Rotary valve internal combustion engine

Information

  • Patent Grant
  • 6513475
  • Patent Number
    6,513,475
  • Date Filed
    Wednesday, April 18, 2001
    23 years ago
  • Date Issued
    Tuesday, February 4, 2003
    21 years ago
  • Inventors
  • Examiners
    • Kamen; Noah P.
    Agents
    • Coats & Bennett, P.L.L.C.
Abstract
An engine comprises an engine block having at least one combustion chamber and a rotary valve rotatably mounted on top of the engine block. The rotary valve includes an intake passage for diverting air into the combustion chamber and an exhaust passage for exhausting combustion by products from the combustion chamber. The engine further includes a head surrounding the rotary valve. Seals surrounding the combustion chamber seat against the bottom surface of the rotary valve. Seals on the circumference of the rotary valve seat against the head. The seals are arranged to provide a double seal for the combustion chamber during the initial portion of the power stroke. The rotary valve may further include a pressure relief valve to reduce pressure and temperature in the combustion chamber during at least a portion of the power cycle.
Description




FIELD OF THE INVENTION




The present invention relates generally to internal combustion engines, and more particularly, to an internal combustion engine utilizing a rotary valve for directing the flow of intake air into the cylinders and exhausting gases from the cylinders.




BACKGROUND OF THE INVENTION




Increasing concerns about the impact of the internal combustion engine on global warming are putting added pressures on the automotive industry to develop more environmentally friendly engines. Generally, the approach is to increase the fuel economy of the engine by reducing the displacement in efforts to burn less fuel. This small displacement engine would be used as a stand alone power plant or as the principal source of power in an electric hybrid configuration. Currently, the most promising approach is to use the most efficient internal combustion engine, the direct injection diesel, and reduce its displacement to as small as operationally possible. It is in this application and as a small cylinder displacement stand alone power source that the Rotary Valve Diesel (RVD) is expected to be particularly well suited.




Previous art on the RVD attempted to reduce emissions by using the same strategy used decades ago with the Otto gasoline engine to increase fuel economy. Thus, as stated above, the displacement of the engine was decreased in an effort to burn less fuel per mile which also would result in reduced emissions. However, this small displacement engine would encounter the same problem as with the Otto engines, namely, reduced output. The RVD again used the same strategy of increasing rpms' to increase output as was done earlier with the Otto engine. Also, some modest increase in efficiency due to improved thermodynamic and volumetric efficiency would add to this output. This increased power would increase consumer acceptance of the engine and with that, both fuel consumption and emissions would decrease.




While the RVD exhibits many advantages over conventional diesels when attempting to build small cylinder displacement engines, it still does not dramatically reduce either emissions or the characteristic diesel noise associated with the—fast burn phase of combustion in comparison to conventional diesels of similar displacements. The diesel noise is potentially problematic because of consumer aversion to this condition.




The art now presented makes major improvements in the reduction of both noise and emissions as well as reductions in cost while increasing durability. A new feature, the Peak Pressure Reducing Valve (PPRV), can reduce or prevent the spike in pressure and temperature by opening a valve during the rapid burn phase of the combustion cylinder and instantly transfer this heat and pressure to the compression cylinder. First, this reduces noise and second it reduces NOx. The PPRV reduces NOx by preventing its creation and performs like an EGR system allowing for the reduction of any NOx that is produced.




The PPRV also reduces HC emissions. HC emissions are produced by incomplete burning in crevice spaces. Most of the crevice spaces in the RVD are located above the piston, around the seals, and above the top most piston ring. Being that the combustion bowl is off center and the opening for the PPRV is at the point located in the seals closest to the center of the engine, the area of greatest concentration of HC emissions is this very same area from which the combustion gas is drawn while the piston is still relative close to the valve. These gases are passed to the cylinder in the compression cycle to become part of the charge to be burned during the next combustion cycle.




Also reducing NOx is the cooled EGR system located on the rotary valve. Adding to reduced emissions is the cooling of the intake charge by the cooling fins placed on the valve housing. A second benefit of cooling the intake charge is an improvement in volumetric efficiency.




Also increasing efficiency is the PPRV. Thermal efficiency should be improved due to the mixing of gas in both the compression and combustion cycle cylinders ultimately creating more complete combustion. This mixing is due to the very rapid exit of gas from the combustion cylinder and injection into the compression cylinder creating turbulence in both cylinders. Another feature increasing efficiency is the thermal transfer plate which transfers heat via conduction from the power stoke to the compression stroke. Both the PPRV and the thermal transfer plate are positioned not to operate until the intake is fully closed. Heat energy is now added to the compression cycle by both elements. This added heat energy is then present at the beginning of the combustion cycle allowing more reliable and quicker ignition. This is especially important as cylinder displacement is reduced and would allow the RVD to operate in cylinder displacements smaller than conventional diesel engines.




Finally, the last two features increase durability. First, the valve shape is changed to a more “bell” shaped configuration and made smaller making it stronger. Lastly, the seal system is changed adding a double piston type seal around the valve. This in combination to the seals on the block allow the double sealing of the initial 60% to 65% of the power stroke.




The last point to be addressed is the use of ceramics or ceramic coatings on the RVD. While this technology can also be used on conventional engines, it should be less costly when used on the RVD. This would be due to fewer parts being affected and the parts affected being relatively easy to coat. In the RVD the same exhaust serves several cylinders and therefore has more heat available to burn soot. This effect can be increased at relatively low cost by coating the exhaust with ceramics.' An additional benefit of this coating would be less heat transferred to the intake charge. Similarly, a ceramic coating on the bottom of the valve would also reduce heat transfer and increase the durability of the valve. Coating both of these elements would be the start of making the RVD a low heat rejection engine.




All the improvements of the RVD are intended to allow a small cylinder displacement diesel to replace the Otto gasoline engines of the same power. The RVD could be used in the preferred embodiment of one rotary valve serving four cylinders or in engines having multiples of four cylinders. Potential markets would include light auto and truck, outboard marine, motorcycles, and light aircraft to name a few. However, given that the RVD appears to have significant emissions and noise advantages, it would be expected that the RVD technology would be applied to Diesels of ever increasing cylinder displacement engines. Therefore the potential market for the RVD is huge. Correspondingly, the potential for fuel savings and reduction in emissions and greenhouse gases is very significant.




SUMMARY AND OBJECTS OF THE INVENTION




The present invention is an internal combustion engine having at least one cylinder. A rotary disk valve is located over the top of the cylinders for rotation about an axis parallel to the axis of the cylinders. The center of each cylinder is equally spaced from the axis of rotation of the rotary disk valve. The valve includes an intake passage for directing intake air into the cylinders and an exhaust passage for exhausting combustion gases from the cylinders. The intake passage and exhaust passage in the rotary valve communicate with each cylinder in succession as the valve rotates, allowing the use of a single valve to serve multiple cylinders. The rotary valve uses piston type seals to prevent the movement of gas from the cylinders past the valve. This valve seal is well lubricated by an oil nozzle to produce a tight seal with minimal friction. Another set of seals is located around the major portions of the tops of each cylinder to prevent the movement of engine gases between cylinders.




In another aspect of the engine, the intake and exhaust valve openings as well as the intake and exhaust passages are increased in size by at least 40% over conventional poppet valve engines. This not only increases pumping efficiency, but also allows the air transport capacity to be increased from at least double to as much as four times that of conventional engines.




While the rotary valve engine herein described could use various fuels, the preferred fuel would be diesel. As such, the rotary valve engine as described, is referred to as the Rotary Valve Diesel (RVD) and further comparisons to conventional engines will be inferred to be poppet valve diesel Engines.




Another feature of the RVD shapes the intake and exhaust valve openings of the valve to minimize valve overlap while maximizing valve opening areas. This allows the engine to be kept very compact without compromising pumping efficiencies. Further, the openings can be shaped to allow the RVD to double seal the first 60 to 65% of the power stroke increasing the RVD's sealing capacity.




The RVD uses twin counter rotating crankshafts in engine configurations of four cylinders and larger. This four cylinder configuration or multiples of this format are the preferred embodiment of this engine. In the four cylinder, this configuration requires that each crankshaft have two crank throws which are adjacent and 180 degrees apart. Each crankshaft has gears attached to it which mesh together to synchronize the crankshafts and transfer power to the crankshaft with the flywheel attached to it. The other crankshaft has a gear on it to drive the valve. This arrangement is very effective in reducing vibration with minimal counter weighting and produces high torque.




The crank throws of each crankshaft overlap as they rotate. This is possible because the crank throws of opposing crankshafts rotate 180 degrees out of phase. The use of this feature allows the cylinders to be placed closer together, thereby making the engine more compact.




The RVD uses several elements to reduce emissions. The most dramatic element is the use of the Peak Pressure Reducing Valve (PPRV). The PPRV is located on the rotary valve and has an intake timed to open at the beginning of the fast burn phase of combustion with the intent of minimizing or preventing the rapid spike in temperature and pressure. The PPRV closes at what would be the end of this normally occurring spike. The PPRV opening transfers gas through a passage located in the rotary valve from this high pressure area to a lower pressure area, the compression cylinder. PPRV opening is sized to only allow enough gas to be transferred from the combustion stroke to the compression stroke to smooth out the pressure and temperature rise. Since the combustion temperature is reduced, NOx emissions are reduced. Also, as the gas escapes from the combustion cylinder, it should take much of the gas caught in the crevice space above the piston and transfer this gas to the compression cylinder to then be burned when this cylinder enters its' own combustion cycle. Since crevice spaces are responsible for increased HC emissions, this should reduce HC emissions. Finally, soot also is reduced due to the rapid exit of gas from the combustion cylinder and the rapid entrance into the compression cylinder causing increased turbulence in both cylinders resulting in more complete combustion in the combustion cycle. Further soot reductions could be made by coating the inside surface of the exhaust with ceramics.




Another key benefit of the PPRV is the also related to reducing the pressure and temperature spike in the combustion cycle. This is the reduction of the noise produced by this event. As this is a major consumer complaint, reducing and possibly eliminating this noise would make the RVD much more attractive to consumers.




The final benefit of the PPRV is its' ability to transfer heat energy to the compression cycle. This heat is transferred as the hot gas moves through the PPRV to the compression cylinder. More heat energy is transferred from the combustion cycle to the compression cycle by the Thermal Transfer Plate. This device is simply a plate made.




It should be noted that the EGR should also reduce HC emissions. This is due to the EGR intake picking up any trapped gas from between the cylinders as it rotates from one to the next. HC rich gas could be present in this area if the seals experience any leakage during the combustion cycle.




The last new feature, is the cooling of the valve housing. Cooling fins are added to the valve housing to cool the intake charge contained within it. Being that the surface area of the valve housing is quite large, it provides ample opportunity to cool the intake air. In addition, a conventional intercooler could also be used to further cool the intake charge.




Based on the foregoing, it is a primary object of the present invention to provide a rotary valve engine which has lower emissions than conventional poppet valve engines.




Another object of the present invention is to provide a rotary valve engine which exhibits lower noise, vibration and harshness than conventional poppet valve engines.




Still another object of the present invention is to provide a rotary valve engine which has both greater pumping efficiencies and air transport capacities as compared to conventional poppet valve engines.




Yet another object of the present invention is to provide a rotary valve engine which has greater thermal efficiencies than conventional poppet valve engines.




Another object of the present invention is to provide a rotary valve engine which is more compact and lightweight than conventional poppet valve engines.




Still another object of the present invention is to provide a rotary valve engine which will increase the rpms compared to conventional poppet valve engines.




Yet another object of the present invention is to provide a rotary valve engine which will increase the power to weight ratio as compared to conventional poppet valve engines.




Another object is to provide a rotary valve engine which is relatively inexpensive to produce.




Still another object of the present invention is to provide a rotary valve engine which is very reliable.




Other objects and advantages of the present invention will become apparent and obvious from a study of the following description and accompanying drawings which are merely illustrative of such invention.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a longitudinal cross-section of the rotary valve engine block through the centers of the two closest cylinders with the rotary valve in elevation view;





FIG. 2

is a cross-section of the rotary valve engine block viewed parallel to the crankshafts and through the centers of the two closest cylinders;





FIG. 3

is a top view of the engine block and in cross-section through the head;





FIG. 4

is a cross-section view of the rotary valve engine diagonally through the center of the engine block taken through line


4





4


of

FIG. 3

;





FIG. 5

is a cross-section view of the rotary valve taken through line


5





5


of

FIG. 4

;





FIG. 6

is a bottom view (reversed from

FIG. 5

) taken through line


6





6


of

FIG. 4

; and





FIG. 7

is an enlarged top view of a typical cylinder demonstrating an alternate semicircular seal notch.











DETAILED DESCRIPTION OF THE INVENTION




Referring now to the drawings, the rotary valve engine of the present invention is shown therein and indicated generally by the numeral


10


. The rotary valve engine


10


includes an engine block


20


, indicated generally at


20


, having a plurality of cylinders


22


in which reciprocating pistons


24


are mounted. A rotary valve assembly


70


is disposed on the top of the engine block


20


for directing air into cylinders


22


and exhausting combustion gases. The rotary valve assembly


70


comprises a valve housing


100


supported by support assembly


115


mounted on head


102


and a single disc-type rotary valve


72


.




The engine block


20


encloses cylinders


22


circumferentially spaced about the axis of rotation of the valve


72


. The center of each cylinder


22


is equidistant from the rotational axis of the valve


72


. A piston


24


is mounted for reciprocating movement within each cylinder


22


. Each piston


24


is connected by a piston rod


38


to a rotating crankshaft


40


. The disclosed embodiment has two, parallel crankshafts


40


each with antibacklash gears


42


which mesh with one another.

FIG. 1

shows each gear


42


has a grove in it to allow oil to be quietly dissipated. The antibacklash gears


42


can also be separated at this grove to allow the use of two distinct gears. This would allow one gear to be staggered by a half tooth to again reduce vibration. The use of cycloidal antibacklash gears could reduce gear friction. As the antibacklash gears


42


mesh together, the two crankshafts will rotate in opposite directions. Each crankshaft


40


includes two crank throws


44


to which respective piston rods


38


are connected. The crank throws


44


on each crankshaft


40


are disposed 180 degrees apart from one another. Thus, even though the circular path of travel of the crank throws on opposite crankshafts can overlap, the crank throws avoid contact by being out-of-phase with one another. This allows the crankshafts to be placed closer together. In addition, compared to an in-line configuration, this twin crankshaft design decreases each crankshaft length by almost two thirds or the combined length by almost one third. Not only does this latter configuration produce a much more compact design, but one that is stiffer and of less mass as well. On the end of one of crankshafts


40


, is placed flywheel


48


. On the opposite end of the other crankshaft, is spur gear


50


, which turns spur gear


52


, and shaft


54


located above crankshaft


40


but midway between them. At the end of shaft


54


is bevel gear


56


which meshes with bevel gear


98


attached to shaft


99


which drives rotary valve


72


at one half the crankshaft speed. Crankshafts with adjacent crank throws 180 degrees apart are better balanced with respect to first and second degree harmonics than is the conventional in-line four cylinder crankshaft. Further, since the RVD uses counter revolving crankshafts geared to each other, any imbalances tend to be cancelled out. Additionally, since there are no reciprocating valves to produce vibrations, but a rotating valve mass which tends to counter residual vibrations from the crankshafts, the RVD should exhibit much lower levels of vibration.




The rotary valve assembly


70


is mounted on top of the engine block


20


. Within valve assembly


70


is a single disc-type valve


72


which is mounted for rotation on the engine block


20


. The rotary valve


72


has a flat bottom surface


74


and a bell shaped upper surface, making the valve very strong. The valve


72


includes an exhaust passage


76


and an intake passage


84


. The exhaust passage


76


includes an inlet


77


on the bottom


74


of the valve


72


and an outlet


78


at the top of the valve


72


along the axis of rotation of the valve


72


. The inlet


77


of the exhaust passage


76


is positioned such that it communicates with each cylinder


22


in succession as the valve


72


rotates. Compounding fins


80


extend across inlet


77


of the exhaust passage


76


. The function of the compounding fins


80


will be described below.




The intake passage


84


includes an inlet


86


disposed at the end of intake passage


84


within valve


72


extending to the bottom surface


74


of valve


72


and intake outlet


88


. The inlet


86


faces the direction of rotation of the valve


72


so that it functions somewhat like an air scoop as the valve


72


rotates, creating pressure that forces air down through the intake passage


84


into the cylinders


22


. In a preferred embodiment, the cross-sectional area of the intake passage


84


is at least 35% of the cross-sectional area of the cylinder.




Of critical importance is the seal system used to control the engine gases. Most rotary valve engines are unsuccessful due to their inability to adequately seal the combustion chamber without excessive friction or excessive oil consumption. This problem is overcome by using a piston ring type seal


62


around the rotary valve. Oil nozzle


75


provides ample lubrication to the seal providing a tight seal without excessive friction. Cylinder seals


60


complete the combustion chamber seal by encircling the cylinders and recess into the head


102


while contacting the bottom edge of valve seal


62


. The cylinder seals


60


fit into grooves


58


surrounding each cylinder


22


. Seals


68


are mounted in a similar manner to seals


60


. Seals


60


and


68


are used to prevent the movement of exhaust gas to adjacent cylinders and are lubricated by the diesel fuel. This system should be very effective in preventing the loss of gas pressure since the gas would have to move past at least two seals during the period of greatest pressure. For example, seals


68


and


60


of adjacent cylinders would prevent the passage of gasses generated by the power stroke of the cylinder in between for the first 65% of the power stroke. Referring to

FIG. 3

, if the cylinder experiencing the power stroke is represented by area


200


, then the seals surrounding areas


201


,


202


, and


203


provide an additional barrier for the first 65% of the power stroke. Therefore, it would be possible to further increase the mean effective pressures generating greater output by designing the engine to allow the pressures to exceed the capacity of the single sealing capacity of seals


60


and


68


, but to be constrained by the second set of seals. The amount of heat energy lost would depend upon the pressure differentials and, the volume of the spaces. The space between the valve and engine block would be limited to the amount needed for thermal expansion of the valve and block and be relative small. Additionally, the pressure in area


203


would quickly equalize to the escaping gas pressure so that little additional pressure would be lost to this area. The pressure that had escaped to area


202


is mostly constrained until after another cycle, when area


202


becomes area


201


. The increased pressure already present in area


201


minimizes the, pressure loss from the new power stroke to this area. Any pressure present in area


201


is finally released as the EGR intake


172


passes above. Oil combustion as a function of output should be less in the RVD as compared to conventional diesels. This is due to the increased rpm levels allowing a smaller displacement engine to produce the same output levels as a larger displacement, but lower rpm engine. As long as the RVD is used in applications in which light load conditions are prevalent and the RVD power output is sufficient at the same rpm rates of the larger conventional engine, then the smaller cylinder surface area of the RVD would have less cylinder oil surface from which to burn oil. While the RVD does have the additional lubricated rotary valve seals to contend with, these surfaces are always covered. For the most part, only excessive oil deposition would increase oil combustion from this source. If necessary, more than one oil nozzle could be used or possibly diesel fuel could be used as the lubricant.




Valve


72


is enclosed by valve housing


100


. Valve housing


100


is cooled by cooling fins


111


. Also enclosed by valve housing


100


is manifold


110


. The head


102


incorporates liquid cooling passages


105


and air cooling passages


106


to control thermal gradients while supporting the upper portions of the engine. Bearing


140


restrains the valve


72


while allowing the valve


72


to rotate freely. Support assembly


115


encloses valve


72


and supports valve housing


100


. Air vents


106


are circumferentially spaced around valve support assembly


115


. Air is drawn through vents


106


by the rotating valve


72


. Air passes through a cooling passage


92


in the valve


72


cooling the interior of the valve


72


. Preferably valve


72


would be insulated by ceramics on the bottom surface


74


, to both reduce heat transfer to the valve and increase wear resistance of the bottom valve surface. EGR vents


178


located above vents


106


in the support assembly


115


are also circumferentially spaced to allow the cooling of EGR


170


. Insulation


118


, is placed at various places in the manifold


110


to reduce heat transfer between the intake and exhaust gases. A seal


114


fits in a groove on top of manifold


110


to prevent the escape of exhaust gases.




Valve housing


100


is mounted on top of support assembly


115


. Valve housing


100


includes an exhaust pipe


112


, preventing the escape of exhaust gases. Valve housing


100


also includes annular cavity


120


used to supply air to intake


84


. Intake opening


122


receives air from the supercharger (not shown) and transports the air into the annular cavity


120


. Fuel injectors


160


are mounted in head


102


. Glow plug


162


is used to aid in starting rotary valve engine


10


.




Also included in the rotary valve


72


are several emissions reducing devices. Peak Pressure Reducing Valve (PPRV)


180


has an intake


182


on the bottom of valve


72


leading to a passage


180


through the valve


72


to PPRV exhaust opening


184


also located on the bottom of valve


72


. Both the PPRV intake


182


and PPRV exhaust


184


are actuated by passing over seal notch


186


. Seal notch


186


is a small segment located in seal


60


. Cylinder notch


188


provides additional clearance for the movement of the gas from cylinder to cylinder and also directs the entrance and exit of the gas to provide turbulence in both the combustion and compression cylinders.




Another emissions reduction feature located on valve


72


is EGR


170


. EGR intake


172


is located on the bottom of valve


72


adjacent to exhaust inlet


77


. Due to the rotation of valve


72


, EGR valve


172


initiates the exhaust cycle allowing a portion of the exhaust to pass through EGR passage


170


. EGR intake


172


separates from the rest of the exhaust structure to direct exhaust through EGR


170


which is cooled by EGR cooling fins


176


. Cooling fins


176


are exposed to ambient air by the flow of air through EGR vents


178


. The gas traveling through EGR


170


is expelled through EGR exhaust


174


into the intake passage


84


.




The last feature located on valve


72


is thermal transfer plate


190


. Thermal transfer plate


190


is located on the bottom surface of valve


72


. The area of the thermal transfer plate


190


is determined by the area on the bottom of the valve


72


exposed to the combustion cycle extending to the compression cycle when the exhaust and intake valves are closed. Heat is transferred from the combustion cycle through the heat transfer plate


190


via conduction to the compression cycle. This heat is now present early in the next cycle, the combustion cycle, to more quickly initiate combustion of the fuel.




In operation, intake air enters the annular chamber of the valve housing


100


from the supercharger or other intake source. As the valve


72


rotates, intake air is cooled by valve housing


100


before it enters the inlet


86


continuing through intake passage


84


, and enters one of the cylinders


22


of the engine block while the piston


24


is moving downward. The downward motion of the piston


24


within cylinder


22


decreases the cylinder pressure within the cylinder


22


so that together with the pressure created by turbocharging, intake air enters the cylinder


22


. Pressure within intake


84


is increased by the air scoop effect and the decelerating air column caused by the closing of intake outlet opening


88


. This increased pressure allows the outlet opening


88


to close after piston


24


starts upward, creating higher charge pressures in cylinder


22


. Further, this effect is maintained as rpm's increase, since pressure from the scoop effect increases with increasing rpm's offsetting increasing drag created by increasing air velocities. The intake charge passes through variable valves


83


before entering the cylinder


22


. Variable valves


83


are regulated by a spring and weight assembly


87


. Assembly


87


uses the centripetal force of the valve to put increasing pressure against the spring to move the variable valves


83


as the velocity of the valve increases, thereby further opening the intake allowing higher volumes of air to enter cylinder


22


. The bottom


74


of the valve


72


rotates over the cylinder


22


to effectively close the valve


72


. The compression stroke begins with the piston


24


moving upward within cylinder


22


with the flat bottom surface of the thermal transfer plate


190


of the valve


72


overlying the cylinder


22


. The upward motion of the piston


24


compresses the air within the cylinder


22


. Just after intake valve


88


closes, thermal transfer plate


190


adds more heat energy to the charge. Still early in the compression cycle, the PPRV


180


forcefully injects combusted gas into cylinder


22


. As this injected gas enters cylinder


22


, it is directed by cylinder notch


188


adding both heat and turbulence to the gas being compressed by piston


24


.




As the piston


24


reaches top dead center, fuel is injected to initiate the combustion sequence within the cylinder


22


. The heat of combustion causes forceful expansion of gas that push the piston


24


downward. The downward force is carried through the piston rods


38


to the crankshaft


40


which is given a powerful turn. Just as the fast burn phase of combustion begins, PPRV intake


182


passes over the seal notch


186


allowing a portion of the gas to escape cylinder


22


. This prevents the rapid pressure and thermal spike normally associated with this phase of diesel combustion. As the piston


24


continues and reaches the bottom of its power stroke, the EGR intake


172


rotates over cylinder


22


. Piston


24


moves upward to expel the exhaust gas. A portion of the combusted gas is expelled through the EGR


170


. Positioned immediately after EGR intake


172


, exhaust inlet


77


follows allowing the remaining gas pressure to exert force on angled compounding fins


80


providing rotational energy to rotary valve


72


. The exhaust gases then pass through exhaust passage


76


. A seal


114


fits in a groove in the flanged end


116


of the exhaust pipe to prevent escape of exhaust gases. Since the valve serves all four cylinders, the exhaust passage


76


remains at higher operating temperatures than does conventional exhaust passages creating increased exhaust temperatures, thus decreasing emissions.




As compared to conventional Diesel poppet valve engines, the rotary valve diesel has many advantages. From a consumer acceptance viewpoint, the main advantage would be the reduction in noise, vibration and harshness. The noise reduction is mainly accomplished by the ability of the rotary valve diesel to reduce or eliminate the thermal and pressure spike produced by the fast burn phase of combustion. Most of the vibration is reduced by the stiff block configuration and the balanced counter rotating twin crankshafts.




Another very significant advantage of the rotary valve diesel is its' ability to reduce emissions levels as compared to conventional diesel poppet valve engines. NOx should be significantly reduced by the peak pressure reduction valve as it prevents the high temperatures produced by the fast burn phase of combustion. Residual NOx would be reduced by the cooled EGR. HC should also be reduced by both of these elements due to the unique way they operate in the rotary valve diesel. Soot is reduced by the cooled intake, the increased turbulence in the compression and combustion cycles and by the elevated exhaust temperatures especially if ceramic coatings are used. Finally, C02 is reduced because the rotary valve diesel burns less fuel on a per mile basis.




This illustrates the next advantage of greater fuel economy than conventional diesel poppet valve engines. The greatest fuel savings is brought about by the rotary valve diesel being capable of increasing the power density of the engine. While a modest efficiency gain is possible to reduce fuel consumption, the power density of the rotary valve diesel can be increased by increasing the rpm levels of the engine. Total power output would remain constant, but the engine displacement would be decreased. This strategy only works in cases where maximum power is required for only a relatively small portion of time during operation of the engine. Of course this strategy was employed decades ago when the Otto gasoline engine experienced its' greatest gains in fuel economy in automobiles. RPMs in the rotary valve diesel can be increased because the temperature of the compression cycle and early combustion cycle are increased; there is more charge mixing in the compression and combustion cycles; and because the rotary valve diesel can pump much more air through the engine than conventional poppet valve diesels.




The ability of the rotary valve diesel to pump much more air than conventional poppet valve diesel engines is another major advantage. The rotary valve diesel as shown can pump almost three times the air when compared to the best conventional popped valve engines. This increases pumping efficiency and aids in the rotary valve diesels' ability to increase rpms. The increased pumping and transport capabilities are due to much larger intake and exhaust openings, and much larger intake and exhaust passages.




Increased rpms are the main component to the next advantage demonstrated by the rotary valve diesel of increased power to weight ratio. Other elements contributing to the increased power to weight ratio are the compact and lightweight construction of the rotary valve diesel. The rotary valve diesel is made compact and lightweight by using twin counter rotating crankshafts with overlapping crank throws in four cylinder versions. This produces a block configuration which is not only compact, but very rigid.




The next advantage of the rotary valve diesel as compared to conventional poppet valve diesels is a modest improvement in engine efficiency. While the rotary valve diesel is not expected to have an advantage in friction, it is expected to exhibit both greater pumping and thermal efficiencies. The pumping efficiency was explained earlier and the thermal efficiency is due to better mixing of the charge in the intake, compression and combustion cycles; the use of the peak pressure reduction valve; and thermal transfer plate to transfer heat to aid in the fuel ignition; the RVD transfers less heat to the intake cycle; and using compounding fins utilizes more thermal energy.




Another very important advantage of the rotary valve diesel as compared to conventional poppet valve diesels is the ability of the rotary valve diesel to reliably operate in small cylinder displacements. In fact, it is expected that this advantage increases with decreasing cylinder displacements.




The next advantage of reliability, is in comparison with previous versions of the rotary valve diesel and other rotary valve engines. The most significant factor is the ability of the rotary valve diesel to double seal the first 60-65% of the combustion cycle while being able to adequately lubricate the seals without excessive oil consumption. Adding to the reliability is the rigid construction of the block, and the more compact bell shaped rotary valve.




The last advantage is again compared to conventional poppet valve diesels. The rotary valve diesel should be less costly to manufacture. This is mostly due to the fewer number of required parts and the simplicity of assembly. Additional cost advantages will occur as the use of ceramics increases in diesels in pursuit of low heat rejection engine technology.




Based on the foregoing it is apparent the rotary valve engine of the present invention has numerous advantages over conventional poppet valve engines. First, it produces less noise vibration and harshness. Second it has reduced NOx, HC, soot, and C02 emissions. Third, it is more fuel efficient. Fourth it has greater engine efficiency. Fifth, it is more compact and lightweight. Sixth, it has a greater power to weight ratio. Seventh, it can operate in smaller cylinder displacements. Lastly, it is less costly to manufacture.




The present invention may of course, be carried out in other specific ways than those herein set forth without parting from the spirit and essential characteristics of the invention. The presented embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, and all changes coming within the meaning and equivalency range of the appended claims are intended to be embraced therein.



Claims
  • 1. A rotary valve engine with a four stroke cycle, said rotary valve engine comprising:(a) an engine block having at least one combustion chamber; (b) a drive member mounted in said combustion chamber; (c) a crankshaft rotatably mounted to said engine block and driven by said drive member; (d) a disc-type rotary valve mounted on said engine block; (e) an intake passage formed in said rotary valve for directing air into said combustion chamber as said rotary valve rotates; (f) an exhaust passage formed in said rotary valve for exhausting combustion gases from said combustion chamber as said rotary valve rotates; (g) a head mounted to said engine block and surrounding said rotary valve to enclose at least a portion of said combustion chamber; and (h) seals extending around said combustion chamber and seating against the bottom surface of said rotary valve; (i) at least one rotary valve seal around the circumference of said rotary valve seating against said head.
  • 2. The rotary valve engine of claim 1 wherein said seals extending around said combustion chambers create a double seal between adjacent combustion chambers for at least a portion of said power cycle.
  • 3. The rotary valve engine of claim 1 wherein said seals create a double seal between adjacent combustion chambers for at least the initial 50% of said power cycle.
  • 4. The rotary valve engine of claim 1 wherein said intake passage has a cross-sectional area of at least 35% of the cross-sectional area of said combustion chamber.
  • 5. The rotary valve engine of claim 1 wherein said drive member is a reciprocating piston.
  • 6. The rotary valve engine of claim 1 having a means to regulate the volume of air through said intake passage whereas said regulating means is a variable valve.
  • 7. The rotary valve engine of claim 1 further comprising a compounding element disposed in the exhaust passage of said rotary valve for recapturing energy from said combustion chamber whereas said compounding element comprises a fin which is angularly disposed with respect to the flow of combustion gases through said exhaust passage.
  • 8. The rotary valve engine of claim 1 further comprising an air scoop located on said rotating valve to pressurize air.
  • 9. The rotary valve engine of claim 1 having said drive member connected to a crankshaft by connecting rods.
  • 10. The rotary valve engine of claim 9 having more than one said crankshaft.
  • 11. The rotary valve engine of claim 10 wherein said crankshafts have crank throws describing overlapping paths with each other.
  • 12. The rotary valve engine of claim 1 having the leading edge of said intake opening having the same geometric shape of said seals.
  • 13. The rotary valve engine of claim 1 having the leading edge of said exhaust opening having the same geometric shape as said seals.
  • 14. The rotary valve engine of claim 1 wherein said rotary valve includes a cooling passage extending through the body of said valve such that cooling air passes through the valve body when said valve rotates.
  • 15. A rotary valve engine, said rotary valve engine comprising:(a) an engine block having at least one combustion chamber; (b) a drive member mounted in said combustion chamber; (c) a crankshaft rotatably mounted to said engine block and driven by said drive member; (d) a disc-type rotary valve mounted on said engine block; (e) an intake passage formed in said rotary valve for directing air into said combustion chamber as said rotary valve rotates; (f) an exhaust passage formed in said rotary valve for exhausting combustion gases from said combustion chamber as said rotary valve rotates; (g) a pressure reducing valve in said combustion chamber open during a portion of said combustion phase of said engine to reduce the pressure and temperature in said combustion chamber during said combustion phase.
  • 16. The rotary valve engine of claim 15 wherein said combustion phase includes a fast burn phase, and wherein said pressure reducing valve is open during said fast burn phase.
  • 17. The rotary valve engine of claim 15 wherein said engine is a diesel engine.
  • 18. The rotary valve engine of claim 15 wherein said drive member is a reciprocating piston.
  • 19. The rotary valve engine of claim 15 wherein said pressure reducing valve comprises a pressure reducing passage in said rotary valve communicating between first and second combustion chambers during the combustion phase of said first combustion chamber.
  • 20. A rotary valve engine comprising:(a) an engine block having a combustion chamber; (b) a drive member mounted in said combustion chamber; (c) a crankshaft rotatably mounted to said engine block and driven by said drive member; (d) a disc-type rotary valve mounted on said engine block; (e) an intake passage formed in said rotary valve for directing air into said combustion chamber as said rotary valve rotates; (f) an exhaust passage formed in said rotary valve for exhausting combustion gases from said combustion chamber as said rotary valve rotates; and (g) an exhaust gas recirculation passage in said rotary valve to recirculate exhaust gasses between adjacent cylinders.
  • 21. The rotary valve engine of claim 20 further including cooling means to cool said exhaust gas recirculation valve.
  • 22. The rotary valve engine of claim 21 wherein said cooling means are fins extending from said exhaust gas recirculation valve.
  • 23. The rotary valve engine of claim 20 wherein said drive member is a reciprocating piston.
  • 24. A rotary valve engine comprising:(a) an engine block having a combustion chamber; (b) a drive member mounted in said combustion chamber; (c) a crankshaft rotatably mounted to said engine block and driven by said drive member; (d) a disc-type rotary valve mounted on said engine block; (e) an intake passage formed in said rotary valve for directing air into said combustion chamber as said rotary valve rotates; (f) an exhaust passage formed in said rotary valve for exhausting combustion gases from said combustion chamber as said rotary valve rotates; (g) a valve housing surrounding said rotary valve, said valve housing defining an annular intake chamber; and (h) one or more cooling fins mounted on said valve housing to cool said annular intake chamber.
  • 25. The rotary valve engine of claim 24 wherein said drive member is a reciprocating piston.
  • 26. A rotary valve engine comprising:(a) an engine block having at least one combustion chamber; (b) a drive member mounted in said combustion chamber; (c) a crankshaft rotatably mounted to said engine block and driven by said drive member; (d) a disc-type rotary valve mounted on said engine block; (e) an intake passage formed in said rotary valve for directing air into said combustion chamber as said rotary valve rotates; (f) an exhaust passage formed in said rotary valve for exhausting combustion gases from said combustion chamber as said rotary valve rotates; and (g) a heat conductive plate mounted to the bottom of said rotary valve and heated by combustion during a combustion phase in a first combustion chamber, wherein said heat conductive plate transfers heat to a selected combustion chamber during a compression phase of said selected combustion chamber.
  • 27. The rotary valve engine of claim 26 wherein said drive member is a reciprocating piston.
  • 28. The rotary valve engine of claim 26 wherein said selected combustion chamber is different from said first combustion chamber.
  • 29. A rotary valve engine comprising:(a) an engine block having a plurality of cylinders; (b) a reciprocating piston mounted in each cylinder; (c) at least two crankshafts rotatably mounted to said engine block; (d) a connecting rod connecting each said piston to one of said crankshafts to rotate said crankshaft as the pistons reciprocate in said cylinders; (e) a disc-type rotary valve mounted on said engine block above said cylinders and having an axis of rotation extending generally perpendicular to the axis of rotation of said crankshafts; (f) an intake passage formed in said rotary valve for directing air into each said cylinder in succession as said rotary valve rotates; (g) an exhaust passage formed in said rotary valve for exhausting combustion gases from said cylinders as said rotary valve rotates; and (h) a head to enclose a portion of said cylinders.
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Foreign Referenced Citations (1)
Number Date Country
4324263 Dec 1993 DE