SYSTEM FOR THE REVERSIBLE TRANSFORMATION OF A RECIPROCATING MOTION IN A ROTARY MOTION
20230059790 · 2023-02-23
Inventors
Cpc classification
F01B9/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B2075/1864
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B57/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01B1/062
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01B2009/061
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01B1/0624
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B75/265
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
System for the reversible transformation of a reciprocating motion in a rotary motion, which may include one or more actuating devices adapted to cooperate with a rotor which has a spiral shaped section, and has at least one interaction surface for interacting with said one or more actuating devices. Each actuating device of said plurality of actuating devices is an internal combustion cylinder and piston device. Each actuating device is associated with a rod which incorporates a slider with a follower which engages with said at least one interaction surface of said rotor.
Claims
1. System for the reversible transformation of a reciprocating motion in a rotary motion, which comprises one or more actuating devices adapted to cooperate with a rotor having a spiral shaped section, and which has at least one interaction surface for interacting with said one or more actuating devices, characterized in that each actuating device of said plurality of actuating devices it is an internal combustion cylinder and piston device, and wherein each actuating device it is associated with a rod which incorporates a slider with a follower which engages with said at least one interaction surface of said rotor.
2. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, wherein said spiral cross section shaped rotor has at least a portion of said at least one interaction surface of the profile of the rotor having a constant diameter, the arrangement being such that when said slider engages the constant diameter portion of said rotor, the volume inside the cylinder of the actuating device is not changed.
3. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, which comprises one or more actuating devices adapted to cooperate with a with spiral section rotor, wherein each actuating device is arranged in a condition inclined with respect to the normal direction of said at least one interaction surface with the rotor.
4. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, wherein the arrangement of each actuating device is such that when the inclination of the device is changed with respect to the normal direction of said at least an interaction surface of said rotor varies the thrust value of the device created onto said rotor, and consequently also varies the torque value to the rotor.
5. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, which comprises one or more actuating devices adapted to cooperate with a with spiral section rotor, wherein each actuating device is arranged in a condition inclined with respect to the normal direction of said at least one interaction surface with the rotor, wherein the arrangement of each actuating device is such that when the inclination of the device varies with respect to the normal direction of said at least one interaction surface of said rotor also varies the expansion/compression phase of each actuating device with respect to a complete revolution of said rotor.
6. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, wherein the arrangement of each actuating device is such that when the inclination of the device varies with respect to the normal direction of said at least one interaction surface of said rotor, the rotation direction of said rotor varies.
7. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, wherein said rotor has at least one interaction surface with said one or more actuating devices which it is inclined with respect to the longitudinal direction of the rotational axis of said rotor.
8. System for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, wherein said rotor has at least one interaction surface with said one or more actuating devices which it is inclined with respect to the longitudinal direction of the rotational axis of said rotor, wherein said at least one interaction surface it is inclined with respect to the longitudinal direction of the rotational axis of the rotor of an angle value comprised between 1 and 89 degrees.
9. System for the reversible transformation of a reciprocating motion in a rotary motion according to according to claim 1, which comprises one or more actuating devices adapted to cooperate with a with spiral section rotor, wherein each actuating device is arranged in a condition inclined with respect to the normal direction of said at least one interaction surface with the rotor, wherein each actuating device it is arranged in an inclined condition with respect to the normal direction of said at least one surface of interaction of said rotor of an angle comprised between −89 and +89 degrees.
10. System for the reversible transformation of a reciprocating motion in a rotary motion according to according to claim 1, which comprises one or more actuating devices adapted to cooperate with a with spiral section rotor, wherein each actuating device is arranged in a condition inclined with respect to the normal direction of said at least one interaction surface with the rotor, wherein said rotor has at least one interaction surface with said one or more actuating devices which is a convex surface.
11. System for reversible transformation of a reciprocating motion in a rotary motion according to according to claim 1, which comprises one or more actuating devices adapted to cooperate with a with spiral section rotor, wherein each actuating device is arranged in a condition inclined with respect to the normal direction of said at least one interaction surface with the rotor, wherein each actuating device it is arranged in a normal condition with respect to said convex surface.
12. A system for the reversible transformation of a reciprocating motion in a rotary motion according to claim 1, comprising one or more actuating devices adapted to cooperate with a rotor rotatable about a longitudinal axis, the rotor having at least one spiral profiled interaction surface for interacting with said one or multiple actuating devices having, the interaction surface comprising at least one ramp, wherein each actuating device of said plurality of actuating devices comprises one or more internal combustion piston cylinders which each incorporate a rod and a slider, and wherein the arrangement of each cylinder with respect to the interaction surface of the rotor always forms an angle of 90 degrees.
13. A system for the reversible transformation of a reciprocating motion in rotary motion, which comprises one or more actuating devices adapted to cooperate with a rotor in an engine block, the rotor having a spiral profiled cross section comprising at least one ramp and which has at least one interacting surface with said one or more actuating devices, wherein each actuating device of said plurality of actuating devices is an internal combustion piston cylinder which incorporates a rod and a slider and a follower, and wherein a lever mechanism it is provided by which the piston return stroke it is performed at the top dead center T.D.C. in the compression phase, said lever mechanism comprising a lever connected in an oscillating manner with said engine block and the lever being fork shaped, said fork having a slider at the end thereof and adapted to cooperate with said interaction surface of said rotor, and wherein said end of said fork lever being adapted to interact with the slider of the piston rod, and wherein during the approach of the rod to said ramp, said lever rises and returns the piston to the T.D.C., and wherein when the cursor reaches the T.D.C. of the piston, said lever disengages from said rod and returns to its initial position.
14. A system for the reversible transformation of a reciprocating motion in rotary motion, which comprises one or more actuating devices adapted to cooperate with a rotor in an engine block, the rotor having at least one interacting surface with said one or more actuating devices, said rotor having a spiral shaped section, and which has at least one interaction surface for interacting with said one or more actuating devices, wherein each actuating device of said plurality of actuating devices it is an internal combustion cylinder and piston device, and wherein each actuating device it is associated with a rod which incorporates a slider with a follower which engages with said at least one interaction surface of said rotor, wherein the rotor includes a first constant diameter profile section, the arrangement being such that during operation said a constant diameter profile section keeps the piston in a stopped position at the top dead center T.D.C. for the combustion phase, thus ensuring complete combustion at constant volume, and wherein the rotor includes a second constant diameter profile section extending from the exhaust valve opening position to the initial compression phase position, the arrangement being such that the piston is kept in a stopped position at the bottom dead center B.D.C. for the complete waste/washing/filling phase of the cylinder, wherein said rotor includes a compression ramp, and an expansion section of the spiral profile of the rotor.
Description
DETAILED DESCRIPTION OF THE INVENTION
[0023] A detailed description of some preferred embodiments of the system for the reversible transformation of a reciprocating motion in a rotary motion of the present invention will now be provided, given by way of non-limiting examples, and with reference to the accompanying drawings, wherein:
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
[0032] With reference now to
[0033] The rotor (53) in
[0034] In
[0035] Thanks to the configuration described above, a better washing of the cylinder (50) is obtained by expelling the burnt gas remaining in the cylinder and a complete filling of the cylinder with fresh air while the piston is not it moves and, therefore, does not interrupt the described cycle, unlike what happens in the current internal combustion engines.
[0036] Both the piston stop solutions to the T.D.C. and to the B.D.C they can be made on the same rotor. In this way, the characteristics and thermodynamic values of the cycles are considerably, improved and more effective.
[0037] In each embodiment, the outer surface of the curvilinear profile of the rotor is in contact with the slider (5) along a coplanar or orthogonal direction. In other words, the cursor (5) transmits a force to the rotor with an angle of 0° (coplanar) or an angle of 90° (orthogonal) with respect to the plane of the rotor.
[0038] Referring now to
[0039] It should be noted that each drive device of this system has a structure similar to that shown in
[0040] It is the external group of devices that inside they are coplanar to the rotor (103). Each actuating device is arranged onto the plate (101).
[0041] The forces of the respective devices are cumulative. In this way, more power can be supplied to a rotor of the same size with respect to the embodiment of
[0042] The number of devices that can be assembled on a rotor depends on its diameter and on the constructive choices. The more groups of devices are mounted on the internal and external profiles of the rotor (103), the more power will be transferred to the rotor. According to this embodiment, the actuating devices operate on the rotor (103) in the manner as already described above and with reference to
[0043] Referring now to
[0044] In this configuration the system (200) provides a plurality of devices, some of which are not arranged on the same horizontal plane containing the rotor (203). The system (200) comprises a shaft (230) connected to the rotor (203).
[0045] The rotor (203) provides curvilinear profiles both on the horizontal (radial) surfaces and on the outer (tangential) surface containing each retraction ramp (205) and (206), respectively.
[0046] More precisely, a first ramp (205) is on an outer surface of the rotor (203). The rotor (203) has a curvilinear spiral profile. One or more actuating devices are arranged both on the horizontal and the vertical plane, to operate on the rotor (203) as said above. Each drive device has a structure as described in
[0047] Some drive devices are positioned perpendicular to the rotor surface (203). The effective force of the devices positioned perpendicularly creates a rotation of the rotor (203) in the same direction (as indicated by the arrow) of those generated by the groups of devices arranged in different positions contained in the horizontal plane containing the rotor, and therefore these forces are cumulative with the forces applied to the rotor by the other devices mounted in different configurations.
[0048] Moreover, in a further alternative embodiment, three different surfaces of the rotor (203) can be engaged at the same time. The actual forces applied by all drive unit groups are combined to generate rotor rotation.
[0049] Therefore, it is possible to simultaneously engaging on the same rotor, groups of internal combustion cylinders fed with different fuels, arranged onto the different profiles of the rotor.
[0050] In the following embodiments, the force applied to the rotor it is transmitted via slider (5) at a different angle from the rotor plane.
[0051] Referring now to
[0052] In the system 400 a combination of actuating devices acts on the rotor (403) at the inclined interacting surface (the devices not being shown in the figure). The system assembly works with an inclination of 45 degrees relative to the rotor (403) and gives a greater net driving force to the rotor (403). The resulting force it is a force as shown by the F1 arrow.
[0053] Changing the angle of inclination of the surface (405) of the rotor (403) the net force applied to the rotor (403) will change accordingly as a result of the variation of the angle because the transmitted force it is a vectoral function of direction.
[0054] While the angle of inclination can vary from 1 to 89 degrees with respect to the plane of the rotor (403), the relative orientation of the whole assembly of actuating devices can be modified in any position between about 1 and 179 degrees with respect to the plane of the rotor (403) or between −89 and +89 degrees with respect to the normal direction of the surface (405) as indicated by the double arrow G.
[0055] According to this system 400, the actuating devices can interact in a direction on the inclined surface (405) or in the opposite mirroring direction on the surface (405′) of the rotor (403), as shown in dashed lines in
[0056]
[0057] In the present embodiment, if the drive unit assembly is positioned orthogonal to the profile (33), in this case, the resulting force is applied with an angle indicated by the arrow F2. In this case, the angle of the profile surface (33) can alternatively vary from about 1 to 89 degrees with respect to the plane and as shown by the dashed surface (435′). Furthermore, the orientation of the device assembly (400) can be comprised at any angle along the double arrow H to provide a variety of different driving forces at different angles, i.e. at any angle corresponding to from about 0 to 180 degrees relative to the plane of the rotor (413).
[0058] Referring now to
[0059] The outer peripheral surface of the rotor (503) it is a rounded surface (505), and extends substantially 360 degrees from a first point of the surface (503a) of the rotor (503) to a second point of the surface (503b) of the rotor (503). The arc length of the rounded surface (505) depends on the thickness of the rotor (503).
[0060] The drive assembly can be arranged in a condition normal to the surface and in any position along the convex surface (505), in the direction indicated by the two-headed arrow “D”. By way of example, a force can be applied by an actuating device along a line as indicated by the arrow F3.
[0061] In this way, a greater net force can be applied by the group of actuating devices (not shown) by adjusting the angle of inclination of the group of devices relative to the plane wherein the rotor (503) resides.
[0062] Referring now to
[0063] The assembly of actuating devices (not shown in the figure) can be oriented in relation to the circular surface of the rotor profile at any position along the surface (515), in the direction of the double arrow E, to have any inclination in relation to the circular surface (515), thus determining the direction of the force of the arrow “F4”.
[0064] Referring now to
[0065] As can be understood from the figures, by changing the inclination of the actuating device (706) with respect to the rotor interacting surface (703) it is possible to obtain different values of forces and consequently different torque values onto the rotor (703).
[0066] More precisely and with particular reference to
[0067] It should be noted here that the cycle phases do not change, so that the expansion and compression phase of the device (706) are always related to the spiral profile of the rotor (703). According to this configuration it is possible to considerably increase the torque on the rotor axis (703) thanks to the choice of the degree of inclination of the device (706). Moreover, it is also possible to vary the stroke of the device (706) proportionally to the inclination of the same with respect to the surface of the rotor (703). In this way a longer or shorter stroke can be obtained, according to the constructive needs, but always corresponding to a complete rotation of the rotor (703).
[0068] Referring now to
[0069] According to this embodiment, a new interaction solution there is provided between one or more piston cylinders and one interacting surface of a rotating rotor about its own longitudinal axis of rotation, wherein the rotor has a circular section, and the interaction surface of the rotor with said one or more piston cylinders it is arranged in a normal direction with respect to the longitudinal axis of the rotor and has a spiral profile with the relevant elevation.
[0070] It should be pointed out here that according to further alternative embodiments, the rotor can have one or more interaction surfaces normal and/or parallel to the longitudinal axis of rotation.
[0071] According to the present embodiment, the positioning of the cylinder (s) provides that each cylinder it is arranged in a manner wherein the contact point of the rods of each cylinder with respect to the interaction surface of the rotor always has an angle of 90 degrees, i.e. orthogonal to the interaction surface.
[0072] This configuration guarantees an ideal distribution of forces on the surface of the rotor, where the same give maximum effect.
[0073] This configuration it is applicable both for internal combustion cylinders, or pneumatic or hydraulic cylinders or other equivalent solutions.
[0074] The force created by the assembly of the piston-cylinders is in this configuration always applied with a right angle throughout the active phase of the cycle, thus transmitting a better energetic effect with minimum energy losses involved.
[0075] With reference now to
[0076] According to this embodiment, an interaction surface of one or more cylinder-pistons of a rotor about a longitudinal axis it is provided, the rotor having a circular cross-section, and the interaction surface of the rotor with the said one or more piston cylinders it is normal to the longitudinal axis of the rotor, and the interaction surface has a spiral profile with a relevant lift ramp.
[0077] It should be noted here that according to alternative embodiments the rotor can have one or more interaction surfaces normal and/or parallel to the longitudinal axis of rotation of the rotor.
[0078] Further, a lever mechanism it is provided which acts during the piston stroke phase at the top dead center T.D.C. in the compression phase. That is, given that the portion of the rotor comprising the spiral profile has a lift ramp with an excessive inclination and therefore creates excessive frictional forces during the stroke of the piston, the presence of the lever allows to provide to the follower a lift force which eliminates such problems during operation.
[0079] More precisely, the lever it is connected to the engine block and therefore does not rotate with the rotor. The lever has a fork shape and a relevant slider or follower placed at the fork end. The ramp acts on the slider, while the end of the lever interacts with the slider of the piston rod. While approaching the ramp, the lever rises and returns the piston to the top dead center T.D.C.
[0080] As soon as the top dead center of the piston T.D.C. is reached, the lever it is released and returns to the starting position. This solution, albeit simple, has the enormous usefulness of limiting the forces engaged, of generating little resistance to the displacement, and the friction is brought to a minimum.
[0081] This configuration is applicable for both internal combustion cylinders, or pneumatic cylinders, or hydraulic cylinders or other equivalents.
[0082] It will be apparent to those skilled in the art that the present invention it is susceptible to other modifications in addition to what has been disclosed herein, without departing from the spirit of the present invention and all included in the scope of the appended claims.