting rod journal.
- inertia pumps takes advantage of the changing speeds of the pistons and connecting rods that occur during each stroke cycle of the engine.
- the acceleration and deceleration forces cause the plunger mass within each the inertia pump to react and cause the pump to become charged with lubricating oil as it approaches its top dead center (“TDC”) position and then to inject a predetermined amount of oil under high pressure between the surfaces of the piston pin and the connecting rod journal as it approaches bottom dead center (“BDC”) position.
- TDC top dead center
- BDC bottom dead center
- the timing of the injection near BDC is selected because the gas forces present on the piston are at their minimum and only the inertia forces on the piston have to be overcome by the output of the inertia pump. This causes a sufficient separation between the surfaces to allow a predetermined charge of lubricating oil to flow there-between.
- a single check valve is employed along with an inertia driven plunger.
- the check valve becomes open and allows oil to flow from an external pressure source (the engine oil pump) into the pumping chamber and out of the inertia pump into the piston pin bearing during the time when the piston decelerates while approaching its TDC in the later part of the compression stroke and also when the piston accelerates during the early portion of the expansion stroke following TDC.
- an external pressure source the engine oil pump
- the check valve closes and the pump plunger forces oil out of the inertia pump under high pressure.
- the closed check valve prevents the oil pumped by the pump plunger from flowing back to the pressure source while the inertia pump forces oil into the piston pin bearing under a high pressure that is greater than the inertia pressure holding the bearing surfaces together. This results in a brief separation of the surfaces and their lubrication.
- the check valve is replaced with a freely sliding inertia mass valve that moves independent of the inertia driven pump plunger.
- the operation is similar to the first embodiment.
- the inertia valve is subject to the inertia induced motion in the valve chamber independent of the same inertia forces that subject the pump plunger to move within the pump chamber.
- the inertia valve can be selected to react earlier or later than the plunger during the stroke cycle to prolong or earlier terminate the flow of oil from the source through the inertia pump.
- One result of earlier termination would be for the plunger to inject more oil into the space forced open between the bearing surfaces.
- FIG. 1 is a cutaway drawing of a two-cycle OPOC engine showing the location of the embodiments of the present invention.
- FIG. 2A is a cross-sectional view of a first embodiment of an inertia pump used in the inner piston connecting rods the OPOC engine shown in FIG. 1 .
- FIG. 2B is a cross-sectional view of the piston plunger of the inertia pump shown in FIG. 2A taken along section lines 2 B- 2 B.
- FIG. 2C is a cross-sectional view of a first embodiment of an inertia pump used in the outer piston connecting rods the OPOC engine shown in FIG. 1 .
- FIG. 2D is a cross-sectional view of the piston plunger of the inertia pump shown in FIG. 2C taken along section lines 2 D- 2 D.
- FIG. 3A is a cross-sectional view of a second embodiment of an inertia pump used in the connecting rods the OPOC engine shown in FIG. 1 near and at TDC of the stroke cycle.
- FIG. 3B is a cross-sectional view of the inertia pump shown in FIG. 3A at the mid-stroke position between TDC and BDC.
- FIG. 3C is a cross-sectional view of the inertia pump shown in FIGS. 3A and 3B near and at BDC of the stroke cycle.
- FIG. 3D is a cross-sectional view of the pumping chamber taken along lines 3 D- 3 D in FIG. 3A .
- FIG. 4A is a cross-sectional view of a third embodiment of an inertia pump used in the connecting rods the OPOC engine shown in FIG. 1 near and at TDC of the stroke cycle.
- FIG. 4B is a cross-sectional view of the inertia pump shown in FIG. 4A at the mid-stroke position between TDC and BDC.
- FIG. 4C is a cross-sectional view of the inertia pump shown in FIGS. 4A and 4B near and at BDC of the stroke cycle.
- FIG. 4D is a cross-sectional view of the pumping chamber taken along lines 4 D- 4 D in FIG. 4A .
- FIG. 5A is a cross-sectional view taken across the axis of a piston-pin within a piston journal when the piston is at its BDC position.
- FIG. 5B is a cross-sectional view taken across the axis of the piston-pin shown in FIG. 5A rotated to one extreme during the stroke cycle.
- FIG. 5C is a cross-sectional view taken across the axis of the piston-pin shown in FIG. 5A rotated to its opposite extreme during the stroke cycle.
- FIG. 6 is a perspective view of an inner piston connecting rod of an OPOC engine such as shown in FIG. 1 .
- FIG. 7 is a perspective view of the underside of an inner piston and associated piston pin of an OPOC engine such as shown in FIG. 1 accommodated for use with the present invention.
- FIG. 8 is a perspective view of the present invention installed within the outer connecting rods of an OPOC engine such as shown in FIG. 1 .
- FIG. 9 is a chart that shows the plot the inertia forces present on an inertia pump plunger during a full stroke cycle of the inner and outer pistons in an OPOC engine, such as shown in FIG. 1 .
- FIG. 1 opposing left cylinder 102 and right cylinder 104 of an OPOC engine 100 are shown in a cut-away view.
- Inner pistons PLI (left) and PRI (right) respectively oppose outer piston PLO (left) and PRO (right) within the corresponding cylinders 102 and 104 .
- Inner connecting (push) rods 120 and 130 provide power connections between the inner pistons PLI and PRI and the crankshaft 110 .
- Outer connecting (pull) rod sets 140 , 141 and 150 , 151 provide power connections between the outer pistons PLO and PRO and crankshaft 110 .
- Each of the connecting rods has a “small” end which is connected to a piston pin.
- Piston pins 180 and 190 are associated with pistons PLI and PRI, while piston pins 142 and 143 are associated with pistons PLO and PRO.
- FIG. 6 a detailed view of push rod 120 is shown, while in FIG. 8 a detailed view of pull rods 140 and 141 are shown.
- each connecting rod an inertia pump is shown as installed to provide the lubrication to the piston pin as discussed above in the Summary of the Invention.
- Inertia pumps 200 , 201 , 300 , 300 ′, 200 ′ and 201 ′ are respectively installed in corresponding connecting rods 140 , 141 , 120 , 130 , 150 and 151 .
- Each connecting rod has oil passages that function in a conventional way to convey lubricating oil from an oil pump through the crankshaft and connecting rods to the piston pins.
- FIGS. 2A and 2B a first embodiment of an inertia pump 200 , such as that shown installed in pull rod 140 in FIG. 1 , is shown.
- Pump 200 has a housing 201 and is shown for use in association with a pull rod and outer left piston PLO.
- a plunger 202 is the core of the pump since it slides within a two stage bore in the pump housing 201 in reaction to deceleration and acceleration forces present in the pull rod over the stroke cycle.
- the plunger 202 is defined to have a first cylindrical mass portion 204 with grooves 203 formed along its length.
- the grooves 203 are sufficiently large to allow the plunger to be moved by inertia forces with little resistance by oil present in the housing and also to allow oil to pass through the pump from the entry port 206 to the outlet port 216 due to pressure maintained by the engine oil pump (not shown).
- the two stage pump bore includes an oil supply section 205 and a plunger bore section 207 .
- the plunger element 202 is also a two stage element that resides within the pump bore and its plunger mass portion 204 resides totally in bore section 213 and its plunger pump portion 210 extends from plunger mass portion 204 to move within plunger bore section 207 .
- a stopper element 209 is located at one end of section 205 to limit movement of the plunger element therein. Stopper element 209 is adjacent an input port 206 through which oil enters inertia pump 200 from the lubricating passages in the connecting rod.
- the embodiment of the inertia pump 200 shown in FIGS. 2A and 2B is exemplified as being in the final portion of its stroke towards BDC, at BDC, or in the early portion of the stroke following BDC.
- the inertia forces continue to push the plunger element to its extreme left position, as the outer left piston PLO would be at BDC, and the oil has been expelled at a high pressure from the bore section 207 by the plunger pump portion 210 .
- a normally open check valve 212 is provided in the pump chamber 214 .
- the pressure provided by the inertia pump and the inertia forces acting on the valve itself cause check valve 212 to close. This closing serves to concentrate the oil being pumped by the plunger pump portion 210 into outlet port 216 and into the piston pin bearing.
- check valve 212 also prevents back-flow into the oil supply passages in the connecting rod.
- check valve 212 In other positions of the stroke, check valve 212 remains open and allows lubricating oil from the engine oil pump to provide oil in a conventional manner through the connecting rod and inertia pump 200 via input port 206 , grooves 203 , passage 208 , check valve 212 , chamber 214 and outlet port 216 . Although such pressure is sufficient to effect lubrication of parts of the piston pin and journal surfaces, it is not sufficient to overcome the forces which cause the portions of the pin and piston journal surfaces to be held together.
- an embodiment off an inertia pump 300 is shown to be suitable for installation in a push rod, such as 120 associated with left inner piston PLI.
- the pump 300 has a housing 301 with an inlet port 306 and an outlet port 316 .
- the pump embodiment shown in FIG. 2C is oriented opposite to the embodiment shown in FIG. 2A , since the inertia forces acting on those pumps approaching and leaving the BDC positions of their associated outer and inner pistons are opposite.
- a plunger 302 is also the core of the pump since it slides within a two stage bore in pump housing 301 in reaction to deceleration and acceleration forces present in the push rod over the stroke cycle.
- the plunger 302 is defined to have a first cylindrical mass portion 304 with grooves 303 formed along its length.
- the grooves 303 are sufficiently large to allow the plunger to be moved by inertia forces with little resistance by oil present in the housing and also to allow oil to pass through the pump from the entry port 206 to the outlet port 216 due to pressure maintained by the engine oil pump (not shown).
- the grooves 303 also provide a path for oil to flow under high pressure when it is pumped by plunger element 302 .
- the two stage pump bore includes a mass bore section 305 and a plunger bore section 207 .
- Mass bore section 305 is also in communication with the outlet port 316 .
- the plunger element 302 is also a two stage element that resides within the pump bore and its plunger mass portion 304 resides totally in mass bore section 305 and its plunger pump portion 310 extends from plunger mass portion 304 to move within plunger bore section 307 .
- a stopper element 309 is located at one end of section 305 to limit movement of the plunger element therein. Stopper element 309 is adjacent a central outlet port opening 316 through which oil exits the inertia pump 300 to the piston pin bearing.
- a normally open check valve 312 is provided in the pump chamber 314 .
- the pressure provided by the inertia pump and the inertia forces acting on the valve itself cause check valve 312 to close. This closing serves to concentrate the oil being pumped by the plunger pump portion 310 through passage 308 , plunger grooves 303 , outlet port 216 and into the piston pin bearing.
- check valve 212 When closed, check valve 212 also prevents back flow into the oil supply passages in the connecting rod.
- the check valve 312 opens and allows lubrication oil from the lower pressure oil pump system to flow in a conventional manner through the inertia pump and into the bearing as discussed above.
- FIGS. 4A-4D illustrate yet another embodiment of an inertia pump 600 that can be utilized in the present invention.
- the Figures illustrate the same inertia pump 600 in three different stages of its operation.
- the associated piston is in the later part of its compression stroke approaching TDC, at TDC or beginning its expansion stroke following TDC.
- oil from the lubrication system pump is allowed to flow through inertia pump 600 and to the associated piston pin.
- Housing 601 has an oil entry port 606 and an outlet port 616 .
- a two stage plunger element 602 has a plunger mass portion 604 and a pump plunger portion 610 that is similar to the other embodiments discussed above.
- the plunger mass portion 604 contains at least one aperture or groove 603 that allows oil to freely flow from entry port 606 and into a pump bore 611 and reduces and resistance to the longitudinal movement of the plunger mass within pump bore 611 .
- a pump chamber 614 surrounds pump plunger 610 and contains a set of grooved openings 618 that allow oil to flow past pump plunger 610 when it is in the position shown in FIG. 4A .
- a cylindrical mass 612 containing a central passage 619 freely moves within a bore 615 and replaces check valve 512 shown in the prior described embodiment.
- Cylindrical mass 612 is neither normally open nor normally closed, as spring loaded check valves are configured. Instead, cylindrical mass 612 is inertia driven, but independent from the plunger 602 .
- cylindrical mass 612 can be configured by its size, its mass and its aperture resistance to open and close the supply opening 617 at precise positions in the stoke cycle and thereby provide for increased timing of the oil flow from the conventional engine pump source while allowing the pump chamber 614 to become primed when plunger 610 is driven as it approaches BDC.
- supply opening 617 is open because inertia forces have caused cylindrical mass 612 to be located at the right side of bore 617 .
- Oil from the conventional source is pumped through inertia pump 600 via entry port 606 , plunger aperture 603 , chamber 611 , grooves 618 , into bore 621 , and oil passage 613 , port 617 aperture 619 , chamber 614 , passage 615 and outlet port 616 .
- Passage 613 is indicated as ghost lines in FIGS. 4A , 4 B and 4 C. Passage 613 is better illustrated in FIG. 4D as being offset from the planar section provided for FIGS. 4A , 4 B and 4 C. Passage 613 provides communication flow of lubricating oil between plunger chamber 611 and pump chamber 614 . In the position illustrated in FIG. 4A , the lubricating oil sourced under normal pressure from the engine oil pump passes through pump chamber 614 , leaving it filled and primed, and into passage 615 to exit through outlet port 616 .
- the inertia pump is shown at a later portion of the expansion stroke when inertia forces are starting to reverse and thereby causing the cylindrical mass 612 to be forced towards the left and closing port 617 .
- plunger mass 602 is also forced towards the left and grooves 618 become blocked.
- high pressure is being developed by the movement of plunger pump 610 in bore 621 . This prevents conventionally pumped lubricating oil from flowing into the bearing while pressure is built up to overcome the forces which cause the bearing surfaces to be forced together.
- pump 600 is shown as having reached the later portion of the expansion stroke approaching BDC, at BDC, or in the beginning of the compression stroke following BDC. In these positions, the inertia forces present in pump 600 become high enough to cause the injection of a predetermined volume of lubrication oil between the piston pin and piston journal surfaces. Forces present at the output port 616 cause the piston pin and piston journal surfaces to be separated sufficiently to allow oil to flow therebetween.
- piston pin 180 is mounted on an inner piston PLI and has a central surface which fit within a journal 188 at the small end of an inner piston connecting rod 120 .
- inertia pumps have not been indicated.
- the ghost lines of FIG. 6 indicate oil passages and a void were an inertia pump is located.
- the connecting rod 120 is constantly being driven by either its associated inner piston or the crankshaft and its small end is subject to oscillatory movement over the limited angles indicated beyond TDC and BDC.
- FIG. 5A illustrates the orientation of a piston pin at both its TDC and BDC positions.
- An axial oil passage 182 is formed in piston pin 180 and is in communication a radial passage 184 .
- An arcing groove 186 is formed on the outer surface of the piston pin 180 and is aligned with the opening of radial passage 184 .
- a journal is formed having a cylindrical surface 188 that is slightly larger in diameter than the piston pin 180 . Spaced apart cross grooves 187 and 189 are formed in the journal surface.
- Oil passage 124 in communication with the outlet port of an inertial pump within the connecting rod, opens through the journal surface 188 and is in constant registration and alignment with arcing groove 186 in piston pin 10 .
- oil flows from the inertia pump when the piston is at BDC in FIG. 5A .
- the oil is injected at a high enough pressure to overcome the inertia pressures forcing the surfaces 185 and 188 together.
- the oil flows from passage 124 into arc groove 186 and spreads over the adjacent area of the abutting surfaces to provide lubrication.
- cross groove 187 becomes exposed to arc groove 186 and oil from the conventional lubrication pump flows into the cross groove. Lubricating oil is then spread over that portion of the abutting surfaces 188 and 185 that pass over cross groove 187 .
- cross groove 189 becomes exposed to arc groove 186 and oil from the conventional lubrication pump flows into cross groove 189 . Lubricating oil is then spread over that portion of the abutting surfaces 188 and 185 that pass over cross groove 189 .
- FIG. 8 an outer piston pin and connecting rod assembly is shown wherein connecting rods 140 and 141 each contain inertia pumps 200 and 201 .
- Connecting rods 140 and 141 are connected to a cross member 145 which supports an outer piston pin 142 .
- the outer piston pin contains a pair of arc grooves 146 and 146 ′.
- Oil passages 144 and 144 ′ are centrally located within each arc groove to provide the injected oil from the inertia pump and oil from a conventional oil pump identical in manner to that explained with respect to the inner piston pins above. That is, the journal of the outer piston (not shown) has spaced apart cross grooves to distribute oil when the inertia pump is not injecting lubricating oil between the abutting bearing surfaces.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
An improved lubrication system and method for the normally contacting and abutting piston pin and connecting rod journal bearing surfaces of an internal combustion engine that includes an inertia pump in a connecting rod. The inertia pump reacts to the movement of the connecting rod and conveys a predetermined measure of lubricating oil at a high enough pressure to overcome the forces which cause the surfaces to normally maintain contact. By separating the normally contacting surfaces of the pin and the connecting rod journal, the surfaces become lubricated. Several embodiments of inertia pumps provide variations in implementing the invention.
Description
- This application claims the benefit of U.S. provisional application Ser. No. 60/832,646 filed Jul. 21, 2006.
- This invention is related to the field of internal combustion engines and more specifically to a lubrication system and method that supplies lubricating oil to the piston-pin bearings of two-cycle engines.
- Some conventional internal combustion engines are configured to provide lubricating oil to piston-pin bearings by pumping the oil into the small gap surrounding much of the circumference of the pin. However because of the way two-cycle engines operate, one portion of the pin is in constant contact with the journal surface of the connecting rod during the entire stroke cycle of the engine. That portion is difficult to lubricate and is subject to wear.
- In some two-cycle engines, such as the Internal Combustion Engine With A Single Crankshaft And Having Opposing Cylinders And Opposing Pistons In Each Cylinder (“OPOC engine”) described in my U.S. Pat. No. 6,170,443 and incorporated herein by reference, lubricating oil is pumped through passages in the crankshaft and connecting rods to the piston pins.
- There is a need to improve the piston-pin lubrication system as it applies to two-cycle engines, since available oil pressure in conventional engines does not overcome the combustion gas forces and inertia forces that act on the piston-pins during the entire stroke cycle in the direction towards the crankshaft to provide effective lubrication. Without sufficient lubrication, excess heat and frictional wear may result.
- The present invention provides several improvements to the piston-pin lubricating system of two-cycle engines. Several embodiments are shown which utilize an inertia pump in a connecting rod to overcome the forces and inject the proper amount of oil between the normally abutting bearing surfaces of the piston-pin and connecting rod journal.
- The use of inertia pumps in the embodiments takes advantage of the changing speeds of the pistons and connecting rods that occur during each stroke cycle of the engine. The acceleration and deceleration forces cause the plunger mass within each the inertia pump to react and cause the pump to become charged with lubricating oil as it approaches its top dead center (“TDC”) position and then to inject a predetermined amount of oil under high pressure between the surfaces of the piston pin and the connecting rod journal as it approaches bottom dead center (“BDC”) position. The timing of the injection near BDC is selected because the gas forces present on the piston are at their minimum and only the inertia forces on the piston have to be overcome by the output of the inertia pump. This causes a sufficient separation between the surfaces to allow a predetermined charge of lubricating oil to flow there-between.
- In a first embodiment of an inertia pump, a single check valve is employed along with an inertia driven plunger. The check valve becomes open and allows oil to flow from an external pressure source (the engine oil pump) into the pumping chamber and out of the inertia pump into the piston pin bearing during the time when the piston decelerates while approaching its TDC in the later part of the compression stroke and also when the piston accelerates during the early portion of the expansion stroke following TDC.
- As the piston passes through its mid-compression stroke and mid-expansion stroke the inertia forces become minimal and the angles of the connecting rods with respect to the piston pins are at their extremes. During these strokes the check valve opens and oil from the external pressure source flows through the inertia pump and into grooves formed in the piston pin and journal.
- In reaction to the inertia caused movement of the pump plunger mass and the check valve mass as the piston decelerates during the later portion of the expansion stroke as it approaches BDC and during the acceleration that occurs during the early portion of the compression stroke immediately following BDC, the check valve closes and the pump plunger forces oil out of the inertia pump under high pressure. The closed check valve prevents the oil pumped by the pump plunger from flowing back to the pressure source while the inertia pump forces oil into the piston pin bearing under a high pressure that is greater than the inertia pressure holding the bearing surfaces together. This results in a brief separation of the surfaces and their lubrication.
- In a second embodiment, the check valve is replaced with a freely sliding inertia mass valve that moves independent of the inertia driven pump plunger. In this embodiment, the operation is similar to the first embodiment. However, the inertia valve is subject to the inertia induced motion in the valve chamber independent of the same inertia forces that subject the pump plunger to move within the pump chamber. By being independently subject to the same inertia forces that are applied to the plunger, the inertia valve can be selected to react earlier or later than the plunger during the stroke cycle to prolong or earlier terminate the flow of oil from the source through the inertia pump. One result of earlier termination would be for the plunger to inject more oil into the space forced open between the bearing surfaces.
- It is an object of the present invention to provide an improved lubricating system and method for a two-cycle engine by providing an inertia pump within a connecting rod to supplement the flow of lubricating oil into the associated piston pin by forcibly injecting a predetermined amount of oil between the abutting piston pin and the connecting rod journal surfaces.
- It is another object of the present invention to provide an improved lubricating system and method for a two-cycle engine by providing an oil pump that acts in response to deceleration and acceleration of the piston as it approaches and exits its BDC portion of the stroke to overcome the forces between the abutting piston pin and the connecting rod journal surfaces and injecting a predetermined amount of oil therebetween.
- It is a further object of the present invention to provide improved inertia pumps suitable for use within the moving components of an internal combustion engine.
-
FIG. 1 is a cutaway drawing of a two-cycle OPOC engine showing the location of the embodiments of the present invention. -
FIG. 2A is a cross-sectional view of a first embodiment of an inertia pump used in the inner piston connecting rods the OPOC engine shown inFIG. 1 . -
FIG. 2B is a cross-sectional view of the piston plunger of the inertia pump shown inFIG. 2A taken alongsection lines 2B-2B. -
FIG. 2C is a cross-sectional view of a first embodiment of an inertia pump used in the outer piston connecting rods the OPOC engine shown inFIG. 1 . -
FIG. 2D is a cross-sectional view of the piston plunger of the inertia pump shown inFIG. 2C taken alongsection lines 2D-2D. -
FIG. 3A is a cross-sectional view of a second embodiment of an inertia pump used in the connecting rods the OPOC engine shown inFIG. 1 near and at TDC of the stroke cycle. -
FIG. 3B is a cross-sectional view of the inertia pump shown inFIG. 3A at the mid-stroke position between TDC and BDC. -
FIG. 3C is a cross-sectional view of the inertia pump shown inFIGS. 3A and 3B near and at BDC of the stroke cycle. -
FIG. 3D is a cross-sectional view of the pumping chamber taken alonglines 3D-3D inFIG. 3A . -
FIG. 4A is a cross-sectional view of a third embodiment of an inertia pump used in the connecting rods the OPOC engine shown inFIG. 1 near and at TDC of the stroke cycle. -
FIG. 4B is a cross-sectional view of the inertia pump shown inFIG. 4A at the mid-stroke position between TDC and BDC. -
FIG. 4C is a cross-sectional view of the inertia pump shown inFIGS. 4A and 4B near and at BDC of the stroke cycle. -
FIG. 4D is a cross-sectional view of the pumping chamber taken alonglines 4D-4D inFIG. 4A . -
FIG. 5A is a cross-sectional view taken across the axis of a piston-pin within a piston journal when the piston is at its BDC position. -
FIG. 5B is a cross-sectional view taken across the axis of the piston-pin shown inFIG. 5A rotated to one extreme during the stroke cycle. -
FIG. 5C is a cross-sectional view taken across the axis of the piston-pin shown inFIG. 5A rotated to its opposite extreme during the stroke cycle. -
FIG. 6 is a perspective view of an inner piston connecting rod of an OPOC engine such as shown inFIG. 1 . -
FIG. 7 is a perspective view of the underside of an inner piston and associated piston pin of an OPOC engine such as shown inFIG. 1 accommodated for use with the present invention. -
FIG. 8 is a perspective view of the present invention installed within the outer connecting rods of an OPOC engine such as shown inFIG. 1 . -
FIG. 9 is a chart that shows the plot the inertia forces present on an inertia pump plunger during a full stroke cycle of the inner and outer pistons in an OPOC engine, such as shown inFIG. 1 . - While the present invention is summarized above as being applicable for several types of internal combustion engines, it is exemplified herein as being installed in a two-cycle OPOC engine, such as that shown in my referenced patent.
- In
FIG. 1 , opposingleft cylinder 102 andright cylinder 104 of anOPOC engine 100 are shown in a cut-away view. Inner pistons PLI (left) and PRI (right) respectively oppose outer piston PLO (left) and PRO (right) within the correspondingcylinders rods crankshaft 110. Outer connecting (pull) rod sets 140, 141 and 150, 151 provide power connections between the outer pistons PLO and PRO andcrankshaft 110. Each of the connecting rods has a “small” end which is connected to a piston pin. Piston pins 180 and 190 are associated with pistons PLI and PRI, while piston pins 142 and 143 are associated with pistons PLO and PRO. InFIG. 6 a detailed view ofpush rod 120 is shown, while inFIG. 8 a detailed view ofpull rods - In each connecting rod, an inertia pump is shown as installed to provide the lubrication to the piston pin as discussed above in the Summary of the Invention. Inertia pumps 200, 201, 300, 300′, 200′ and 201′ are respectively installed in corresponding connecting
rods - In
FIGS. 2A and 2B , a first embodiment of aninertia pump 200, such as that shown installed inpull rod 140 inFIG. 1 , is shown.Pump 200 has ahousing 201 and is shown for use in association with a pull rod and outer left piston PLO. Aplunger 202 is the core of the pump since it slides within a two stage bore in thepump housing 201 in reaction to deceleration and acceleration forces present in the pull rod over the stroke cycle. Theplunger 202 is defined to have a firstcylindrical mass portion 204 withgrooves 203 formed along its length. Thegrooves 203 are sufficiently large to allow the plunger to be moved by inertia forces with little resistance by oil present in the housing and also to allow oil to pass through the pump from theentry port 206 to theoutlet port 216 due to pressure maintained by the engine oil pump (not shown). - The two stage pump bore includes an
oil supply section 205 and aplunger bore section 207. Theplunger element 202 is also a two stage element that resides within the pump bore and itsplunger mass portion 204 resides totally inbore section 213 and itsplunger pump portion 210 extends fromplunger mass portion 204 to move withinplunger bore section 207. Astopper element 209 is located at one end ofsection 205 to limit movement of the plunger element therein.Stopper element 209 is adjacent aninput port 206 through which oil enters inertia pump 200 from the lubricating passages in the connecting rod. - The embodiment of the
inertia pump 200 shown inFIGS. 2A and 2B is exemplified as being in the final portion of its stroke towards BDC, at BDC, or in the early portion of the stroke following BDC. At this position the inertia forces continue to push the plunger element to its extreme left position, as the outer left piston PLO would be at BDC, and the oil has been expelled at a high pressure from thebore section 207 by theplunger pump portion 210. (See the plot of forces approaching and leaving 0 (360) degrees or BDC position inFIG. 9 .) - A normally
open check valve 212 is provided in thepump chamber 214. In the shown position, the pressure provided by the inertia pump and the inertia forces acting on the valve itself causecheck valve 212 to close. This closing serves to concentrate the oil being pumped by theplunger pump portion 210 intooutlet port 216 and into the piston pin bearing. When closed,check valve 212 also prevents back-flow into the oil supply passages in the connecting rod. - In other positions of the stroke,
check valve 212 remains open and allows lubricating oil from the engine oil pump to provide oil in a conventional manner through the connecting rod andinertia pump 200 viainput port 206,grooves 203,passage 208,check valve 212,chamber 214 andoutlet port 216. Although such pressure is sufficient to effect lubrication of parts of the piston pin and journal surfaces, it is not sufficient to overcome the forces which cause the portions of the pin and piston journal surfaces to be held together. - In
FIGS. 2C and 2D , an embodiment off aninertia pump 300 is shown to be suitable for installation in a push rod, such as 120 associated with left inner piston PLI. In that embodiment, thepump 300 has ahousing 301 with aninlet port 306 and anoutlet port 316. The pump embodiment shown inFIG. 2C is oriented opposite to the embodiment shown inFIG. 2A , since the inertia forces acting on those pumps approaching and leaving the BDC positions of their associated outer and inner pistons are opposite. - In
FIG. 2C , aplunger 302 is also the core of the pump since it slides within a two stage bore inpump housing 301 in reaction to deceleration and acceleration forces present in the push rod over the stroke cycle. Theplunger 302 is defined to have a firstcylindrical mass portion 304 withgrooves 303 formed along its length. Thegrooves 303 are sufficiently large to allow the plunger to be moved by inertia forces with little resistance by oil present in the housing and also to allow oil to pass through the pump from theentry port 206 to theoutlet port 216 due to pressure maintained by the engine oil pump (not shown). Thegrooves 303 also provide a path for oil to flow under high pressure when it is pumped byplunger element 302. - The two stage pump bore includes a
mass bore section 305 and aplunger bore section 207. Mass boresection 305 is also in communication with theoutlet port 316. Theplunger element 302 is also a two stage element that resides within the pump bore and itsplunger mass portion 304 resides totally inmass bore section 305 and itsplunger pump portion 310 extends fromplunger mass portion 304 to move withinplunger bore section 307. Astopper element 309 is located at one end ofsection 305 to limit movement of the plunger element therein.Stopper element 309 is adjacent a centraloutlet port opening 316 through which oil exits theinertia pump 300 to the piston pin bearing. - A normally
open check valve 312 is provided in thepump chamber 314. In the shown position, the pressure provided by the inertia pump and the inertia forces acting on the valve itself causecheck valve 312 to close. This closing serves to concentrate the oil being pumped by theplunger pump portion 310 throughpassage 308,plunger grooves 303,outlet port 216 and into the piston pin bearing. When closed,check valve 212 also prevents back flow into the oil supply passages in the connecting rod. - In positions other than approaching and leaving BDC, the
check valve 312 opens and allows lubrication oil from the lower pressure oil pump system to flow in a conventional manner through the inertia pump and into the bearing as discussed above. -
FIGS. 4A-4D illustrate yet another embodiment of aninertia pump 600 that can be utilized in the present invention. In this embodiment, the Figures illustrate thesame inertia pump 600 in three different stages of its operation. InFIG. 4A , the associated piston is in the later part of its compression stroke approaching TDC, at TDC or beginning its expansion stroke following TDC. In this position, oil from the lubrication system pump is allowed to flow throughinertia pump 600 and to the associated piston pin.Housing 601 has anoil entry port 606 and anoutlet port 616. A twostage plunger element 602 has aplunger mass portion 604 and apump plunger portion 610 that is similar to the other embodiments discussed above. As in the prior embodiment, theplunger mass portion 604 contains at least one aperture or groove 603 that allows oil to freely flow fromentry port 606 and into apump bore 611 and reduces and resistance to the longitudinal movement of the plunger mass withinpump bore 611. - A
pump chamber 614 surroundspump plunger 610 and contains a set ofgrooved openings 618 that allow oil to flowpast pump plunger 610 when it is in the position shown inFIG. 4A . - A
cylindrical mass 612 containing acentral passage 619 freely moves within abore 615 and replacescheck valve 512 shown in the prior described embodiment.Cylindrical mass 612 is neither normally open nor normally closed, as spring loaded check valves are configured. Instead,cylindrical mass 612 is inertia driven, but independent from theplunger 602. In this configuration,cylindrical mass 612 can be configured by its size, its mass and its aperture resistance to open and close thesupply opening 617 at precise positions in the stoke cycle and thereby provide for increased timing of the oil flow from the conventional engine pump source while allowing thepump chamber 614 to become primed whenplunger 610 is driven as it approaches BDC. - In
FIG. 4A ,supply opening 617 is open because inertia forces have causedcylindrical mass 612 to be located at the right side ofbore 617. Oil from the conventional source, is pumped throughinertia pump 600 viaentry port 606,plunger aperture 603,chamber 611,grooves 618, intobore 621, andoil passage 613,port 617aperture 619,chamber 614,passage 615 andoutlet port 616. -
Passage 613 is indicated as ghost lines inFIGS. 4A , 4B and 4C.Passage 613 is better illustrated inFIG. 4D as being offset from the planar section provided forFIGS. 4A , 4B and 4C.Passage 613 provides communication flow of lubricating oil betweenplunger chamber 611 and pumpchamber 614. In the position illustrated inFIG. 4A , the lubricating oil sourced under normal pressure from the engine oil pump passes throughpump chamber 614, leaving it filled and primed, and intopassage 615 to exit throughoutlet port 616. - In
FIG. 4B , the inertia pump is shown at a later portion of the expansion stroke when inertia forces are starting to reverse and thereby causing thecylindrical mass 612 to be forced towards the left andclosing port 617. Independently,plunger mass 602 is also forced towards the left andgrooves 618 become blocked. Withport 617 being closed bycylindrical ass 612 andgrooves 618 blocked byplunger mass 602 being forced towards the left, high pressure is being developed by the movement ofplunger pump 610 inbore 621. This prevents conventionally pumped lubricating oil from flowing into the bearing while pressure is built up to overcome the forces which cause the bearing surfaces to be forced together. - In
FIG. 4C , pump 600 is shown as having reached the later portion of the expansion stroke approaching BDC, at BDC, or in the beginning of the compression stroke following BDC. In these positions, the inertia forces present inpump 600 become high enough to cause the injection of a predetermined volume of lubrication oil between the piston pin and piston journal surfaces. Forces present at theoutput port 616 cause the piston pin and piston journal surfaces to be separated sufficiently to allow oil to flow therebetween. - With reference to
FIGS. 5A , 5B, 5C, 6 and 7, the piston pin and connecting rod journal lubrication distribution system for a piston is shown. In the figures,piston pin 180 is mounted on an inner piston PLI and has a central surface which fit within ajournal 188 at the small end of an innerpiston connecting rod 120. In these drawings, the inertia pumps have not been indicated. However, the ghost lines ofFIG. 6 indicate oil passages and a void were an inertia pump is located. The connectingrod 120 is constantly being driven by either its associated inner piston or the crankshaft and its small end is subject to oscillatory movement over the limited angles indicated beyond TDC and BDC. -
FIG. 5A illustrates the orientation of a piston pin at both its TDC and BDC positions. Anaxial oil passage 182 is formed inpiston pin 180 and is in communication aradial passage 184. An arcinggroove 186 is formed on the outer surface of thepiston pin 180 and is aligned with the opening ofradial passage 184. In thesmall end 122 of connecting rod 120 (FIG. 6 ), a journal is formed having acylindrical surface 188 that is slightly larger in diameter than thepiston pin 180. Spaced apart crossgrooves Oil passage 124, in communication with the outlet port of an inertial pump within the connecting rod, opens through thejournal surface 188 and is in constant registration and alignment with arcinggroove 186 in piston pin 10. - In operation in conjunction with the inertia pump, oil flows from the inertia pump when the piston is at BDC in
FIG. 5A . The oil is injected at a high enough pressure to overcome the inertia pressures forcing thesurfaces passage 124 intoarc groove 186 and spreads over the adjacent area of the abutting surfaces to provide lubrication. - When the engine cycles past BDC and the connecting rod approaches the extreme limit of its angle in a first direction,
cross groove 187 becomes exposed toarc groove 186 and oil from the conventional lubrication pump flows into the cross groove. Lubricating oil is then spread over that portion of the abuttingsurfaces cross groove 187. - Likewise, when the engine cycles past TDC and the connecting rod approaches the extreme limit of its angle in a second direction,
cross groove 189 becomes exposed toarc groove 186 and oil from the conventional lubrication pump flows intocross groove 189. Lubricating oil is then spread over that portion of the abuttingsurfaces cross groove 189. - In
FIG. 8 , an outer piston pin and connecting rod assembly is shown wherein connectingrods Connecting rods cross member 145 which supports anouter piston pin 142. In this case, the outer piston pin contains a pair ofarc grooves Oil passages - From the foregoing, it can be seen that there has been brought to the art a new and improved system and method for lubricating the normally contacting surfaces of a piston pin and connecting rod journal in an internal combustion engine. It is to be understood that the preceding description of the embodiments is merely illustrative of some of the many specific embodiments that represent applications of the principles of the present invention. Clearly, numerous and other arrangements would be evident to those skilled in the art without departing from the scope of the invention as defined by the following claims.
Claims (20)
1. A system for lubricating normally abutting bearing surfaces between a piston pin and the small end journal of a connecting rod of an internal combustion engine in which said piston pin and said small end journal together provide a rotatable connection between a piston and its corresponding connecting rod, comprising:
a source of lubricating oil being pumped under a first level of pressure;
communicating passages formed in the crankshaft and connecting rods of said engine for delivering lubricating oil from said source to said abutting bearing surfaces;
a pump installed within a connecting rod in communication with said passages to receive said lubricating oil from said source;
wherein said pump provides a predetermined measure of lubricating oil between said abutting surfaces as said piston reaches bottom dead center portion of its stroke cycle.
2. A system as in claim 1 , wherein said pump reacts to the movement of the connecting rod in which it is installed to provide said predetermined measure of lubricating oil between said normally abutting surfaces as said piston reaches bottom dead center portion of its stroke cycle.
3. A system as in claim 2 , wherein said pump contains elements which are movable in directions parallel to the longitudinal inertia forces created in said connecting rod during the stroke cycle.
4. A system as in claim 3 , wherein said pump contains valving elements which remain open to allow oil to flow from said source and through said pump to said normally abutting surfaces at a first pressure level that is a function of the source pressure and the resistance presented by said passages and the valves over other portions of the stroke cycle.
5. A system as in claim 4 , wherein said pump valving elements are closed when deceleration forces reach a predetermined level as said piston reaches the bottom dead center portion in the stroke cycle and said movable elements force said predetermined measure of oil to be injected between said abutting surfaces at a second pressure level that is higher than said first pressure level.
6. A system as in claim 5 , wherein said second pressure level is sufficient to cause temporary separation between said normally abutting surfaces and to allow lubricating oil to be distributed therebetween.
7. A system as in claim 2 , wherein said pump contains an unbiased reciprocating plunger element within a bore that is oriented within said connecting rod to allow movement of said plunger along its longitudinal axis within said bore and such movement is an inertia reaction to acceleration and deceleration forces generated by the reciprocating movement of the piston during its stroke cycle and communicated into said connecting rod.
8. A system as in claim 7 , wherein said pump further contains valving elements which remain open to allow oil to flow from said source and through said pump to said normally abutting surfaces over other portions of the stroke cycle at a first pressure level that is a function of the source pressure and the resistance presented by said passages and the valves.
9. A system as in claim 8 , wherein said plunger element serves as a valving element over other portions of said stroke cycle.
10. A system as in claim 9 , wherein said plunger element is a two stage mass, including a first stage portion that slides within a first portion of said bore and contains several longitudinally formed passages to allow oil to flow therethough when said plunger element moves within said bore; and
a second stage portion that slides within a second portion of said bore to provide the injection of a predetermined measure of lubricating oil from said second portion of said bore out of said pump and between said normally abutting surfaces.
11. A method of lubricating normally contacting surfaces of a piston pin and the small end journal of a connecting rod of an internal combustion engine in which said piston pin and said small end journal together provide a connection between a piston and its corresponding connecting rod, comprising the steps of:
providing a source of lubricating oil at a first level of pressure;
providing the crankshaft and connecting rods of said engine with communicating passages for the delivery of lubricating oil from said source to said normally contacting surfaces;
providing a pump within a connecting rod to be in communication with said communicating passages to receive said lubricating oil from said source; and
injecting a predetermined measure of lubricating oil between said normally contacting surfaces as said piston reaches bottom dead center portion of its stroke cycle.
12. The method of claim 10 , wherein said pump is provided to react to the movement of its associated connecting rod to provide said predetermined measure of lubricating oil between said normally contacting surfaces as said piston reaches bottom dead center portion of its stroke cycle.
13. The method of claim 12 , wherein said pump is provided to contain elements which are movable in directions parallel to the longitudinal inertia forces created in said connecting rod during the stroke cycle.
14. The method of claim 13 , wherein said pump is provided to contain valving elements which remain open to allow oil to flow from said source and through said pump to said normally contacting surfaces at a first pressure level over other portions of the stroke cycle; and
said first pressure level being a function of the source pressure and the resistance presented by said passages and valving elements.
15. The method of claim 14 , wherein said pump valving elements are closed when deceleration forces reach a predetermined level as said piston reaches the bottom dead center portion in the stroke cycle and said movable elements inject said predetermined measure of oil between said contacting surfaces at a second pressure level that is higher than said first pressure level.
16. The method of claim 15 , wherein said second pressure level is sufficient to cause temporary separation between said normally contacting surfaces and to allow lubricating oil to be distributed therebetween.
17. The method of claim 12 , wherein said pump is provided to contain an unbiased reciprocating plunger element within a bore that is oriented within said connecting rod to allow movement of said plunger along its longitudinal axis within said bore and such movement is an inertia reaction to acceleration and deceleration forces generated by the reciprocating movement of the piston during its stroke cycle and communicated into said connecting rod.
18. The method of claim 17 , wherein said pump is provided to contain valving elements which remain open to allow oil to flow from said source and through said pump to said normally contacting surfaces at a first pressure level that is determined by the source pressure and the resistance presented by said passages and valving elements over other portions of the stroke cycle.
19. The method of claim 18 , wherein said plunger element is provided to serve as a valving element over other portions of said stroke cycle.
20. The method of claim 19 , wherein said plunger element is provided as a two stage mass, including a first stage portion that slides within a first portion of said bore and contains several longitudinally formed passages to allow oil to flow therethough when said plunger element moves within said bore; and
a second stage portion that slides within a second portion of said bore to provide the injection of a predetermined measure of lubricating oil from said second portion of said bore out of said pump and between said normally contacting surfaces.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/818,660 US20080017164A1 (en) | 2006-07-21 | 2007-06-14 | Piston-pin bearing lubrication system and method for a two sroke internal combustion engine |
US12/583,913 US8651085B2 (en) | 2006-07-21 | 2009-08-27 | Piston-pin bearing lubrication system and method for a two-stroke internal combustion engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US83264606P | 2006-07-21 | 2006-07-21 | |
US11/818,660 US20080017164A1 (en) | 2006-07-21 | 2007-06-14 | Piston-pin bearing lubrication system and method for a two sroke internal combustion engine |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/583,913 Division US8651085B2 (en) | 2006-07-21 | 2009-08-27 | Piston-pin bearing lubrication system and method for a two-stroke internal combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
US20080017164A1 true US20080017164A1 (en) | 2008-01-24 |
Family
ID=38970260
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/818,660 Abandoned US20080017164A1 (en) | 2006-07-21 | 2007-06-14 | Piston-pin bearing lubrication system and method for a two sroke internal combustion engine |
US12/583,913 Expired - Fee Related US8651085B2 (en) | 2006-07-21 | 2009-08-27 | Piston-pin bearing lubrication system and method for a two-stroke internal combustion engine |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/583,913 Expired - Fee Related US8651085B2 (en) | 2006-07-21 | 2009-08-27 | Piston-pin bearing lubrication system and method for a two-stroke internal combustion engine |
Country Status (1)
Country | Link |
---|---|
US (2) | US20080017164A1 (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080314688A1 (en) * | 2004-06-10 | 2008-12-25 | Achates Power, Inc. | Internal combustion engine with provision for lubricating pistons |
US20100212638A1 (en) * | 2009-02-20 | 2010-08-26 | Achates Power, Inc. | Opposed piston engines with controlled provision of lubricant for lubrication and cooling |
US20100212613A1 (en) * | 2009-02-20 | 2010-08-26 | Achates Power, Inc. | Multi-Cylinder opposed piston engines |
US20100212637A1 (en) * | 2009-02-20 | 2010-08-26 | Achates Power, Inc. | Cylinder and piston assemblies for opposed piston engines |
CN102042217A (en) * | 2010-09-19 | 2011-05-04 | 长沙中联重工科技发展股份有限公司 | Piston lubricating system for concrete cylinder |
CN102226427A (en) * | 2011-05-25 | 2011-10-26 | 中国兵器工业集团第七○研究所 | External connecting rod of two-cycle internal combustion engine with opposed air cylinders and opposed pistons |
CN103016092A (en) * | 2012-12-12 | 2013-04-03 | 优华劳斯汽车系统(上海)有限公司 | Lubricating system and method of engine |
CN103174538A (en) * | 2013-04-01 | 2013-06-26 | 优华劳斯汽车系统(上海)有限公司 | System and method for piston pin bearing lubrication of two-stroke internal-combustion engine |
CN103322019A (en) * | 2013-06-09 | 2013-09-25 | 安徽中鼎动力有限公司 | Opposed-piston opposed-cylinder free piston engine crankshaft |
CN103696853A (en) * | 2012-09-27 | 2014-04-02 | 郑州天力内燃机械有限公司 | Two-cylinder and four-piston contraposition type linear motion two-stroke engine system |
CN104295487A (en) * | 2014-09-28 | 2015-01-21 | 山推楚天工程机械有限公司 | Internal lubricating system for concrete pump hydraulic control type concrete piston |
US20150128920A1 (en) * | 2013-11-08 | 2015-05-14 | Achates Power, Inc. | Lubricating Configuration for Maintaining Wristpin Oil Pressure in a Two-Stroke Cycle, Opposed-Piston Engine |
WO2017140188A1 (en) * | 2016-02-16 | 2017-08-24 | 梁国富 | Oil-free high-pressure plunger pump |
JP2019138452A (en) * | 2018-02-15 | 2019-08-22 | トヨタ自動車株式会社 | Connecting rod |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10180115B2 (en) | 2010-04-27 | 2019-01-15 | Achates Power, Inc. | Piston crown bowls defining combustion chamber constructions in opposed-piston engines |
CN102947545B (en) | 2010-04-27 | 2015-11-25 | 阿凯提兹动力公司 | For the combustion chamber structure of opposed piston type engine |
US9512779B2 (en) | 2010-04-27 | 2016-12-06 | Achates Power, Inc. | Swirl-conserving combustion chamber construction for opposed-piston engines |
US9163505B2 (en) | 2010-08-16 | 2015-10-20 | Achates Power, Inc. | Piston constructions for opposed-piston engines |
JP5946831B2 (en) | 2010-08-16 | 2016-07-06 | アカーテース パワー,インク. | Fuel injection spray pattern for opposed piston engine |
US9309807B2 (en) | 2011-05-18 | 2016-04-12 | Achates Power, Inc. | Combustion chamber constructions for opposed-piston engines |
US8677951B2 (en) * | 2011-10-07 | 2014-03-25 | Mahle Koenig Kommanditgesellschaft Gmbh & Co. Kg | Opposed piston engine |
US20130104848A1 (en) | 2011-10-27 | 2013-05-02 | Achates Power, Inc. | Fuel Injection Strategies in Opposed-Piston Engines with Multiple Fuel Injectors |
DE102012104212A1 (en) * | 2012-04-18 | 2013-10-24 | Ecomotors International, Inc. | Symmetrical engine with opposed pistons and opposed cylinders |
US9211797B2 (en) | 2013-11-07 | 2015-12-15 | Achates Power, Inc. | Combustion chamber construction with dual mixing regions for opposed-piston engines |
US9470136B2 (en) | 2014-03-06 | 2016-10-18 | Achates Power, Inc. | Piston cooling configurations utilizing lubricating oil from a bearing reservoir in an opposed-piston engine |
US9995213B2 (en) | 2015-03-31 | 2018-06-12 | Achates Power, Inc. | Asymmetrically-shaped combustion chamber for opposed-piston engines |
US9840965B2 (en) | 2015-07-31 | 2017-12-12 | Achates Power, Inc. | Skewed combustion chamber for opposed-piston engines |
CN112177773B (en) * | 2020-09-29 | 2021-08-06 | 山河智能装备股份有限公司 | Aviation piston engine |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3131785A (en) * | 1962-06-14 | 1964-05-05 | Ingersoll Rand Co | Machine bearing lubrication apparatus |
US5724863A (en) * | 1995-08-17 | 1998-03-10 | Daimler Benz Ag | Connecting rod |
US6170443B1 (en) * | 1998-09-11 | 2001-01-09 | Edward Mayer Halimi | Internal combustion engine with a single crankshaft and having opposed cylinders with opposed pistons |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2843221A (en) | 1955-05-04 | 1958-07-15 | Nickles Machine Corp | Force feed lubricating device for pistons |
-
2007
- 2007-06-14 US US11/818,660 patent/US20080017164A1/en not_active Abandoned
-
2009
- 2009-08-27 US US12/583,913 patent/US8651085B2/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3131785A (en) * | 1962-06-14 | 1964-05-05 | Ingersoll Rand Co | Machine bearing lubrication apparatus |
US5724863A (en) * | 1995-08-17 | 1998-03-10 | Daimler Benz Ag | Connecting rod |
US6170443B1 (en) * | 1998-09-11 | 2001-01-09 | Edward Mayer Halimi | Internal combustion engine with a single crankshaft and having opposed cylinders with opposed pistons |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7861679B2 (en) | 2004-06-10 | 2011-01-04 | Achates Power, Inc. | Cylinder and piston assemblies for opposed piston engines |
US20100012055A1 (en) * | 2004-06-10 | 2010-01-21 | Achates Power, Inc. | Cylinder and piston assemblies for opposed piston engines |
US20080314688A1 (en) * | 2004-06-10 | 2008-12-25 | Achates Power, Inc. | Internal combustion engine with provision for lubricating pistons |
US8281755B2 (en) | 2004-06-10 | 2012-10-09 | Achates Power, Inc. | Internal combustion engine with provision for lubricating pistons |
US20100212613A1 (en) * | 2009-02-20 | 2010-08-26 | Achates Power, Inc. | Multi-Cylinder opposed piston engines |
US20100212637A1 (en) * | 2009-02-20 | 2010-08-26 | Achates Power, Inc. | Cylinder and piston assemblies for opposed piston engines |
US8550041B2 (en) | 2009-02-20 | 2013-10-08 | Achates Power, Inc. | Cylinder and piston assemblies for opposed piston engines |
US9328692B2 (en) * | 2009-02-20 | 2016-05-03 | Achates Power, Inc. | Opposed piston engines with controlled provision of lubricant for lubrication and cooling |
US20100212638A1 (en) * | 2009-02-20 | 2010-08-26 | Achates Power, Inc. | Opposed piston engines with controlled provision of lubricant for lubrication and cooling |
US8539918B2 (en) | 2009-02-20 | 2013-09-24 | Achates Power, Inc. | Multi-cylinder opposed piston engines |
CN102042217A (en) * | 2010-09-19 | 2011-05-04 | 长沙中联重工科技发展股份有限公司 | Piston lubricating system for concrete cylinder |
WO2012034451A1 (en) * | 2010-09-19 | 2012-03-22 | 长沙中联重工科技发展股份有限公司 | Piston lubrication system for concrete cylinder |
CN102226427A (en) * | 2011-05-25 | 2011-10-26 | 中国兵器工业集团第七○研究所 | External connecting rod of two-cycle internal combustion engine with opposed air cylinders and opposed pistons |
CN103696853A (en) * | 2012-09-27 | 2014-04-02 | 郑州天力内燃机械有限公司 | Two-cylinder and four-piston contraposition type linear motion two-stroke engine system |
CN103016092A (en) * | 2012-12-12 | 2013-04-03 | 优华劳斯汽车系统(上海)有限公司 | Lubricating system and method of engine |
CN103174538A (en) * | 2013-04-01 | 2013-06-26 | 优华劳斯汽车系统(上海)有限公司 | System and method for piston pin bearing lubrication of two-stroke internal-combustion engine |
CN103322019A (en) * | 2013-06-09 | 2013-09-25 | 安徽中鼎动力有限公司 | Opposed-piston opposed-cylinder free piston engine crankshaft |
US20150128920A1 (en) * | 2013-11-08 | 2015-05-14 | Achates Power, Inc. | Lubricating Configuration for Maintaining Wristpin Oil Pressure in a Two-Stroke Cycle, Opposed-Piston Engine |
US9038593B1 (en) * | 2013-11-08 | 2015-05-26 | Achates Power, Inc. | Lubricating configuration for maintaining wristpin oil pressure in a two-stroke cycle, opposed-piston engine |
CN104295487A (en) * | 2014-09-28 | 2015-01-21 | 山推楚天工程机械有限公司 | Internal lubricating system for concrete pump hydraulic control type concrete piston |
WO2017140188A1 (en) * | 2016-02-16 | 2017-08-24 | 梁国富 | Oil-free high-pressure plunger pump |
JP2019138452A (en) * | 2018-02-15 | 2019-08-22 | トヨタ自動車株式会社 | Connecting rod |
JP7127293B2 (en) | 2018-02-15 | 2022-08-30 | トヨタ自動車株式会社 | connecting rod |
Also Published As
Publication number | Publication date |
---|---|
US20100224162A1 (en) | 2010-09-09 |
US8651085B2 (en) | 2014-02-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8651085B2 (en) | Piston-pin bearing lubrication system and method for a two-stroke internal combustion engine | |
US7509937B2 (en) | Piston ring, piston skirt and cylinder liner lubrication system and method for an internal combustion engine | |
US3545569A (en) | Lubrication of bearings of reciprocating engines or pumps | |
US20170204784A1 (en) | Single supply port activated connecting rod for variable compression ratio engines | |
US9038593B1 (en) | Lubricating configuration for maintaining wristpin oil pressure in a two-stroke cycle, opposed-piston engine | |
US8397685B2 (en) | Fuel injection system | |
US10393012B2 (en) | Internal combustion engine | |
JP2016515177A (en) | Swing journal bearings for 2-stroke cycle engines | |
US9482123B2 (en) | Lubrication system for the piston ring and cylinder liner of an internal combustion engine | |
EP3296539A1 (en) | Oil pressure generating device and crosshead engine | |
JPH0323732B2 (en) | ||
US8622042B2 (en) | Bearing connection, engine cylinder, and engine with the bearing connection | |
JP5852561B2 (en) | Lubricating oil pump, cylinder lubricating system, and internal combustion engine | |
JPS61164066A (en) | Fuel injection pump | |
US8381691B2 (en) | Fuel injection system | |
KR20200109369A (en) | Internal combustion engine | |
US6622706B2 (en) | Pump, pump components and method | |
US4261303A (en) | An internal combustion engine | |
JP5412570B2 (en) | Fuel pump for turbocharged large two-stroke diesel engines | |
CN112292516A (en) | Double-acting piston engine | |
WO2011027140A1 (en) | Internal combustion engine | |
US5836749A (en) | Piston type liquid fuel pump with an improved inlet valve | |
JPH02215966A (en) | Fuel injection system for internal combustion engine | |
US2538463A (en) | Pump for charging two-stroke internal-combustion engines | |
US2918142A (en) | Device for automatic lubrication of cylinders |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: ADVANCED PROPULSION TECHNOLOGIES, INC., CALIFORNIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HOFBAUER, PETER;REEL/FRAME:019655/0560 Effective date: 20070718 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |