1. Field of the Invention
The present invention relates to an improved system for transformation of rectilinear motion into curvilinear motion, or vice versa, particularly for internal combustion engine.
2. Brief Description of the Art
More specifically, the invention concerns a system of the above kind allowing obtaining the above mentioned transformation of the motion, optimising all the phases or strokes of an internal combustion engine, both for a two stroke engine and for a four stroke engine.
Obviously, the solution suggested can be used also for other kind of structures requiring the transformation of the motion.
Arrangement according to the invention is based on the principle providing the motion in an imaginary point of a Archimedean polar spiral, which, when stressed by an outer force, moves in a direction opposite to the direction of the force acting on the same. Imagining that said an arm to the centre of the spiral connects point; a curvilinear continuous motion is obtained until the application of the outer force is interrupted.
The system according to the invention, realised on the basis of the above-mentioned principle, in function of the direction of the force acting from outside with respect to the spiral, or the direction of the force acting from inside with respect to the spiral, can be realised according to different constructive modes.
Improved system for transformation of rectilinear motion into curvilinear motion, or vice versa, particularly for internal combustion engine, the system comprising a rotor element and a stator element, one of the rotor element and stator element having a closed spiral profile, the spiral profile having a continuous curvilinear portion for at least 270°, and a ramp portion joining the ends of the continuous curvilinear portion, wherein the continuous curvilinear portion extends for about 340°-345° for four-stroke engine and for about 350°-355° for two stroke engines.
Preferably, according to the invention the continuous curvilinear portion extends for about 300°, preferably for about 340°-345° for four-stroke engines and for about 350°-355° for two-stroke engines.
Always according to the invention, the profile can be realised on the outer surface and/or on the inner surface of the rotor element.
Still according to the invention, the profile can also be provided on the upper surface and/or lower surface of the rotor.
According to the invention, a sliding or rolling means can operate, with the lowest possible friction, coupled at the end of the rod of a piston, the piston acting within a cylinder.
Preferably, according to the invention, a plurality of sliding or rolling means-piston-cylinder assemblies can act on the rotor element.
Furthermore, according to the invention, a plurality of rotors, parallel each other, can be provided.
Still according to the invention, the rotor can be provided inside a cylinder-supporting block, i.e. outside a cylinder-supporting block.
Always according to the invention, the sliding or rolling means-piston-cylinder assemblies can be provided either inside or outside.
By the solution suggested according to the present invention the following advantages are obtained:
The present invention will be now described, for illustrative but not limitative purposes, according to its preferred embodiments, with particular reference to the figures of the enclosed drawings, wherein:
Preliminarily, it must be noted that the system according to the invention provides a spiral profile, preferably an Archimedean spiral profile, with a portion of the profile, that can vary on the basis of the specific needing, but in any case not lower than 270°, for the expansion phase of the engine, while a very limited portion of the profile, even only 2°, is destined to the other phases of the engine cycle. In line of principle, it will be of about 6-10° for a two-stroke engine and of about 12-20° for a four-stroke engine.
Observing first
The cylinder supporting block 2 has an inner circular shape, and it is concentric with respect to the rotation axis of the rotor disc 1.
Curve space obtained between disc 1 and block 2 is the expansion space for the piston (pistons) 4.
Each cylinder 5, with the piston 4, rod 6 and wheel 7, is mounted with an inclination angle optimum with respect to the curvilinear shape of rotor 1, and in such a way that the corresponding wheel 7 always is in contact with the disc 1.
Examining the shaped profile of rotor disc 1, ascent-ramp 8 of the spiral shaped curve, or compression ramp, is that part of the rotor curve 1 along which the compression of piston 4 occurs, and at the beginning of the ramp 8 the Bottom Dead Centre (B.D.C.) is provided.
Embodiment shown in
Coming now to observe
Notwithstanding all the other features of the embodiments shown in
Each one of the solutions shown in
Distribution of cylinders 5 (15) must in any case be symmetric with respect to the rotor 1 (11). Number of cylinders 5 (15) only depends on the dimension of the disc 1 (11), so that it is possible realising a large ray disc 1 (11), with a longer arm on which n cylinders 5 (15) will act.
It must be noted that disc 1 (11) ray has no effect on the dimensions of the cylinder 5 (15)-piston 4 (14) group, since the two components are not linked to a fixed point, being thus possible that the cylinder 5 (15)-piston 4 (14) groups are realised with reduced mass dimensions, instead acting on a long rotation arm, thus creating a high momentum with large power, requiring a lower amount of fuel.
Coming now to observe
As it can be noted from the enclosed
An embodiment of an engine according to the invention is shown
Finally, it can be noted from
Cylinder inclination angle (reference position) ensures the realisation of the maximum spiral rotation momentum. Moving away the wheel (when the piston exits from the cylinder) the normal force greatly increases, reaching the maximum value in the position outside the piston. Increasing the inclination of the cylinder, the quick increase of the normal force value is reduced during extraction of piston and in this way also the torque of the piston critic section.
Practically, it is necessary that increasing the inclination of the cylinder, the torque value in the piston critic section is reached, ensuring the wished duration of the piston and the “not disturbed” operation of the curvilinear mechanism.
Piston stroke values, as well those of the reaction forces, of the normal forces and their momentum are given by tables and diagrams by which it is possible individuating the value variations. Spiral rotation in the direction opposite with respect to the motion direction of the piston is demonstrated by the position of the normal force that, for the whole duration of the piston motion, creates a torque about the spiral shaped disc axis.
Only the resistances in the cylinder-piston system are taken into consideration during the studies. Other resistances of the mechanism are not taken into consideration since they are not important. When analysing the results, after having chosen the optimum inclination of the cylinder, it would be necessary taking care to the optimisation of the spiral curve of the disc in correspondence of the zone of passage from the minimum to the maximum ray, in order to prevent shocks during the operation thus promoting a longer lasting of the mechanism.
The present invention has been described for illustrative but not limitative purposes, according to its preferred embodiments, but it is to be understood that modifications and/or changes can be introduced by those skilled in the art without departing from the relevant scope as defined in the enclosed claims.
Number | Date | Country | Kind |
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RM2004A0583 | Nov 2004 | IT | national |
This application is a continuation of International Patent Application No. PCT/IT05/000525, filed on Sep. 15, 2005, which designated the United States and claims priority to Italian Patent Application No. RM2004A000583 filed on Nov. 26, 2004, which is incorporated by reference in its entirety herein.
Number | Name | Date | Kind |
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2120657 | Tucker | Jun 1938 | A |
2249951 | Fulton | Jul 1941 | A |
3841279 | Burns | Oct 1974 | A |
4149498 | Ferrell | Apr 1979 | A |
Number | Date | Country |
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654870 | Dec 1937 | DE |
4344545 | Jun 1995 | DE |
692293 | Nov 1930 | FR |
457876 | Dec 1936 | GB |
Number | Date | Country | |
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20070199525 A1 | Aug 2007 | US |
Number | Date | Country | |
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Parent | PCT/IT2005/000525 | Sep 2005 | US |
Child | 11736826 | US |