CA2593551A1 - Rotating and turbine drive machines (last work) - Google Patents

Abstract

The object of the present invention is to complete our work on rotary and turbine engines by showing, the mechanical links between each of them, and for each, which are the conditions of maximum power and minimum friction, and how to generalize these conditions, and this by completing the range of inductions relating to standard rotary machines, and by showing how and why and how to use peripheral inductions for turbines.

Description

Disclosure: first party Reminder of the definitions The present invention ob ~ and generalize the concepts of addition geometric, Induction gear with peripheral supFort gear, and angulation of the inductions, presented in our previous passages, first of all in with other examples, then making an appropriate commentary the applying to turbines. Inversemernt, we will show how realize in standard diunamics of the tests carried out in the turbines, especially in the poly induction with a coin or gear poly intermediates induction.

For a better understanding we remind you of the following (Fig.l) Induction set of gears, -s resulting in the planetary retrorotation of a element Support gear: all 1 -s inductions have a support gear, and in the simple inductions, or in the compound induction i iduction, these gears are fixed to the body of the maacine. In the case of semi mechanics tranmission, the armament is reduced to the axis this support of the gear of inverion of the Senzi transnùssion. In composite inductio i, a second support gear may be on the one hand-securely attached to the crankpin's crankpin, or On the other hand mounted planetary on a crankshaft mmchon.

Induction gear: this and grinding is generally, the induction first degree, rigidly fixed to the pistachine, or to the blade of the machine. In the inductions compound, it is connected rigidly or is itself simultaneously the gear of support of the sevonde induction. In turbinating machines, the gears of cylinder are also applied cylindrical indiction gears.

Intermediate gears, oi to hoop, these gears bind, in certain inductions the support gears and the inductions gears Crown gears: These are generally internal type gears.
binder several intermediate gears of the same size or size different Polycammed gears, or accelerated decelerative heats: engrnages of which the forms do are not circular, but rather akin to basic geometric shapes, triangles, squares, ellipses.

The post rotary inductions, mono induction. : Generally, it's about the link direct from a pali gear; of type internal to a support gear of type external. These induction drives - usually post machine fomers presses.

Retrorotative Induction Induction Induction: Usually this is the bond directly from an internal gear type gear to an induction gear Of type external. These methods of suppo -t blades cause, when they are used alone, forms of so-called retro-rotating machines, The induction by poly inductic n: these inductions compressnet several gears Induction mounted on a vile wequin master and coupled to the same gear of support.
These induction gears are provided with crank pins on which the blade is willing.
When the extra gears of these machines are of the external type the mechanical realize post rotary machining processes. When the gear support of these machines is of internal type ,. c -s mechanical réakisent forms den type machines retro rotary.

Leins inductions by force behind and by previous force, or so called springboard, or scissors, are distinguished according qi ie the work of the blade is carried out so préoménente on the front or on the back of the blade, the opposite part entering into mechanical blockage Mono insuction and poly nduction are, in the case of post machines rotary posterior force inductions, while the other inductions, are of the type earlier.
L: Gears lined with intermediate support gears and / or induction made in duplicate.

The semi transmission is center-to-center.
accélérativice, inversive, or accelero inverses, Inheritable Peri Support Gears: These are support gears rigidment attached to the vilebrwequin of a master induction and induce induction secondaitre Planetary ophthalmic support gears. these are usually gears mounted planetary on the crankshaft and a member being connected, and acting as gear of supp ~ or: to a peripheral induction.

We have indeed shown in our previous work that we could add up inductions in such a way that the induction gear of one of them is fixed rigidly to the gear of su) port of the other induction, this producing a gearing of support itself planet. We have also shown that by inductions leading to standard intermittent induction gears, or to type gears planetary inductivity increased the size of the gears will. This allowed to magnify the engrena; e induction of blade, and change the angles attacking this one. As a result, the hinge po nt of the blade was located more back, this which canceled the forging generally found in this type of machine and allowed a much more positive and profitable thermodynal stewardship.

The first feature of the present invention is to show that the notion addition Geometric can be applied to induction gear gears.

In the present invention, the pinion geared luction will be realized in inserting in the gearbox is a gear type gear.It will be realized by the a doubled of intermediate gears, rE united by a rotary means and will couple the blade gear itself: geared to the second gear of the double gears intermediate gears. (Fig.2) Improvement of the induction of induction induction by peripheral induction In the original poly induction, it is known that rear induction, producing being descent a niecanic blockage behind which the blade, comnie in the rotary motors to induction inductive mono, had a negative effect ,. This blockage could be mitigated by the geometric addition achieved by extending the rods relative to the crankshafts Subsidiaries, including the induction gears, and the feed gear have were shrunken.
(Fig3a) This improvement was also improved by subtracting partially or all teeth on certain parts of the support (or induction) during the period blocking, thus leaving the blade only on the crankshafts before. (Fig.3 b In the present invention, we are inspired by the mechanics we have already produced, with the rotatably mounted intermediate gears, in dynamic translational turbinator, sw crank pinions fixed rigidly in the side of the machine, to apply them ~: n dynamic to standard rotary machines, or to turbinating machines, don: the blade is pale sitrictly Translational.

Indeed, here we see that the) n can improve the last method in surajoutant, around the gears of induction a gear crown, which will link by therefore those from outside. We can say that this crown can be realized by the means of a internal internment but also my chain. (Fig 3. c) As a consequence we realize that induction can be improve, a again, producing an intermediaore geared over geonically. the first E: intermediate gear will be mounted on three gears intermediaries, they themselves mounted planetary on a gear of support.
The intermediate internal gear and its double will therefore be trained rotationally forward The second internal gear will result in therefore the gears of the crankshafts. This way will recall that already used of turbinative manner and here genera on the rotary poly induction maehines.
These contributions are important because they allow, once again, to prove that the poly induction can be achieved without back furrows on the blade, and that when these methods are used in urban dynaamics, translatioonnel or not, these against efforts are also canceled. Indeed, the in eret of these is to cancel totally the counter effect back of the mechanicals because the induction gears of these are not directly , but rather by geographical addition in angulation, in relation to the gears of support In consequence, as will be shown later, and as we have already of aiU.eurs mentioned, the design of the piston surface may be modified to way to better realize the thermodynamic conditions of this type of machine. .
Second aspect of advance of poly induction derived from machines turbibatices.
In turbinating machines, i the translational type, we showed that we could, starting from external type gears mounted on axes rigidly mounted in the side of the machine, cause the induction gear of the cylinder, cylinder, by their coupling to the internal gears of the cylinder to gears reversal intermediaries themselves coupled with the gears of the vuilebrequins subsidiary rotatively driven on c-axis fixed in the body of the machine. (Fig 3.
d) We can show here that this method4 can be dynamiqyue, and that in this case, the gear of the cylinder deviuea 1 the support gear of the machine, and the gears of support become the intermediary engri .nage, this time fixed on the crankshaft ma.itre and coupled to engrenaj; es of inductions also arranged rotatively on the machons of old, brequin masters of the machine and supporting the blade by their crank pins.
In the same way as previously, this arrangement ennhiles the cons efforts back of the machines because the pi -ints of mani.tons forces are never , as well as gears that support them, have the same place as the coupling points of the gears dynamic and fixed gears. (Fig 3.2) We will see further on overworked he will be of aportance theimo c ynamic capital that the gears of support, in dynamic, and the gears this cylinder in turbibatives, are preferably internal type gears. On the contrary, we only use this reappropriation dynamics of mechanical turnery also allows to reiterate the possibility to realise peripheral active gear gears induction, this gear of support being here realized in the form of the c) uronne.

Improvements to qexible weapons In our previous work we have also shown that angulation and modifications of the gears arresting points made it possible to modify the machinery in such a way as to avoid uneven thrusts on the blade, more compatible with particular kinetics; of these types of macyhines.

More specifically, we have shown that by making gears intermediate whose support axis was not pa; rigidly fixed the crankshaft, one succeeded in to produce an armament in realm and a rotary action of the crankshaft. (Fig 4 at ) In the present invention we simply add on this subject that the supports of the intermediate gear can be made by simple slide or double slides.
This method is to realize, as: the methods already specified by ourselves, a arming the external gear not from its center of filming, ma.is to from the gear teeth5 on which it is supported. (Fig 4 b) Other examples of gec metric addition by planetary addition in line or angulated As we have shown in our previous work, the gears induction planetary models make it possible to positively modulate the work of the gears of support, which in conventional machines they are negative.

In the present invention, , please specify again that all the Inductions can serve as in luction entering the induction composition at engrenages of the peropterical supports, and that the lined gears induction Supports can be internal, external only, or internally External.

A first additional example is to perform a mono induction post rotatifve as basic induction, and w [e mono-induction retrorotative as induction peripheral. In this case, the external type induction engi nage is coupled to a support gear type E xterne. This induction gear is coupled rigidly to a support gear of t; planetary pe, of internal type, which will govern I'engrenage external type induction of the blade. (Fig. 5 a) It will be noted that the prephase induction can also be angulated, such as we have it shown in our earlier work. In addition, it can be noted that this can also be realized on a free crankshaft, and even, in cverta.ins case, without crankshafts the suppo 1 peripheral induction gear being simply a gear of laâson fixed support gears and ~ inductrion blade.

A second exekmple consists: ei again, to realize the induction central type mono induction rotary post, This time we will fix the induction gear of the central induction a second outer type gears, which will result in a induction peripheral also of post rotational inductive mode, (Fig. 5 b) In both cases the effect is po: itif.

In the first case, since it is an induction with prominence previous report center gears will be affected by the thrust at the bottom of the gear, and will have a rotational incidence on the crankshaft. (Fig 5 c) In the second, the size of [support gear, peripheral will be enlarged, this which will allow the rotary action of the blade to receive a point of support much more backward and consequently anguish the strength of the blade. (Fig. 5 d) Here, several positive effects are found. First, the hinge of the pale is more back and do not make counterforce. Then, the rise of this hinge, at opposite of damage to the machine, allows a greater ease of tounage of the party before.
Lastly, as it will be easier to see in the mechines turbinative, the effect of the gear of suppo, t, to the lie of is sutritably réalsctionnet and leading the strict rotation of the gearing i induction will also cause the viiebrequin, on the other hand , when the machine is at standard kinetics, and by active force, when the macliine is from Turbine type.

In a third, complementary example, a master induction by gear heel. the retro rotati year of the induction gear of this induction will lead the retrorotation of the gear the planetary support which is fixed. (Fig 5 e) Again, once, the gear of pale pt iurra will be from then be realized with a dimension upper, and and the point of encircling, or hinge of the blade in the course of descent will be further back, this making it possible to achieve an opening of the vernal blade, and positive about the entire surface of it.

A fourth complementary example will be realized by producing a poly induction retrorotative, whose plae will be replaced by a gear type external.
This gear retrorotational sun gear to act as a support gear for the blade.
Fig 5 f) As can be seen, all the inductions can lend themselves to this type of arrangement, of combination, and the result is always the know, a reengineering the balancing equilibrium on the blade, which may lead to pale deseng allowing better dynamics. In all cases, the point opening, or hinge, the blade is pushed towards the bitter, and the blade works on the whole surface on his side.

Adding modifrcatric method? : Types of gears Gearing can be successfully modified by producing reports gears whose teeth would prevent them from fatteners of the gears generally attracted to these gears.

Here, it is interesting to note that with female gears, one can produce more volunous gears, whose ratios of size and teeth will changed. For example, it is possible to produce engrensges whose ratio of size are three out of four, and the teeth to three out of two. In consequent, the point inking which, in the machinery, will result from the use of this type gear, will still allow there to work d +; the ple on all its surface. (Fig. 6) In result , the angulation makes it possible to modify the length and the size of the gears a report of size for example of three; quarter but with a teething ratio of gears remaining of three: ur two., or the number of sides of the machine to realize., which will result in a re ~ ul of arming without changing the ratio backward gears It should be noted that, in addition, the teeth of the gears can be modified categories of material, so that the effects of use polycammed gears.

Second part: generalization of balancing methods surface of blade work.

Recall of all these n [ethodes. (Fig 7) By cerc, au, chain or off-axis gear induction By poly camation By direct arming gear meshing with intermediate gear By falcified gears Step induction with planetary support heats Flexible support gear induction Overlap of time n ort of compressive parts We have shown that several methods can increase the yield of the rotary kinetic machines, tandard. Generally speaking, all these methods induction can be used to completely or partially forces that are there usually found. Although tense, this rebalancing of forces, at the same time tempos that he increases the previous power: on the blade, simultaneously decreases the effect of anvil lever of this, which will reduce the friceon, and all the more so as the crankshaft of these machine are already, at this level the speed, on solicited. This rebalancing of energy on the blade increases the possibility of desing it and will allow remove a better thermo dynamic energy efficiency. .

This is evident first of all in the hoop gear method, plus especially when the element linking the support gears and induction is a chain. In this type of induction noitho, the course of descent retro rotationally oriented 4 xercalized on the blade does not succeed or less to produce a rotational force lever on the crankshaft. This effect is neutralized because the force transforms into traction. The Hocage thus produced transforms the fore rotational Orientation of the blade on itself in drilling this turning of the crankshaft.

As a result, the forces of the crankshaft Wurnage, even by action of filming of the blade on itself are superior to the rotational forces of the blade on her nzême.
The blade works so much good. (Fig 7a) In the same way, if the machine is made by gear induction hoop, and that care is taken to correct this gears, modifying its support barrel, or / and add one-third gears, the rotational tection of the blade will be transformed in traction force, and results in the rotational force of the Crankshaft Mayitre to be superior to the rotationeli orientational force. The contradictions of the machines will be therefore not only attenuated, but also tranformets in rotational fonts of vilebr.> quin. (Fig 7 b) The polycamation method is also a very efficient method of control of the orientational rotational power of the blade and its transformation into power rotational positional of the v [ebrequin. It can be used in multiple entdoit in rotary machines, in rotary piston machines, and in machines to pistons. With the use of poly camé gearing, both the point back of the blade, and it momentarily falcifies its speed of rotation by compared to the crankshaft. The shape of the cylinders is therefore and rightly the thermodynamics of the machine. The polycammed cages of blade and cylinder can be diispased in different directions They can be in the sense of cylinder or in opposite directions. In all ~ 1 cases, the origina, lités of this support method consists of the fact that the point of armament is at a variable distance from the center of the machine. Therefore, I, rear armament, downhill can be product more Near the center, or farther away, is the initial orientation of the gears. ( Fig 7 c) In In the latter case, the artillery armament being lowered allows the pale of subtract from the counter force against and transform them into forces of rotation on the crankshaft, and overhanging the crankshaft's vitresse by speed ratio retrorotatiion of the blade, which omnuits the differential contradiction between these parties.

Similarly, the direct arming method of intermediate gears gears support and induction is p. In this method, the gears in.termediaries are not supported by axes rigidly crankshaft. In consequences, during the rotation n negative of the induction gear, the effort of the intermediate gear, for which the arming point has been modified, will have for effect to cause the rotation of the equine vilebi in the right direction, whatever the meaning rotation of the intermediate gear. The machine is destabilized positively.
(Fig 7d) Additions relating to the deferred armoring method In our previous work, we have shown that deferred armaments made with the use of this method could be obtained by gears intermediates on supports; pivoting, with members of blockages. The introduced to the effect of specifying that intermediate gears could also to be intalled on axes mounted on sliding parts made in conjunction with or the crankshaft. In a first this, for example, the sliding parts are made of This is how to hook up the crankshaft and the crank pin. In second way, a slide is inserted,: in the crankshaft manchione, and a member supporting intermutaneous gear is engaged in this way of being able to let attaching this gears to the gears of support and induction but also from nlanière not to let him distance himself -. (Fig 8) In both cases, gold produces exactly the same effects, and the method for To produce them is identical, to know how to defer the weapon of the gear intermediate of in such a way that it is no longer reachable. The technique of realization, by sliding part here is different.

Geared method The geared method (FIG. 9) is also the subject of the present invention.
invention.

As we have shown in the case of turbines with motion slinky, in the type of polycammed gears, oi in the induction stage with gears planetary support, the magnification of the blade gear is important because allows to move the point of erection of this one towards the back, canceling or canceling even against forces made by the anterior part of the blades when lowering.
In this part of this invention we suippospns, for the purpose of reduce the number of rooms so that it is possible to carry out gears more big, while respecting their 3 contributions of distances between them, but in faltering their natural dentition ratio, that is, by producing teeth of which the perniet forms that the distance separating each of them be diflerent for each gear, without however, this is a challenge.
real tehcnique, but far from impossible. This type of gear will certainly increase the friction between the gears, May: will significantly soften the knock, which will that In total, this rotten modification is advantageous. (Fig 6) The teeth as well sought will necessarily receive more lateral friction, but at the same time friction, and even of vertical knock, F t therefore, has total, this type of gears could improve the machine.

The staging method of producing such a way to produce a gear of platen secondary blade support.

This method is based on the fact that the blade always requires some quantum of derotation by quantum of rotation of the crankshaft to achieve the shape of cylinder sought. But this quantum t, e derotation is not necessarily 'to be realized by a single induction.

he If we realize a first induc Lion of pale whose quantum of déoptation is inferior to the one that is necessary, we can add a new induction suipplémentaire, it also of failbe degree of der eration, leading to the blade in such a way that the sum derotations of inductions s At equal to the exact derotation that requires the shape of blade and cylinder provided ..

Moreover, if the removal of; the first central rotation is more important that the Derotation sought, we can pass this derotation to the gear of support, and to reduce sufficiently this eng = enage, or to enlarge the gearing Induction of the enough to make up for, again, the lack of derotation that the first one induced induction as well.

Finally, if the induction of pb m produces a post rotational induction, one can couple it to an intermediate engrenae which will invert it, and to use thereafter this gearing intermediate conune engrenagc support of complementary induction higher. Of how will the suipterous induction be supplemented in retrorotation and in induction lower.

In all cases, the induction induction of the blade will be more voluminous and its inking point is located more back of the blade during the descent.

We wish to repeat that all the inductions can be used to achieve these types association of inductions. Here we have listed near inductions different, the combination will achieve nearly four hundred. It is by consequent impossible to list and present all these inductions.

We would, however, like to present some examples additional to those presented in our initial inwntion, in such a way as to show a once again the simplicity of realization that they brings. In the first example, it's about to add two post-rotating mono induc tions whose degree of retrorotativity is poor in such a way as to end up with the required d +: retrorotation option (Fig 7.1) In the second case, we on backwash the induction genesis, and we shrink it all by increasing the size of the higher induction. These changes will lead to report of retrorotation sought. (Fig 7. I) In the third case, we realize a mono induction post rotary, and it is superpo; e a mono induction retrorotative very failbe content rétrorotative. This is possible by the geometric additions that make the point of turning of the upper internal port gear almost zero. (Fig 7..1 ) In one Another example is the use of the first level of a gear induction.
intermediate, and this is completed by a single post rotary induction. (Fig 7..1) Dan.s one last For example, a retrorotative induction is made at the first level, and we use the internal gearing inductioi. conune gear gear crown of INTERMEDIATE
connected to a centri gear receiving the blade.

Poly uneven induction It is possible to modify the curvature of the cylinder by using poly Intermediate gear induction of unequal size.

Indeed, if a poly induction is used as induction complementary, and determines that the intermediate gears that result in. gear central to the center will be of different size, no i only this gear will be iI planetary, amais at on top of it, his positioning is like that of the same planet. This will result in aches curved, or acute: as during the realization of poly camtion (Fig 11) Flexible support gears v In all semi-transinductive inductions the work of the crankshaft but the gears of the same active suypport, acts in bieocage, again, because he can produce or train alone, the planetary tilt of the blade, and gear induction thereof. For this reason, the gear of suppourt must to be attacked by the crankshaft.

This can be mechanically improved by realizing a gearing fixed to the semi transmiession by the recou rs to springs ensuring a sag before, who will allow the vehicle to reach the blade first. (Fig 12) Applications to turbines (Fig 13) In our work on genetic properties, we have specified that exist first two major types of supports the these machines, either by poly induction, and by induction Central. These supports of which for damentalement different because of a party divided the internal time of the blade in d different units, and then by that in the first case, in momo induction, the pal is connected directly to the gearing induction, then that in the second, ewn pol, ~ induction, the blade is connected to the crankpins who even are attached to it.

Then we speci ed that they exist, besides the macaniques retro-active or post rotating, mechanics act in scissors, or acting as a springboard.
Dams the In the first case, the rearward orientational retrorotational effort is greater than to the post effort Orientational rotational forward In the second, it's the opposite. It is why do the monono induction post rotativi, s are generally preferred for example to mechanical by simple intermediate gearing.

Fioally, we speci ed that there were three major subcategories mechanical permitting the correct activatic n mechanical parts of the machione, pale cylinder and crankshaft and gear wheel.

As for the turbinating machines, let us recall moreover the following, that, in these, the cylinder and blade inductions could all be grouped according to what were connected by dynamic gear gears, the gears intermediaries, crankshafts, the blade.

We noted that the suppori of the clok wise type, the indusctions by poly induction were very liquid and profitalb s. The reason for this is that 'they were made by geonetric addition of connecting rods or double gears We also realized that the; inductions related by the crush were very profitable. The crankshaft controlled the blade by induction and by the other side control the cylinder by semi-transmission. Moreover, we noted that the inductions bound by the blade, or linked by 1, dynamic support gear from the semi transmission were more serious.

The reason for this is clear and ci) nstitute niajeur defect of any machine rotating art previous, and this same setting in cinnamic. We can not, from a gear of central support of external tytpe cause a planetary action of the induction gear without the simultaneous participation of self in a semi transmission crankshaft.
In other words, a central circular movement can, from the point of movement rotation of an element whose center of rotation is different, for example a internal type engrengage is -translated correctly. But a movement rotational do not cause a single, rotational effect of wider or similar amplitude, if this one at an identical center In other words, the wrong of the gear of dynamic support can not entain, without recourse to third inouvenient of the crankshaft. Now conmae this movement of this crankshaft is included dansd the movement planetary to waitews of the pa e and are inductive gearing, it in results that the rotational movement of the,, support rebage can cause the movement planetary.

As we have just heard in the turbines, the work of derotation from blade is usually increased:, while the work of the crankshaft is decreased This is the cylinder that will attenuate the derotation of the blade, and increase the rotation of crankshaft ,. As usual -. the tranlational blade model is the most obvious. We see that at the same time that the blade has realized a faster derotation by report to his crankshaft, that arrives at its limited expansion angle after a hundred eighty degrees of turning, the cylinder having i ~ alise foury ten. The total remains a hundred and four twenty degrees, which is not b: case when blade and cylinder turn in the same meaning.
It is therefore important to consider that any improvements to rotary motors in their standard kinetics pc will find its correlation in the engines turbinatifs.
But, however, the modificati + -n will not necessarily be the same magnitude. It is necessary in fact, take into account that, for example, when the cylinder makes thirty three percent of the rotation of the vilebrequih, it is not necessary for him to produce thirty three inches of the complementary power c; w a much stronger degree of power will be accumulated in the cyluindre which served as a training wheel, Taking this into account, it will not be necessary maybe twenty percent d .- the strength of the cylinder to equal the lump of the blade.
which may possibly have the edge. Therefore, it is strong, possible, around when The use of floating segments, whether the separation of inductions, or in other words, their link strictly by the crankshaft are enough to balance the machine , between pale crankshaft and cylinder. We know, read slonky kinetics in eight o'er a rotation of crankshaft and cylinder of eeg: e be thirty-five degrees each by compression. We know from a tree that the dynaniic clokwise allows the crankshaft of turn from one hundred eighty de3; res and the cylinder to turn from four came dux. Tenat account of the kinetic energy has nassées by the cylinder equihûre force the more perfect, may be between these two pc The methods of control of the force orïuentationnel of blade will be applicable quai t nipem with profit.

It is first important d; mention that during pale and cylinder differentiated, that is to say, doni the crankshaft is the common element between these, we have can of contradiction sde pale I. cylinder, except that produced by the segmentations. We can even use any nduction orientational cotrol of blade, to adjust perfectly the machine. (Fig 13) Moreover, although it is possible that the phenomenon of training do not render It is not necessary to modify induction inductions by resorting to pale, it's up to to say the descending energetic inductions, we think that in these cases also, we to carry out all the inductio a decendantes with recom control the orientation of the blade already en) ncées. (Fig 13) We will therefore speak of induction of poiycamé scentante, in calibration of dentition, by chain hoop gear and so on. We will finally speak induction with Planetary gears of cylinder induction. To do this, as for induction up, we will install on the 1 nanchin crankshaft unaxe allowing receive the double inductive gearing - peropteric induction and carrier support the induection central, and they are connected Is .uer induction.

Only two examples are enough. First, we will be able to realize induction by addition of mono inductions. Then, we can achieve induction by gears hoop of retro indution. (Fig 13) Another version of the application will be to realize the rising inductioin semi tranmittives with the stated methods of directional control. Of this way , even if the cylinder is connected to the suypport gear dynamic, aural ion destroys the monodic orientation ratio between the latter and the blade. The machine will be improved. (Fig 13) Other modifications of the induci ions As we have already underlined, the connections of the inductions of blade and cylinder in the turbine engines can, 4re realized by means of the crankshaft, of the gear of support senzi transmittit or by the blade.

Here it is advisable to add two other means of seasoning, first of all , one of elements of the semi transmissio: i, for example the inversion gear,, or again, planetary gears, which cost one in the descending inductio as well activate, when split.

In the first example, the F ngrena.ges crowns of semi transmission, when are to crown, can be split, one of them can then actir the gear of Dynamic support of the insducl ion and the other the cylinder, These two gears crowns can be activated by e; intermediate igrenages of coarse different, and so realize different rotatioa i reports. (Fig 14) When the transmission will be carried out by pignoes gears, gear inversion can be carried out in duplicate, and one of these gears will be able drive the spindle gear this rotation of the support gear of the machine, while that the other will cause the engrem ge of the cylinder (Fig 14) In addition, the semi-transmission may also cause a gear planetary and an axis, one of them engages the engorer age of support the other the cylinder (Fig 14) The crankshaft may drive intermediate gears that will cause a crown to which will be fixed ca blade support gear. These same engregages Zntermediaries can be doubled on the other side and control retrorotatively turning of the cylinder (Fig 14) Also one of the gears of the doubled gearing of the rising induction at planetary gears to be able to serve as a gearing gear gear induction of cylinder, which will then be either internal or external type case. (Fig 14) Poly planetary induction Let us mention in the last analysis that inductions by poly induction can from from the same crown, receive a second set of intermediate gears of size Of course, these gears activate a gear in which the blade will be fixed.

From then on, the blade will have a planetary motion, its arrest bonds.
can be too strong back.

Note also, in the last year.aiy,: e, that the crankshafts of the induction lower can in some cases be free, and strictly relied on by the gears induction, poly induction, and semi free, in i <s other induction, ie retrnus by the gears, and by an arm of retention, and cc similarly to the intermediate gearing induction by intermediate gears.

In addition, these gears can be polycammed, or by chain, or toothed recalibrated.
This means that the various calibration methods of orientationality payroll, or the power of the cylinder when the machine is realized in its formae turbinartive can be performed simultaneously.

Increases in the number of amoeioration of oruientaitonelle content As we have shown previously, the realization of two induction participant to a single range of blades to be used to minimize the forces Orientations for to transfer to rotatiox forests, and this, mainly by avoiding the friction. It is important to note that the number of under induction can be number greater than two, in the measure; or the sum of the total derotation of induction respects the derotation of the machine.

Example of a mix Moreover, as we have <<I said, we can achieve a mixed way several modes adjustment of the positive attitude of the mechines. A single example will suffice.
We will be able example realize a supoport with planetary gear from outside a induction by internally, and at the same time realize this induction by gearing armed intermediates directeme it by semi free support, and finally, connect this semi-tranmissive induction of poly cameo type. (Fig. 8) Semi planetary and polycarbonate planetary transmission As we have already done, we can use the gears polycammed in any part of the machine, whether it is rising, descending, or semi tranmission to modify the speeds of the vilegrequin and the pale between them, and consequently, of the blade and the cylinder, in the machines rotary and turbinatives.

In the case of the cylinder, it is éident that one can for example polycamer many intermediate gears, the in corre grenades, or support, following the one who is couple. As a result, we have already shown it for our semi trubnoives differential, producing a perfectly circular motion, but accelerometers decelerative. This movement comes to mofdify the thermodynamics of the machine. ( Fig 11, and 14) But, if this method is valid to accelerate and decelerate several pieces of different moments and successiv, as was the case in the turvbines differential, can idi, accelerate and decelerate the cylinder several pfis consecutive by pie with less of parts.

To do this, it is necessary to produce the activation of a support gear polycamé, whose center of rotation is off-center, t couple this polytached support gear has a Cylinder induction gear, also poly cameo, whose center is the center of cylinder. In this way, the cylinder will be engulfed circularly, and central way, but will undergo accelerations of elerations which will positivemtn positivemtn the rooms of compressions and the dynamic tehrmo of the machine. We will have to choose the report polycammed gears of you how to make the number acceleration desired decelerations. For example, for a turbinator type gearing polycamé of three sides will be couched to one of two. Moreover, for a n machine rated, for example eight, we will choose gear gears of nine on eight, or eight out of seven, depending on the case. This very simple method will be semi-interactive since of a by the gear or the doublé of engrages which the command will be simultaneously inverter, and will be siutueé de axon axis, K when the gear of nduction will be located in the center, and to carry out the desired report of i etrorotation.

It can be noted that the plycamé coupling of a cylinder and a polycamé blade mounted each strictly rotational on different axes, will allow realize the Turbine machines at their pleasure. These machines, will only explode only once per turn, which may be of interest to some occations.

It should also be noted that, as we have already mentioned, the linkages polycamation are achievable at; if in induction descentdante. The villains a Turbine-driven translational machines can therefore be interrelated between them, but the blade can be equipped with a gears polycamé
activating, in mechanics goes down the polycamé gear of cylinder. the reports from dimensions and shapes will be k entiques to standard polycamé machines.

Rotary motor p slinky pistons: reminder and precisions As we have already mounted, rotary motors can also be realized with a saving parts by making one piston per center, each part of this piston performing in turn a compression and an expansion. They are even these types of dynamic that we have re-examined with real machine blades rotary, and constructing slinky synthetic kinetics. Come we already have it specified on this subject, the great difficulty of realizing this type of machine is that if we want the piston goes back by the centtre, it must produce a mechanical post or retrorotative with rather large biublbes, which, by the way, means perceptions, than those they will be too large and will not produce accelerations decelerations of the cylinder, but, likewise, consecutive declines, which is impossible or difficult to achieve. We have already mentioned that accelerated rotation r decelerative of the cylinder, or a cotrc the planetary bulbs created by the displacement of Piston could be obtained by +; ngrenagess polycamés. The type of semi transmission more High shown applies. Enm e8> t, we can arrange on the gear of center, an axis of attachment which will correspond to the center of the peripheral gear .. Cetci will ensure that the pisotn which is attached to it passes well through the center. By the way, cylinder can be equipped with an intermediate gear that will couple it to the steering gear of the piston.
The machine will thus be more compact, and will satisfy the followers of engines to pistons. (Fig. 15) Inner surface work of the piston As we have already done, our work has mainly consisted of in together, to produce dynan toques of machines, or even niechanics, or kinetics that allowed to proc uire a thrust on the blades that was better balanced and produces less friction. As a result, our work helped to change the moment explosion and cylinder surfaces, and therefore pistons. As the effort are therefore better distributed on this one, we can modify the vcreusets routinely used in em to cause the consequent ignition of bvougies, to rather allow a lightning that on the one hand will occur on the part before, but at overpolished will leave some of the power on the back of the blade who los in requiem.

So we can imagine that the uset piston will be convenient to forward back of it, but also that it will be affected by the thrust, which arrier will not be null, but simply weak. 011 will therefore practice a mini crucible for allow axplosion. In addition, ci: crucible, or small rails of ventilation will allow pass the gax back to the air before the delayed ignition of this type of machine. We will also simply be redeemed; the piston surface by lowering the rear part (Fig. 17) Urbinatifa: accumulated force dd in the cylinder, heating the cylinder and the blade It is important to emphasize that while only spending energy on acceleration and deceleration, the blade and the vilelx cquin of a rotary machine do not produce little of kinetic energy. In turbine engines, mainly in machines of motor type, part of the movement of the blade, and the movement of the crankshaft found in the cylinder, and the directional feedback that existed between the blade and the Cylinder is found in an element itself. That's why this contortion is for so to say, and his nuisance is reduced. Indeed, the number of degrees of rotation missing the crankshaft will be re dsed by the cylinder, as the number superior of Missing reversion to standard kinetics will be realized by the blade and its against party in the cylinder this it e; It is important that the crankshaft requires always a some new quantum of, energy to restart his couse, and the blade to realize its retrorotation. This energy will be enamaginated in the cylinder.

It is important to underline, read if the point clokwise represents a point nia.jeur birotative type machine, the directional pointy tip on the blade of this machine type being perfectly equilibrated with each copied, the fact remains that the crank shaft of a machine of this type of technology of 180 degrees while the cylinder in travels 90.

Another kinetics must therefore be considered polar. he this is the Slinky kinetics in eight. In this 11th, the crankshaft and the cylinder in effect run through exactly the same number of i degrees of rotation and rotation, ie one hundred thirty five degrees with each compression. D, -in the measure or less, by the various processes that we have already mentioned, the differences in thrust ratios oruientationnelle on the blade, we have the machine 1 ossibly even more perfect than the niachine clokwise, who herself is beautiful, oup more perfect than the standard machine.
Synthetic movement It is important to note that nou; have already mentioned that we consider the kinetics of which blades and cylinder moved in opposite motion, as motor and that whose blades and cylinders were moving in the same direction, compressive.
Whereas the last contributions of control of the quantitative levels, applying everything both mechanics in cisc as mechanical springboard, we think It is relevant to add that, in fact, the blades and cylinders of certain so-called kinetic compressors travel in the same direction, some kinetics, which realize no only a virtual race, but also synthetic, close to the moment clokwise, will be cosidered as motor; Indeed, it is the synthetic realization of the machine which allows, by the raealisa.tion of the faces in more than one turn of the machine, to realise this one with reports of engages that make it possible to modify the point weapons, in these cases more before, in this one referably by mechanical scissors, by therefore to advance this one worm; the front of the machine. In our opinion, does not remain not less, however, that the loss of these machines, being one hundred four vimt degrees in total, will not offer a relevant thermo dynamic Combined motor axis There is no doubt that the main axis of turbine engines is survommandé. Good heard, it can be redecommended by the tranmission of maohine. But, this does not remove not the friction on this one. Actually, the motor axis of the machines rotary should be simply the maaneton axis of b. blade. We think that the support axis positional of the blade may be an accessory axis, and the induction mechanics of the pale could be made outside on a very oiled crankshaft. Not only this strategies would it limit the friction in the machine, but in addition, it will allow carry out the oiling of the crankshaft. master importantly, while insulating the parts compresives and mechanics of rêrates way, that decreasing the pears of éyanchéités of these. (Fig. 16) In the machines of the prior art, the resistance strength of the materials necessary in the The type of mechanics used is necessary to enable resist the friction resulting from oversupports that the blade, and its contortions on the gear of support and this, even if it was housed close to the blade .. But these friction being practically canceled, it is possible to read the blade on a crankshaft in crankpin, and realize the macanique from a crankshaft or eccentric in cson specific box, which will have a powerful oil, but completely separate high parts of the blade.

Successive, simultaneous and suction injection In rotary or centrifugal machines, the overpressure is canceled out the back part of the blade, or the little expa.nsive fc rce of it leads us to think that gas contained in this part of PC would rather have simply a support function pressure of those, in expansic n of the front part. We can therefore think that the Reassembly of the back part of the combviustion chamber could be Realized different from that of the Lie before, by filling it, by example of vienx gas, or of air., oi still gas whose carburation will be more low.

To be fair one can think mainly three methods. First, we can dispose of the gas outlet in a different way in such a way that minimize the dump the gax in this part.

Then, we can change the place that the introduction of gases. If this one is delayed, the gases the front part of the cylinder and send the used gases the back (Fig 12.2) But we can also order the entrance of the gax by the same mentrées, by a game of successive valves related to this same inlet, the first valves allowing entries of gas, and the second of spent gases, air, or gas containing different. Of this way the used gases will be in the back part of the hcambre when ignition.
Finally, another way of integrating the gas will be to reallise integration with two different holes, one aspiring, and the other agazing nine. Of such a great distribute at their location, depending on whether the machine is chisel or springboard, we will practice in the ploi; a pipe that will allow gases admitted to be conveyed to the front of it, as the accepted agz will be routed in the axrière.

In this way, the rear gases will serve as pressure springs, and the machine will be more economic, since this type of macghine must work more forward, in the door.
Polycentric piston drill Of course, the shapes of cylinders obtained by poluycamations gears will result in appropriate pisto forms. We will see to draw them in force of the strength obtained on the back part>. the thrust, their fearmtting a little explosion or none of them are mechanical ones.

Segmentation, modification of cylinder shape and thermodynamic We have previously shown that segmentation by pivoting segments simple and in double articulation allowed to realize a floating segnientation deands them rotary and turbinating machines; , which in our opinion will limit friction, Consequently power loss and wear and tear, while ensuring better performance rate of compression.

It is also important to add that the segmentation in double seginent swinging can help soften the curve; the cylinder, and allow make the machine with a ratio of vile) modified rerquin, that is to say, bigger, for a same blade, which will increase the -, orple of the machine, or, for a even crankshaft, a smaller blade, which will dimun consumption.

This contribution can not be used in standard machines, in which draw the anterior part of the blade and the cylinder on the basis of coindifying their form at maximum and so limit the fc rece explosive in this place. But , since in us machine, we succeed by many nioyencs to make trsavawiller positivenzent the behind the blade, the accentuation of the cylinder's pormeme for the same blade crankshaft crease will accentuate the rear descent of the blade and his effort. The righteousness of the curved bend by bowing more than the segment pivoting will therefore be a (a) appreciable port. (Fig 7.3, 12.1) Absorption Pistans We can realize the machines st, indtrad with a piston absorber, to The back of the blade, which will restore the force of cogn.enw it of the explosion during descent, this who would still allow it to realize blade curving machines and cylinder aniéliorées.

Triple geared and double geared gears Coomme we have already onn, all the inductions can, when the machinery are carried out in a turbointive manner, be carried out with control and especially by polycanation, or induction by gears of peripheral planetary sytems.

It is important to add to this r ropos that it will be inductions of such so that not only the F ales, but also the cylinders are made with the use of induction gearing with support gears pérériphériques.

In such a way to perform the machining with a condensation of gears maximum he will be relevant to use the same induction ma.itre that can feed both Peripheral and planetary induction of cyllinders and pale. In In these cases, the peripheral inductive gears will be either fixed or rigidly connected to support gears of blade, i, t of cylinder support, what we will name a tripled induction, supopport, supp-) ert, or still be, the indcion masters may give rise with two independent secondary induction using the same strategy. In this case, Induction will occur with two double induction gears.
gearing peripheral support, the engren; induction time of these two gears of support devices that can be the same. This is what we can see all of the Figures 25, 26, 27, 28, 29.

Part II; Alterations 1 ar overlap In rotary machines a.rd stand, whether post rotary and retro rotary, the blade realizes a retrorotation all around the crankpin or the eccentric of crankshaft on which is rotatively mounted. Simultaneously, she rotates more general around the central axis of the city uin. (Fij 801) It is more particularly this first movement, this rotation in sense reverse which is to the origin, during the expansion, of the well known volumetric loss in type of machines.
Indeed, it is the lati ral displacement of the front tip of the blade, to from the high point of this one up to the center of the bomba e of the cylinder which produces this loss volumetric. (Fig.
801 (b) In no earlier inventions, we have stated to minimize the loss vohtmetric rotary machines A by raising the degree of rotativity of the machine by an induction Subsidiary Subsidiary ^ in polycam laughs one of the gear sets of one of the inductions ^ flapping or straightening the crankshafts of superimposed inductions for a third compressive part Moreover, we already have spi cified application of the increase of degrees by adding induction and by polycamation was feasible also with regard to machinery rotating, when done in a turbulent manner. In this invention we Let's continue more precisely li: work previously stated in commenting more precisely how complete are the mechanics when the machines are so high (Fig.4.3).

In a second step, we will show that the loss reduction volumetric is also increased by the overlap of two inductions alone, simultaneously parts combined compressive.

Earlier acquisitions We have shown, beforehand, that we could achieve machines rotative type of motor by increasing the degree of rotativity of these, this degree of rotativity being understood as the number of induction steps necessary to support of the com] iressive part (s) leading to the realization of a cylindrical shape given for a pale soul.

Thus, for example, the mechanical support of a blade could be erected by the superposition staggered from one or crankshafts so ibsidiaires to a crankshaft niaître central. So we could example, increase the compression of triangular motors, and increase the couple of post rotary engines. (Fig 802) In addition, it has also been shown that the distribution of movement, instead of being obtained by the addition of subsidiary movements, could at contrary to be divided, segmented, 11 totality of the movement being able be divided between the cylinder and the blade, since chm read by this division of the movement initial part compressive planetary will be distributed in the blade and the cylinder. This procedure allowed show the possibility of producing turbines-type machines, these machines, having the characteristic, especially when the movement of the blade is contrary to movement of cylinder, to erase the known defects of rotary kinetic motors standard. The figure the most emblematic of this type; machine is the synthesis of the post niachines rotating and retrorotative more than in this one; movement of the blade does not realize any change orientational during his race, c -, which was named movement transitional or Clockwise of blade. (Fig 803) Subsequently, we have shown that it is possible, as is the case with machinery standard, to increase the degree of rotativity of the turbines. (Fig 804). Indeed, as for standarized machines, the degree of rotativity can in these machines to be increased by addition of induction, polycaina.tion thereof.

Turbine machines with planetary cylinder Rotary or basic turbine turbines are made with a blade in one translational niovement and a rotational cylinder, or the opposite by a rotational blade, and a planetary cylinder. Also, let's remember that the machines turbines form a complete range of machines, including translational machines constitute a pole of division important, or prole fifth of these. Indeed, several machines Hybrid turbines can be produced by lying midway between machines turbines, and standard kinetics rotary machines.
Again, in the Basic version, the cylinder is r (itational and the planetary blade.
(Fig.803.2) However, we have already shown that one could increase the level of rotativity of these machines by the addition of a rotary calf to one of the induction or part. Most simple expression of this consisi c to move the rotational movement of the cylinder to a movement itself planetary. So, the planetary motion of the cylinder will be of preferably realized in such a way that its lowering towards the blade is simultaneously realize the rise of the blade towards it, the convergence of these movements entrâant a increased compression; t torque.

More precise mechanization We have already shown that we can list several mechanical allowing to better support and guide the blade 1w + rs of standard kinetics. Thereafter, we acons shown that when these imchines were made in a turbinative manner, one had to always realize mechanics that allow to coordinate the virtual movement of the blade and his aspect rotational movement material, 1 of the cylinder. It has been shown that one must généralenient a) perform mechanical induction of the compressive part and induction semi transmittive of the rotational office b) perform a transnational induction sem of the planetary part, and connect directly the rotation axis of the bet ie rotation to the dynamic support gear of semi transmissive induction, c) perform a moni ante induction of the planetary part, and an induction down of the rotational part.

The present invention intends prec: ser that, when the rotational part has been increased rotatively, and is now planetary in nature, the inductions are not not realized directly on its axis rotatio i, but on the axis of rotation of the crankshaft governing his induction. So, whatever the inductions used, we will obtain the configurations of cordination of the following:

a) the induction of blade, and the inter-cylinder interposition connected by semi transmission dumultiplicative, and according to k case, inversive b) the induction of one of the seni transmissive type parts, the gear of support dynamics of the one directly leading to the axis of rotation of the induction of the part compressive complement and silence, c) the inductity of one of the elements being a standard induction, realized with recourse to one of the inductions of i remier degrees, and the induction of the part complementary being carried out with the receiver to a first degree induction, the crankshaft of this induction being activated by the use of a downward induction carried out at from 1 Compressional part.

So we always have two induc tions and a semi transmission or three inductions.
(Fig. 804.2) The following mechanics, already listed by us, will remain relevant, just as much for the blade and the cylinder:

the mechanics ^ by mono induc Jon by gearing i: -termediate ^ by gear c> beam ^ by stepped gears ^ by poly inducti) n ^ by simple semi-transmission ^ by gear c: piece of poale by gearing ^ by structure ena; renagic As for the semi transmission, they are either accelerating, by means of existing gears by external gearing or inverting accelerator by gears, sprockets.
by internal management by double-external gear Note finally that the mechanics of poly induction are possible and even desirable and that since for this, the phase shift can be realized either by crankshaft master, or be by the subsidiary crankshaft.

The present invention: the smoothing of up and down dead times and the mechanical support for turbinating machines of higher degrees We have already shown that c n could overlap the movements of two parts compressive. In piston engines, we have come up with this eventuality assuming, as we will see it more precisely later in this exposed, a succession of pistons and cylindrt s attached to two crank pins arranged successively on a same crankpin. In standard kinetic rotational motors, this possibility is realized by the complicity of psitons and a blade.

Explanation To understand more easily the scope of the present invention, we serve examples formulated in the field of piston engines.

In our invention titled Mote rs annihilated dead time, we showed that attaching the rods of two Pisi Dns whose cylinders were arranged consecutively the engine, that is to say, one behind the other, these connecting rods being elsewhere attached to two crankshafts of the same range of crankshafts made out of phase one of the other, we produced a phase shift of the teml -s niorts of the two pistons. Indeed, everyone two pistons reached its top dead center at a different time than the other.

This phase shift therefore led to the stabilization of a stable compression extending over a given period, for the top of LL rise of the pistons, since the primer of descent, and by consequence of compress on loss, carried out by one of the pistons, was compensated by the continuation and completion of the r. iontée, and consequently compression piston compiice.

In addition, it must be added that lor,; of ignition, when one of the pistons was in At the same time, the accomplice piston was in a cambered position, its dead time being completed. (Fig 805.1 a) A second example may be formulated as follows. suppose that we insert in the same cylinder two pistt ns face to face, and that each of these pistons be connected by the a crankshaft the following series between them by the use of a third party, for example, a chain, a gears.
Suppose later that the position of the sleeves of the crankshafts is organized such so that the respective downtime and downtime of the pistons are, as préeédemment phase. (Fig. 805.1 b) As previously, therefore, the beginning of the descent of one of the pistons will correspond to the completion: it of the rise of pistons coniplémentaire.
In therefore, compression will be maintained until the piston complementary primer he likewise his descent. At this precise point in which will take place the ignition, the piston latecomer will still be at his pi ~ int dead high, while the piston will have finished his, and offer an interesting angle of attack and systemic breaking.

Another form of this possibility has been shown for the case of machines rotary to standard kinetics. Indeed, we have shown, in our titled invention machinery rotative, reverberant, and birotative motive power, which could be insert into the piston of these cylinders receives sub-pistons attached by connecting rods to a crankpin offset from the center d - the eccentric supporting the blade. (Fig 805.2) This invention intends to specify this eventuality, and show the main mechanical likely to allow the realization of this type of arrangement.

Solution for rotary and turbo engines: additional action ride of superimposed crankshaft for a4 same blade and action rolled blade cylinder Action ride of crankshaft, ns master and subsidiary As we have said before, we have already shown that we can, in the rotary motors realize the suppc rt of the blade by the use of two induction scaffolded one over the other. Let us add, in the context of these presents, that we can phase out the dead time top and bottom of each of these creations and thus allow the realization dead time nonexistent of any of the induction during ignition. More precisely, here, it will be synchronize the high point of a blade with that of one of the crankshafts, mailre or secondary education, and to carry out the complementary vileb -equin, master or secondaire, such that its high point or ba is different, somewhat out of phase.

Action overlapped pale and cylindrical Moreover, in turin engines, we know that the cylinder and the blade are both compressive parts. In addition, in turbines produced in increase of degrees, the cylinder each of these> parts will be realized planetary way, Consequently will also have his times high and low.

As a result, as in the above examples, intentionally realize the m zchine taking care of the time shift dead high and bottom of the blade dead time h damn and low cylinder.

Mechanical method When carrying out the ma.chint s, care should be taken to crankshafts of the blades and of the cylinder of these machines of te IIe way that the dead time top of the blades do not be identical, but rather that it is before or behind that of the cylinder.

As a result, as in the piston engines, while one of these items will begin its descent, and realize: has a loss of compression, the accomplice party will continue and complete its climb, which will make up for this loss.
and keep the pressure ratio intact.

Examples A first example of this type of embodiment consists in making a machine with a simply translational blade movement. (Fig.806) This is obtained in supporting the by two auxiliary crankshafts equipped with induction gears, they even connected between them by an upport gears. The initial dimension of this gear was established, in its turbinative version of b-- se in such a way to articulate directly the retrorotation of the cylinder. Here, the size of this gear will be established in such a way to train the crankshaft of induction, this time planetary cylinder, which will equipped with a gear of induction coupled to the 4th support gear disposed in the side of the machine. The Cylinder will thus realize him of even dead times up and down. We must note that the positioning and direction of these high and low deaths is variable. We suppose here that the top dead time of the cylinder when it comes closest to the surface explosion of the blade, and that the direction of the cylinder, to achieve such time is opposite to that of the pale-neme.

In this version, we will further increase the degree of machine in degrading the crankshafts of in luctions, such as the time dead top of the blade either, for example prior to celi ü, descending, of the cylinder. Consequently, the descent of the The blade will be compensated by the momentary drop of the cylinder, and the loss of compression will be canceled for a given period +. The explosion may take place at the end of this period, the pale then pursuing its descent, and the cylinder commencing its ascent.

The same strategy can be applied when the blade is also planetary and non transla.tionnelle. Suppose a: turbinating machine having as elements of parts compressive one triangular blade and cylinder eight. For this niachine, suppose, among several possible, the following turbinator type realization.

In it, a 120-degree rotation of the blade is supported on it.
nieme for each compression. Here, we determine this constant of retro rotation for a post rotation of the crankshaft of the order of 150 of res. In a turbinating machine of first degree, the cylinder movement will be rotational, and here will be on the one hand in sense contrary to that of the pale, and on the other hand achieve a: 30 degree revorotation, this retrorotation used to compensate for the missing 30 degrees of rotation of the crankshaft that one should find if we were in a dynamic st., ndard.

As we have already noted, we can increase the degree of rotativity of the cylinder in the passing from simply rotational to planetary motion.

As a result, we will realize 1 tn planetary movement that will allow a lowering cylinder to the blade and an elevation in counter-direction of the blade at each 60 degree, each of these parts of motion born; siting 30 degrees. Of course, these lowering and successive elevations will be made against the direction of the elevations and of the blade, such as to increase the numbers and expansions.

Let's add this. If we have divided L, length of the initial crankpin of the blade of such that the one of the crank pins of the blade and the cylinder are equal to the length original, shape cylinder will not be modified. Moreover, if the sum of lengths of paddle and cylinder cranks -st greater than the initial length before division, shape the cylinder will be more domed in the arc and more acute in the tips.

In addition to providing better, shorter, shorter expansion time and an absence of dead time, the overlapping of the up and down dead times of blade and cylinder will modify the shape of the rollers in such a way as to soften the tips of cylinder while lengthening the sum of litters.

Additional notes The opposition of dead times Ik, uts and low can be realized of such way that the parties compressive enters into opposition of meaning during the descent, or during their time death. These opposites of moving compressive parts will realize exactly the same forms of cylinders as I) rs of embodiment of machines with double crankshafts staged, either raised, taller and more curved cylinders, or balloon cylinders, plus low and long.

In the case of turbines, this overlap will increase the degree of rotativity of the machine and accordingly the soul of the cylinders once again modified, as if had realized the machine of standard way but with stepped crankshaft and the axés, or still comnie if one had realized; the machine with recourse to polycammed gears.
Degrees of superior rotativity It is important here to reiterate that if the disadvantage of rotating machines first degree is too much rotativity of compressive parts, that of pistons is at on the contrary, too much linearity of the compressive parts, too strong deceleration acceleration.

To problems, the solution of the increase of the degrees of rotativity of machines rotatives allows for a well-balanced n achine between the necessities and the disadvantages of accelerating) decelerative aspects of the compressive parts of machinery presses. Now, the distribution of this; degrees increase between the blade and the cylinder, the phase shift or overlap of this distribution, and accelerated realization decelerative this distribution overlap p, ir polycamation are certainly methods technically feasible and with only a few negative effects in part positive effect generated.

So it is important here to note that these increases in degrees can be realized in combination. The machine can therefore be made turbinatively, with planétérisation of augmented degree, in a cured fashion, and moreover in a polycammed manner.

Advantages The realization of these elevations in the turbines will allow realize the Advantages of Degrees Elevations of Standard Machines Without Meeting the defeats, either mainly the technical difficulty of realization which will lead to strong vibrations, e Difficult control of the management of the final movement of the blade. These achievements will reaffirm the number of dynamic adjustments that have not been machinery rotating, and will also allow you to take advantage of blade configuration, and turbulence interesting.

Here, one of the important contributions of these procedures realization the explosion of delayed way directly leads to a more concentrated downhill. In fact, instead of achieve in 270 degrees, as is the case in rotary engines, or else in 180 degrees, the case in piston engines and basic turbo engines, it is will do here approximately 120 to 140 degrees, which shows the appearance too short, if not zero the nwrt time of the machine.
This rapid expansion is compatible with the type of burning of gas. Otherwise, the length of the compression equalized will allow the double ignition, all as much in the diesel and gas, this double> 1 allu.mage can even be a mix of these two types of fuel.

In addition, it should be noted that this project will also have the advantage of to permit increasing the length of; manetons, which translates into a increase in couple of the machine. Finally, these achievements will increase noticeable way the compression ratio of the motors and consequently to achieve the engines Of type turbines in their form dieseL

Types of machines and semi machineries By aiileurs, it is also about corr, take that type machines turbines are the machines rot, atïves standard, c ivisibles machines with prominences retro-active, and retrorotative pre-vention. In the case of turbines, we do not must not only take into account the temperature of the blades and cylinders, corn also, and maybe more of the virtual form than realizes the blade. Indeed, when the report the shape of the blade and the virtual cylinder is retrorcative, even for a material form post rotating, the cylinder and blade travel in the same direction.

Conversely, when and the blade t the virtual cylinder are post rotary, the blade and cylinder travel in the opposite direction.

As a result, the crankshafts supporting the blade and cylinder will coordinated by a seedling transmission, which in the first case will simply ensure the difference speed of these elements, and which in the second ace, will ensure in addition their inversion.

In all cases, it will be a question of the initialization of the initial positioning due crankshaft, when pale and cylinder are at their respective times, so that these are not not oriented on the same right - but rather angulated one by report to the other.
For the purposes of this presentation, we will not agree in the description drawings, as an example for each of these possibilities that counts multiple.

Part 3: Systems of accessories for rotary engines and turbinatifs In a turbines engine, where the candles are arranged either on the rotational cylinder, either on the blade of the machine. (The ig, 901) In both cases, it is a question of moving a piece of electrical current rotating. Most simple methods to achieve this implementation consists of provide rotational cylinder of a magnel om arranged next to the candle, and connected to she by a conductive element, This magneto will pass successively in front of the magnets, these magnets being arranged in the the periphery of the crankcase, or alternatively, on the side of it.
magnets and magnets will produce the electric discharge, necessary for the candle, It will also be possible to connect the candle through a conductive fii to elements producing electricity successively located outside such as for example by ignition electronic and cam, these methods being well known.

What is important here is that we can move the current of a stationary piece to a room king itive mainly in two ways, All first, we will equip. the thread leading to the candle of a point placed in the side of the rotor.
This point will consequently produce a circular motion. This movement will be realized in such a way that this one, you a rotor of a distributor m passes necessarily in front of the metal plates m deposited in the wall of a fixed receptacle m these plates being successively supplied with electricity by conventional systems.

Each passage of the rant point 1, one of the plates will pennettra so 1 mcheminement from 1, electricity to the candle, ~ Fig, 902) Moreover, it will also be possible to break into the fixed cylindrical cavity metal donut receiving the electric discharge jets produced by the electrical system.
Supposing that the use of a brush ante flow on this donut, the common thread d`électricité
will always stay in touch so it will receive landfills electrical 11 candle power supply (Fig. 903).

In a turbines engine, the oz the candles are arranged either on the rotational cylinder, either on the blade of the machine. (ig, 901) In both cases, it is a question of introducing a piece of electrical current rotating. Most simple methods to carry out this diet consists of provide rotational cylinder of a magne: om arranged next to the candle, and connected to she by a conductive element, This magneto will pass successively in front of the magnets, these magnets being arranged in the on the periphery of the housing, or on the side of it the frolenzent of the magnets and magnetzrts will produce the ek etric discharge necessary for the candle, We can also connect the candle iar a thread to elements producing electricity successivet are located outside as for example by ignition electronic and cam, these methods being well known.

What is important here to ascend is that we will be able to pass the current of a stationary room to a room ro ative mainly in two ways, All first, we will equip the lead 1 leading the candle with a point placed in the side of the rotor.
This tip will consequently produce a circular motion. This movement will be realized in such a way that the latter, such as a rotor of a distributor passes necessary in front of the metal plates m deposited in the wall of a fixed receptacle m these plates being successively supplied with electricity by conventional systems.

Each passage of the tip of N 1 ant, one of the plates will therefore 1 mcheminement from 1, electricity to the candle, (lg, 902) Moreover, it will also be possible to dispense with the fixed cylindrical cavity metal donut receiving the electric discharge jets produced by the electrical system.
Supposing that the use of a floating brush; on this donut, the common thread power will always stay in touch and will therefore receive landfills electrical necessary to supply the candle (Fig. 903).

Brief description of the figures: Part one Figure 1.1 provides a brief reminder of the terms we use nonnalement for conunent otative and turbine machines Figure 1.2 shows that in 1; s turbine machines, as recalled in g) the 11 cylinder gears sound. also applied induction gears of cylinder.

Figure 1.3 shows that these methods of supporting the blades cause, when they are used alone, fornies of m; so-called retro rotary ichines, in inducxions by poly induction 1), several induction grids are mounted on a crankshaft master and coupled to the same gear dF support.

Figure 1.4 continues the rappe: started in 1 In b of the figure, we give exe nple doubled n gears Figure 1.5 motre in a, b, c, nc of the figure represents the three main types of senii transmission. Semi-tra ismissiona are induction from center to center they are accelerative, inverse, or inverse w, Figure 2 of the present invention shows how induction is achieved by gearing intermediate with the use of gear wheels.

Figure 3.1 shows how) n generalizes the improvement of poly induction standard.
Figure 3.3 shows how to bring standard dynamics back into dynamics tuebibatives and vice versa.

Figure 4 reiterates in a) our 1 previous work, in which we have showed that making intermediate gears whose support axis was not rigidly fixed hard the crankshaft, but rather to a pivoting memeber, one managed to produce a arming by performing a rotary actuation 1 of the crankshaft.

Figure 4 shows in b some technical additions to the arming method delayed Figure 5.1 gives additional examples of geometric addition by addition.
planetary line or angled Figure 5 (b) shows an exe sample, where b is here again, to achieve the central induction of the type mo io post rotary induction.

Figure 5.2 shows a three; th e complementary example, we realize a induction master gear heel.

Figure 6 shows that it is possible to reengineer the teeth of the gears of such way to falcify the reports of wholesale; past, while preserving their report of difference in size 80 and leu - number of teeth.

Figure 7.1 recalls the different methods that we produced at this time.
day for reduce the difference in force between the opposite parts of the blades, reducing the force derotatiot reports. orientation of the blade with respect to strengths rotational crankshaft Figure 7.2 reminds us in d that if we perform a reengineering of the provision of teeth of the gears and distancing the teeth of one in such a way power in increase the size, we can increase the size of two gears entering an induction, thus reversing axially the anointing of the gears, while not changing their size difference, as well as the ratio of their number of teeth before corresondre to the number this sides of blade and cylinder.

Figure 7.3 in g shows that the curvature of the cylinder is accentuated by the reduction the size of the blade, this curve can be softened by the use of segments swivel. In h of the figure, oi, shows that if one installs in the part previous the blade of a rotary motor, a pitch mounted on springs 104, and said piston absoerbeurs, this one will absorb the blow of the e. : plosion and will restore it in the course of descent, transferring a part of this energy to the 1 artie front of the blade, which is more mobile that part back.

FIG. 7.4 shows the hoop gear induction method 105, more especially when it links the support gears and induction is a chain.

Figure 7.5 shows that the polycomation methode is also a very method effective control of the orientational rotational power of the blade and its conversion into rotational positional power of the crankshaft.

Figure 8 shows that all s the method of modifying the ratios of strength orientation and rotation can be used and realized in combination. In a, we have an induction machine by chain engage, and moreover of type Polycamée Finally, this niotage receives> urplus pivoting segments In b of the figure, we see that there is use of induction with gears induction periphneric and flat support, this being done with a poly camation and a their misalignment, as well as a change in the shape of the piston.

Figure 9 shows that the crown and support gears can be connected of a poly induction by intermediate gears of different sizes, this driving the retrofit of the gearing at the same time as its planétérisation. We can therefore link the lx to this gear.

Figure 12.1 shows that, with these contributions, we can redraw the blade design and of the cylinder. All these methods of balancing forces redesign curvatures of the cylinders and pe them in such a way to accept the energy produced by rearward parts of the blades, and dirr, simultaneously leverage before this one, this which will decrease the friction, and it all the more so as the crankshaft of these machine are already, at the level of the speed, sir solicited. to the use of segments pivoting, as shown in Figure 12.2 shows that one can make sure that the pistons, will aborber the rear work of the p's, and maxiimize his work before.

Figure 13.1 shows that to .is the methods of modifying the ratio of strength orientational and rotational can be applied in kinetics turbinative ..

Figure 13.2 shows that the pa e and the cylinder, re can be linked indirectly by the other elements.

Figure 14 shows how to perform a semi transmission polccd with a number minimal gear ..

Figure 15 recalls in a) the kinetic slinky motion that we have product previously.

FIG. 16 shows that the axis the positional support of the blade 220 can to be an axis accessory, and thus to fulfill the crankpin function. Since then , the mechanics Induction of the blade could be performed externally on a crankshaft or one exemtric very oiled. The age of blade induction, should therefore to be provided an accessory part, 221 it p -rmettat to be coupled to the crankshaft master 222, and this gearing will be directly, ot by the use of a third party being fixed 223, connected to the light 224 .. This will allow to carry out the oiling of the crankshaft master way important, while at the same time compressing and mechanically best way, celi decreasing the losses of sealing of hules of these ci.

In the machines of the prior art, the resistance strength of the materials necessary in the The type of mechanics used is necessary to obtain resist the friction resulting from oversupports that the blade, and its contortions on the gear of support and this, even if it was housed close to the blade .. But these friction being practically canceled, we can then arrange the blade on a crankshaft crank pin 225, inserted into a wrist 2:: 6, before the blade and the cylinder are posed.

Figure 17 shows that we can manage the gas inlet of rotating machines of many ways.

Figure 18 shows in a) that in the standard niachines, since the blade work negatively on its amiè -e part, it grows it in such a way to soften the curvature of the cylinder has a point: such that this curvature is attached to that of the pale, 'in the first part of the descent,:, making in this sevtion the explosion innefficace.
As mentioned above, this can be corrected by the use of floating swivel segments, 1 that we can draw the curvature of the holding cylinder account of this ability of piv:> ment. This curvature can be adoucire.

Figure 19.1 is reminiscent of a figu-e of our previous control vestiaux Orientational blade by support gear (ynamic and planetary.

In b, of the figure, a central retrorotative mono in luction also allows what we fix the idling gear to the same axis or directly to.
the gear of support of the mono induction, i; ette time ci post rotary machine.

Figure 19. 2 shows that this is possible for any induction.

In b of the figure, the atrial inductance is also an induction by hoop gear, and gear blade induction the peripheral planetary support a induction by intermediate gear.

Figure 20 shows, once d; more than that is possible for any combination induction.

Figure 23 shows other similar figures, this time made with the recourse to semi gear transmission pign:) ns plnaétaire -FIG. 24 gives another example of induction by support gearing.
pérophérique planetary. Here the induction of cenre is an induction by mono induction retro-active, and the induction of a blade inducting by intermediate gear.

Figure 25 shows the combina sound of two post rotary induction. Indeed , right here the support gear of the first induction is of external type and its gearing induction of internal type. .

Figure 26 shows, if we have the best ways to apply induction BNPH
Peripheral support gears for turbines.

Figure 27 the center sipip gear, rigidly attached to the body of the machine is internal type. The induction gear that is coupled to it will be connected here regularly support gear periphery of cylinder and blade.

Figure 28 has, reminds us of heel gear induction, and proposes that she might also be interpreted as a toilet induction superposition resulting in planetaryization of support gear.

In b, of the figure, and this always on the same principle as previously, since , at the same time the planet, blade, and cylinder support gears, are connected from rigid way to the gear of inc citon of the central induction.

In FIG. 28, an induction mixture is produced in a different way, that is to say not, as previously, by tripled gears, naais, by double doubled n gear.

Here the central induction support gear is of external type, and gear Peripheral induction is of internal type, and it will be coupled second gear internal, which will be considered as a peripheral support gear common to two blade inductions and ci, lindre the engree ionduction type Irternate feeds two dissecting inducion.

Figure 30 shows that induction horns by gears peripheral devices planetary can also do 1 part of the inductive étagenient, and so reduce Oriental contortions that they entail.

Figure 31 shows a case in which the intermediate gear from induction to its axis in the center of the machine, the support gear simultaneously gearing induciton of the peripheral induction, or else the intermediate gear of a senv transmission.

Figure 32 recalls that the use of polycammed gears for cases détagement Induction also cancels in a significant way the distortions orientation of this type of machine.

Brief description of figures s: second part FIG. 33 shows in a), dane, a rotary machine of standard type, the retro deployment rotationally of the blade on itself during its rotation around the axis central crankshaft.

In b) of the same figure, we can see that the double movement reaches its maximum degree in the middle of the descent, thus dragging the convex shape of the center of the cylinder.

Figure 34 shows three machine degree elevation exenples rotating when these are performed with standard kinetics. In a), we see that the superposition of crankshaft makes it possible to increase the elevation of the blade at the end of its climb, and reduce the penetration of the PC inte of this one into the corner of the cylinder during the descent. In b) of the same figi ire, it is seen that polycamant gears induction of the blade, it is possible to produce>, accelerations and decelerations of the retro movement rotation of the blade in relation to its eccentric during the descent, this which modifies geometrically the shape of the cylinder, and which kinetically deports the moment of the explosion making it favorable: to sleep the blade during his dead point.
In c of the same figure, the intentional misalignment of one of the crankshafts makes it possible to increase again the positive variations of the curvatures of the cylinders, and the case the angulation these ..

Figure 35 recalls the basic considerations that allowed us to achieve machines turbinatives. From the beginning, the rotational speed of these machines is not increased, as in the previous ones, but rather subdivided, then distributed between the blade and the cylinder.

Figure 36 shows a realization of the turbine machine whose kinetic is between those of the more pola expressions. res, the turbine-powered turbine translational and standard naachine dynamics, and realizes a hybrid dynamic whose shape virtual is eight sides, which makes it possible to produce eight compressions per revolution cylinder. (1 explosion at 8 explosions) Figure 37 recalls that it is possible to increase the degree of rotativity of these machines.
In a), first of all adding a degree of rotation of the blade induction.
For example, here, it will move from simply to triangular-translational In b, it is shown that one can, in another way, increase the rotativity of the cylinder and to bring him to become himself. In c of the figure, we see that the deformations of cylinders made by making them possible can be accentuated by a increase of rotativity, for example by the axation or overlap of inductions.
In d, we see that the cylinders can also be modified by using gears polycamés Figure 38 shows how to mpleat the three major induction methods Parties compressives of turbulent machines when they are made with planetaryization of each of the compressive parts and shape cylinder realization swivel rotary.

Figure 40 recalls our invi ntion in which a series of cylinders was willing in the blade of a rotary engine, each of these cylinders receiving a piston, connected by a connecting rod to a crankpin integrated between the original excenti ique. Here, the crankpin is no only arranged according to a center farther from the center of the crankshaft's axis of rotation, but also be more before, or further back than that of the center of the eccentric. The figure show me how to realize a phase shift of the compressive elements of a turbinating machine, here Translational.

Figure 42 shows schematically, all the movements that can be made by a compressive part, either in a) the rotational movement b) the global movement c) the oscillatory movement d) the stepped planetary gear e) the simple tranlational movement f) the translational movement g) the polycatné movement h) move to contrary inductions in the dish i) the movement with opposite induction in the convex part j) riding on horseback Figure 39 shows several possible possibilities for rotating machines and turbines.
Figure 40 shows that all ~ post rotating and retro rotating figures can be made standard to 1), curved to 2), or balloon to 3) In bl, b2, one vozt that further increasing the induc tions of standard machines, by crankshafts and by polycamation, the cymes are made angularly.
In b 3 and b 4,1 we see that these cylinder, so to speak third degree are also achievable for turl-in-motion machines, by polycamës gear, and by overlap inductions.

Figure 41 shows that these mi ~ difications of cylinder shapes are also possible for retrorotative machines.

Figure 42 shows that all blade figures can also be used, either by paddle simple in a, multiple blades in 1 ~, or by palic structure in c.

Figures 43.1, 43.2, 43.3, 43. ~, 43.5, 43.6, 43.7, 43.8, 43.9, including achievements more detailed de fi nitions obtained not overlapping inductions Sumptuous description of the figurations 3 part Fure 44 shows that 1, we can install a magneto directly on the cylinder and connected to the candle, The figure shows in b that bot bot can be connected by the use of a wire from induction to a point rigidly and isolated laughs arranged in the side of the cylinder.

Figure 45 shows that the end of the thread of the candle can be equipped with a broom mounted floating <. on a metal donut, fixed rigidly and singly in the cylinder wall for this purpose the cylinder being rigidly fixed to the housing.

Figure 46 shows that the same procedure can be used to feed the candles that will be located sar 1 (: piston of the machine Figure 46 shows that pa can be iastalled directly on the cylinder for the refroirdir.

Similarly ,. In b, we can see that cooling dissolves can also to be installed on the cylinder In FIG. 47, it can be seen that the cylinder disks can be intertwined with crankcase disks, so that it can be better loss of heat from cylinder mania In Diagram 48 we show in a) that the water pump, if necessary maybe erected planetary and rerégée to the cylinder. In b, this one will be realized by a In (c) we see how the liquids will be exchanged.

Detailed description of the figures: first part Figure 1.1 provides a description of the terms we use normally to comment on the rtative and turbinative machines In, a, and b, we represent x inductions. The inductions are set gears entraining the planetary retraction of an element induction includes a supr ort gear. In simple inductions, or in inductions composite induction masters, these gears are attached to the body of the maachine 1. The coupling point of these inducti) n is called armament. 4 In the case of mechanical by semi tranmission, as shown in c, the arming 4 is reduced to the axis of support 5 of the inverion gear 6 of the transmission itself. In the inductions composed, d and e a second support gear can be phrpheric or on the one hand rigidly fixed at the crankpin of the visilebrquin 6, oi, else by mounted planetarily on a sleeve of crankshaft.7 The induction gear 8 is generally in the inductions first degree, rigidly attached to the piston or to the blade of the machine. In the inductions compound, such as in f and g, it is rigidly connected or is itself simultaneously the peripheral support gear 9 of the second induction.

Figure 1.2 shows that in the; turbines, as recalled in g) 11 cylinder gears are also applied induction gears of cylinder. The intermediate gears 12, where i to cerceaul3, these gears bind, in some inductions the gears of so port and the gears of inductions engnages crown 13, as found in the seniio tnsinission to crown or dan the poly inductions as shown in b) they are generally type gears internal.
binding several intermediate gears of same size or size different polycopy ten gears, mc ntés in i), or accelerated decelerative gears are engrnages whose forms are not circular, but are rather similar to forms geometric basic, triangle ,, square, ellipses. Post inductions rotary mono induction, in j) are induci ions in which the connection of a gear type of blade Integral to an external type carrier gear is direct. These induced induction usually post-working women. Induction retrorotatives to mono induction, in j) are realized pa - the direct connection of a gear of type support internal to an external type of gearing.

Figure 1.3 shows that these methods of supporting the blades cause, when they are used only, forms of so-called retro rotary michines, in the inducxions by poly induction 1), a plurality of induction gears 20 are mounted on a crankshaft master 21 and coupled to the same carrier ige 22. These induction gears are equipped crank pins 23 on which the blade is arranged. When the gears support of these machines are of type exter ~ s 25 the mechanics realize fomers of machinery post rotatives 26. When the support of these machines is internal type 27,. these mechanics make these machines retro-style machines rotary 28.

Figure 1.4 continues the report 1 at 1 in E (a).
inductions by force posterior and by anterior force, or said on a springboard, or in scissors, distinguish according to that the work of the blade is carried out pre-venously on the front or on the back of the blade, the opposite part eni rant in mechanical lock Mono insuction and poly are, in the case of post-rotating machines, inductions to posterior force, whereas the other inductions,; have anterior type.

In b of the figure, we give exe nple doubled 30 .L: es lined gears are Intermediate support and / or induction gears in duplicate. II
is gears attached to each other; and turn on the same axis, one being trained, by a gear, and the other is going one too. These doubles can in induction, or still in the semi tramnission.

The figure 1.5 motre in a, b, c, n, of the figure represents the three main types of semi transmission. Semi trai tsmissiona are induction from center to center eites are accelerative, inverse, or inverse, Figure 2 of the present invention is known to achieve induction by gear i intermediary with the use of gear gears. Induction to pinion gear will be achieved by inserting into the aachine a support gear type to pinion.36 On will then realize a pair of intermediate gears 37 38, put together between them by a way. rotary 39 and we couple ra gear blade it also provided with a gear to pinion 40 to the second engrenafi e double gear gears intermediate.

Figure 3.1 shows how to generalize the improvement of poly induction standard.
In the original poly induction in a), it is known that the rear induction 41, producing in course of descent a mechanical lock 42 behind which the blade, like in the Inductive rotary motors m (no inductive, had a negative effect ,.
blocking could be attenuated by geoxetric addition 43 achieved by lengthening the connecting rods with respect to subsidiary crankshafts, including: induction gears, and gearing spport have were shrunken.

As shown in b) This induction was improved by subtracting partially or all of the teeth on certain parts of the support gear (or induction), during the blocking period, thus letting the blade work only on the crankshafts before.

In the present invention, we are inspired by the mechanics we have already produced, with the rotatably mounted intermes-dynamic translational turbulence, if crank pinions are fixed rigidly in the side of the machine, to apply them dynamically to standard rotary machines, or to turbines, the blade is not pale sitrictly Translational. As we recalls in o, in the turbine machines, the gears were coupled to a crown .
In fact, we can see that if we think about this mechanics in dynamics, we can improve the last method by poly indu ~ tion all the while by adding, around gears Induction a 45-speed gear, which will therefore bind them by outside.
It can be noted that this crown can be realized by means of a internally but also a chain.

As a result, we take into account, as shown in d) that induction can to be improved, once again, producing a doubled gears intermédiaores added geometrically. e first inter-intermediate gear 46 will be mounted on three external external gears, themselves mounted planetary on a gearing of support.

The inner gear in crown -1 47 and its doubled 48 will therefore trained rotationally forward.:, e second internal gear will result in therefore the gears of secondary crankshafts 49. This way will be reminiscent of already used turbinative manner and here generalii: e to rotary poly induction machines . These contributions important because they allow, once again, to prove that the poly induction can be carried out without counter-faith these backs on the blade, and that when these methods are used in translational and non-translational dynamics, these against efforts are also canceled. Indeed, the ini er of these is to cancel totally the counter effect mechanical mechanisms, because the induction gears of these are not not directly but rather by geometric addition in angulation, in relation to the gears of support Figure 3.3 shows how to transfer standard dynamics to dynamics tuebibatives and vice versa. Gg, .ally the induction engrnage of cylinder 50 in type turbina.tif, deviuent the engrenaj; e support 51 of the machine, and the gears of support 52 of the turbine machine 54 become the gearing intermediates 55 this time fixed on the crankshaft u.in master and coupled to the gears of inductions too rotatively arranged on the m sockets of the old machine master trainee and supporting the blade by their crank pins. fixed,.

Figure 4 recalls in a) our previous works, in which we have showed that making intermediate gears 56 whose support axis was not fixed rigidly hard the viiebrequin, nains rather to a pivoting memebre 57, one succeeded in produce an armament by performing a rotary action of the crankshaft.

The figure shows in b some technical techniques to the arming method delayed In a, we recall that the delayed payments made with the use of this method could be obtained by installing the intermediate gears on supports pivoting, with members of blockages. This has the effect of specifying that intermediate gears may also be installed on mounted axles on parts sliding made in conjuncion or even the crankshaft. In first case, by For example, the sliding parts are made in such a way crochet at crankshaft and to the axis of maneto n.58 In a second m.aziière, a slide is inserted in the crank shaft, and a member supporting the gear intermediate is there committed to tell how to let that gear gears of support and induction, but so aw so as not to let him stand distance. 58 Finally, let us add that deferred items can be realized for all induction. , such as hoop gear induction, for which will rintall the barrel support of this gear was a semi free member, as those already commented for the intermediate gear of the intermediate geared luction. note also that Peripheral support gears can also be installed from the same way, either with a revolving vilax, an axle oulissant or other technique, connected with non-rigid way main crankshaft.

Figure 5.1 gives additional examples of geometric addition by addition.
planetary line or angulated As we have shown in our previous work, the planetary induction gears allow to positively modify the work of support gears, which in conventional machines is negative.
In the present invention we wish to:, specify again that all the inductions can serve as an induction errtr tnt in the induction composition to gears of peropteric support, and that the lined induction gears suppport can be internal only, external only .enzent, or external internal.

A first example, in (a), is to produce a mono post induction rotary induction, 60 and a mono induction retrorotative as Peripheral induction.61 In this case, the internal type induction gear 62 is rigidly fixed to a gear 63 of external type support. This gear induction is rigidly coupled to a planetary type support bracket 64, internal type 65, who will govern the gear; external type induction of the blade 66.

It will be noted that the initial induction can also be angulated 67, as we have it shown in our previous work. In addition, it can be noted that this can also be realized on a free crankshaft, even in some cases, without crankshafts the suppor: peripheral induction gear is simply a gear of laison of fixed support and blade inductrion gears. It will be noted that the crank shaft governate the induction of center may be ddfférent the viulebrerqui governing the induction of blade, by semi lib e compared to the ui, which will allow armament different, as for the cases, previously intermediate gears to position fliexible.

Figure 5 (b) shows an ex-dpleple, where b is here again, to achieve the central induction type mu io post rotary induction 70. This time we will fix the induction gear of the central power a second gear type external 71, which will lead to a peripheral induction also of mono inductive type post rotary 72 Figure 5.2 presents a third complementary example.
induction master by gear heel. 73A retro rotation of the induction gear of this induction will cause the planetary gear gear 74 to shrink back who is fixed. Once again, the blade will be able to be realized with a higher dimension, with a post rotary induction i 75 In d of the figure, we find im fourth complementary example will be made in producing a reorientative poly induction, 76 the plae will be replaced by a gear type external. This retrorotational planetary gear can to serve of support gear at pal 77.) As can be seen, all inductions can lend themselves to this type of storage, combination, and the result is always the same, namely, a reengineer e of the balancing equilibrium on the blade, which will leads to a desperate desire for better dynamics. In all cases of figures, the point of opening, oi of hinge, of the blade is pushed towards the back, and the pale works on all the surface of his side.

FIG. 6 shows that it is possible to reengineer the teeth 78 of the gears of FIG.
such way of improving the size ratios of the last 79, while preserving their difference ratio of big ir 80 and their number of teeth 81. We could so back off the arming point 81 of the enfoldings during descent. In the figure we show the ratios of size and dmts satandard gears. In good shows that differences in size were preserved, as well as their tooth ratio.
But their size has been modified.

It should be noted, in addition that the teeth of the gears may be modified from different ways, such as to imitate the effects of the use of gears polycamés.

Figure 7.1 recalls the different methods we have produced at this time.
day for to reduce the differences of fon es between the opposite parts of the blades, reducing the force of orientational derotatio ratios of the blade with respect to strengths rotational crankshaft In a 1 and a2, we find the n ecanique by gear hoop offset, and realized with the use of a chain. In both cases the rotation or derotation of gear induction of the blade under pressure causes traction 83 of the chain or the hoop gear which is rotating in rotation of the crankshaft.

In b, we find the realization of gears of support and induction of type plolycamés. As can be seen, when the gears are placed in a certain position, they cause B5 a recoil, going down from the point d, armament negrenages In c of the figure, one finds a method by arming on point of support not fiuxe.
As we can see, al Drs that the arming of the intermediate gear should to be its support axis 86, this; it becomes rather the other gear 87 this who trains negation of negative forces that could have been generated by a rotation of gear induction.

Figure 7.2 reminds us in f, that if we perform a reengineering of the provision of teeth of the gears and distaning the teeth of one 90 in such a way power in to increase the size 91, one will increase the size of two gears incoming in an induction, backing away if the arming point of the gears 92, any by not not changing their size difference 93, as well as the report of their number of teeth 94, before corresondre u number of sides of blade and cylinder.

In e) of the figure we give still another example of induction staged with doubled d, peripheral and planetary gearing and induction gear. Here, the first induction is a detorotative mono inductive system 95 composed of a gear of support internal type 96 and an external type induction engrage. 97. At this gear will be rigidly securing the planetary gear 98 of the machine, on which will be built an induction by intermediate grooming 99. As can be to note, the ostional effort of the pali is over-ordered, compared to his effort in one machine, and consequently, this lack of orientational power himself transofrmentra power of rotation of the vilebrrequin, this respecting the thermo point dynamic.

In f of the figure, we show qw if we link the dynamic support gear of semi tranmission by springs 1U) to the transmission axis, we will so that the attack the crankshaft is always more powerful than the orientation attack.

Figure 7.3 in g, goes up only if the curvature of the cylinder is accentuated 101 over there reducing the size of the ruler, this curvature can be softened by the use of pivoting segments 102 In h of the figure, we show qi Ge if we install in the front part of the blade of a rotary motor, a piston mounted on springs 104, and said piston absoerbeurs, this one will absorb the blow of the explosio i and restore it during the descent, transferring a part of this energy to the e share before the blade, which is more mobile than the back part.
FIG. 7.4, recalls the hoop gear induction method 105, more especially when the element linking the support gears and induction is a chain. 106. In this type of induction method, during the descent retro force Orientational rotation shriveled on the blade does not succeed or less produce a rotational force in lever on the crankshaft. This effect is neutralized because the force transforms into traction.
rotational Orientation of the blade on the same drill this turning of the crankshaft.
In Consequently, the crankshaft rotation forces, even by filming of the blade on itself are super strong with the rotational forces of the blade on herself.
The blade works so much, better.

In the same way, if the machine is made by gear induction hoop, and that care is taken to correct this (gears, modifying its support barrel, or / and add a third gear 108 the orientational rotational force of the pale will tranfy in force of tractioi E, and will lead aisni the rotational force crankshaft master to be superior to faith this orientational rotationelle. The contradictions of the machines will accordingly; also not only strongly attenuated, but aus surplus tranformets in crankshaft of crankshaft.

Figure 7.5 shows that the method by polycania.tion is also a very method effective control of the power, rotational orientation of the blade and its transformaton in rotational po> itional power of the crankshaft. She can be used in multiple places in rotary machines, in machines rotary piston, and in piston machines. ~, with the use of poly cam gear, we falcify at the times the rear dot of the blade 109, 110, and falcify momentarily his speed of rotation compared to crankshaft. We therefore falcify form of cylinders and forcibly the modynamic thei of the machine. The gears polycamés of blade and cylinder can be arranged in different directions can be in the direction of the cylinder or in direction. In all cases, origina, lities of this method of support considers that the point of armament is at a distance variable from the center of the machu e. Therefore, tal than shown in a and b of the figure , rear arming, during descent, can be produced closer to the center, or more far, depending on the initial orientation of the gears. In this last case , the rear armenient in the process of descent, the blade is prevented from escaping back and transform into rotational forces; i on the crankshaft, and in addition to diminish the crankshaft compared to vitess retrorotating the blade, which reduces the Differential contradiction between these parts.

Figure 8 shows that all the method of modifying the ratios of strength orientational and rotational tools can be used and realized in combination. In a, we have an induction machine by chain rebar 120, and moreover of type polycamée 121 - Finally, this wording is included in the surplus of the pivoting segments 123.

In b of the figure, we see that there is use of induction with gears induction Peripheral and pediatric support 124, this being realized with a poly cama.tion 125 and a misalignment thereof 1A '6, as well as with a modification of the form of piston. 127 We wish to repeat that all the inductions can be used to realize these types association of inductions. Cojune we listed nearly twenty inductions different, the combination will achieve nearly four hundred. It is by consequent impossible to list and present all these inductions.

FIG. 9 shows that it is possible to link the crown gears 130 and support 131 of a poly induction by intermediary sizes different 132, this causing the induction gear 133 to be reversed at the same time as her planétérisation. The blade 134 can therefore be connected to this gear.

In this figure, it is shown that the support gears may be arranged on their element indirectly, either by the recesses to springs. 135 This will allow, mainly in semi-transmission or induction method down, at this that the crankshaft attacks the plane before the cylinder.

Figure 12.1 shows that, at endu these contributions, we can redesign the design of the blade and of the cylinder. All these methods of rebalancing forces make it possible to redraw the curvatures of the cylinders and p islands of such nranière to accept the energy produced by rear parts of the blades, and din both simultaneously leverage anvant of it, this which will reduce the friction, and, all the more so as the crankshaft of these machine are already, at the level of speed,; ur solicited. This rebalancing of energy on the blade increase the possibilities of (.esing of it and will allow to draw a better thermodynamic energy efficiency.

Among the main modifications that can be made to the cylinder, II
there's one accentuation of the curvature 14), and a subsequent correction 141 pernicious by resort to the use of pivotal segments 142, as shown in a, it is necessary to also add that the use of this type of segm: nt reduced the length of the blade without increase corner formed by the meeting of the cylinder ares, which allows, of another way, to mitigate the defective orientation reports of this type of machines relative proportions required: gears necessary to achieve the required support, in mono induction.

Figure 12.2 shows that we will be sure that the pistons, or blades, will aborb the rear work of the blade, and maximize his work before. In Therefore, we will release the rear part of the piston 143 poi xy allow expansion of the explosion, and we will increase the volume of the cylinder in the piracy before 144, so that the explosion is more powerful. To do this, pre-erence, desinera the cruset interior to piston 146 of such that it is not m equal width 147, but while holding account that his depth 148 allow parto was a good explosion and a good expansion of it.
Figure 13.1 shows that the methods of modifying the ratio of strength orientational and rotational can be applied in kinetics turbinative ..

In our work on turbines, we have specified that existed three large subcategories of medical devices permitting the correct activation mechanical parts of the machione, pale cylinder and crankshaft and support gear.

In this figure, we will show that the balancing methods of energy Both rotational and rotational can be used in any induction of machinery turbinative. It is important first of all to mention that during pale inductions and cylinder differentiated, that is to say, whose crankshaft is the element between those here, there is little contradiction from blade to cylinder, except that produced by the segmentations.
It can even be used to this induction induction cotrôle of pale, to adjust perfectly fine.

In a) we will apply a deferred rutting to a mechanical bound by the crankshaft 151, the latter coi.umandant one by one mono induction leading to the governor of the blade, and an invert transmission, leading to the control of the cylinder.
First of all, it is important to mention that during pale and cylinder differentiated, that is to say, doni the crankshaft is the common element between these, we have little contradiction from blade to cylinder, except that produced by the segmentations. We can as well as to use any inductance in orientational cotrôle of blade, for adjust perfectly the machine.

Moreover, whatever is possible that the training phenomenon does not make not necessary to modify the induction associations through the use of the pale, it's up to say rising inductions, we think that in these cases also, we able to carry out all the inductive activities with recourse to control methods the orientation of the blade already en) ncées. We will talk about induction polycamé descendant, in teething calibration, by chain hoops and so on.
We will talk finally of induction with planetary enlrehages of the inducton of cylinder. For this As for the rising inductio, we will install on the manchine of the crank shaft unaxe allowing to receive li double induction induction gear perispherical and support of central induection, and we connect them lauer induction.
In b of the figure, it is not necessary that the induction of blade can standard house, here for example by mono i iduction, the induction of the cylinder, here a induction descendant 154, can be done with a control modification Orientational induction, here by gearing p Aycamés 155 Finally, in the following, we note that when machines are linked by the dynami support gear read 156, we can as is the case here, manage that this cnamic support gear is the support gear of a induction of which the value orientaitonelleelle mo mo, lifiée, as for example here, by securely deferred. 157 Figure 13.2 shows that the p of and the cylinder can be linked indirectly by the other elements. C) as we have already mentioned, liaison of the Pipe and cylinder inductions in the turbines can be realized by the means of the crankshaft, the eng = senvi transmittive support gear, or by the blade.

It would be advisable to add two other means of liaison, , one of semi transmissio n elements, for example the inversion gear,, or again, planetary gears, which can be seen in the downward inductive as well activate, when split.

In the first example, the crown gears of the semi-transmission 170, when they are crown, I will be split, and realized in one single piece with 1, the support gear of the pa le, one of them can then activate the support gear dynamics of insduction and 1 '. the cylinder, These two gears crowns will be activated by gearing: intermediate to coalesce different, and thus achieve different rotation ratios.

When the semi transmissions will be carried out by gear gears 171, gear of inversion can be carried out 4 in the split way, and one of these gears will be able drive the gear of the axis this rotation of the support gear of the machine, while that the other will cause the engrena ge of the cylinder By the way one of them engrena.ges read doubled gearing of the rising induction at planetary gears to be able to serve as a gearing gear gear induction of cylinder, which will then be either internal or external type case.

Note also, in last year; that crankshafts induction lower can be in some cases free, and rc held strictly by gears induction, poly induction, and semi-free, in other inductions, that is to say retrnus by the gears, and by a retention arm, and similar to the gearing Intermediates of induction by intermediate gears.

FIG. 14 shows how to realize a semi-transmitted transmission with a number minimal gear. As we have already pointed out, we can use the gears poiycamés in you part of the machine, nzontante induction, down, or in semi-transmission) to niodify gear ratios of the vilegrequin and of the blade between them, and consequently of the blade and the cylinder, in the rotary machines and turbines.

In the case of the cylinder, it is obvious, as we have shown for the governs blade of semi turbines, which can for example be polycamer several gears intermediates 190, the gear horn 191, or conversely, ebntel that shown in b) the intermediate gears e: 190 the support gear 192, and by this Game d, gear, get a circular rotational motion but accelerate decelerating bet that will be linked to the axes 4 the intermediate gears.

Here, we can simplify the invention by showing that we can the support gear 200 an intermediate gear 201 to which will be attached a second gear intermediate, this time polycammed 202. If,> n torque to this polycammed gear a second gearing polycamé driven 203 rotation -llement, and this in such a way that the center 104 of this second gear polycamé co incides with the center of rotation of the machine and cylinder 205 to which it will be attached, we will obtain a movement of cylinder accelerometers decelerative research.

Figure 15 recalls in a) the movement of kinetics slinky that we have product previously.

In this amchines, as I am b) the cylinder 210 must be made of way decelerative accelerometer, by con; eqeuent, the type of transmission of gouvergne upper utterance 211 can be used for the integer. By the way, the planetary niece piston 212 go through the center 213 and must not produce bulb on the periphery 214, what would produce an andard planetary action. This is also possible in connecting its axis 215 to an inductive gear also has polycamé 216.

With such a set of gears, (n will succeed in producing with a single piston, the work of several pistons, and that without it, which will ensure the smallness of the systènye.

FIG. 16 shows that the positional support axis of the blade 220 can to be an axis accessory, and so to say er unplir the crankpin function. Therefore, the mechanical Induction of the blade could be carried out on a crankshaft or one exemtric very oiled. The blade induction gear, must therefore to be provided an accessory part, 221 it) ermettat to be coupled to the master crankshaft 222, and this gear will be directerrarnt, cu by the use of a third party being him fixed 223 connected to the light 224 .. This will affect the oiling of the vîl.ebrequin master of nlanière important, while isolating the compresive and mechanical parts of best way, celi decreasing the sealing losses;

In the machires of the prior art, the strength resistance of the materials necessary in the type of mechanics used is quite necessary to allow for resist the friction resulting from oversupports of the blade, and its contortions on the gear of support and this, even if it was housed close to the blade .. But these friction being practically canceled, we can then arrange the blade on a crankshaft crank pin 225, inserted in a wrist 2: '6, before the blade and the cylinder are posed.

FIG. 17 shows that it is possible to manage the gas inlet of rotating machines of many ways.

In c of the figure, we propose that the head of the piston will be equipped with a leads 234 allowing the training of the gases to penetrate into the cylinder by this leads. As to the spent gases, they can penetrate through another orifice 235. A conduct Release, practiced in the piston to the side of the cylinder can also enable to generate it.

In, it limits the output of the burned back gases of the machine, modifying their place of exit. One could also produce, by a set of valves an injection successively, which allows the gaseous gases are first integrated in the cyliundre, so in before that him, the used gases, by the following +:, therefore back. This will make an explosion lower quality back d; the blade.

Figure 18 shows in a) qi e in standard machines, since the blade work negatively on its rear part, we enlarge it in such a way to soften the curvature of the cylinder has a curt t such that this curvature mounts to that of the pale, 'in the first part of the descent -, making in this sevtion the explosion innefficace.
But the price to pay is a defective crankshaft ratio, that is to say in which the crankshaft is too small. By 1g: s different dynamics that we have shown, one can make work on the back of the positive blade. Therefore , we can accentuate it by accentuating, for the same blade, the size of the vilebrequihn., which will lead to a more acute realization of the meeting ares forming the cylinder.

As mentioned earlier, this can be corrected by the use of floating swivel segments 24 D, so that we can draw the curvature of the cylinder in taking into account this ability! pivoting. This curvature can therefore to be softened.

This will not only help satatard machine curves, but also those of polycotated gear machines 242, which can also, by their nature, and according to the the orientation of the gears to have a larger crankshaft, and a blade scaled down.

In this figure, we 2 joustons that if these segments are realigned in a way unequal, we will deport once more this positively the thrust orientation towards the in front of the blade.

Figure 19.1 recalls a figi re of our previous control Orientational blade by support gear, lynamiclue and planetary.

Ic support gear 400 + 401 poly induction, is rigidly fixed to the gear induction circuit 402 of a retrotrotative mono-control device whose gearing support 403 is an internal gear.

In b, of the figure, a central retrorotative mono-duction also allows what we steadily fix the id gear 404 to the same axis or directly to 1 enbgrenage support of the mono inductic n, this time post rotary machine 406.

Figure 19. 2 shows that this is possible for any induction. Thus, here is recalled Figure 1.1.2 of our p. = edents work, in which it has, induction Central is a gear induction this piece 407, the gear gear inductio planetary peripheral a rotational postindependent inductor 408.

In b of the fig, the c? Ntral induction is also a gear induction hoop 410, and the blade induction with a planetary support gear induction by intermediate gear. 410 Figure 20 shows, once (as much as possible for all combination induction.

In a, we have an induction by er. standard intermediate grading.41 1. In a 2, we realize a planetaryization of the gear% the support of induction by coupling it to induction by mono induction retrorotative.

At 3, the machine is made using the intermediate gear as center of turning of the viulebrequin 413, which makes it possible to carry out the strategy previous way even more condemned.

In b 1, the induction is a hoop gear indi ction. 414 Eb b

2.1 's gear support 415 of this induction is coupled to the induction gear of a induction by mono induction retrorotative. ~ 16 Figure 23 shows other similar items, this time made with the recourse to semi gear transmission by means of phiaetary gear. In a) the inversion gear has climbed planetary 418, and consequently the support gear 419 in a way accelerated, what entails the eng -enage of induction 420 backwardly 421.

In b of the figure, the gear output 422 of the semi tranmission leads to an induction by intermediate gear 4'A 3, of which the second gear is disposed at the center of the machine 427 In c of the figure, the semio tran: mission has also a output gear offset 428, which allows to train the gearing of an induction by intermediate gear 429 Figure 24 gives another example of induction by support gearing pérophérique planetary. Here the induction of ceil is it an induction by rnono induction retro-active, and the induction of a blade inductic n by intermediate gear.

Figure 25 shows the combination of two post rotary induction. In efpet, here the support gear of the induction plate is of external type 431 and his gear induction of internal type. 4_ 2. At the induction type gear is fixed rigidly a 433 outer-type sua -port gear, which will serve gear inductive induction device 434 to which is connected the blade In b of the figure, the induction of the center is also a mono induction post rotary composed of a 435 external type gear and a gear induction of internal type .366, and to this st induction grinding is attached in a manner rigid one Inverter 4347, which will serve as a support gear planetary to the induction gear 438 of the peripheral retrotorative induction of the machine.

Figure 26 shows, for one, the best ways to apply them.
aapr induction support gears peripheral to turbine machines. Like us l have previously mentioned, the gear mechanism i-mechanics device, or any other method of control can be used in any induction, uplink, descendant or senii transmitti ie.

In the next figures, ni -us will show that 1L, we can appoliques these inéthgodes simultaneously with induction and sem transmission. As a result, onon only the blades, but also the cylinders, will be driven by plankanate induction.

A first example is shown in this figure. Here we find a first support gear, rigidly fixed to machine 600 This gear receives complicity of an induction gear 601 of the center induction, here a gear of typed internal. Central induction is therefore a mono induction post press.
At this engrene induction planar staire will be fixed a support gear of induction of cylinder 602, which will cause the rotation of the induction gear of fixed cylinder rigidly to the cylinder. Through this cylinder induction gear will be fixed rationally to 1, the peripheral gear of the blade 604, which in turn will result the induction gear .605 .. The cylinder and blade inductions will be by both consequent inc uction parmono post rotary induction planetary.

In b of the fogiure we perceive 11 embodiment of the invention in section. Such we can note, the ondiut gear tone of the central induction is fixed rigidly to support gear of cylinder and blade. So we talk about tripple gear induction / support / support Figure 271, center gear, fixed rigidly to the body of the machine is internal type. 606. The engrena ge of induction which is coupled there will be connected here rogidement to the carrier perishing gear of cylinder and blade 608, 609. These last in turn will be coupled to the respective induction gears. , 610, 611, the first being connected to the cylinder 612 and the z utre to the blade.613.

Figure 28 has, recalls noting heel gear induction, and offers that she might also be interpreted as an induction superposition leading to the planetaryization of the support gear 615.

In b, of the figure, and that always on the same principle as previously, since , simultaneously planetary gears of blade, and cylinder 616, are connected in a consistent manner to the induction cleavage 614 of the central induction.
Gears support are respectively connected to the blade 618 induiction gear ety to the induction gear of cylit dre. 620.

There is therefore a triplet of induction gear, suppport medium.

In FIG. 28, an induction mixture is produced in a different way, that is to say not, as previously by tripled gears, may, s, double doubled not gear.

Here the support gear of the central induction is of external type 619, and the gear Peripheral induction is of internal type, 620, and it will be coupled second 621 internal gear, which will be considered as a support gear peripheral common to both blade and cylinder inductions the ion-inducing internal type feeds two different inducion es. Toiuyte d, abor, at the bottom, it feeds , a double d, gears of use 620 that feed the induction gear 622de cylinder 623. By the way, from the top the peripheral support grinding receives i gear Blade induction 624 In FIG. 29, the peripheral device gear, fixed rigidly to 1 gear 631 central induction, drives the cylinder induictin gear, and this last one is itself rigidly coupled to the peripheral support gear the gear inductance 634 of the d-blade induction So here we have a double doubling of gears.

Figure 30 shows that the low gear inductions peripheral devices Planetary 650 may also be part of induction staging, and thereby reducing orientational contortion that they entail.

Figure 31 shows a case lh nite, in which the intermediate gear of induction 700 has its axis in the center of the chimney 701, the support gear simultaneously Inductive gearing of the peripheral indu, or the gearing intermediate of a semi transmission.

Figure 32 recalls that the use of polycammed gears 705 for removal case Induction also cancels out the orientation distortions of this type of machine.

Detailed description of figures part two FIG. 33 shows in a), in a rotary machine of standard type, the retro deployment rotation of the blade on itself 801 during its rotation around the axis central crankshaft 802.

In b) of the same figure, we can see that the double movement reaches its degree maximum in the middle of the descent 803, thus driving the curved shape of the center of the cylinder. This bending is the geometric result of kinetics leading to a loss volumetric 805, this loss lying between there right lowered from the end from the 804 blade to his dead point, and the curvature bomb ~ ~ e of the cylinder that cuts this line.

Figure 34 shows three examples of degree elevation of rotating machines when these are made with standard inetics. In a), we see that the superposition of crankshaft 806 allows to increase the acnter the elevation of the blade 807 during the end of his climb, and to reduce the penetration of the tip of it into the corner of the cylinder 808 during lowering. This double procedure makes it possible to increase both the ratio Compression and torque of the machine. The retro rotary tia.chines become by this procedure achievable with enough pressure to produce engines.

In b) of the same figure, we see the polycamant gears 809 of induction of pale, we succeed in producing celiacs and decelerations of the motion of retro rotation of the blade relative to its eccentric during the descent, this which modifies geometrically the shape of the cyl ndre, and what, kinetrically, moment of the explosion by favorably sleeping the blade during its dead point.
Note that The shape of the cylinder varies not only according to the degree of angulation will give gears, but also according to the orientation of this angulation, which limit can be done in the same sense as that of 1L blade and cylinder, but also in sense opposite.

In c of the same figure, the intentional misalignment of one of crankshafts 810 allows to further increase the positive variations of curvatures of cylinders, and the case appropriate, the angulation of these i. How to use gears polycamé, the dead time in these machines is lengthened and the moment of the explosion deported favorably.
Figure 35 recalls the basic considerations that allowed us to achieve machines turbinatives. From the outset, the dE the rotativity of these machines is not increased, as in the previous ones, but rather subdivided, then distributed between the blade and the cylinder.

As a result, as seen in the figure, the retrorotation of the blade itself in relation to his eccentric axis was going to be orised until each of them was equal to the other. In Consequently, the orientation of the blade 811 remains unchanged in any position for a ride complete machine. This rncification to the planetary action of the blade is counterbalanced by the activation of the cylinder in reverse st 12 and in a determined ratio.

In fact, the initial planetary motion of the blade is subdivided into movement translational and i otational, the former being granted to the pale and the second to cylinder.

Figure 36 shows a realization of the turbine machine whose kinetic is between those of the more polaù zs expressions, namely the turbinative dynamics with pale transitional and the standard machine dynamics, and achieves a hybrid dynamic whose shape virtual is eight sides, which allows for eight compressions per round of cylinder. (1 explosion at 8 explosions) Figure 37 recalls that it is possible to increase the degree of rotativity of these machines.
In a), first by adding a degree of rotation of the blade induction.
For example, here, it will shift from simply nsational to triangular-translational 813.

In b, it is shown that one can, in another way, increase the rotativity of the cylinder and to lead him to become himself a planaire 15. In c of the figure, we see that deformations Cylinders made in planets can be accentuated by a raise of rotativity, for example by the (esaxation or overlap of inductions 814. In d, it can be seen that the cylinders can be modified by use.
polycammed gears Figure 38 shows how to use the three major induction methods Parties compression of turbulent machines when they are made with planetaryization of each of the compressive parts and shape cylinder realization swivel rotary. Usually here, it is a question of realizing, by semi-transmission, or by induction descending, no longer the rotational rudder of the cylinder,: but rather the rudder of the crankshaft of induction the supporting.

In our work on machines; basic turbines, we already have showed that one could list several mec. to better support and guide the blade when of standard kinetics. By the following:, we showed that when these machines were made turbinatively, the oi. always had to carry out mechanical which allow coordinate the virtual movement -1l of the blade and its material aspect to rotational movement of the cylinder. It has been shown that 1) realize u sc mechanical induction of the compressive part and a Inductive induction of rotating rotation 2) to realize a semi transmissive induction of the planetary part, and connect directly the rotation axis of the rotating part to the support gear dynamic of iu semi transmissive lduction,

3) realize a: induction rising of the planetary part, and an induction descending of h, rotational part.

The present invention intends to specify that, when the rotational part has been increased rotationally, and is now this planetary nature, the inductances are not not realized directly on its axis of rotation: on, but on the axis of rotation of the crankshaft governing his induction. So, whatever the inductions used, we will obtain configurations of cordination of these following *:

a) the inductance crankshaft of blade 879, and that of the induction of cylinder 880 are interrelated by semi transfer of information and, as the case may reversive 881 b) the induction of one of the half-lives is of the semi-transmissive type 882, and the gear of dynamic support of this one 883 directly drives the 884 axis of rotation of the induction of the complementary mpressive cc part, c) the induction of one of the compressive pities being a standard induction 85, completed with the use of one of 3 first degree inductions, and the induction of the part supplemented by the use of first-degree induction 887, the crankshaft of this action ind 889 being activated by resorting to a induction descendant 886 made from the complementary compressive part.

In 5b, we can see that we can poch the gears of one of the inductions, for example here that of blade, and consequently still produce there, a machine turbinator with a degree of superior rotativity.

Figure 39 recalls solutic ns of desaxation or cheva.uchement carried out on mechanical piston engines. We have already recalled that dexaxation crankshafts in rotary machines eleva.i; further the degree of rotativity of these niachines and allowed to further delay the ideal moment of the explosion.

In this figure, we show%. in a and b how does this apply with not only two crankshafts and a single compressive part, but with two crankshafts and two compressive parts distine es.

In figure a), we recall our invention engine time-out annihilated. In this version, the sleeve of a crankshaft 817 has two crank pins 818 successively arranged and to which are connected ~ connecting rods 819 and pistons 820 disposed in cylinders successive, but attached to each other at their summit 821.

We see that the dead time of the rear pi ston is delayed compared to that of the front piston.
As a result, the depressive phase is achieved by initiating the descent of the front piston is compensated by the continued rise of the rear piston. As a result, compression remains stable during this period), and the explosion may occur at the end of it. By Therefore, at the moment of exfosion, while the rear piston is at most its dead time, the piston before 'has already passed, and is already in phase of break and descent.

In example b), two quickdraws are connected to two connecting rods 819 and 820 pistons arranged end-to-end of a cylit dre 820. A central gear, or a chain 824 connects the two gears respectively 25 disposed on the crankshaft of such way of synchronize. These crankshafts were initially organized and intentionally of such way that the dead time read of each one do not be simultaneous with the time dead top of the complementary system. In sequence, as before, while one pistons 826 began its descent, the se achieves the completion of its ascent, and by therefore, the compression remains stable over this period of time until that the piston The latecomer has completed his climb. The explosion can then be realized and the piston before will be in the phase of deconstructed - advanced and relevant systemic.

Figure 40 recalls our invention in which a series of 870 cylinders was willing in the blade of a rotary engine, each of these cylinders receiving a piston 871 , refitted by a 872 connecting rod with a crank 873 int ~ '% d between the original eccentric. Here, the crankpin is no only arranged along a center, ~ farther from the center of the axis of rotation crankshaft 74, but also further ahead or further back than the center of the eccentric. The The top dead time of the blade is different from that of the piston, which leads to momentary preservation of the pressure and an explosion involving least one of already relaxing elements.

Figure 41 shows how to repeat a phase shift of the compressive elements of a thing: e turbinative, here translational.

In the previous examples, ax piston systems operate in different cylinders but connected or in the same cylinder. One can make a similar effect this time in taking in complementarity the pa e and the cylinder of a turbinative maclùne whose degree of In this way, rotativity will have been raised by planarization of the cylinder, organizing the times dead high and low parts horn. ipressive in such a way that they do not happen so at the same time, but rather in a way.

In the present figure, the blade rees a translational movement and for do this she is supported by two rotary crankshafts 831 rotativenzent mounted in the side of the machine. This time, as the ~; ylindre was increased by degree, its movement is no longer rotational but rather planétaix -1. As a result, the support gear dynamic 832 uniting and activating the vilebreqi ins subsidiary will be caubed from it way to activate the axis the crankshaft 830 of induction d; cyiindre. This one is composed of a gear of a cylindrical induction gear. -e 835 and support 836.

In such a way as to realize a ride-on nduction, the crankshaft of blade induction is misaligned intentionally with respect to the blade crankshafts. In the present kinetics, while these will hurry downhill, the crankshaft of cylinder will finish the which will preserve the com pression until the explosion, which will be realized when the blade will have begun its systemic deconstructiveness. Several other kinetics are possible.
Mainly, when the cylinder is on the contrary behind the blade.
Then, when the sense of the parts is rather contra ire in the curved parts of the cylinder and no in the parts flattened of it.

Figure 42 shows schematically, all the movements that can be made by a compressive part, either in a) the rotational movement b) the global movement c) to move it. Oscillatory d) Staggered planetary motion e) the simple tranlational movement f) the translational motion g) the polycamé movement h) movement with contrary inductions in the dish i) the contrary induction movement in the convex part (j) the riding movement Figure 39 shows several possible kinetics of rotating machines and turbinatives. In the cylinder and the blade are rotating nels, but around center of rotation different. This kinetics is attributable to Wanke _ In b, the cylinder is Sxe, and the blade planetary. This kinetic is from Wankel. We have proposed many methods of mechanization additional for this one. In c, the planetary motion blade and the cylinder one oscillatory movement. In d, the blade has a translational movement and the cylinder one rotational movement. In fact, the body has a rectilogno-translational and cylinder has a rotational movement. In i; the blade has a double planetary movement and the cylinder is fixed. In g, the blade has a planetary motion and the cylinder a movement curl. In h, the blade and the cyllister each have a pianetary movement, in contrast to direction of height at the ap ati of the cylinder and the blade. In i, the blade and the cylinder have each one a planetary movement, in contrario at the level of the height at the level of the bulging of the cylinder. In j, the induction of p ile is carried out by gears polycanzés. In k, the blade realizes a planetary movement and a virtual figure, and the cylinder a movement curl. In l, the blade and the cylinder each have a planetary movement, but whose the top and bottom dead spots are cheva ichès, that of the cylinder being late. In m, the blade and the cylinder each have a planetary motion, but whose top dead point and low are overlaps, that of the blade was late. Finally, the blade is moving translational and cylinder in motion planetat e. In o, the blade is fixed and the cylinder in movement planetary.

Figure 40 shows that all post rotary and retro rotary figures can be made standard to 1), curved 12), or balloon to 3). At 4, 5, and 6.1 can see that identical figures are achieved by increasing the degrees of the machines turbinatives.

In bl, b2, it can be seen that by increasing the inductions of standard machines, by crankshaft misalignment, and pir polycama.tion, the cylinders are made so angular.

In b 3 and b 4,1 we see that these cylinder, so to speak third degree are also realizable for the native turbines, by polycammed gear, and by overlap inductions.

Figure 41 shows that these changes in cylinder shapes are also possible for retrorotative machines.

Figure 42 shows that all blade figures can also be used, either by paddle simple in a, multiple blades in b, or by palic structure in c.

Figure 43.1, 43.2, 43.3, 43.4, 43.5, 43.6, 43.7, 43.8, 43.9, including achievements more detailed de fi nitions obtained i overlapping inductions Detailed description of figures 3 part Fure 44 shows that I, we can install a magneto 901 directly on the cylinder and connected to the candle 902. This magnet will pass successively plates qadarites 903 arranged rigidly in this sensor and will thus produce the landfill electrical necessary for 1, food of the candle, The figure shows in b that the candle 906 can be connected by the use of a induction at a point rigidly 396 and isoement disposed in the side of the cylinder `
This tip will drill metal plates 30 7 'fed successively by running these plates being rigidly arranged in the wall of a cylindrical cavity fixed to motor housing.
FIG. 45 shows that the end of the lead wire 907 of the candle can to be provided a broom floated on a metal donut 908, fixed rigidly and isolated in the wall of the cylinder for this purpose this cylinder being rigidly to the casing. The donut will receive and treat electrical discharges necessary to the power of the candle.

Figure 46 shows that the same procedure can be used to feed the candles that will be located on the piston of the machine 909 Figure 46 shows that pals 910n, 911 can be installed directly on the cylinder for the refroirdir.

Similarly ,. In b, we see that cooling dissenses can also to be installed on the cylinder.912 In FIG. 47, it can be seen that the cylinders of the cylinder can be compressed intertwined with crankcase discs, such as to make the best fvacon loss of heat of mamnae to the cylinder In the 48th difure we show; in a) that the water pump, if necessary maybe erected in a planetary manner and fitted to the cylinder. In b, this one will be realized by a pump, E c) we see how the liquids will be exchanged.

Figure 51 shows a hoop gear mechanism, with angulation of the induction , in 1000. In b of the figure, we see that the third gears supporting gear scoop, can serve as a support gear to the induction gear of cylinder, when the machine is made turbinatively, in 1001

Claims

claims Claim 1 A machine of rotary, rotary, or turbinative type, which in its form rotating induction a birotative poly induction, the support gear of the crankshaft master supporting two sets of gears, one activating the crown, and the other of the crown , being provided with maneont, and supporting the blade Claim 2 A machine of rotary, rotary, or turbinative type, which in its form rotating the induction is of the type of biritative poly induction, eLe vielbrquin supporting pairs d, external gears coupled to each other, one being a gear intermediate coupled to the support gear the internal type, fixed rigidly in the machine, and the other, being the induction gear each one of a crankpin and support the blade Claim 3 A machine, whose kinetics is of turbinative type, and whose blade and the cylinder are both, by an induction with planetary support gear peripheral, these induction being preferably carried out partially in a confused manner, of tlle a way that the induction gear of the central induction is connected rigidly to planetary blade and cylinder support gears Claim 4 A machine, as defined in, whose planetary support gear moon induction is coupled to the support gear of the first induction, Which one is coupled to the induction gear of the master inductor Claim 5 A machine, including the intermediate gear of the gear induction intermediate to planetary support gear, is arranged in the center of the machine Claim 6 A machine, whose pivoting segments are non-centered, this shifting the compression and explosion receiving surface of the blade and the cylinder.

Claim 7 A machine whose piston head is perforated in such a way as to to realize ducts allowing the gaxz to be integrated at a point in the pisotn, and penetrates years cylinder to another place, the same being valid for exhausts, Claim 8 A machine as defined in one, including the supporting crankshaft central induction n, is not the same as that supportnatn the device iduction, these two vilebrequinsétant however secured together by means of support, the crankshaft supporting the peripheral induction gear that can even be totally subtracted Claims 9 A machine, whose support gears respect the ratios of differences of fat between them, the ratio of teething ratio between them, but have reports from different sizes of their dentition ratio, this being the result of the modification of the form teeth of the gears.

Claim 10 A machine, having pitpons mounted in cylinders made in the cylinder main, these pitons being supported on springs, and these pistons serving shock absorber the explosion Reendication 11 A machine, whose support gears are larger, and supported by a crankshaft excenrique master arranged in the side of the machine, the blade not being supported only by a standard crankpin Claims 12 A machine, whose upper cavity of each face of the piston is open from way controlled hard the entire surface of the piston.

Reendication 13 A machine using a semi-transmission whose intermediate meshes do not are not the same size, it goes to the crown, or the central gear to act so planetary.

Claim 13 A machine of rotary, rotary, or turbinative type, which in its form rotating birotative machine, the crankshaft of it leading to a run by the use of in a set of intermediate gears, and this crown leads to gearing of induction of blade and its blade, by the use of a set of gears intermediate of different sizes.

Claim 14 Any machine whose support gear is dynamically driven by a semi transmission of the inductive poly type, the support gear of which is cylinder is from internal type Claim 15 Any machine having the intermediate gear or the hoop gear is axle of in the center of the machine and whose planetary support gear is mounted lanétairement in the engrna of fixed support of the machine, the induction by gearing intermediate or by hoop gear being angled Claim 16 A machine of birotative type, whose grosseuirs gears sioont enlarged, everything enconserving the same number of teeth realtive to the number of sides of the blades and cylinder, and and the same distance between them equal to the radius of rotation of the crankshaft Claim 17 Turbine type machine, including cylinder and semi gear tranmittive of blade are coupled by the use of the same set of crowns Claim 18 A turbn-type machine, including dynamic support gears and gearing of cylinder are coupled by a set of lined intermediate gears Claim 19 A machine of tudbinative type, whose double planetary gears of pale swert also a support gear for the induction of the cylinder.

Claims 20 A machine of rotary or turbinative type, whose combinations of induction of center and peripheral induction to planetary gears are applied in turbine machines:
~ to the semi-tranmittive rising induction, ~ at induction high ~ to the descending induction Claim 21 A machine whose intermediate gear is fixed on a sliding part attached directly or indirectly to the crankshaft, this gearing arming on the to have gears in such a way as to monimize the counter-thrust effect orientational of the blade.

Claim 22 A machine whose combined inductions are carried out as a result of crank shaft different, the second vilebrwquin popuvant be rotational or or joined to the first by slides or other methods, such that the removal of the gearing support planetary induction causes mo: sn counter-push.

A rotary or turbo machine carrying out in complicity more than one of methods following controlo controls:

~ by polycamation of any gear of the machine ~ by arming the intermediate gears directly geared to anegrenage ~ by angulation inductior ~ by addition of induction e realization of the support gear of induction of planetary way ~ by chain drive or gear hoop deaxeé
~ by modif8cation d gear ratios and teeth gears ~ by semi polycarnated tranmission Claim 23 A machine as described in 1 are the number of inductions the gear of support is planetary is greater than twoc Claim 24 A machine as defined and 21, whose semi transmission is carried out at from a Polycentric interlocking in the center is off-center this gear being driven directly or by the use of a gear doubled by a central gear, this gear being coupled to a polycammed gear in which the center is the same as that of the axis central the machine, the cylinder and the rotational part of the machine being connected to this gear.

Claim 25 A machine, of semi-differential differential type, whose blades, or curved istons are driven by a polycamé transmission.

Revemndication 26 A machine piston such ase define in 1, the dig is distributed according to lal, amplitude of the effort produced by the explosior.

Claim 27 A machine whose weight of the cylinder is determined by depressing its accumulation energy.

Claim 28 A machine whose crankshaft ~ born, is realized in the form of lifeboat or d, eccentric to the axret of the position of the blade, in a box closed, this crankshaft supporting the induction gear with recourse to a part of this one 1, including this induciton gear being coupled to the support gear of such way of forming alone or with the recoours to other gears a induction, the blade being mounted on a wrist mounted around unmantons, this pojnat receiving préférnce a lifetime for life Claim 29 A machine whose gases are ge ~ ed in such a way as to preserve at the back of the compression chamber viue ~ ga, or a non-carbureted area, this being obtained by a ~ late remelissage of the gases, ~ by a successive replacement of new and used gas, ~ oar filling by different mouths, these embouchueres leading, by Practical piping in the piston, at different ends of the bedroom acceptance of gaxz z girls, or worn.

Claim 30 A rotating machine of the turbinative type, one of the compressive part has been increased by one of the following procedures:

- the addition of a degree of rotativity - the use of polycammed gears, - the overlap of ix inductions Claim 31 A machine as described in 1, including planetary blade inductions and cylinder are realized:

~ coordinating each of these by the use of their crankshafts, these crankshafts being indirectly joined together by the use of a semi transmission ~ by performing one of the semi transmissive type induction, and that of such way that the dynamic support gear of this induction being rigidly connected to the crankshaft of the induction cde the complementary compressive part ~ by carrying out the support of one of the compressive parts by an induction rising and, starting from this same compressive part, realizing an induction down whose rotational and central induction gearing will realize the steering of the crank shaft induction codes the complementary compressive part.

Claim 32 A machine as defined in which the cylinder will be said to be bi-rotating, this cylinder can be bulging, when it will have a smaller width and a higher height that the form of standard cylinder, or balloon, when it has a lower height than the height standard and an upper width between its two arcs.

Claim 33 A machine, as defined in 1, including the matching of parts compressive ones are in the flattened region of the cylinder of the machine, in which join the cylinder ares and the remoteness in the arches of it Claim 34 A machine, as defined in 1, including the distances of the parts compressive ones are in the region of the arcs joints of the machine, and the reconciliations in the ares of that this Claim 35 A machine as defined in 1 including the dead times up and down the pale and cylinder are respectively in the same regions or dials Claim 36 A machine as defined in 1, the dead times of the blade and bottom of the cylinder, and inversely, the top of the cylinder and the bottom of the blade are respectively in the same regions or dials Claim 37 A machine as defined in 1, including overlapping dead time up and down blade and cylinders is by delay of the cylinder.

Claim 38 A machine as defined in 1, including overlapping dead time up and down blade and cylinders is by delay of the blade Claim 39 A machine as defined in 1, to which are simultaneously conferred more than one a method of elevation of degrees, this making it possible to cylinder more oblique, so-called trirotational.

Claim 40 In a rotating machine of the turbinative type, a power supply which created the electrical contact between an electrical element disposed on the part compressive and a other compressive part, on the crankcase Claim 41 A power supply of a turbine machine whose magneto is rigidly attached to the rotating cylinder and connected to the candle, this magneto drilling successively magnets arranged in the housing of the machine Claim 42 A power supply whose candle is connected by a common thread to a dot rigidly and singly arranged on the cylinder of the machine, this point brushing successively contact plates arranged preferably in the wall of ,a cylindrical cavity rigidly fixed to the housing these plates receiving their current of a power source and transmitting it through this tip to the candle.

Claim 43 A power supply in aquelle the wire connecting the candle is fixed to his second end with a brush disposed on the side of the rotor cylinder m this brush being made to have a floating circular action on a donut feeding arranged in a cylindrical cavity rigidly fixed to the housing m this donut receiving and transmitting successively electrical discharges necessary for the power supply of the drums, Claim 44 A power supply as defined in 2.3.4 m whose candles will be arranged on the blade.

Claim 45 A power supply as defined in 1 m whose electric discharge jumps from the candle on a conductive metal part and disposed on the compressive part complementary.

Claim 46 A turbinator type machine, whose rotational cylinder is entwined by a induction gear, external or internal, itself driven by a gear of peripheral planetary support.