a is a top view of the venting that may be employed around the external wall of the cylinder.
Referring now to the drawings in
Combustion commences generally at a time when a lower wall 12a of the piston 12 of the device 10 is in a lower position. A biasing is provided by back pressure communicated to the upper wall 12b of the piston 12 in the upper chamber 18 of the device 10 from a pump or steam generator, or other means for generation of pressure 20. The upper chamber 18 and lower chamber 19 are separated by a center wall 24 which allows translation of a rod portion 14 of the piston 12. This force maintains the piston 12 at a substantially lower position closest to the engine cylinder 11 until the pressure in the communicating combustion chamber 21 formed by the engine cylinder 11 above the engine piston 17, exceeds the pressure within the upper chamber 18. At this point, the piston 12 translates inside the device cylinder 22 bisected by a center wall 24 toward the upper chamber 18 and provides a means to temporarily increase the volume of the combustion chamber 21 by communicating expanding gases in the combustion chamber 21 for a time period. This temporary expansion of the combustion chamber 21 provides means to control the pressure spike in the combustion chamber 21 at the point of the ignition of fuel and air. Temporarily lowering the compression or pressure at the pressure peak, by temporarily increasing combustion chamber size, thereby eliminates high octane requirements in gasoline engines which currently must match the octane of the fuel to the compression ratio yielding the peak pressure in the combustion chamber 21 to avoid pre-ignition.
Further, such engines as they increase the power and compression of the fuel and air combusted in the combustion chamber 21 must have increasingly heavy and sturdier structural components to communicate that power to the vehicle without damage to moving structural components of the engine. This is particularly true in high compression racing gasoline engines with blowers or other means for pressurized fuel mixture input, and as required by diesel engines which employ a very high compression of the fuel mixture in the combustion chamber to increase temperatures therein sufficiently to ignite the fuel mixture.
When engaged to a gasoline engine through the spark plug hole, or a fuel injector aperture, or as original equipment with formed engine block or head passages, the device 10 will allow the use of diesel fuel in the engaged cylinder 11 thereby converting it to a diesel engine without the conventional requirement for a heavy and strengthened engine structure. This is accomplished from the temporary relief of peak pressure at the pressure spike point of ignition and subsequent communication of stored pressure and energy back to the expanding compression chamber 21 as the engine piston 17 moves away from the device 10.
In operation engaged to the combustion chamber 21 portion of the cylinder 11 of any gas or diesel engine, once a peak pressure in the combustion chamber 21 is reached, which is substantially equal to that of the upper chamber 18 of the device, the communicated gas and pressure in the lower chamber 19 is forced back into the combustion chamber 21. This is caused when the piston 12 in the device 10 moves downward away from the pressurized upper chamber 18 by the higher force of pressure in that chamber caused when the piston 12 is driven toward the upper chamber 18 by gasses from the engine combustion chamber 21.
Subsequently the gases stored under pressure in the lower chamber 19 is forced by the higher pressure in the upper chamber 18, back into the combustion chamber 21. This particularly enhances performance since it provides continued even pressure and force to the engine piston 17 of the communicating cylinder 11 to continue to drive the engine piston 17 downward. This is unlike conventional operation where pressure in the combustion chamber peaks and then drops dramatically as the size of the combustion chamber increases.
In operation the pressure of gasses in the upper chamber 18 provides means to resist movement of the piston 12 and a resulting increase in the volume into which exploding fuel mixtures in the combustion chamber 21 may expand. Thus, a unique and novel ability is provided through the increasing and decreasing of the pressure in the upper chamber 18. Increasing the pressure in the upper chamber 18 will cause the piston 12 to begin to translate toward the upper chamber 18 at a higher pressure and raise the resulting peak pressure in the cylinder combustion chamber 21. Conversely, lowering the pressure of the upper chamber will cause an earlier piston 12 translation resulting in an earlier expansion of the effective volume of the combustion chamber 21, and lowering the peak pressure in the combustion chamber 21. Thus, by regulating the pressure of the upper chamber 18, the compression ratio and volume of the combustion chamber 21 available to expanding gasses may also be adjusted. Pressure to the upper chamber 18 is provided by means for pressure generation such as an air pump engaged to the engine, or steam produced using engine exhaust heat and water. The resulting pressurized gas is fed to the upper chamber 18. A regulator 30 operatively engaged to a means for control such as an electronic control 32 that operates the regulator 30 to maintain a desired pressure in the upper chamber 18 to yield the peak pressure in the combustion chamber 21 desired.
The device 10 and method of employment thus provides a means to make an internal combustion engine operate on any octane gasoline without pre-ignition by adjusting the upper chamber 18 pressure to yield a correct peak pressure for the fuel. Infinite adjustability of the peak pressure and compression ratio of the engine combustion chambers 21 may be obtained by varying the pressure of the upper chamber 18.
The device 10 thus also provides a means for increasing the volume for expansion of exploding fuel mixtures in the compression chamber 21 and means to store the energy thereof by compressing the gas stored in the upper chamber 18 to thereafter expand and force the piston 12 to communicate the gas back into the combustion chamber 21 under force during the stroke of the piston 17 therein. This variable expansion of the combustion chamber 21 by the translating piston 12 of the engaged device 10, and the storage of energy from the exploding fuel mixture by compression in the high pressure upper chamber 18, and communication thereof back to the combustion chamber 21, also provides means for control of or elimination of the pressure spike which exists in all such internal combustion engines close to the time of detention of the fuel and air mixture in the combustion chamber 21. As such, a much smoother power stroke of the engine piston 17 is yielded by more constant communication of an even force over time from the stored energy in the device 10, back into the combustion chamber 21 as it is increasing in volume.
The use of a means for pressure generation and means to regulate the pressure in the upper chamber 18 allows the user to adjust the device to accommodate many types of fuel in the engine to which it is engaged. For instance, a piston driven airplane that runs on high quality aviation gas could use jet fuel or other fuels if needed by adjusting the pressure in the upper chamber 18 and thereby the peak pressure in the engine combustion chamber 21. Vents 23 communicate with the chambers 18 and 19 for venting of gas during their reciprocation.
While all of the fundamental characteristics and features of the method and apparatus for modulation of the pressure spike occurring in internal combustion engine cylinders has been described herein, with reference to particular embodiments thereof, a latitude of modification, various changes and substitutions are intended in the foregoing disclosure and it will be apparent that in some instance, some features of the invention will be employed without a corresponding use of other features without departing from the scope of the invention as set forth. It should be understood that such substitutions, modifications, and variations may be made by those skilled in the art without departing from the spirit or scope of the invention. Consequently, all such modifications and variations are included within the scope of the invention as defined herein.
This application is a continuation-in-part to and claims the benefit of U.S. Provisional Application No. 60/842,498 filed Sep. 5, 2006 and incorporated herein in its entirety by reference. The disclosed device relates to internal combustion engines. More particularly it relates to an apparatus and method engageable either during OEM manufacture or as a retrofit, which provides a secondary pressure chamber as a means to infinitely vary the compression ratio of a communicating engine cylinder and thereby concurrently vary the fuel required to run the engine. Further, the device and method provide a means to modulate the pressure spike occurring during cylinder combustion and particularly during combustion of diesel fuel in an internal combustion engine. Further, when engaged to a gasoline engine, the device and method herein will allow burning of diesel type fuels without reinforcement to the engine structure.
Number | Date | Country | |
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60842498 | Sep 2006 | US |