EP1295012A1

EP1295012A1 - Poly-induction energy turbine without back draught

Info

Publication number: EP1295012A1
Application number: EP01940611A
Authority: EP
Inventors: Normand Beaudoin
Original assignee: Nivesh SA
Current assignee: Nivesh SA
Priority date: 2000-05-23
Filing date: 2001-05-22
Publication date: 2003-03-26
Anticipated expiration: 2021-05-22
Also published as: WO2001090536A9; CA2310488A1; ATE382775T1; WO2001090536A1; EP1295012B1; AU2001274132A1; DE60132202D1

Abstract

The invention concerns a method for generating internal combustion turbines with safe and reliable support parts, having maximum floating-type segmentation capacity. Further, the invention concerns a method for producing counter-turbines designed to be used as compressor, depressor or auxiliary turbines. Finally the invention concerns a method for producing said internal combustion turbines, in solid, expansive or reductive, or truncated form, and finally either with multiple support or supported in one single point.

Description

POLY TURBINE ENERGETIC AND ANTI-BACKFLOW

In the applicant's previous inventions, that is to say semi-transmittive induction motor which is the subject of Canadian patent application no. 2,045,777-5 filed on June 26, 1991 for “Energy machine with semi-transmittive induction” on the one hand, poly induction motor object of Canadian patent application No. 2,302,870 filed on March 15, 2000 for "Poly induction energy motor" and of international patent application PCT / FR 01/00753 filed on March 14, 2001 under priority of the previous second part, and energy motor with traction rods object of Canadian patent application No. 2,310,487 filed May 23, 2000, for "Energy motor traction" third part, it has been shown how to induce non-rectilinear movement of the driving parts of an engine so that they are other than pistons. In these first cases, such as that shown in FIG. I, which is a reproduction of FIG. XXII of the invention having the title "Poly induction energy motor", each end of the blade always touches the opposite parts of the cylinder. . On the other hand, as in Figure III of the applicant's invention entitled "Traction energy motor", it has been shown that the pistons can be cut off, thus allowing the connecting rods to become blades.

The aim of the present invention is to produce, as a continuation of these inventions, internal combustion turbines, entirely supported by internal mechanics and consequently receptive to lubrication and, secondly, capable of accepting efficient segmentation, therefore at precise points. , blades.

More specifically, in the present invention, the applicant intends to show the possibility of designing an engine the rotary core of which will consist not of a single blade, but rather of a flexible set of blades which can move semi-rotationally in a cylinder in ensuring the highest seal, and this in at the same time that it will be fully supported by a reliable and well lubricated mechanism.

The present technical solution therefore stems from the desire of the applicant to dynamically and mechanically configure the subsequent deformations of a set of blades connected together so as to form a flexible turbine core. The basic embodiment will, for the present invention, an embodiment in which all of the blades will be joined in the manner of a quadrilateral. Indeed, if we study the movement of the traction rods of the applicant's invention entitled "Traction energy engine", we can notice that they pass successively from the diamond shape to the square shape, to then move to the complementary diamond shape FIG. III.

By now designing this quadrilateral, no longer as a set of traction rods, but rather as a set of blades forming a turbine core rotating at the same time as it undergoes these transformations, we will realize that we can arrange this set in a cylinder whose shape is of ovoid type, and so that at all times the four points of attachment of the sides of the blade assembly touch the sides of the cylinder. Figure III shows how, in an ovoid cylinder, a progressive deformation of the quadrilateral occurs in its square to diamond phases, then again from diamond to square, successively and alternately.

But, even if this system already has sealing qualities, since segments can be arranged in specific places located at the points of attachment of the blades, it still remains quite random since the progression of the deformation between the square and the rhombus, simply supported here by the cylinder whose surface serves both as a support, is infinitely variable. In addition, this pressing on the cylinder will quickly wear out the parts of the turbine core and the segments. Indeed, even if this dynamic is in a good direction, it must be admitted that the variability of such an engine, assuming segmentation at each point of attachment of the blades, and moreover in an unlubricated and highly gasified environment, leaves much to be desired.

As in the depositor's previous inventions, he intends to propose here a simple method for supporting the parts, this time from the inside, so as to ensure a blade support mechanism that is safe and easily lubricated and segmentation without excessive support or friction, therefore of the floating type. Note that although there are semi-supported ways to support these parts, the applicant aims by the present invention, the most complete supports possible for the parts.

In order to produce adequate mechanical support for the parts, it is necessary to study with a magnifying glass the behavior of one of the points of the parts constituting the blade assembly. Several can be chosen. The depositor prefers to start the analysis by choosing a point situated at the ends of the blades, that is to say at the points of attachment of the blades between them. Thus, we see that, in an ideal situation, the point chosen travels a trajectory whose shape is compared to that of an oval, similar to that of the cylinder.

The support mechanism of the present invention must therefore be capable of producing this type of figure at the ends of the parts constituting the core of the turbine.

The first mechanical support for the parts suggested is as follows: we will suppose, in the body of the turbine, a crankshaft rotatably mounted and provided with two crankpieces arranged in opposite directions. To each of these crankpins will be rotatably connected a gear which will be called the connecting gear of the connecting rod. This gear will be provided with a crankpin and will itself be nested with a gear of the internal gear type, rigidly disposed in the side of the motor. In that case, this internal gear must be twice the size of the induction gear. Each crankpin of the induction gear will be, for example by using a connecting rod, connected to an opposite attachment point of the blades between them. Therefore, if we follow the trajectory of the attachment points during the rotation of the crankshaft, we will realize that at the same time that it undergoes the elongations induced by the crankshaft, it undergoes the rotations induced by the gear of induction to which it is linked, and that the combined result of these two movements corresponds to the desired ovoid shape.

Therefore, indeed, the assembly will describe during the rotation of the crankshaft, very exactly through the proposed cylinder shape, the alternating square / rhombus predescribed, and this it is important to emphasize, in a perfectly sustained and autonomous manner, which means completely independent of the cylinder. Indeed, at their lateral end, the connecting rods will find themselves at the same time in their most prominent state, which will stretch the diamond over its width. Then, when the connecting rods are found halfway between their extension and their maximum retention, the shape of the turbine core will be squared. Lately, when the connecting rods are at their lateral center of travel point, that is to say at their innermost point, the reverse diamond will form.

As we have seen, during the square position, the induction rods will be halfway between their output and their maximum input. This angulated position is therefore very favorable to the torque, since it occurs at the same time as the square shape of the core of the turbine, and when consequently the external combustion chambers are narrowed to their maximum.

In fact, the parts will describe the movement sought, and this, even in the absence of the cylinder. This is what will ensure the fluidity of the engine and the absence of friction or knocking usually caused by parts both in friction and in rapid change of direction. By replacing this set again in a suitable cylinder, the segments can then be arranged, being arranged in a floating manner, at precise points, that is to say simply sliding on the cylinder with a slight pressure which can come from small springs, without possibility of wear premature. The use of a mechanical support forces the choice of ideal shape of the cylinder compared to any other random shape.

This dynamic succession of forms may give rise to the four stroke of the engine or to the two stroke construction of the engine, or to a continuous ignition of the internal turbine type. Of course, several sets can be used simultaneously.

Lately, these types of engines can receive a type of anti-backflow gas burning, defining the times as they have been described in the aforementioned invention of the applicant having as title "Backflow energy motor", that is that is to say by producing the admission by effect of the suction of the burnt gases into the combustion chamber of the burnt gases. One hundred percent clean turbine will then be produced.

Let us now note how this arrangement has an advantage, in terms of torque, over rotary motors and over other blade motors.

In rotary or other blade motors, the force during the explosion is equal in torque and anti-torque, since there is in the first moments of the explosion as much pressure on each side of the piston . The torque therefore does not really start until after the parts have been dismantled. In the present case, even the force on the back of the blade is used and has a positive torque. The torque is therefore viable not only over half the surface of the blade, but over its entire surface, which doubles the torque of the engine. There is therefore no back pressure, like that found in single blade motors. But there is more: we can indeed note on the anterior side of the blade itself, a leverage effect. The adjustment of the engine explosion moment can therefore accept quite a bit in advance. As already pointed out, the connecting rods are at this moment in an angular position.

A second way of producing a mechanical support for this turbine consists this time of using external support gears. This is indeed assumed this time, an external type gear, rigidly connected to an axis, which axis is in turn rigidly connected to the body of the motor. Next, two external gears are assumed, which will be called induction gears, each connected to one end of a rotary sleeve, the center of which is rotatably mounted around the support axis of the main support gear. The two induction gears will be nested on the one hand with the support gear, and on the other hand provided with crank pins, each of them being subsequently connected to the opposite point of attachment of the quadrilateral of blades forming the core of the quasi-turbine.

As before, if we follow the trajectory described by a point located on the crankpin of the induction gears during the rotation of a full revolution of the support sleeve of the support gears, we can verify that it travels very exactly the desired oval, namely the ideal shape that the cylinder must have so that the progressive deformations of the nucleus in successive squares and diamonds are perfectly synchronized. As before, the cylinder has no effect on the movement of the parts, and this, so much so that the quadrilateral of the turbine will produce exactly the same successive shapes with or without cylinder.

Therefore, by replacing everything in the cylinder, we can segment the blades in a floating and safe manner, and without risk of wear, second effect sought by the depositor. As before, note the angular position of the induction crankpins during the square shape of the core and therefore during the explosion, which ensures a reinforced torque and without knocking. It should be noted, in addition to this way of doing things, that we can as it will be shown below, arrange the crankpins of the induction gears outside their circumferences, which will make it possible to create a cylinder, well still ovoid in shape, but this time deformed, bulging, approaching that of an eight and therefore capable of delaying the explosion and benefiting from a much improved torque.

A third way, for this shape of cylinder, to produce a mechanics of adequate support of the parts, is to suppose a crankshaft provided with four crucibles in the shape of arc, capable of receiving semi-rotationally parts, which one will call supports of blades. These blade supports will then be nested, each with a crankshaft crucible. We can provide each blade support with a gear, each gear being by its two sides, connected to the neighbor. This procedure aims to ensure that the four blade supports will act in synchronism. Each of these supports will be provided with a sliding means, capable of receiving a blade.

Yet another way of implementing the system is to provide each point of attachment of the blades with a push rod, this rod being in turn inserted in a sliding manner in a second mobile unit, and this, so that it is, at its second end, supported on an ovoid type cam. In this way, always at least two pushers will ensure the location of the components of the FIG turbine. XI.

The applicant continues below his demonstration in the direction of improving the shape of the blades forming the quadrilateral of the turbine core. We can indeed see that it is possible to modify the interior design of the blades in order to take advantage of it internally.

It will be assumed that each blade constituting the core of the turbine is drawn in the manner of an isosceles triangle, and that all of these isosceles triangles, while continuing to describe the outside square / rhombus / square movement described above, is mounted internally around a square axis, the length of the sides of which is equivalent to the length of the equal sides of the isosceles triangles. It must also be assumed that this central square axis has its sides directed in the same direction as that of the outer square of the turbine core when it is in this phase, and that its rotation speed thereafter is equivalent to the half that of the core FIG. XIV.

Consequently, by following the course of the internal movement of the turbine in its main moments, we will be able to note that when the core of the turbine is in square phase, the internal points of the isosceles triangles of each blade are at equal distance the from each other, and that these internal points touch the center of each side of the square axis disposed in the center of the engine.

Then, after an eighth of a turn of the pieces, half of the adjacent sides of the triangles will join while the other half will follow the shape of the internal square.

All internal rooms will therefore be closed. With this type of drawing, we therefore see that we can introduce internally, an additional turbine, a turbo pump, or even a suction pump, thus producing a backdraft motor. It should also be noted that this first centrifugal turbine, here opening the door to the idea of poly turbine.

Another configuration resulting from the first could be called quasi turbine elision. We can, after having more specifically defined the way of obtaining the movement of the parts, keep for example for the quasi-square cylinder turbine only a number of four blades instead of eight, these blades being supported - since this does not change the gear ratio in any way - as if it were was an eight-sided core.

Likewise, a different way of supporting the blades can be used, that is to say supporting them both by their center and one of their ends, rather than by each of their ends.

Thus, in the present case, we can assume a center piece having four points of attachment to the center of each blade. Then, a point of attachment at the end of each blade, connected to one of the two systems previously stated, namely either at the end of a connecting rod oscillating around a crank pin while being driven by a gear interlocked with an internal gear, or is connected to the crankpin of an induction gear mounted on a sleeve and nested with an external gear. In order to avoid having to use a second set, the part can be supported by a slide nested in the central support part. This slide must be irregular, so as to absorb the differences in size of the core, if the cylinder is regular.

Whether it is one or the other of the ways described above, the cylinder will no longer participate in securing and stabilizing the parts, and floating segments may be used.

In the following figure, we show that the turbine is not strictly designed with a core on four sides. We can indeed assume a turbine core for example of six, or eight sides. These nuclei of six, or eight sides will normally evolve in triangloid cylinders, that is to say quasi triangular, rounded, or squareoid, that is to say quasi square, rounded. In the case of a quasi-square cylinder for example, a similar deformation of the octagon will occur, deforming and reforming it successively.

In the same way as previously, the blades can be supported mechanically, but this time it will be necessary to provide four deformations / reformations per revolution, these being moreover, smaller. By using a gear ratio of the induction gears relative to the support gears, whether internal or external, we will get the exact movement of the blades we need.

So far, we have studied what we could call expansive turbines, in the sense that the deformation of the turbine core forces an expansion of the shape of the cylinder, from the round to the oval, from the octagon to the semi square.

The next realizations will show how we can produce impressive turbines, that is to say where it will be the core which will have to absorb the lack of space caused by the displacement of the parts.

The present embodiment assumes that the blades, for example here four in number, are not this time connected together directly, but rather by the detour of small connecting rods which we will call connecting rods (FIG XVIII). Then, these connecting rods will each be connected to an induction rod. In turn, these induction rods will be connected as before to the crankpin of an induction gear mounted on a rotary sleeve and nested with a support gear. If the four induction rods are so connected and the induction gears are in a ratio of one in four of the support gear, in this case there will be, in each case of the engine, four pulls and successive and alternative thrusts on the attachment points of the induction rods, and of the connecting rods. These push-ups and push-ups will bring together and to successively distance the points of attachment between them, and consequently, the successive sizes of the squares which form the core. We will therefore go from a full square to an overlapping square, smaller, and therefore capable of occupying an angular position relative to the surface of the cylinder.

Another embodiment capable of producing an impressive turbine type turbine can be obtained by supposing rounded push rods, terminated by a pad, actuated by a cam to activate the sides of the turbine core. So that the cam can not only take out the sides, but also make them enter, we can imagine for each side a small rocker, attached to both the rod and a point of attachment. The rod and the rocker each undergoing all the effect of the cam, the blade will obey these suction. Yet another way is to use an octagonal support structure, mounted on a square cam, the parts will therefore always act in return for the others.

It will be noted that, as previously, it is possible to draw the parts of the center of this type of turbine, so as to produce a poly turbine.

So far, we have shown how to produce turbines and turbines with almost the shape of the cylinder was regular, for example in perfect ovo ^'lde in almost perfect square, almost triangular, and moreover, obtues. Of course, these shapes are generative and can be multiplied, for example for octagonal blades, twelve, sixteen sides, and so on.

The previous embodiments have also, on the whole, shown how to produce these turbines by using the limit points of the blades as points of attachment to the mechanics of the turbine. Subsequent embodiments of the present turbine will show how one can rather use the quadrilateral, blades previously described, as a support quadrilateral articulated around a cam, to which blades will be attached, this time by their center and not by their end.

This original configuration, in addition to creating (FIG XXI) piston blades made up of double parts, will also allow, internally, to produce an additional internal internal turbine, which, as before, can act as compressor, sucker or still poly turbine.

In this case, the external compression of the blades is obtained by the play of two complementary blades at the same time. As before, we can draw this type of turbine like a poly turbine. You can also, taking into account the curvature of the cylinder, draw the parts so that each end always touches the surface of the cylinder. Therefore, it will be necessary to compensate inside the blade structure, by the appropriate rounding, if one wishes to keep the internal compressions.

As for the mechanical support of these types of turbines, it is similar to the previous ones. It will also be noted that while the previous turbines resulted in ovoid, triangloid or quasi-square cylinder shapes, the present ones result in rectangular shapes.

Note, in this same perspective of supporting the parts, if as before we generalize, that we can end up with different tenfold forms of the present embodiment. To name just one, a poly support with six sides connected centrally to blades, but always with gears whose resultant is ovaloid, can give a blade with six sides in an almost rectangular cylinder.

Another embodiment of the invention consists in producing a quasi piston turbine. Based on these considerations, we can show that we can use the support structure as poly cam, engaging it for example around an oval cam. The advantage of this way of doing things, is to no longer cause a round trip of the piston per revolution, but two or more. Here, only two pistons are attached to show the use of the cam.

Another embodiment of the invention, when the blades are supported by. the center, consists in connecting them to the central support piece by a set of crossed connecting rods, which makes it possible to produce a domed cylinder shape, where one can take advantage, by delaying the explosion, of a multiplied torque in strength and angle.

Lately, we may decide to mechanize the poly turbines rather by an internal attachment point. In this case, the poly turbine can be mechanized by attaching the internal points of the triangles, describing - as opposed to the oval of the ends - a square, for example equivalent to the rotating inner square. To do this, we will use an induction gear provided with a crank pin, and nested with an internal gear four times its size. The resulting figure, with regard to the crankpin, will be the square sought, will then have to be placed in time to follow the movement of this shape in real time. The same procedure can be applied to figures of different numbers, by adjusting the gear ratio.

Brief description of the figures

Figure I is a reproduction of Figure XXII of the applicant's invention entitled "Poly-induction energy engine". It can be seen there that the induction of a single blade is obtained in a completely mechanical manner, and that consequently the blade, here, a triangular boomrang motor, can therefore be provided with floating segments. Figure II is a reproduction of Figure III of the applicant's invention entitled "Traction energy engine". In this figure, we can see four traction rods which, devoid of their pistons, and mechanically secured, will serve as the basis for the developments of the present series of internal combustion turbines.

Figure III is a schematic cross section showing the two main times of a first embodiment of an energy turbine. Here, unlike Figure I, the turbine core is formed by a set of blades, for which it will be necessary to design both the cylinder and the appropriate mechanics. The dotted lines show the displacement and the progressive deformations of the turbine core, since the cylinder of this first embodiment is the oval.

It can be seen that the core of the turbine, during its rotation, passes successively and alternately from square to diamond. The small chambers, in thin hatching, will be the combustion chambers and will expand in wide hatching, during the expansion of the gases, and so on for admission, compression and exhaust.

Figure IV shows a first poly inductive way of ensuring the movement of the turbine core. Two connecting rods connect two opposite attachment points of the blades to the crankpins of the induction gears, these induction gears, both mounted on a crankshaft crankpin and engaged with an internal support gear. This set ensures the perfect movement of the parts.

Figure V is a cross section of the mechanics shown in Figure IV.

Figure VI is a three-dimensional view of the previous figure, where the exhaust gas intake ducts have been added, for example. Figure VII shows a second mechanical way of carrying out the invention, this time from an external support gear.

Figure VIII shows the sequence of motor phases.

Figure IX shows how to make the motor curved, obtuse.

Figure X is a three-dimensional view of the previous ones.

Figure XI shows a third way of supporting the parts inside, but this time with the use of a cam. Indeed, in this case, it will be necessary to connect each point of attachment of the blades to a push rod, slidably engaged in a central support piece, so that the other end is in contact with the cam of oval shape. Note that you can also only use two rods, using a four-part cam belt structure.

Figure XII is an embodiment similar to the previous one, but where, using a cam sheath, more than two push rods are used.

Figure XIII is a view of a different mechanism, and also on five sides. Around a central axis rotatably mounted and provided with five internal arcs capable of receiving the blade supports, are semi-rotatably mounted five blade supports accepting the circular portion of the movement. The four blades are, in addition to being attached, slidably mounted on the supports. A set of cohesive gears is added, in order to secure everything.

Figure XIV shows how to use the interior space of the first embodiment, like a poly turbine, or booster pump. Figure XV shows how to make a quasi-turbine, this time comprising a core of eight sides, and inserted in a quasi-square cylinder.

Figure XVI shows, as opposed to the previous ones, how to make an impressive turbine. In this type of turbine, the core parts do not expand, but rather inward. This is why it will be said that this turbine is impressive, instead of being expansive.

Figure XVII shows the location of the main two-stroke parts of the impressive turbine, and its support mechanics.

Figure XVIII shows how to use rods and rocker arms as a support mechanism.

Figure XIX shows, this time, a set of poly blades supported at a cross, which ensures backward movement or advance of the parts relative to each other. This way of supporting the blades makes it possible to obtain a domed cylinder structure, more conducive to the torque of the engine.

Figure XX shows the geometric expression of the previous one.

Figure XXI shows how, using a quadrilateral like the one already used as the turbine core, but this time taking it as a support structure, we can support a set of semi-squares forming the core. Here, the external compression is ensured by the cohesion of two squares. As before, the interior points can be drawn so as to create a poly turbine.

Figure XXII represents a poly turbine preferably connected by the center points. In this case, these points are connected to a crankpin mounted on a gear. of induction embedded in an internal gear four times its size. The result will be the square sought. This form will then be mechanized so as to occur over time.

Detailed description of the figures

Figure I is a reproduction of Figure XXII of the applicant's invention entitled "Poly induction energy engine". In this type of triangular boomerang engine, we can see that an internal mechanism has been developed allowing, among all the possible random forms of an engine, to choose the ideal shape capable of accepting a mechanical support, and from there, to obtain a floating type segmentation which, implanted at precise points, keeps the compression of the motor tight at its maximum.

Figure II is a reproduction of Figure III of the applicant's invention entitled "Traction energy engine". In this invention, by a set of traction rods 1, connected together so as to form a quadrilateral connecting the piston to the crankshaft 3, the applicant has shown how the deformations of this quadrilateral produce the thrust in a tenfold manner on the crankshaft . In the present invention, advantage will be taken more particularly of the design aspect produced by these connecting rods, namely of the series of diamonds, squares / diamonds, in order to then transform their function in an original manner. Indeed, we will show how these alternative deformations and reformations will be included in a dynamic which will make the whole obey in the manner of a quasi rotation.

Figure III is a schematic view of the aforementioned alternative deformations of the quadrilateral assembly subjected to a semi rotation. Here, a set of blades 4, connected together at each of their ends to form a flexible quadrilateral, will be inserted into the cylinder 5 of an engine, this cylinder being of ovoid shape. In the continuation of the two sequences which are presented, it can be seen that the sequence of displacements and deformations of the assembly occurs inside the cylinder and will result in a fluid, progressive and alternating passage of the square / diamond shapes. All of the parts are however, in this figure, supported by the cylinder which causes knocking, friction and wear.

To solve these problems, it is necessary, as done previously for motors with rotary and triangular blades, to find the specific mechanical arrangement which will ensure the reliable internal support, oiled and fluid, of the parts, thus allowing the segments to be arranged in a way floating.

FIG. IV represents another method making it possible to mechanize the rotation of this assembly so that the series of figures is produced, so that the succession of square / diamond figures occurs, while retaining the shape of the cylinder. In the present figure, the core assembly is left in dotted lines, for the sake of clarity of this mechanism. On the crank pins 6 of a crankshaft 7 rotatably mounted 8 in the body of the machine, two gears have been rotated, which will be called induction gears 11. Thanks to a crankpin, these gears will be connected, by the connecting rods d induction at opposite attachment points of the blades. The second end of these connecting rods will be connected to two of the opposite attachment points 10, blades forming the core. These induction gears will also be each coupled to an internal type gear, in the present case, twice as large, rigidly disposed in the sides of the engine block, and which will be called support gear 12.

Each of these systems is built on one side of the turbine core and attached to the opposite attachment point. For more synchronism, we can join two crankshafts by gears nested on a common axis. By following the drawing that will produce, from this mechanics, the crankpins and the rods of induction, one will realize that they describe a quasi rhombus, which is the figure that the opposite attachment points of the blades must travel through when they follow the cylinder. The two complementary attachment points will also describe the same form.

In summary, the dynamics of this assembly is as follows: during the rotation of the crankshaft, the induction gears, mounted on the crankpins and nested with internal support gears, will be subjected to a rotary 100 and anti-rotary action. The result will be that their ends will produce an almost oval movement. However, as these ends are connected by the connecting rods, at the corresponding specific points of the blades, they will force this same movement, which is the desired movement, since in duplicate, while allowing to follow exactly the shape of the cylinder, they will force the reproduction of the square / diamond sequence. It is not necessary to provide the mechanism with four crankpins, since the two complementary attachment points will make the same route, by complementarity. Having thus secured the entire system, we can rotate the parts in the same way, even without the cylinder. This is the reason why it can be said that the core set can be segmented with segmentation at specific locations, and this, in a floating manner.

Figure V shows a cross section of the mechanics previously exposed. We find the crankshaft 7, its crank pins 10, the induction gears 11, the support gear 12, the induction rods 9, the cylinder 5, the blades 4. For clarity, this movement is shown at from the rotation of the crankshaft, as if the engine was in compression. A push on the blades would, of course, produce the same set of movements.

FIG. VI is a three-dimensional view of the previous embodiment, to which the standard locations for carburetion 25, exhaust 26, ignition 27, as well as the floating segments 28 have been added, for example. Figure VII shows a second mechanical way of supporting the core assembly. The elements relating to the body of the engine 1, the cylinder 5, and the core of the turbine, being the same, we will focus on the mechanical support part. In the present case, there is a rigid arrangement of an external type of gear - which will be called support gear 12 - on an axis 30, an axis itself rigidly connected to the body of the motor. Then, there is rotatably around this axis, a means for supporting the induction gears, said means being provided with two opposite sleeves to which the induction gears 11 are rotatably connected. These sleeves will be called induction sleeves 31. Each induction gear is imbricated with the support gear, and is provided with a means such as a crankpin 32, in turn connected to two opposite attachment points of the blades. Of course, the induction gears are nested with the support gear so that the crankpins are in opposite positions, that is to say simultaneously in their most distant times, or close together.

The dynamics of this arrangement are as follows: when the support of the induction gears is rotated about its axis 101, the induction gears which it supports and which are driven by the support gear to which they are nested . Consequently, the crank pins with which they are provided, will undergo both the effect of their own rotations and that of the rotation of the gear support. The result of this poly movement will be oval. So therefore, if these crankpins are each connected to one of the opposite attachment points of the blades constituting the core, then these points will describe the exact design of the cylinder and the core assembly will perform alternative square / diamond deformations, which have already been commented on. Of course, as before, we mean a correct quadrilateral of the gears, normally one in two, and a correct position of the crankpins in relation to the circumferences of the induction gears, which will result in ideal shapes, curved or flattened, ovals. Figure VIII dynamically shows the succession of the location of the parts in the main phases of engine rotation. It can be seen, in view (a), that when the crankpins of the induction gears are at their most laterally protruding points 102, they induce the formation of the rhombus. In view (b) the crank pins of the induction gears being half retracted 103, this results in the square shape of the turbine core, and finally, in view (c) this results in an opposite diamond, since the crank pins of the induction gears are at their innermost points 104. If we now observe the dynamics of the movement of the parts, we will see that as before, the two attachment points will be trained to follow the oval of the cylinder.

Figure IX schematically shows how, by placing the crankpins 6 of the induction gears outside their circumferences, we obtain a set of parts rotating in an ovaloid shape but approaching that of an eight 39. This arrangement is very interesting since it makes it possible to keep the smallness of the combustion chambers 40 longer and this, until the moment when the thrust 41 and the torque will be greatly improved.

Figure X shows a three-dimensional view of the previous ones, where intake 25, spark plug 27, exhaust pipe 26 has been added.

Figure XI shows how a cam structure can be used to move the parts. Here, each point of attachment of the blades 10 of the turbine core is additionally connected to a push rod 41, itself slidably engaged in a slide of a central rotating part 42, so as to ensure its movement. These push rods are supported at the second of their ends, to a cam 43 of oval shape. Pushing on two of the opposite rods 44 causes traction on the blades which, in a contrary and complementary manner slide 45 towards the cam, and so on, alternately. Here, FIG. XI shows schematically the two main times of such a type of arrangement, namely firstly when all the pushers are also depressed, and secondly when they are in opposite positions.

Figure XII shows the use of a cam sheath making it possible to use only two push rods. Here, the cam 43 is surrounded by four parts connected together and forming a cam sheath 46. Only two attachment points 200 are connected to the induction rods 47. It should be noted that this structure could be used for other inventions of the filing, as for example his inventions relating to piston turbines in order to produce them with fixed rods.

Figure XIII shows another additional way of ensuring the movement of the turbine blades. Here, the parts have been drawn taking into account the two movements that constitute the deformation of the square to the rhombus, namely a rotational movement and an elongation movement. With this figure, we realize a five-sided blade structure.

Each set of parts therefore produces its share of movement and the sum of these movements gives the desired movement. Assuming in fact a crankshaft rotatably disposed in the body of an engine 7, this crankshaft can be provided with four crucibles in the form of a half-arc 48, capable of receiving parts rotatably. In these arcs will be rotatably arranged supporting pieces 49 of the blades which, on one of their sides will be formed in an arc - and consequently capable of producing the rotary part of the movement - and on the other side provided with a slide 50 with which each blade will be slidably coupled.

Various gears can be added so as to additionally ensure the cohesion of the parts, in particular four cohesion gears nested with one another. Figure XIV shows how the geometry of the present turbine can be made profitable to its maximum by drawing each blade constituting the core of the turbine so that, in addition, the center of the turbine is efficient.

Indeed, we can see, through the two drawings showing the positions of the turbine core how, if we draw each blade in the manner of an isosceles triangle having these two sides with a length equal to that of each side 52 of a semi-square cam, rotatably inserted in the center of the engine, there will alternately be an expansiveness of the parts, then a total folding of the parts on themselves. At first, in fact, the points of the triangles 53 will be found in the center of each side of the square, and this at the same time as the sides will be at their most distant phase. The chambers produced, hatched 54, will therefore be at their maximum opening. During the next time, in pairs, the sides of the triangles forming the blades will join to each other 55, while the complementary sides will join to the square 56, which will completely close the rooms.

The internal use of these chambers can therefore be made in several ways, such as for example as an auxiliary gas pump effect, or as an exhaust pump as in the case of backdraft motors, or even as an extra. An original way to use them would be to make them participate in the flow of gas from the turbine, for example reversing the direction of the gas outlet, maximized for example by the center, thus producing a poly turbine. We can push even further by making the gas flows travel between the external turbine and the internal turbine in order to cause a continuous ignition, because there will necessarily be a compressive field between these two turbines of different forces. Lately, it should be noted to the extent that we are ready to accept a certain friction on the cylinder due to the very resistant current materials such as for example ceramics, that the system can function without the support mechanisms already mentioned, by using and of the cylinder and the rotary cam, as support points for the triangular blades of the turbine core.

FIG. XV shows how the above ideas can be applied to turbines with more than four sides 203. For example here, the core of the turbine 60 has eight sides and evolves in a cylinder whose shape is almost square. Eight times per turn, it is deformed and reformed. The same mechanics can be applied to support the parts, taking account of course of the technicality of the drawing, for example here, the core passes eight times per revolution from the octagon to the deformed octagon. The sequence of two of these moments is shown here. It will be understood that it is therefore necessary to adapt the relationship between the induction and support gears. More specifically, the induction gears will have to be built in a ratio of one in eight, to make eight reciprocating movements per revolution, to the parts. In the same way as above, this turbine can be constructed in the form of a poly turbine. It should also be noted that turbines with six, twelve, sixteen sides are possible, and so on. However, the larger the number of sides, the lower the expansiveness and compression of the parts, which limits the efficiency of the engine.

Figure XVI is an impressive type turbine. It is so named because necessarily, the rotation of a squareoid, or almost square, piece in an almost square space requires, as shown for the oval, the alternative expansion of this space.

However, the turbine can be designed in the opposite way, that is to say by acting on the core, by reducing it and enlarging it alternately. This is a first way to rotate a squareoid piece, that is to say of an almost square shape, in a space also squareoid.

Figure XVI therefore shows two successive times of an impressive type turbine. Indeed, in the first step (view (a)), the quadrilateral formed by the core is full 204 and fills practically the entire space of the quasi-quadrilateral delimiting the space of the cylinder, each side of which, in hatched form, is compressed to its maximum 61.

In the second time, (view (b)), the ends of the blades acted in overlapping 62 and thus it was the core of the turbine itself which accepted the expansion of the combustion chambers, rather than the shape of the cylinder. We therefore see the expansion of the hatched rooms, compared to view (a)).

Figure XVII shows how to support this type of movement mechanically.

The main idea of this type of support is to connect all the blades together indirectly by using two connecting rods 63 by attachment point. These connecting rods will themselves be connected together at a point of attachment to induction rods 47, themselves attached for example to crankshafts. Consequently, a pushing or a pulling of this point of attachment will result in a crossing or a uncrossing of the blades, and consequently in an expansion or in a reduction in the size of the core, which is the desired effect.

The thrust and traction on the attachment points of the connecting rods can be obtained by various mechanical means similar to those already exposed. Gears provided with a crankpin and rotating around a support gear can be installed on the turbine core and therefore be calibrated, in this case, to rotate four times per revolution. As with the previous turbines, the poly turbine effect can be obtained from this type of turbine. It should also be noted, as before, that this type of turbine can be designed with eight, sixteen sides and so on, or with an odd number of sides.

Figure XVIII shows how to build this type of turbine, with the help of a cam. In the present figure since the four sides of the core act not alternately but rather simultaneously, it will be seen that not only does the cam push the blades outwards, but also brings them back, the objective of the present invention still being to support parts mainly internally. The preferred way here, and to use, to bring the blades, a rocker push rod, thus reversing the thrust of the cam in traction of the blade. If the end of each push rod of the blade 41 is in fact connected to a rocker arm 69 here at the fork end, and this rocker arm is itself semi-rotary connected to an anchoring point 70 located on the body of the core, it will be seen that the cam 43 pushing alternately on the connecting rod itself and on the rocker arm, will provide the back and forth necessary for the reductive and magnifying formation of the cylinder core.

Figure XIX is a representation of a turbine not of expansive or impressive type, but rather adventitious, in that it is from advance and delay in the management of the dynamics of the forms, that we succeed in propose a curved turbine. Indeed, the way to produce such a turbine is to attach each blade 73 of the turbine in a way that is both split and inverted 74 to a central hub 75 rotatably mounted in the engine 1.

In the present case, a central hub 75 is arranged in the cylinder 5 of the body of an engine. On each side of this hub are arranged two attachment points 76, to which are connected connecting rods 77 which, crossed between them, are then connected to two attachment points by blade 73. This arrangement is very interesting since it allows, by delaying the opportune moment of the explosion, to obtain a truly rotary thrust in a better angle of attack and with a canceling effect on the blades since they unfold and fold excessively. In addition, the expansiveness of the chambers is increased even for an elegant turbine.

As shown above: on the one hand a turbine in four moving in a space in four is, for all practical purposes an electrified turbine, on the other hand, the crankpin of the induction gears can be placed outside the circumferences of these gears if we want to get the obese way of form.

On the basis of these two considerations, it will be much easier to specify the supporting mechanics of this arrangement which otherwise might prove difficult to resolve.

But taking into account these data, we can suggest that by using as if it were an octagonal nucleus with an obese cylinder, induction gears eight times smaller than the support and more, by placing the crank pins outside the center, we can then connect the crank pins by an induction rod to one of the two attachment points of each blade. These attachment points will thus be attracted and pushed back in ideal proportions, and the already described support structure of each blade will do the job.

Figure XX shows the geometry that achieves the exaggerated effect of folding the blade. Indeed, we can see that when obeying two centers, the blade must obey two arcs. The two folds, either from the rear or from the front, are exaggerated, which makes it possible to benefit from a delay and a good explosion angle.

This figure shows the position of the two blades in two different moments 206, 207. It is clear that since the support is from two points, the position of the blade is always in conjunction with these two arcs 208, and that the only blade where it is symmetrical is in the center.

Similarly, we can, as in the mechanical already exposed, use the additional expansions and compressions of the parts in order to create a counter turbine or even a poly turbine. As before, this type of turbine can be used with three, four or other number of sides, so as to preserve the main necessities of an engine, gas expansion relationships, drag, compression.

Figure XXI is a type of turbine where the support of the parts making up the core of the turbine was rather produced by the center of each blade. In the present case, the face on each side of the turbine core will consist of two faces of joint blades 80. The segments will be arranged at the outer corner of each turbine part 81. A set of connecting rods 82 will connect the four parts of the core. It will be through these points of attachment that the engine will be mechanized by one of the mechanics that the depositor has commented on.

In the present case, four semi-squares are thus added to form the core of the turbine. Taking into account the ovaloid appearance of the cylinder of the turbine, the squares will be imperfect since two of their sides will be rather in arc, thus weakening one of the points of its external perimeter, so that it does not exceed the shape of the cylinder. We will call segmentation tip 81, this meeting point on both sides in an arc, since it will be on it that the segments will be arranged. It will therefore be noted that the side of the core will consist of two sides of the blade.

This figure shows first of all the two limiting moments of the turbine here commented on in figure XXI. During its passage from the semi-square shape to the semi-diamond shape, two of the points will slide towards the center and the other two outwards 83. This figure therefore also shows, how the internal surface of the square can also be used as a backup turbine, or as an injection or suction pump, or as a poly turbine.

Figure XXII shows how the first type of turbine can also be mechanized from the center. Indeed, as opposed to the external points which produce an ovaloid type design, the points draw a square. The tips must indeed follow the squareoid surface. We must first attach the tips of the blades to the crankpins of the induction gears 230. As before, these induction gears 11 are nested with an internal support gear 12 four times their size. The crankpins will be statically run through the desired square shape. We now need to mechanize this dynamic of the square, because it takes place over time, that is to say that the pieces that shape the square are themselves over time. This involves putting the internal gear into action and accelerating the crankshaft accordingly. Thus, if the depositor was on a pivoting plate, he would see a square. It is therefore necessary to add to the crankshaft a gear 210, indirectly coupled to the assembly of the internal gear 211 which has become rotary, by means of a pinion gear by doubling the speed 212. This configuration, simple and sparing with space, with a large oiling capacity and a propensity for poly turbine, sums up well the position of depositor in terms of motorology. In addition, this version has a strong sealing capacity on the sides. Additional gears should also be placed to activate the square part, rotating twice as slowly as the tips. Several means are possible. For example, a small pivot gear 213, transmitting the action of the induction gear to a drive gear of the square piece 214, could be used if one wants to keep the mechanics all on the same side.

Claims

• CLAIMS -

1. A machine, such as an engine, a pump, a compressor, comprising in composition:

• a block of the machine in which a cylinder of the machine is rigidly inserted, of ovaloid shape,

• four blades connected to each other at their ends by the points of attachment, so that the assembly forms a quadrilateral, this assembly itself being arranged semi-rotationally in the engine cylinder.

2. A machine, such as an engine, a pump, a compressor, comprising in composition:

• four blades connected to each other at their ends by the attachment points, so that the assembly forms a quadrilateral, this assembly itself being arranged semi-rotationally in the engine cylinder,

Two induction rods connected to two of the opposite attachment points of the set of blades forming the core, and at their second ends rotatably mounted to the opposite crank pins of a crankshaft, and rigidly provided with induction gears,

• induction gears rigidly connected to the induction rod and coupled to the support gear, • a support gear rigidly disposed in the engine block, a crankshaft rotatably mounted in the machine block and whose crank pins are connected to the induction rods.

3. A machine, such as an engine, a pump, a compressor, comprising in composition:

Two induction rods connected to two of the opposite attachment points of the set of blades forming the core, and at their second ends mounted rotatably to the crankpins of induction gears,

Induction gears rotatably mounted on a support of induction gears and coupled to a support gear of the external type, and provided with crank pins connected directly or indirectly to the opposite attachment points of the blades,

• an external type support gear, rigidly mounted to the motor body, indirectly by a support pin,

A support pin rigidly mounted in the body of the motor, on which the support gear is rigidly fixed, and around which a rotary sleeve is rotatably disposed at the ends of which the induction gears are rotatably mounted, • a support gear rigidly disposed in the engine block, a crankshaft rotatably mounted in the machine block, the crank pins of which are connected to the induction rods.

4. A machine according to claim 2, in which the crankpins of induction gears are not the circumferences of these gears.

5. A machine, such as an engine, a pump, a compressor, comprising in composition:

• a body of the machine, in which a cylinder is arranged,

• four blades forming the core of the turbine, and connected together by their ends at attachment points,

• four push rods inserted in a sliding manner in the hub of the turbine, one of their ends being connected to the point of attachment of the blades, and the opposite end of which is in abutment against a central block,

• a central cam arranged transversely in the center of the machine.

6. A machine according to claims 1, 2 and 3, the shape of each blade is triangular and the center of the turbine core is of almost square shape, this machine using the center, as against turbine, turbo compressor, pump backflow prevention, poly turbine, additional turbine.

7. A machine according to claims 1, 2, 3 and 5, comprising in combination several systems and comprising a different number of sides and the relationships of the gears of which have been calibrated. A machine, such as an engine, a pump, a compressor, comprising in composition:

• a machine block in which a cylinder is rigidly inserted,

• a cylinder in which the core of the turbine is arranged semi-rotationally,

A set of blades forming the core, connected indirectly to each other by means of connecting rods,

Two connecting rods each having one of their ends connected to the blade and their opposite end connected to the rod of the consecutive blade as well as to its induction rod,

Induction rods, one of their ends of which is connected to the connecting point of the rods to each other and the second of which is connected to the crankpin of an induction gear,

Induction gears provided with a crank pin coupled to the induction rod and rotatably mounted on a support axis so as to be coupled to the support gear,

A support gear rigidly and indirectly mounted in the block by means of a support pin,

A support axis on which an induction gear support is rotatably mounted, this support axis being able to be used to convey the power to the outside of the engine,

• a set of blades connected to each other at their ends and slidably engaged on blade support parts,

• blade support parts arranged semi-rotationally on the crankshaft and provided with a sliding structure capable of receiving the blades, • a crankshaft rotatably mounted in the body of the engine, fitted with crucibles capable of accepting the blade supports semi-rotationally.

9. An engine according to claim 8, comprising in composition several pre-described assemblies.

10. An engine according to claims 8 and 9, the central parts of which are arranged so as to create a backup compressor or an anti-backflow pump or a secondary turbine, or else a poly turbine.

1 1. An engine according to claims 2, 3 and 8, the number of blades of which is in elision with respect to the ideal number and the core of the turbine of which comprises a central part completing the system and ensuring the impermeability of the turbine.

12. A machine, such as an engine, a pump, a compressor, comprising in composition:

• a body of. the machine in which is placed the cylinder in the center of which is fixedly disposed a cam,

A set of blades indirectly connected to each other towards their center by means of a set of connecting rods,

• connecting rods each connected at their end to a blade, to a push rod,

• a set of push rods, each of them being connected to the connecting point of the connecting rods together and slidingly inserted in the hub of the engine and each having their second end both supported on a cam and provided with a rocker arm,

• a set of rocker arms, each one connected to the end of the push rod, and semi-rotary to the body of the engine, and provided with an elongated part allowing the cam to draw the attractive effect from it on the push rod.

13. An engine according to claim 12, but whose mechanical effect is rather obtained by a sheath of connecting rods rotatably mounted around a cam and connected to the attachment points of the blades.

14. A machine, such as an engine, a pump, a compressor, comprising in composition:

• a body of the machine in which a cylinder is arranged,

• a rotary support for the blades rotatably mounted in the block and provided for each blade with two attachment points,

A set of blades each having two separate attachment points connected by means of support rods to the rotary support,

• two support rods per blades, which, crisscrossed between them, connect the blades to the rotary support.

15. An engine according to claim 14, comprising in composition several systems and designed internally so as to produce a poly turbine.

16. An engine according to claim 14, mechanically supported by a semi-transmittive support.

7. A machine according to claim 14, one of the attachment points of each blade is connected to a support mechanism by means of an induction rod, itself connected to a crankpin of the induction gear.