EP1540139A1 - Endothermic rotary engine with two parallel rotation axes - Google Patents

Endothermic rotary engine with two parallel rotation axes

Info

Publication number
EP1540139A1
EP1540139A1 EP03790932A EP03790932A EP1540139A1 EP 1540139 A1 EP1540139 A1 EP 1540139A1 EP 03790932 A EP03790932 A EP 03790932A EP 03790932 A EP03790932 A EP 03790932A EP 1540139 A1 EP1540139 A1 EP 1540139A1
Authority
EP
European Patent Office
Prior art keywords
engine
rotor
stator
slider
expansion
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.)
Granted
Application number
EP03790932A
Other languages
German (de)
French (fr)
Other versions
EP1540139B1 (en
Inventor
Ruggero Libralato
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LIBRALATO Ltd
Original Assignee
LIBRALATO Ltd
Libralato Ruggero
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by LIBRALATO Ltd, Libralato Ruggero filed Critical LIBRALATO Ltd
Publication of EP1540139A1 publication Critical patent/EP1540139A1/en
Application granted granted Critical
Publication of EP1540139B1 publication Critical patent/EP1540139B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/18—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
    • F01C1/44—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • F01C21/0809—Construction of vanes or vane holders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/10—Outer members for co-operation with rotary pistons; Casings

Definitions

  • the invention relates to an endothermic engine of the rotative mass type, particularly efficient for the optimal exploitation of the thrust stroke, generated by the firing of a combustible mixture, and by the other strokes of expansion and discharge of the burned gases, and wherein suction and compression of the combustible material are properly arranged, whereby the exploitation of the thrust results in a high power production relative to the minimal size of the engine and to its operative and constructive easiness, and besides to a reduced consumption of combustible material.
  • the pistons of the actual linear engines acting alternatively along their axis, require a transformation of their alternative movement to a rotative movement with proper crank mechanisms, in order to exploit the strength produced on the rotative engine shaft, hence determining a further reduction of the available power.
  • the rotating mass does not comprise any more a single block, but three different elements, that allow the accomplishment of different volumes in the zone of suction of the mixture and the zone of expansion of the burned gas , and thus allow a better and more complete exploitation of the combustion thrust.
  • the practical embodiment of this solution has, in fact, highlighted some mechanical and functional problems that have suggested a series of constructive improvements, which are the object of the present improved endothermic rotative engine.
  • the main object of this invention is still that of improving and optimizing the thermodynamical cycle of the endothermic rotative engines , reaching the ideal ratio between the volumes of the zone of expansion and the volumes of the other zones assigned to the other strokes of the cycle, in order to allow the greatest exploitation of the usable thrust of expansion and an optimal path of the flue gases , and the combustible mixture to be compressed and brought to the firing stroke .
  • a main innovative feature of this invention is that of introducing a cinematic arrangement based on a rotor comprising two semi-cylindrical parts and rotating in the same direction on two parallel rotation axes, with a hinging slider in between, then achieving with such rotor the better exploitation of the thrust during the usable expansion stroke, and the adjustment of the other strokes of suction, compression of the combustible material and discharge of the burned gases, wherein said rotor is held in a stator whose chamber presents two cylindrical openings intersecting each other, and on the flat cover walls of which the seats for the two parallel axes of the rotor are provided, and being provided with proper seats to feed and blast the combustible material and discharge the burned gases.
  • the present improvement pursues the object of making industrially feasible an embodiment of an endothermic rotative engine that is particularly able to exploit fully the power produced during the stroke of expansion, with respect to the different volumes of its zones of suction and compression, determining, under same supplied power, a minimal overall bulk of the engine.
  • Another object of this invention is that of assuring the best conditions of intaking the cooling air and of the combustible material, as an effect of the mutual movement of the parts of the rotor at a suction position prearranged on the stator.
  • a further object of this invention is that of optimizing the form and the volume of the combustion chamber, with respect to the thermo-dynamical yield that a rotating mass engine can allow.
  • Still another object of the present invention is that of allowing a proper scavenging and cooling stroke of the different zones of the engine during its usual working.
  • Another object of the invention is that of facilitating the most efficient arrangement of the tight packings between rotor and stator.
  • Fig. 1 shows an exploded perspective view of the main components of the stator and the rotor that form an engine of the present invention
  • Fig. 2 shows a cross-sectional view of the central part of the stator of the engine of Fig. 1, provided with its cover or back wall;
  • Fig. 3 shows a cross-sectional view of the same central part of the stator of Fig. 2 with the elements of the rotor of Fig. 1 housed therein;
  • Fig. 4 shows a perspective view of a rotating compression element that forms a part of the rotor of Figs . 1 and 3;
  • Fig. 5 shows a perspective view of a slider or hinging and sliding element between the compression element of Fig. 4 and the expansion element of Fig. 6 of the rotor of Fig. 1;
  • Fig. 6 shows a perspective view of an expansion rotating element of the rotor of Figs. 1 and 3, cooperating with the compression element of Fig. 4 and linked and hinged thereto by means of the slider of Fig. 5;
  • Fig. 7 shows a perspective view of the rotor completely assembled, comprising the compression rotating ele- ment of Fig. 4 and the expansion rotating element of Fig. 6 joined and linked to each other by the slider of Fig. 5, the rotor being illustrated in its minimal bulk or closing condition;
  • Fig. 8 shows a perspective view of the rotor, similar to the perspective view of Fig. 7, but with its components arranged in the greatest bulk or opening condition, this condition being in this case illustrated with the rotor turned by about 180° with respect to the situation of Fig. 7;
  • Fig. 9 shows a perspective view of a rotating conduit for the discharge of the burned gases, whose rotary movement is provided by the rotary force of a main shaft of the engine;
  • Fig. 10 shows the arrangement of the stator and the rotor at the moment of the firing, that starts the expansion or usable phase of the cycle;
  • Fig. 11 shows the arrangement at the moment immediately following the firing stroke;
  • Fig. 12 shows the arrangement in a middle moment of the expansion stroke
  • Fig. 13 shows the arrangement at the moment of maximal expansion and exploitation of the burned gases
  • Fig. 14 shows the arrangement at a middle moment of discharge of the burned gases and with the contemporary beginning of the new stroke of suction:
  • Fig. 15 shows the arrangement at the final moment of discharge of the burned gases and of scavenging of the engine with the air or fresh mixture previously sucked in;
  • Fig. 16 shows the arrangement at the moment immediately following the discharge stroke with the scavenging in the final stroke
  • Fig. 17 shows the arrangement at an initial stroke of compression of the mixture
  • Fig. 18 shows the arrangement at a final moment of the stroke of compression of the mixture that precedes its firing stroke and the beginning of a new cycle;
  • the same parts are represented or are understood as represented by the same reference number, while, for representation and interpretation practicality, the different elements are sometimes illustrated with full lines even when they overlap with other elements and should be represented with dotted lines.
  • the endothermic engine at issue is fundamentally formed by a stator A that is in turn formed by a central body Al, by a head cover wall A2 and by a back cover wall A3, while its rotor B, in turn, is formed by a rotating compression element B2, by an expansion rotating element BI and by a slider (or linear linking and hinging element) B3.
  • the central body Al of the stator is fundamentally formed by a pair of cylindrical hollows 1, 2, passing and intersecting each other, said hollows 1, 2 being aligned with vertical axes X and
  • the hollows 1, 2 are contained in a substantially double cylinder-shaped center annulus 4 provided with external cooling fins 5.
  • a hole 6 with an inner thread is provided for the housing of a spark plug or injector 7 (cf. Fig. 2), said hole 6 being allowed to communicate with an open compartment or combustion chamber 8 arranged between the hole 6 and the hollows 1, 2.
  • the chamber 8 is shaped with a substantially rounded surface and opens toward the hollows 1, 2.
  • the chamber 8 is placed substantially between the two vertical axes X, Y.
  • a chamfer 9 of the chamber 8 links and connects the combustion chamber 8 with the upper part of the hollow 2.
  • a cylindrical exhaust port 10 is provided in the lower part of the central body Al, in a proper position of a lower part 4" of the annulus 4, a cylindrical exhaust port 10 is provided.
  • the exhaust port is arranged at a side face of the annulus 4 and is connected with flares 11 that are open along the inner surface of the cylindrical hollow 1.
  • the exhaust port 10 is arranged with an inclination ⁇ equal to about 20° with respect to the axis X of the hollow 1 (cf. Fig. 2).
  • the central body Al is completed by the presence of a series of holes 12, into which plugs and/or screws are applied, for steadily fixing the central body Al to the opposing head and back covers or walls A2 , A3.
  • the covers A2 , A3 are substantially formed by flat bodies externally finned, and are provided with opposing flat surfaces
  • the outer perimeter of the covers A2, A3 corresponds to the outer perimeter of the center annulus 4 of the central body Al , to which they are steadily fixed, for example by means of screws and/or plugs passing through holes
  • Both covers A2 , A3, at their opposing surfaces 20, 40 contacting the central body Al have a cylindrical groove or hollow 22 that is coaxial to the axis YZ, being thus concentric to the hollow 1 of the central body Al .
  • Each of the cylindrical grooves 22 determines, in its inner side (or better axial bottom) a circular surface 23 having a circumference equal to the inner diameter of the groove 22.
  • An axially raised portion or plane 24 is provided on a part of the surface 23, its edge being determined partially by the inside radius of the groove 22 and on its opposite side by a corresponding radius centered on the axis XZ of the hollow 1 of the central body Al.
  • a hole 25 that is preferentially tilted and provided with an inner flare 26, is provided on each of the raised portions 24 of the covers A2 , A3.
  • the flare 26 is placed at the lower part of the covers A2, A3 and turns inwardly.
  • the hole 25 is placed between the axes X, Y of the hollows 1, 2, constrained within the cylindrical part of the respective groove 22.
  • a cylindrical tang 27 projects from the raised portion 24.
  • the tang or support 27 projects toward the inner side of the hollow 1 and is arranged concentrically to the axis XZ . Further, the tang 27 is provided with an axial hole 28 that communicates with the respective outer surfaces of the covers A2 , A3.
  • the covers A2, A3 each further comprise a cylindrical through hole 29 that is placed in such a position to be coaxial to the port 10 of the central body Al, and a through hole 30 shaped, as shown, as a circular segment and intended to communicate with that zone of the hollow 1 that is near the flares 11 which communicate with the exhaust port 10 of the central body Al .
  • the circular segment shape of the hole 30 is determined by the necessity of facilitating at its best the exhaust stroke, during opening and closing thereof, regulated by the passage of particular points of the elements Bl, B2.
  • rotor B substantially comprises the expansion rotating element Bl hinged by means of the slider B3 (or hinging or sliding element) .
  • the rotating compression element B2 is housed in the hollow 2 of the stator A, and is provided to rotate around the axis YZ of the stator A, this being meant to achieve the best compression of the mixture, before firing it in the combustion chamber 8.
  • the compression element B2 is formed by a circular segment outer surface wall 50 having a radius substantially identical to the radius of the hollow 2, and being supported by a pair of side walls 51, 52 that are linked on their respective outside surfaces, to a pair of rings 53 and 54, respectively. Being placed outside the side walls 51, 52, the pair of rings 53, 54 presents a reciprocal distance that is equal to the width of the circular segment surface wall 50, which is, in turn, substantially identical to the width or depth of the central body Al, in the hollow 2 of which said compression element B2 is meant to rotate.
  • the rings 53, 54 of the compression element B2 are inserted into the respective holes or cylindrical grooves 22 of the covers A2, A3 which have diameters corresponding thereto and being properly provided with antifriction and lubrificant means .
  • the compression element B2 is allowed to rotate inside the hollow 2 of the stator A, guiding its rings 53, 54 within the grooves 22 that engage them on the longitudinal axis YZ of the stator A.
  • the side walls 51, 52 of the compression element B2 have an end provided with hinging loops 55, 56 that are linked to each other by an end portion 50' of the circular segment-shaped outside surface wall 50, and that are preferentially provided with bushes or antifriction bearings 57, 58.
  • the expansion rotating element Bl of the rotor B comprises a circular segment-shaped surface wall 60 having an outer radius substantially identical to the radius of the hollow 1 of the stator A, in which hollow 1 the element Bl is housed to rotate on its axis XZ , in order to assure the best tight conditions during the usable stroke of expansion.
  • the expansion rotating element Bl is to be connected to the compression element B2.
  • the circular segment wall 60 has a width substantially identical to the width of the central body Al of the stator A.
  • the segment wall 60 extends over a portion of the circumference of less than 180° and is provided with side surfaces 61 substantially plane and meant to slide on the flat surfaces 20, 40 of the stator covers A2 and A3, respectively, except for interposing of proper tight packings, as already specified in the previous Italian patent application (cf. Fig. 6).
  • Said side walls or surfaces 61 have a depressed zone 62 near a hub portion 63 through which a through hole 64 is provided, in which two portions 80', 80" of a main shaft 80 are keyed or otherwise fixed (cf. Fig. 7).
  • the depressed zone 62 allows the walls 51, 52 of the compression element B2 to rotate without contacting neither of the element Bl and the walls 24 of the stator covers A2 , A3.
  • a groove or further depression 65 with limited corner width is provided on the depressed zone 62, and in particular on both sides of the hub 63 of the side walls 61.
  • the hub 63 is further provided with, besides the through hole 64 able to house and steadily fix the main shaft 80, a radial shoulder 66 and a radial flat surface 67 that will be used as thrusting surfaces during the expansion stroke of the engine at issue.
  • the expansion rotating element Bl is completed by the presence of a radial through hole 68 which starts at the outer wall of the shoulder 66 of the hub 63, and reaches the outer side of the edge or circular segment wall 60.
  • the through hole 68 has a rectangular cross section, with one of its inner surfaces aligned to the thrusting flat surface 67.
  • the rotor B is completed by the presence of a slider B3 able to connect, hinge and make the compression element B2 interact with the expansion element Bl inside the stator A, so as to achieve the different strokes foreseen in the thermodynamic cycle of the engine at issue.
  • the slider B3 is shown in detail in Fig. 5.
  • the slider B3 comprises a rod or shaft 70 having a rectangular cross section, or, in any case, a cross section substantially identical to the cross section of the through hole 68 provided in the expansion element Bl, and being provided with a T-shaped head 71.
  • the width of the head 71 is identical to the width of the circular outer surface wall 50 of the compression element B2 and the circular segment surface wall 60 of the expansion element Bl.
  • a pivot 72 is fixed, arranged parallel to the axis XY.
  • the lower end (portino) of the head 71 has a hollow partially cylindrical surface 74 that determines a cylindrical port 73 concentric to the pivot 72 and able to house the head surfaces of the loops 55, 56 at the side walls 51, 52 of the element B2.
  • the port 73 achieves a gas tightness by means of proper tight sealing segments placed on the surface 74.
  • the slider B3 is linked to the compression element B2 upon insertion of the two sides of the pivot 72 into the through holes of the loops 55, 56 of the side walls 51, 52 of the compression element B2.
  • the pivot 72 of the slider B3 hinges the loops 55, 56 of the compression element B2.
  • the head portions of the loops 55, 56 are thus housed in the circular port 73, delimited by the pivot 72 and the cylindrical surface 74 of the head of the slider B3.
  • the assembly proceeds then with the insertion of the rod 70 of the slider B3 into the through hole port 68 of the element Bl, starting from the part of the flat surface 67.
  • the compression element B2 is forced to rotate on axis YZ , being forced by its cylindrical rings 53, 54 supported within the grooves 22 of the stator covers A2 , A3, the expansion element Bl is forced to rotate on the axis XZ because it is linked to the main shaft 80.
  • the main shaft 80 is supported at the axial hole seats 28 of the stator covers A2, A3.
  • a reciprocal relative rotating movement of the elements Bl, B2 is allowed by the contemporary or simultaneous translation of the slider B3, that moves its hinged pivot 72 along the axis of the through hole port 68, and the rotation of the element B2 on the pivot 72 of the slider B3.
  • the rotating movement of the compression element B2 and the consequent displacement of the slider B3 are caused by the rotating movement of the expansion element Bl that is forced to rotate on its axis X , as a consequence of the blast or ignition of the combustible mixture in the combustion chamber 8.
  • the expansion element Bl at the beginning of the combustion, presents its minimal thrust flat surface 67 to the expanding combusting mixture, the minimal thrust flat surface being just sufficient to make it move. But with the fast development of the expansion, a force is immediately generated that forces the element Bl to turn in the only possible direction, presenting the gas thrust an increasing thrust surface 67, and, consequently, the expansion volume of the burned gases increases to completely obtain and use the power of the firing process.
  • the stroke of the largest circumferential divergation or relative circumferential rotation between elements Bl and B2, as illustrated in Fig. 8, determines also the greatest suction volume of air or fresh mixture, to which is also relevant the position of the holes 25 provided on the covers A2, A3 of the stator A and the position of the groove or depression 65 of the hub 63 present on the expansion element Bl.
  • the compression element B2 cooperates with the surface 67 of the element Bl, with the head 71 of the slider B3 and with the side walls of the hollow 1 of the stator A, for forming the expansion volume and for exhausting the burned gases that, by means of the flares 11 and the lateral draft through holes 30, are forced toward the exhaust port 10.
  • the port 10 does not directly accomplish the task of exhausting the burned gases, but it houses a rotating conduit 90, that, as illustrated in Fig. 9, has holes 91, 92 in correspondence to the bored flares 11 and through holes 30 of the central block Al of the stator A, and able to be aligned with said flares and holes 11, 30, respectively, but only during the stroke of exhausting the burned gases, while in the other strokes, the conduit 90 is induced to turn so as to present its closed cylindrical surface adjacent to the holes.
  • conduit 90 With its exhaust holes 91, 92, constitutes the exhaust valve of the engine at issue, thanks to which the suction of the exhaust of the engine at issue is avoided.
  • the arrangement and adjustment of the holes 91, 92 of the conduit 90, in order to present them to the holes 11, 30 of the stator A for the desired exhaust stroke of burned gases is achieved, for example, by means of a crown gear 93 driven by the main shaft 80, by interposing another crown gear, a belt or a chain, or any other element able to achieve the proper reduced rotation rate, so that the desired exhaust phasing is achieved.
  • operation starts with the end portion 50' of the compression element B2 being placed near the chamfer 9, so as to facilitate the access of the combustible mixture into the combustion chamber 8 of the stator A; that means that the element B2 has already run along the whole cylindrical portion of the hollow 2 and has already brought the combustible mixture MC within chamber 8 to its greatest degree of compression.
  • the spark plug 7 ignites its ignition spark, that fast but gradually fires the mixture MC, causing its expansion.
  • the combustible mixture MC is compressed in the compression chamber 8 and is kept therein, both by the action of the end portion 50' of the cylindrical surface wall 50 of the compression element B2, and by the end of the surface wall 60 of the expansion element Bl, that is placed tight on the side surface of hollow 1, and also by the head 71 of the slider B3 that is interposed sealingly tight between the elements Bl and B2 , and that in that situation, induces the elements Bl, B2 to their largest circumferential divergation, corresponding to that illustrated in Fig. 8.
  • the suction holes 25 of the stator covers A2, A3 are placed over the depressed groove 65 of the expansion element Bl, allowing the flow of fresh mixture MF from the outside of the engine, and its expansion ME in any free space that the largest circumferential divergation between elements Bl, B2 provides within the hollows 1, 2, and so in any free space between the expansion element Bl and the compression element B2.
  • the expanded mixture ME helps in cooling the walls of the hollow 2, and the inner walls of the elements Bl, B2, said expanded mixture ME being gradually compressed corresponding to the increase of the volume of the combusting mixture MS.
  • Fig. 13 represents the maximum development of the stroke of expansion or usable thrust stroke of the combusting mixture MS, because, when continuing its rotation, the expansion element Bl meets the draft holes 11, 30 that connect to the hole 10, where the exhaust pipe 90 is open with its holes 91, 92 aligned with the draft holes 11, 30, so as to begin the stroke of exhausting the burned gases, as represented in the following Figs. 14 and 15.
  • Fig. 14 represents the situation, in which the burned gases are reduced under environmental pressure, just before the hollows 1, 2 are connected because of the approaching of the end of the wall 50 at the chamfer 9.
  • the entry of the fresh gas into the expansion area of hollow 1 determines the complete discharge of the residual combustion material via the still open holes 91, 92 of the exhaust pipe 90.
  • the forming of the suction volume MF occurs without possibility of communication with the hollows 1, 2, as can be seen in Figs. 14 to 17, assuring thus its maximum capacity and rapidity of accomplishment.
  • FIG. 14 it is highlighted how the embodiments of the groove 65, not represented in Fig. 14 but shown in Fig. 6, and the shape of the contiguous portions of the hub portion 63 of the compression element Bl, and the inner portion of the end portion 50 of the element B2 cooperate to determine an initial suction volume practically equal to zero, for the maximum efficiency of the following suction stroke.
  • the hub portion 63 of the element Bl is engaged on the inner wall of end portion 50 of the suction element B2, in order to achieve a sufficient sealing tightness against the mentioned inner wall, to isolate the suction volume MF from the expanded mixture ME.
  • the potentiality of the suction stroke is determined by the concomitant conformation of the elements Bl, B2, B3 of the rotor B, according to what has been described above and illustrated in Figs. 14 to 17, achieving a sufficient isolation of the initial volume. Proceeding in the rotation of the expansion element Bl, the condition of Fig.
  • the suggested embodiment has a bulk and size that is minimal with respect to the power that it can produce, according to other specified objects. Also, the reciprocal movement of the expansion and compression elements Bl, B2 inside the sealing tights in the hollows 1, 2 supports to improve the suction of the fresh air, besides the scavenging and exhaust stroke, according to other specified objects.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

The object of the invention is an endothermic engine of the rotating mass type. An innovative feature of the invention is that of presenting a kinematic mechanism based on a rotor comprising two parts (B1, B2) of semi-cylindrical shape and rotating in the same direction on two contiguous axes with interpositioning of a slider (B3) hinging the parts (B1, B2), said parts being contained in the hollows (1, 2) of a stator (A) in which is provided a combustion chamber (8) and an opposing exhaust pipe (90) for the burned gases. The inventive engine achieves an expansion stroke (MS) able to greatly exploit the power of the firing, while a conduit (25) assures the contemporary suction stroke, supported by the ability of the parts (B1, B2) to circumferentially diverge, and the part (Bl) provides for the consequent stroke of compression of a combustible mixture (ME).

Description

ENDOTHERMIC ROTARY ENGINE WITH TWO PARALLEL ROTATION AXES
The invention relates to an endothermic engine of the rotative mass type, particularly efficient for the optimal exploitation of the thrust stroke, generated by the firing of a combustible mixture, and by the other strokes of expansion and discharge of the burned gases, and wherein suction and compression of the combustible material are properly arranged, whereby the exploitation of the thrust results in a high power production relative to the minimal size of the engine and to its operative and constructive easiness, and besides to a reduced consumption of combustible material.
In the actual endothermic crank mechanism engines there are notoriously cylindrical pistons that can intake at most the same volume of mixture as the volume of greatest expansion of the burned gas, it being well-known that the suction stroke occurs in the same chamber that is then used for the expansion or usable phase of the engine.
Since, notoriously, the explosion and combustion of the compressed mixture determines a greater volume with respect to the volume of the same mixture before the blast, it is clear that in the actual alternative engines that use the same chamber both for suction and for expansion, not all the available pressure is exploited for the thrust, causing in effect, an inner loss of the usable work of the piston.
Furthermore, the pistons of the actual linear engines, acting alternatively along their axis, require a transformation of their alternative movement to a rotative movement with proper crank mechanisms, in order to exploit the strength produced on the rotative engine shaft, hence determining a further reduction of the available power.
Finally, the linear and axial arrangement of the pistons and of their sliding chambers of the actual endothermic engines not only requires the necessary presence of the above-mentioned crank mechanisms, but also determines their big bulk and consequent great size, with respect to usable volume of the expansion stroke, and leads to a structure necessarily steady, complex and heavy that further reduces their efficiency and practicality, still without eliminating vibrations and loudness of the actual engines. Many studies and attempts at solutions improving the known alternative piston engines foresee the presence of a piston or mass, that is allowed to rotate in a cylindrical opening communicating with proper predefined suction, compression, firing and expansion spaces, so that a single rotative element can accomplish at the same time these strokes, passing, with its specific perimeter part, through each specific zone of the stator, thus eliminating any actual vain travel and giving directly the rotatory movement to the shaft of the engine.
All these rotative solutions have been revealed as scarcely useful in practice, mainly because of the difficulties of removal of the heat of the rotative piston, with consequent difficulty in adjusting its expansions and managing its sealing tightnesses with respect to the stator containing it, so as to avoid the dispersion of the combustible mixture and flue gases into the not relevant zones.
Also, the structure of the chamber of combustion in the actual rotating engines presents difficulties in coordinating their optimal form for the combustion with respect to the desired compression parameters.
Another great disadvantage of the rotating piston engines accomplished until now is that of having never foreseen an expansion opening having a bigger volume than the suction opening with the consequence that these endothermic engines do not exploit the greater volume of the expansion stroke and they do not improve the yield of the thrust stroke. In order to overcome all these disadvantages and difficulties and thus making all the advantages of a rotating mass engine feasible, with respect to the known alternative mass engines, the Italian patent 1 250 184 dated April 3, 1995 has been lodged, in which a rotating mass engine is proposed, based on a stator having two centers of rotation, and on a rotor comprising two parts indicatively semi-cylindrical and rotating in the same direction, each on one of the two axes of the stator, such parts being linked to each other by means of a sluice board or slider that acts as a hinge between the two parts of the rotor and allows their mutual sliding and divergation during rotation.
According to this proposed solution, the rotating mass does not comprise any more a single block, but three different elements, that allow the accomplishment of different volumes in the zone of suction of the mixture and the zone of expansion of the burned gas , and thus allow a better and more complete exploitation of the combustion thrust.
Still according to this solution already proposed, a better gas-tightness is possible, since the packings are placed on cylindrical and flat surfaces that act on sealing surfaces and not on sealing lines any more, as in previous rotative engines.
The practical embodiment of this solution has, in fact, highlighted some mechanical and functional problems that have suggested a series of constructive improvements, which are the object of the present improved endothermic rotative engine. The main object of this invention is still that of improving and optimizing the thermodynamical cycle of the endothermic rotative engines , reaching the ideal ratio between the volumes of the zone of expansion and the volumes of the other zones assigned to the other strokes of the cycle, in order to allow the greatest exploitation of the usable thrust of expansion and an optimal path of the flue gases , and the combustible mixture to be compressed and brought to the firing stroke .
A main innovative feature of this invention is that of introducing a cinematic arrangement based on a rotor comprising two semi-cylindrical parts and rotating in the same direction on two parallel rotation axes, with a hinging slider in between, then achieving with such rotor the better exploitation of the thrust during the usable expansion stroke, and the adjustment of the other strokes of suction, compression of the combustible material and discharge of the burned gases, wherein said rotor is held in a stator whose chamber presents two cylindrical openings intersecting each other, and on the flat cover walls of which the seats for the two parallel axes of the rotor are provided, and being provided with proper seats to feed and blast the combustible material and discharge the burned gases.
The other objects, already mentioned and pursued in the above- mentioned patent, relate to the constructive easiness, to the possibility of maximum cooling and better tightness of the packings, to the silence and to the absence of vibrations, which objects are better achieved in the present improved constructive solution, as well. In particular, the present improvement pursues the object of making industrially feasible an embodiment of an endothermic rotative engine that is particularly able to exploit fully the power produced during the stroke of expansion, with respect to the different volumes of its zones of suction and compression, determining, under same supplied power, a minimal overall bulk of the engine.
Another object of this invention is that of assuring the best conditions of intaking the cooling air and of the combustible material, as an effect of the mutual movement of the parts of the rotor at a suction position prearranged on the stator.
A further object of this invention is that of optimizing the form and the volume of the combustion chamber, with respect to the thermo-dynamical yield that a rotating mass engine can allow.
Still another object of the present invention is that of allowing a proper scavenging and cooling stroke of the different zones of the engine during its usual working.
Another object of the invention is that of facilitating the most efficient arrangement of the tight packings between rotor and stator.
These particular objects and those already mentioned in the above-mentioned patent, the content of which being incorporated herein by reference, are in effect perfectly achieved with the improved endothermic rotative engine of the present invention, which, in the following, is described and illustrated in one embodiment only exemplary and not limitative, shown in the drawings, in which:
Fig. 1 shows an exploded perspective view of the main components of the stator and the rotor that form an engine of the present invention;
Fig. 2 shows a cross-sectional view of the central part of the stator of the engine of Fig. 1, provided with its cover or back wall;
Fig. 3 shows a cross-sectional view of the same central part of the stator of Fig. 2 with the elements of the rotor of Fig. 1 housed therein;
Fig. 4 shows a perspective view of a rotating compression element that forms a part of the rotor of Figs . 1 and 3;
Fig. 5 shows a perspective view of a slider or hinging and sliding element between the compression element of Fig. 4 and the expansion element of Fig. 6 of the rotor of Fig. 1;
Fig. 6 shows a perspective view of an expansion rotating element of the rotor of Figs. 1 and 3, cooperating with the compression element of Fig. 4 and linked and hinged thereto by means of the slider of Fig. 5;
Fig. 7 shows a perspective view of the rotor completely assembled, comprising the compression rotating ele- ment of Fig. 4 and the expansion rotating element of Fig. 6 joined and linked to each other by the slider of Fig. 5, the rotor being illustrated in its minimal bulk or closing condition;
Fig. 8 shows a perspective view of the rotor, similar to the perspective view of Fig. 7, but with its components arranged in the greatest bulk or opening condition, this condition being in this case illustrated with the rotor turned by about 180° with respect to the situation of Fig. 7;
Fig. 9 shows a perspective view of a rotating conduit for the discharge of the burned gases, whose rotary movement is provided by the rotary force of a main shaft of the engine;
Figs. 10 to 18
schematically show some aspects of the typical working strokes of a cycle of the engine at issue, the strokes being illustrated with the rotor moving anticlockwise for graphical practicality and for uniformity with the previous views of the components of the engine, wherein:
Fig. 10 shows the arrangement of the stator and the rotor at the moment of the firing, that starts the expansion or usable phase of the cycle; Fig. 11 shows the arrangement at the moment immediately following the firing stroke;
Fig. 12 shows the arrangement in a middle moment of the expansion stroke;
Fig. 13 shows the arrangement at the moment of maximal expansion and exploitation of the burned gases;
Fig. 14 shows the arrangement at a middle moment of discharge of the burned gases and with the contemporary beginning of the new stroke of suction:
Fig. 15 shows the arrangement at the final moment of discharge of the burned gases and of scavenging of the engine with the air or fresh mixture previously sucked in;
Fig. 16 shows the arrangement at the moment immediately following the discharge stroke with the scavenging in the final stroke;
Fig. 17 shows the arrangement at an initial stroke of compression of the mixture;
Fig. 18 shows the arrangement at a final moment of the stroke of compression of the mixture that precedes its firing stroke and the beginning of a new cycle; In all drawings, the same parts are represented or are understood as represented by the same reference number, while, for representation and interpretation practicality, the different elements are sometimes illustrated with full lines even when they overlap with other elements and should be represented with dotted lines.
According to the embodiment proposed in the different figures of the drawing, and in particular with reference to Fig. 1, the endothermic engine at issue is fundamentally formed by a stator A that is in turn formed by a central body Al, by a head cover wall A2 and by a back cover wall A3, while its rotor B, in turn, is formed by a rotating compression element B2, by an expansion rotating element BI and by a slider (or linear linking and hinging element) B3.
The central body Al of the stator is fundamentally formed by a pair of cylindrical hollows 1, 2, passing and intersecting each other, said hollows 1, 2 being aligned with vertical axes X and
Y parallel and spaced to each other by a distance 3, and with a common horizontal axis Z. The intersections between the axis X,
Y and the axis Z determine the longitudinal axes XZ and YZ , which are orthogonal to the axes X, Y, Z, are parallel to each other, and concentric to the respective cylindrical walls of the hollows 1, 2. The hollows 1, 2 are contained in a substantially double cylinder-shaped center annulus 4 provided with external cooling fins 5.
In the upper part of the central body Al, in a proper position of an upper part 4 ' of the annulus 4 , a hole 6 with an inner thread is provided for the housing of a spark plug or injector 7 (cf. Fig. 2), said hole 6 being allowed to communicate with an open compartment or combustion chamber 8 arranged between the hole 6 and the hollows 1, 2. The chamber 8 is shaped with a substantially rounded surface and opens toward the hollows 1, 2. The chamber 8 is placed substantially between the two vertical axes X, Y.
A chamfer 9 of the chamber 8 links and connects the combustion chamber 8 with the upper part of the hollow 2.
In the lower part of the central body Al, in a proper position of a lower part 4" of the annulus 4, a cylindrical exhaust port 10 is provided. The exhaust port is arranged at a side face of the annulus 4 and is connected with flares 11 that are open along the inner surface of the cylindrical hollow 1. The exhaust port 10 is arranged with an inclination β equal to about 20° with respect to the axis X of the hollow 1 (cf. Fig. 2).
The central body Al is completed by the presence of a series of holes 12, into which plugs and/or screws are applied, for steadily fixing the central body Al to the opposing head and back covers or walls A2 , A3.
The covers A2 , A3 are substantially formed by flat bodies externally finned, and are provided with opposing flat surfaces
20 and 40, respectively. The outer perimeter of the covers A2, A3 corresponds to the outer perimeter of the center annulus 4 of the central body Al , to which they are steadily fixed, for example by means of screws and/or plugs passing through holes
21 and 41, respectively, that are aligned to the holes 12 presenting themselves at the side faces of the central body Al . Both covers A2 , A3, at their opposing surfaces 20, 40 contacting the central body Al , have a cylindrical groove or hollow 22 that is coaxial to the axis YZ, being thus concentric to the hollow 1 of the central body Al .
Each of the cylindrical grooves 22 determines, in its inner side (or better axial bottom) a circular surface 23 having a circumference equal to the inner diameter of the groove 22.
An axially raised portion or plane 24 is provided on a part of the surface 23, its edge being determined partially by the inside radius of the groove 22 and on its opposite side by a corresponding radius centered on the axis XZ of the hollow 1 of the central body Al.
A hole 25 that is preferentially tilted and provided with an inner flare 26, is provided on each of the raised portions 24 of the covers A2 , A3. The flare 26 is placed at the lower part of the covers A2, A3 and turns inwardly. The hole 25 is placed between the axes X, Y of the hollows 1, 2, constrained within the cylindrical part of the respective groove 22.
A cylindrical tang 27 projects from the raised portion 24. The tang or support 27 projects toward the inner side of the hollow 1 and is arranged concentrically to the axis XZ . Further, the tang 27 is provided with an axial hole 28 that communicates with the respective outer surfaces of the covers A2 , A3.
The covers A2, A3 each further comprise a cylindrical through hole 29 that is placed in such a position to be coaxial to the port 10 of the central body Al, and a through hole 30 shaped, as shown, as a circular segment and intended to communicate with that zone of the hollow 1 that is near the flares 11 which communicate with the exhaust port 10 of the central body Al .
In particular, the circular segment shape of the hole 30 is determined by the necessity of facilitating at its best the exhaust stroke, during opening and closing thereof, regulated by the passage of particular points of the elements Bl, B2.
After having described the main components constituting the stator A of the engine at issue, the main components of the rotor B, which are to be housed in the hollows 1, 2 of the stator A, are hereinafter described.
As already mentioned, that rotor B substantially comprises the expansion rotating element Bl hinged by means of the slider B3 (or hinging or sliding element) .
The rotating compression element B2 is housed in the hollow 2 of the stator A, and is provided to rotate around the axis YZ of the stator A, this being meant to achieve the best compression of the mixture, before firing it in the combustion chamber 8.
The compression element B2 is formed by a circular segment outer surface wall 50 having a radius substantially identical to the radius of the hollow 2, and being supported by a pair of side walls 51, 52 that are linked on their respective outside surfaces, to a pair of rings 53 and 54, respectively. Being placed outside the side walls 51, 52, the pair of rings 53, 54 presents a reciprocal distance that is equal to the width of the circular segment surface wall 50, which is, in turn, substantially identical to the width or depth of the central body Al, in the hollow 2 of which said compression element B2 is meant to rotate.
By application of the covers A2 , A3 to the sides of the central stator body Al, after introduction of the compression element B2 into the hollow 2, a consequent theoretical contact between the outside surfaces of the walls 51, 52 of the compression element B2 and the inside flat and opposing surfaces 20, 40 of the covers A2, A3 is reached, except for the foreseeable clearances for the application of the side tight sealing segments as already indicated in the previous Italian patent application.
By the application of the covers A2 , A3, further, the rings 53, 54 of the compression element B2 are inserted into the respective holes or cylindrical grooves 22 of the covers A2, A3 which have diameters corresponding thereto and being properly provided with antifriction and lubrificant means .
Within this embodiment, the compression element B2 is allowed to rotate inside the hollow 2 of the stator A, guiding its rings 53, 54 within the grooves 22 that engage them on the longitudinal axis YZ of the stator A. The side walls 51, 52 of the compression element B2 have an end provided with hinging loops 55, 56 that are linked to each other by an end portion 50' of the circular segment-shaped outside surface wall 50, and that are preferentially provided with bushes or antifriction bearings 57, 58. The expansion rotating element Bl of the rotor B comprises a circular segment-shaped surface wall 60 having an outer radius substantially identical to the radius of the hollow 1 of the stator A, in which hollow 1 the element Bl is housed to rotate on its axis XZ , in order to assure the best tight conditions during the usable stroke of expansion.
The expansion rotating element Bl is to be connected to the compression element B2. The circular segment wall 60 has a width substantially identical to the width of the central body Al of the stator A. The segment wall 60 extends over a portion of the circumference of less than 180° and is provided with side surfaces 61 substantially plane and meant to slide on the flat surfaces 20, 40 of the stator covers A2 and A3, respectively, except for interposing of proper tight packings, as already specified in the previous Italian patent application (cf. Fig. 6).
Said side walls or surfaces 61 have a depressed zone 62 near a hub portion 63 through which a through hole 64 is provided, in which two portions 80', 80" of a main shaft 80 are keyed or otherwise fixed (cf. Fig. 7). The depressed zone 62 allows the walls 51, 52 of the compression element B2 to rotate without contacting neither of the element Bl and the walls 24 of the stator covers A2 , A3.
On the depressed zone 62, and in particular on both sides of the hub 63 of the side walls 61, a groove or further depression 65 with limited corner width is provided. The hub 63 is further provided with, besides the through hole 64 able to house and steadily fix the main shaft 80, a radial shoulder 66 and a radial flat surface 67 that will be used as thrusting surfaces during the expansion stroke of the engine at issue.
The expansion rotating element Bl is completed by the presence of a radial through hole 68 which starts at the outer wall of the shoulder 66 of the hub 63, and reaches the outer side of the edge or circular segment wall 60. The through hole 68 has a rectangular cross section, with one of its inner surfaces aligned to the thrusting flat surface 67.
As already mentioned, the rotor B is completed by the presence of a slider B3 able to connect, hinge and make the compression element B2 interact with the expansion element Bl inside the stator A, so as to achieve the different strokes foreseen in the thermodynamic cycle of the engine at issue. The slider B3 is shown in detail in Fig. 5.
The slider B3 comprises a rod or shaft 70 having a rectangular cross section, or, in any case, a cross section substantially identical to the cross section of the through hole 68 provided in the expansion element Bl, and being provided with a T-shaped head 71. The width of the head 71 is identical to the width of the circular outer surface wall 50 of the compression element B2 and the circular segment surface wall 60 of the expansion element Bl. At the same end of the rod 70, but on the side opposite with respect to its longitudinal axis (rectangular portino), a pivot 72 is fixed, arranged parallel to the axis XY. The lower end (portino) of the head 71 has a hollow partially cylindrical surface 74 that determines a cylindrical port 73 concentric to the pivot 72 and able to house the head surfaces of the loops 55, 56 at the side walls 51, 52 of the element B2. The port 73 achieves a gas tightness by means of proper tight sealing segments placed on the surface 74.
After having thus described the main components of the stator A and the rotor B, their assembly and interconnection procedure is hereafter summarized with particular reference to Figs . 7 and 8.
Firstly, the slider B3 is linked to the compression element B2 upon insertion of the two sides of the pivot 72 into the through holes of the loops 55, 56 of the side walls 51, 52 of the compression element B2.
In this way, the pivot 72 of the slider B3 hinges the loops 55, 56 of the compression element B2. The head portions of the loops 55, 56 are thus housed in the circular port 73, delimited by the pivot 72 and the cylindrical surface 74 of the head of the slider B3.
The assembly proceeds then with the insertion of the rod 70 of the slider B3 into the through hole port 68 of the element Bl, starting from the part of the flat surface 67.
Since the compression element B2 is already linked and hinged to the pivot 72 of the slider B3, it is clear, that through the slider B3, the expansion element Bl and the compression element B2 , besides being hinged to the pivot 72, are also allowed to slide linearly to each other along the rod 70 of the slider B3, and so along the thrusting flat surface plane 67, till they reach their smallest bulk or closed condition, as illustrated in Fig. 7.
Furthermore, since the compression element B2 is forced to rotate on axis YZ , being forced by its cylindrical rings 53, 54 supported within the grooves 22 of the stator covers A2 , A3, the expansion element Bl is forced to rotate on the axis XZ because it is linked to the main shaft 80. The main shaft 80 is supported at the axial hole seats 28 of the stator covers A2, A3. Thus, a reciprocal relative rotating movement of the elements Bl, B2 is allowed by the contemporary or simultaneous translation of the slider B3, that moves its hinged pivot 72 along the axis of the through hole port 68, and the rotation of the element B2 on the pivot 72 of the slider B3.
This constraint among the elements Bl, B2, B3 induces the compression element B2 to rotate on its axis YZ, touching lightly with its outer surface wall 50 concentrically the cylindrical wall of the stator hollow 2, so as to achieve the compression of air or a combustible mixture that may be between them and that is, anyway, unable to escape.
Such compression is assured also by means of the radial contact of tight sealing means placed on the expansion element Bl and on the cylindrical wall of the stator hollow 1.
Furthermore, the rotating movement of the compression element B2 and the consequent displacement of the slider B3 are caused by the rotating movement of the expansion element Bl that is forced to rotate on its axis X , as a consequence of the blast or ignition of the combustible mixture in the combustion chamber 8.
The expansion element Bl, at the beginning of the combustion, presents its minimal thrust flat surface 67 to the expanding combusting mixture, the minimal thrust flat surface being just sufficient to make it move. But with the fast development of the expansion, a force is immediately generated that forces the element Bl to turn in the only possible direction, presenting the gas thrust an increasing thrust surface 67, and, consequently, the expansion volume of the burned gases increases to completely obtain and use the power of the firing process.
As already mentioned, with the rotation of the expansion element Bl and with the constraint of the slider B3 that can only slide inside its guiding through hole 68 and that has to drag the hinged compression element B2, and with the constraints of the rotation axes XZ and YZ, a translation of the slider B3 is achieved, whereby a contemporary rotation and divergation (divarication) between the elements Bl and B2 rotating on their respective own axes XZ and YZ and a consequent series of strokes of expansion and compression of the combustible mixture inside the hollows 1, 2 of the stator A, forming main strokes of the gas engine, are made possible.
The stroke of the largest circumferential divergation or relative circumferential rotation between elements Bl and B2, as illustrated in Fig. 8, determines also the greatest suction volume of air or fresh mixture, to which is also relevant the position of the holes 25 provided on the covers A2, A3 of the stator A and the position of the groove or depression 65 of the hub 63 present on the expansion element Bl.
The rotation of the compression element B2, besides along the cylindrical side of the hollow 2, where it carries out its specific task of compressing the mixture previously taken in, continues of course inside the area of the hollow 1, without touching its cylindrical wall that remains far apart.
In this stroke of rotation, the compression element B2 cooperates with the surface 67 of the element Bl, with the head 71 of the slider B3 and with the side walls of the hollow 1 of the stator A, for forming the expansion volume and for exhausting the burned gases that, by means of the flares 11 and the lateral draft through holes 30, are forced toward the exhaust port 10.
As a matter of fact, according to the proposed embodiment, the port 10 does not directly accomplish the task of exhausting the burned gases, but it houses a rotating conduit 90, that, as illustrated in Fig. 9, has holes 91, 92 in correspondence to the bored flares 11 and through holes 30 of the central block Al of the stator A, and able to be aligned with said flares and holes 11, 30, respectively, but only during the stroke of exhausting the burned gases, while in the other strokes, the conduit 90 is induced to turn so as to present its closed cylindrical surface adjacent to the holes.
The presence of the conduit 90, with its exhaust holes 91, 92, constitutes the exhaust valve of the engine at issue, thanks to which the suction of the exhaust of the engine at issue is avoided.
The arrangement and adjustment of the holes 91, 92 of the conduit 90, in order to present them to the holes 11, 30 of the stator A for the desired exhaust stroke of burned gases , is achieved, for example, by means of a crown gear 93 driven by the main shaft 80, by interposing another crown gear, a belt or a chain, or any other element able to achieve the proper reduced rotation rate, so that the desired exhaust phasing is achieved.
After having thus described the main components of this invention, and after having explained one embodiment of its rotor B and of the arrangement of the rotor B with respect to the stator A, and after having illustrated their respective function, their operation is hereafter described, in particular with reference to Figs. 10 to 18, so as to verify that they comply with the specified objects of the invention.
With reference to Fig. 10, operation starts with the end portion 50' of the compression element B2 being placed near the chamfer 9, so as to facilitate the access of the combustible mixture into the combustion chamber 8 of the stator A; that means that the element B2 has already run along the whole cylindrical portion of the hollow 2 and has already brought the combustible mixture MC within chamber 8 to its greatest degree of compression. According to the invention, when the compression element B2 reaches the edge of the chamfer 9 to the compression chamber 8, the spark plug 7 ignites its ignition spark, that fast but gradually fires the mixture MC, causing its expansion.
It can be noticed that the combustible mixture MC is compressed in the compression chamber 8 and is kept therein, both by the action of the end portion 50' of the cylindrical surface wall 50 of the compression element B2, and by the end of the surface wall 60 of the expansion element Bl, that is placed tight on the side surface of hollow 1, and also by the head 71 of the slider B3 that is interposed sealingly tight between the elements Bl and B2 , and that in that situation, induces the elements Bl, B2 to their largest circumferential divergation, corresponding to that illustrated in Fig. 8.
In the situation of Fig. 10, the suction holes 25 of the stator covers A2, A3 are placed over the depressed groove 65 of the expansion element Bl, allowing the flow of fresh mixture MF from the outside of the engine, and its expansion ME in any free space that the largest circumferential divergation between elements Bl, B2 provides within the hollows 1, 2, and so in any free space between the expansion element Bl and the compression element B2.
The combustion of the mixture MC in the chamber 8, as already mentioned, causes a gradual but fast combustion of all the mixture with the consequent thrust to the expansion element Bl, that is so induced to rotate toward the positions shown in Figs. 11 to 13, allowing the combusting mixture MS to reach its maximum usable thrust volume. With reference to Fig. 11, it is highlighted that after having accomplished a rotation movement of the expansion element Bl equal to few degrees, its depressed groove 65 exits the zone of the suction hole 25, determining the end of stroke of suction of the fresh mixture MF, while the already intaken mixture ME remains free and keeps on expanding inside the free spaces of the hollows 1, 2. The mixture ME is, however, subject to a relative compression under effect of the reduction of the circumferential divergation between the elements Bl, B2, as can be inferred from Figs. 12 to 14.
From Fig. 11, it can also be inferred that the combusting mixture MS pushes on the shoulder surface 67 of the expansion element Bl, causing its usable rotation movement that is transferred to the main shaft 80, and forces also the compression element B2 to rotate through the slider B3 hinged by pivot 72 to element B2.
From Figs. 12 and 13 it can then be inferred that the expanded mixture ME helps in cooling the walls of the hollow 2, and the inner walls of the elements Bl, B2, said expanded mixture ME being gradually compressed corresponding to the increase of the volume of the combusting mixture MS.
In particular, Fig. 13 represents the maximum development of the stroke of expansion or usable thrust stroke of the combusting mixture MS, because, when continuing its rotation, the expansion element Bl meets the draft holes 11, 30 that connect to the hole 10, where the exhaust pipe 90 is open with its holes 91, 92 aligned with the draft holes 11, 30, so as to begin the stroke of exhausting the burned gases, as represented in the following Figs. 14 and 15.
Fig. 14 represents the situation, in which the burned gases are reduced under environmental pressure, just before the hollows 1, 2 are connected because of the approaching of the end of the wall 50 at the chamfer 9.
As a matter of fact, as it can be inferred from the following Fig. 15, as the end of wall 50 goes beyond the edge of the chamfer 9, a direct passage, through the combustion chamber 8, between the wall of the hollow 2 and the wall of the hollow 1 is accomplished, determining thus the scavenging stroke, caused by the passage of the expanded mixture ME, already partially compressed but still fresh, from the hollow 2 toward the combustion chamber 8 and toward the following hollow 1.
The entry of the fresh gas into the expansion area of hollow 1 determines the complete discharge of the residual combustion material via the still open holes 91, 92 of the exhaust pipe 90.
With reference to Figs. 14 and 15, it can be noticed that in these strokes a new stroke of suction of fresh mixture MF begins, because of the fact that the hole or conduit 25 of the stator covers A2, A3 goes again over the depressed groove 65 of the element Bl. Such superposition of the hole 25 over the groove 65 determines the opening thereof and the beginning of the suction stroke that can be adjusted according to their respective shapes and sizes .
The suction of the fresh mixture MF through the holes 25 of the covers A2, A3 is caused by the expansion of the closed space between the elements Bl, B2 of the engine, that switch from the undiverged condition of Fig. 7 to the diverged (open) condition of Fig. 8.
The forming of the suction volume MF occurs without possibility of communication with the hollows 1, 2, as can be seen in Figs. 14 to 17, assuring thus its maximum capacity and rapidity of accomplishment.
In particular, in Fig. 14, it is highlighted how the embodiments of the groove 65, not represented in Fig. 14 but shown in Fig. 6, and the shape of the contiguous portions of the hub portion 63 of the compression element Bl, and the inner portion of the end portion 50 of the element B2 cooperate to determine an initial suction volume practically equal to zero, for the maximum efficiency of the following suction stroke.
As a matter of fact, the hub portion 63 of the element Bl is engaged on the inner wall of end portion 50 of the suction element B2, in order to achieve a sufficient sealing tightness against the mentioned inner wall, to isolate the suction volume MF from the expanded mixture ME. Finally, the potentiality of the suction stroke is determined by the concomitant conformation of the elements Bl, B2, B3 of the rotor B, according to what has been described above and illustrated in Figs. 14 to 17, achieving a sufficient isolation of the initial volume. Proceeding in the rotation of the expansion element Bl, the condition of Fig. 17 occurs, in which the end of the circular segmented arch-shaped wall 60 of the expansion element Bl contacts the wall of the hollow 1, thus closing any passage between the chamber of combustion 8 and that of expansion (hollow 1), while the wall 50 of the element B2 contacts the wall of the hollow 2, determining the complete closing of the volume of mixture under compression MC .
In this condition of Fig. 17, the mixture under compression MC contained in the hollow 2 begins to be compressed inside the chamber 8 by the arch wall 50 of the element B2, and the arch wall 60 of the element Bl, and by the head 71 of the slider B3.
Proceeding with the rotation of the expansion element Bl, under the effect of the acquired energy during the usable thrust stroke of the element Bl, the condition of Fig. 18 occurs, whereby the mixture MC is compressed more and more into the hollow 2 and into the communicating combustion chamber 8, while the strokes of expansion and of suction of the fresh air reach their maximum volumes as an effect of the largest divergation between the elements Bl, B2.
In the stroke of Fig. 18, the different sealing tights between the elements determining the initial suction volume MF open, determining the accomplishment of a single volume with the preexisting expanded mixture ME. This volume ME continues its expansion under the effect of the reciprocal movement between the elements Bl, B2, B3, calling for more fresh mixture MF from the holes 25 of the covers A2 , A3, that are still in communication with the respective grooves 65 of the expansion element Bl, until the condition of Fig. 10 of a new cycle is reached.
Comparing the situation of Fig. 13, regarding the volume of maximum expansion MS, with the situation of Fig. 17, regarding the volume of maximum compression MC, it can be inferred also that the present solution of a rotative engine allows a better exploitation of the expansion thrust according to one of the specified objects.
It is apparent then that the suggested embodiment has a bulk and size that is minimal with respect to the power that it can produce, according to other specified objects. Also, the reciprocal movement of the expansion and compression elements Bl, B2 inside the sealing tights in the hollows 1, 2 supports to improve the suction of the fresh air, besides the scavenging and exhaust stroke, according to other specified objects.
Of course, the embodiment till now described and illustrated is to be understood, as already specified, to be purely exemplary and not limitative.
As a matter of fact, it is possible to feed the engine only with air and inject the combustible gas directly into the combustion chamber, as it is possible to replace the spark plug 7 with proper injectors near the chamfer 9, for a better nebuli- zation of the combustion gas . It is, furthermore, possible to replace the described supporting system (tang 27) for the main shaft 80, placing it onto the outer surface of the head covers A2, A3, increasing consequently the diameter and the solidity of the shaft 80, as it is possible to change and adjust the strokes of the engine, adjusting the position of the different elements of the stator and the rotor.
It is then possible to determine the firmness and size of the volumes of suction, compression and expansion, both by changing the depth of the hollows 1, 2 of the stator A, and by modifying lightly the distance and/or the bending radius of the walls 50, 60 of the rotor B.
It is also possible to provide the different illustrated parts as single blocks or as different components properly and steadily linked to each other, as it is possible that the semi- cylindrical portion of the element Bl is provided in solid with the function of a hand wheel or with a hollow inside.
These and other similar modifications or adjustments are understood as belonging to the scope of protection as defined by the appended claims .

Claims

Claims
An endothermic engine with double-rotation center, comprising a stator (A) having two intersecting circular hollows (1, 2), and a rotor (B), the rotor (B) comprising two approximately semi-cylindrical rotor parts (Bl, B2 ) that are adapted to rotate within the respective hollows (1, 2) and a slider (B3) arranged there-between and linking the two rotor parts (Bl, B2) together, the slider (B3) being adapted to hinge the two rotor parts (Bl, B2 ) such that the rotor parts (Bl, B2 ) are allowed to make a relative movement in circumferential direction between an open and a closed position.
The engine of claim 1, wherein the two rotor parts (Bl, B2) and the slider (B3) form, during a certain stroke of the engine, a suction volume (MF) sealed from any other volumes between the rotor parts (Bl, B2) and the hollows (1, 2).
The engine of claim 2, wherein the suction volume (MF) is increased by the relative movement between the two rotor parts (Bl, B2 ) .
The engine of claim 3, wherein the relative movement for increasing the suction volume (MF) is induced by an ignited combusting gas (MS) that acts only on one (Bl) of the two rotor parts (Bl, B2).
An endothermic engine with double-rotation center, comprising a stator (A) having two intersecting circular hollows (1, 2), and a rotor (B), the rotor (B) comprising two approximately semi-cylindrical rotor parts (Bl, B2 ) that are adapted to rotate within the respective hollows ( 1 , 2 ) and a slider (B3) arranged there-between and linking the two rotor parts (Bl, B2) together, the stator (A) comprising an exhaust port (10), wherein the exhaust port (10) comprises a rotating conduit (90) with at least one opening (91, 92) that is, depending on the rotary position of the conduit (90), exposed to the inside of the stator (A) or closed against the inside of the stator (A) .
An endothermic engine with double rotation center, comprising a kinematic arrangement with a rotor (B) moving within a stator (A), said rotor (B) comprising two approximately semi-cylindrical parts (Bl, B2) hinged to each other by means of a slider (B3) which, by sliding on one of the two parts (Bl, B2) allows their reciprocal divergation and closing in circumferential direction, in order to generate variable volumes inside a pair of hollows (1, 2) of said stator (A), said hollows (1, 2) being cylindrical and are arranged parallel and intersecting each other inside the stator (A), one rotor part (B2) being guided to rotate coaxially within one stator hollow (2) to determine an expansion zone of a combusting mixture (MS) and producing a usable thrust, a second rotor part (Bl) being guided to rotate coaxially within a second hollow ( 1 ) to determine a zone of compression of a combustible mixture (MC) , a combustion chamber (8), into which the combustible mixture is forced, being located between the two hollows (1, 2), and a conduit (90) for the collection of exhaust gases being placed near the end of the hollow (1), opposite the combustion chamber ( 8 ) , wherein the suction of gas is generated by the expansion between the two parts (Bl, B2 ) of the rotor (B) during a divergation stroke thereof.
7. The engine of claim 6, wherein the stator (A) comprises a central body (Al), a head cover (A2) and a rear cover (A3), the central body (Al) being shaped as a double intersecting cylinder (4) with optional outer cooling fins (5), and with an inner smooth surface comprising the two cylindrical and intersecting hollows (1, 2), the cross sections of which being arranged on an axis (Z) that is preferentially horizontal, and on respective orthogonal axes (X, Y) which together determine the respective longitudinal axes (XZ, XY) of the hollows (1, 2).
8. The engine of claims 6 and 7, wherein the combustion chamber (8) is provided on one side (4') of the central stator body (Al) and wherein the chamber (8) is provided with a large swell at its upper portion, while its base is open to a connecting portion of the hollows (1, 2) between the axes (X, Y), and wherein the chamber (8) is provided with a threaded hole ( 6 ) for the application of a plug or an injector (7), and is provided with a proper connection (9) to the hollow ( 2 ) , particularly in the form of a chamfer
(9).
9. The engine of claims 6 and 7, wherein exhaust holes (10, 11, 30) for exhausting the burned gases are provided at a zone (4") of the stator (A) opposite to the combustion chamber side (4') thereof, the exhaust holes (10, 11, 30) being offset by an angle (β) with respect to the axis (X), and the circumferential width thereof corresponding to an angular opening of the rotor parts (Bl, B2).
10. The engine of claim 9, wherein during the burned gases exhaust stroke, the covers (A2, A3) cooperate by means of holes (29, 30) provided therein.
11. The engine of claim 10, wherein the cover holes (29, 30) house a rotating conduit (90) provided with holes (91, 92) so as to allow the collection and expulsion of the exhaust gases, when, during its rotation, said holes (91, 92) go over and communicate with the exhaust holes (11, 30) of the stator (A) , wherein the rotation of the rotating conduit (90) can be made by means of a crown gear (93) or any other control system.
12. The engine of any of claims 7 to 11, wherein the covers (A2, A3) are linked to the central stator body (Al), said covers (A2, A3) being provided on their inner faces (20, 40) with cylindrical grooves (22) coaxial with respect to the axis (YZ), an inner surface (23) of the grooves (22) being provided with a raised portion (24) with a port (25) for the suction of air or a fresh combustible mixture from the outside of the respective covers (A2, A3), said ports (25) and optional draft flares (26) thereof being placed on the same nominal radius as a depression (65) of the rotor expansion part (Bl).
13. The engine of claim 12, wherein on the raised portion (24) of the inner faces (20, 40) of the covers (A2, A3), supports (27) with holes (28) are provided to key or otherwise fix half shafts (80', 80") for the rotor (B), said supports (27) being placed on the axis (XZ) that is aligned with the hollow (1) of the stator (A).
14. The engine of claim 6, wherein the rotor (B) comprises a rotating expansion part (Bl) provided with a radial hole (68) that houses and guides a rod (70) of the slider (B3) of the rotor (B), which slider (B3) is hinged to the compression part (B2) of the rotor (B), said parts (Bl, B2) and said slider (B3) being shaped and sized to be contained in the hollows (1, 2) of the stator (A) and being adapted to diverge or close in accordance to the different strokes of the ther odynamic cycle.
15. The engine of claim 12, wherein the rotating compression part (B2) comprises an arch surface wall (50), two side walls (51, 52), to which a pair of rings (53, 54) is linked, said rings (53, 54) being shaped so as to be housed in the grooves (22) of the covers (A2, A3), guiding consequently the rotation of the part (B2) on the axis (YZ) in contact with the wall of the hollow (2).
16. The engine of claim 15, wherein the side walls (51, 52) comprise seats (55, 56) for housing a hinging pivot (72) of the slider.
17. The engine of any of claims 6 to 16, wherein the expansion rotating part (Bl) of the rotor (B) is provided with a semi-cylindrical surface wall (60), with side walls (61) and side depressions (62), a hub (63), and further side depressions (65), said latter side depressions (65) being provided along a reduced arch of the hub (63) with a mean radius corresponding to the distance between the axis (XZ) and the center of a suction hole (25) of the covers (A2, A3) .
18. The engine of claim 17, wherein the expansion rotating part (Bl) comprises a radial hole (68) having a coplanar side with a thrust stroke wall (67) thereof, and comprises a hub (63) with a port (64) so as to allow the rotation of the part (Bl) with its wall (60) engaging the surface of the hollow (1) of the stator (A).
19. The engine of claim 16, wherein the slider (B3) between the expansion rotating part and the compression rotating part is applied slidingly into a port hole (68) of the expansion part (Bl), so as to allow a pivot (72) of the slider (B3) to be housed in seats (55, 56) of the compression part (B2), so that the compression part (B2) can widely open with respect to the expansion part (Bl) in circumferential direction, guided by the slider (B3) so as to allow a rotation of the compression part (B2) on the axis (YZ), constrained by the rings (53, 54) guided by the grooves (22) of the covers (A2, A3), while the rotation of the part (Bl) remains constrained to the axis (XZ) as an effect of the housing of the half shafts (80', 80") led and passed through the holes (28) of the covers (A2, A3).
20. The engine of claim 19, wherein the pivot (72) hinging the compression part (B2) to the expansion part (Bl) is provided on the end of a head (71) of the slider (B3), that is coplanar to a surface used for the sliding of the slider (B3), while the pivot (72) is placed near the side opposite the head (71), without projecting from the sliding surface.
21. The engine of claim 19, wherein the slider (B3) has a head (71) with a port (73) coaxial to the pivot (72), a cylindrical surface (74) of the port (73) as well as its head surface and opposite surfaces (50') of the compression part (B2), and further any other necessary part of contact between the parts (Bl, B2) and the slider (B3), and of these elements with the hollows (1, 2) of the stator (A) being properly provided with sealing tight strips .
22. The engine of claim 17, wherein the hub (63) of the expansion part (Bl) engages an inner surface of the wall (50) of the compression part (B2) during their relative movement, to cause the sealing tightness during the initial stroke of suction of the fresh mixture.
EP03790932.2A 2002-08-28 2003-08-28 Endothermic rotary engine with two parallel rotation axes Expired - Lifetime EP1540139B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ITBL20020014 ITBL20020014A1 (en) 2002-08-28 2002-08-28 ENDOTHERMAL ROTARY MOTOR WITH DOUBLE ROTATION CENTER
ITBL20020014 2002-08-28
PCT/EP2003/009549 WO2004020791A1 (en) 2002-08-28 2003-08-28 Endothermic rotary engine with two parallel rotation axes

Publications (2)

Publication Number Publication Date
EP1540139A1 true EP1540139A1 (en) 2005-06-15
EP1540139B1 EP1540139B1 (en) 2013-12-11

Family

ID=31972174

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03790932.2A Expired - Lifetime EP1540139B1 (en) 2002-08-28 2003-08-28 Endothermic rotary engine with two parallel rotation axes

Country Status (6)

Country Link
EP (1) EP1540139B1 (en)
AU (1) AU2003266318A1 (en)
ES (1) ES2450165T3 (en)
IT (1) ITBL20020014A1 (en)
PT (1) PT1540139E (en)
WO (1) WO2004020791A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9874098B2 (en) 2012-11-30 2018-01-23 Libralato Ltd. Ignition engine of the rotary type with a double rotation center
IT201600123578A1 (en) * 2016-12-06 2018-06-06 Ruggero Libralato Steam engine, with stator and piston with double rotation center

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005027017A1 (en) * 2005-06-07 2006-12-14 Hydrotech Holding Ag Apparatus and method for compressing and / or displacing a fluid, in particular rotary piston reciprocating compressor
ITBL20080014A1 (en) * 2008-09-19 2010-03-19 Libralato Ruggero THERMO-DYNAMIC CYCLE OF COMBUSTION ENGINE, IN PARTICULAR OF THE ROTARY TYPE WITH DOUBLE ROTATION CENTER AND MOTOR SO AS IT IS MADE
ITBL20100003A1 (en) * 2010-02-03 2011-08-04 Ruggero Libralato STRUCTURE OF PERFECTED ROTARY ENDOTHERMAL ENGINE OF THE DOUBLE-CENTER TYPE OF ROTATION
IT202100006404A1 (en) 2021-03-17 2022-09-17 Litm Libralato Innovation Thermal Machines S R L IMPROVED STEAM ENGINE, WITH DOUBLE CENTER OF ROTATION PISTON
IT202100007868A1 (en) 2021-03-30 2022-09-30 Litm Libralato Innovation Thermal Machines S R L IMPROVED STEAM ENGINE WITH DOUBLE CENTER OF ROTATION PISTON

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR964897A (en) * 1950-08-26
US3324839A (en) * 1965-10-08 1967-06-13 John R Erwin Rolling piston engine
DE2338962A1 (en) * 1973-08-01 1975-02-13 Walter Kral Manual or power driven rotary piston pump - has tooth shaped piston and an eccentrically mounted rotary piston valve
IT1250184B (en) * 1991-06-04 1995-04-03 Rotary endothermic engine with two centres of rotation

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2004020791A1 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9874098B2 (en) 2012-11-30 2018-01-23 Libralato Ltd. Ignition engine of the rotary type with a double rotation center
IT201600123578A1 (en) * 2016-12-06 2018-06-06 Ruggero Libralato Steam engine, with stator and piston with double rotation center
WO2018104878A1 (en) * 2016-12-06 2018-06-14 Ruggero Libralato Steam motor with stator and piston with double center rotation

Also Published As

Publication number Publication date
WO2004020791A1 (en) 2004-03-11
ITBL20020014A1 (en) 2004-02-29
ES2450165T3 (en) 2014-03-24
PT1540139E (en) 2014-02-25
AU2003266318A1 (en) 2004-03-19
EP1540139B1 (en) 2013-12-11

Similar Documents

Publication Publication Date Title
US10196970B2 (en) Isochoric heat addition engines and methods
US5433179A (en) Rotary engine with variable compression ratio
AU2003210463B2 (en) Internal combustion engine
JP2004529285A (en) Rotary machine and heat cycle
US5415141A (en) Rotary engine with radially sliding vanes
WO2011130285A2 (en) Internal combustion engine and components therefor
JPH09144551A (en) Four-cycle rotary engine
AU2018101638B4 (en) Internal combustion engine with paired, parallel, offset pistons
EP1540139B1 (en) Endothermic rotary engine with two parallel rotation axes
EP1125041A1 (en) Toroidal internal combustion engine
CN110439677A (en) A kind of rotary engine
JP2010513792A (en) Rotary engine with cylinders of different shapes and volumes
US4546743A (en) Arrangements to rotary valves for engines compressors, motors or pumps
US20030131808A1 (en) Pivoting piston rotary power device
CA2435723C (en) Rotary combustion engine
CA2179206C (en) Rotary engine
CN115045753B (en) Vane rotor engine
WO2010031585A1 (en) Method for providing a thermo-dynamic cycle of a combustion engine, in particular of a rotary type with a double center of rotation
US3818886A (en) Rotary internal combustion engine
US4471729A (en) Valve arrangement preferred for engines
US20030131723A1 (en) Pivoting piston rotary power device
CN101000016A (en) Rotating piston engine with compressing working independent chamber
CN112065575B (en) Cavity-changing type rotor engine
WO2001042634A9 (en) Z-engine
CN201013447Y (en) Double-shaft compression-ignition separate cylinder type rotary-piston explosive motor

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20050329

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20070627

19U Interruption of proceedings before grant

Effective date: 20120712

19W Proceedings resumed before grant after interruption of proceedings

Effective date: 20130301

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20130718

RIC1 Information provided on ipc code assigned before grant

Ipc: F01C 21/18 20060101ALI20130716BHEP

Ipc: F01C 19/00 20060101ALI20130716BHEP

Ipc: F01C 21/08 20060101ALI20130716BHEP

Ipc: F01C 1/44 20060101AFI20130716BHEP

Ipc: F01C 21/10 20060101ALI20130716BHEP

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: LIBRALATO LTD.

RIN1 Information on inventor provided before grant (corrected)

Inventor name: RUGGERO, LIBRALATO

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 60345434

Country of ref document: DE

Owner name: LIBRALATO LTD. PENSION PLAN, GB

Free format text: FORMER OWNER: LIBRALATO, RUGGERO, BELLUNO, IT

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 644730

Country of ref document: AT

Kind code of ref document: T

Effective date: 20140115

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 60345434

Country of ref document: DE

Effective date: 20140206

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: STOLMAR AND PARTNER, CH

REG Reference to a national code

Ref country code: PT

Ref legal event code: SC4A

Free format text: AVAILABILITY OF NATIONAL TRANSLATION

Effective date: 20140219

REG Reference to a national code

Ref country code: RO

Ref legal event code: EPE

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2450165

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20140324

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20131211

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

Free format text: REGISTERED BETWEEN 20140320 AND 20140326

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

REG Reference to a national code

Ref country code: SK

Ref legal event code: T3

Ref document number: E 16008

Country of ref document: SK

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCAR

Free format text: NEW ADDRESS: SEEFELDSTRASSE 69, 8008 ZUERICH (CH)

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 60345434

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

26N No opposition filed

Effective date: 20140912

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 60345434

Country of ref document: DE

Effective date: 20140912

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E021460

Country of ref document: HU

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140828

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 60345434

Country of ref document: DE

Representative=s name: STOLMAR & PARTNER PATENTANWAELTE PARTG MBB, DE

Ref country code: DE

Ref legal event code: R081

Ref document number: 60345434

Country of ref document: DE

Owner name: LIBRALATO LTD. PENSION PLAN, GB

Free format text: FORMER OWNER: LIBRALATO LTD., MANCHESTER, GB

REG Reference to a national code

Ref country code: PT

Ref legal event code: PC4A

Owner name: LIBRALATO LTD. PENSION PLAN, GB

Effective date: 20150902

REG Reference to a national code

Ref country code: CH

Ref legal event code: PFA

Owner name: LIBRALATO LTD., GB

Free format text: FORMER OWNER: LIBRALATO LTD., GB

REG Reference to a national code

Ref country code: CH

Ref legal event code: PUE

Owner name: LIBRALATO LTD. PENSION PLAN, GB

Free format text: FORMER OWNER: LIBRALATO LTD., GB

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: STOLMAR AND PARTNER INTELLECTUAL PROPERTY S.A., CH

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140312

REG Reference to a national code

Ref country code: ES

Ref legal event code: PC2A

Owner name: LIBRALATO LTD. PENSION PLAN

Effective date: 20160705

REG Reference to a national code

Ref country code: HU

Ref legal event code: FH1C

Free format text: FORMER REPRESENTATIVE(S): ERDELY PETER - DANUBIA SZABADALMI ES JOGI IRODA KFT., HU

Representative=s name: DANUBIA SZABADALMI ES JOGI IRODA KFT., HU

Ref country code: HU

Ref legal event code: GB9C

Owner name: LIBRALATO LTD. PENSION PLAN, GB

Free format text: FORMER OWNER(S): LIBRALATO LTD., GB

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 14

REG Reference to a national code

Ref country code: SK

Ref legal event code: PC4A

Ref document number: E 16008

Country of ref document: SK

Owner name: LIBRALATO LTD. PENSION PLAN, MANCHESTER, GB

Free format text: FORMER OWNER: LIBRALATO LTD., MANCHESTER, GB

Effective date: 20160331

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 15

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCAR

Free format text: NEW ADDRESS: RUE DU CENDRIER 15 CP 1489, 1201 GENEVE (CH)

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IE

Payment date: 20170726

Year of fee payment: 16

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: E. BLUM AND CO. AG PATENT- UND MARKENANWAELTE , CH

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CZ

Payment date: 20190225

Year of fee payment: 16

Ref country code: GB

Payment date: 20190219

Year of fee payment: 16

Ref country code: ES

Payment date: 20190219

Year of fee payment: 16

Ref country code: DE

Payment date: 20190221

Year of fee payment: 16

Ref country code: RO

Payment date: 20190225

Year of fee payment: 16

Ref country code: IT

Payment date: 20190221

Year of fee payment: 16

Ref country code: CH

Payment date: 20190227

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20190220

Year of fee payment: 16

Ref country code: SE

Payment date: 20190227

Year of fee payment: 16

Ref country code: HU

Payment date: 20190220

Year of fee payment: 16

Ref country code: AT

Payment date: 20190221

Year of fee payment: 16

Ref country code: FR

Payment date: 20190221

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SK

Payment date: 20190225

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PT

Payment date: 20190220

Year of fee payment: 16

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 60345434

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 644730

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190828

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20190828

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200228

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190829

Ref country code: RO

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828

Ref country code: HU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190829

REG Reference to a national code

Ref country code: SK

Ref legal event code: MM4A

Ref document number: E 16008

Country of ref document: SK

Effective date: 20190828

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190831

Ref country code: SK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180828

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190831

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200303

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20210107

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190829

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190828