EP1295012A1 - Poly turbine energetique et anti refoulement - Google Patents
Poly turbine energetique et anti refoulementInfo
- Publication number
- EP1295012A1 EP1295012A1 EP01940611A EP01940611A EP1295012A1 EP 1295012 A1 EP1295012 A1 EP 1295012A1 EP 01940611 A EP01940611 A EP 01940611A EP 01940611 A EP01940611 A EP 01940611A EP 1295012 A1 EP1295012 A1 EP 1295012A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blades
- support
- induction
- turbine
- machine
- 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
Links
Classifications
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- 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
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- 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
- F01C1/22—Rotary-piston machines or engines of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
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- 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
- F01C5/00—Rotary-piston machines or engines with the working-chamber walls at least partly resiliently deformable
- F01C5/02—Rotary-piston machines or engines with the working-chamber walls at least partly resiliently deformable the resiliently-deformable wall being part of the inner member, e.g. of a rotary piston
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
Definitions
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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 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.
- a second way of producing a mechanical support for this turbine consists this time of using external support gears.
- an external type gear rigidly connected to an axis, which axis is in turn rigidly connected to the body of the motor.
- 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.
- 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.
- Each of these supports will be provided with a sliding means, capable of receiving a blade.
- 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.
- the cylinder will no longer participate in securing and stabilizing the parts, and floating segments may be used.
- the blades can be supported mechanically, but this time it will be necessary to provide four deformations / reformations per revolution, these being moreover, smaller.
- 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.
- 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.
- 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.
- the external compression of the blades is obtained by the play of two complementary blades at the same time.
- 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.
- 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.
- 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.
- the same procedure can be applied to figures of different numbers, by adjusting the gear ratio.
- 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.
- 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.
- the core of the turbine 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.
- 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.
- 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.
- the external compression is ensured by the cohesion of two squares.
- 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.
- Figure I is a reproduction of Figure XXII of the applicant's invention entitled "Poly induction energy engine”.
- 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”.
- 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 .
- 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.
- 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.
- 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.
- 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.
- the core assembly is left in dotted lines, for the sake of clarity of this mechanism.
- induction gears 11 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.
- 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.
- 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.
- 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.
- a means for supporting the induction gears said means being provided with two opposite sleeves to which the induction gears 11 are rotatably connected.
- 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.
- a means such as a crankpin 32
- 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.
- 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.
- 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.
- 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.
- FIG. XI shows how a cam structure can be used to move the parts.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- FIG. 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.
- FIG. XV shows how the above ideas can be applied to turbines with more than four sides 203.
- 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.
- 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.
- 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.
- Figure XVII shows how to support this type of movement mechanically.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- the expansiveness of the chambers is increased even for an elegant turbine.
- 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.
- 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.
- 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.
- FIG. XXI 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.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Hydraulic Turbines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA002310488A CA2310488A1 (fr) | 2000-05-23 | 2000-05-23 | Polyturbine energetique et antirefoulement |
CA2310488 | 2000-05-23 | ||
PCT/FR2001/001570 WO2001090536A1 (fr) | 2000-05-23 | 2001-05-22 | Poly turbine energetique et anti refoulement |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1295012A1 true EP1295012A1 (fr) | 2003-03-26 |
EP1295012B1 EP1295012B1 (fr) | 2008-01-02 |
Family
ID=4166361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01940611A Expired - Lifetime EP1295012B1 (fr) | 2000-05-23 | 2001-05-22 | Poly turbine energetique et anti refoulement |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP1295012B1 (fr) |
AT (1) | ATE382775T1 (fr) |
AU (1) | AU2001274132A1 (fr) |
CA (1) | CA2310488A1 (fr) |
DE (1) | DE60132202D1 (fr) |
WO (1) | WO2001090536A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8951028B2 (en) | 2008-11-12 | 2015-02-10 | Vincent Genissieux | Rotary machine of the deformable rhombus type comprising an improved transmission mechanism |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6899075B2 (en) * | 2002-03-22 | 2005-05-31 | Roxan Saint-Hilaire | Quasiturbine (Qurbine) rotor with central annular support and ventilation |
EP1507956A1 (fr) * | 2002-05-17 | 2005-02-23 | Normand Beaudoin | Machines motrices retro mecaniques, post mecaniques, bi mecaniques |
FR2936272B1 (fr) | 2008-09-22 | 2012-07-13 | Vincent Genissieux | Machine rotative a losange deformable multifonctions |
FR2950926B1 (fr) | 2009-10-05 | 2011-12-02 | Pk Enr | Moteur a pistons rotatifs |
US9926927B2 (en) | 2011-10-14 | 2018-03-27 | Gullivert Technologies Inc. | Belt and support for a rotor mechanism in a rotary apparatus and rotary apparatus comprising same |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1551115A1 (de) * | 1966-09-29 | 1970-06-11 | Alfred Jordan | Rotationskolben-Verbrennungsmotor insbesondere luftgekuehlter Rotationskolbenmotor fuer das Gas-Luftgemisch oder luftgekuehlter Rotationskolben-Dieselmotor |
ES416371A1 (es) * | 1973-06-27 | 1976-05-16 | Martin Artajo | Maquina de embolos giratorios articulados. |
GB1521960A (en) * | 1975-10-01 | 1978-08-23 | Wilson G | Rotary piston machine |
CA2045777A1 (fr) | 1991-06-26 | 1992-12-27 | Normand Beaudoin | Machine energetique a induction semi-transmittive |
JPH11506518A (ja) * | 1995-06-06 | 1999-06-08 | ピー デー ティー エンジニアリング テクノロジー リミテッド | 回転容積形流体機械 |
FR2738285A1 (fr) * | 1995-08-30 | 1997-03-07 | Paris Laurent Guy | Moteur rotatif thermique a rotor unique, portant quatre pistons oscillants actionnes par bielles et vilebrequin |
CA2302870A1 (fr) | 2000-03-15 | 2001-09-15 | Normand Beaudoin | Moteur energetique a poly induction |
CA2310487A1 (fr) | 2000-05-23 | 2001-11-23 | Normand Beaudoin | Moteur energetique a traction |
-
2000
- 2000-05-23 CA CA002310488A patent/CA2310488A1/fr not_active Abandoned
-
2001
- 2001-05-22 AT AT01940611T patent/ATE382775T1/de not_active IP Right Cessation
- 2001-05-22 WO PCT/FR2001/001570 patent/WO2001090536A1/fr active IP Right Grant
- 2001-05-22 DE DE60132202T patent/DE60132202D1/de not_active Expired - Lifetime
- 2001-05-22 AU AU2001274132A patent/AU2001274132A1/en not_active Abandoned
- 2001-05-22 EP EP01940611A patent/EP1295012B1/fr not_active Expired - Lifetime
Non-Patent Citations (1)
Title |
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See references of WO0190536A1 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8951028B2 (en) | 2008-11-12 | 2015-02-10 | Vincent Genissieux | Rotary machine of the deformable rhombus type comprising an improved transmission mechanism |
Also Published As
Publication number | Publication date |
---|---|
CA2310488A1 (fr) | 2001-11-23 |
EP1295012B1 (fr) | 2008-01-02 |
AU2001274132A1 (en) | 2001-12-03 |
ATE382775T1 (de) | 2008-01-15 |
WO2001090536A1 (fr) | 2001-11-29 |
DE60132202D1 (de) | 2008-02-14 |
WO2001090536A9 (fr) | 2002-07-18 |
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