JP5655076B2 - System for the construction of compressors and rotary engines with dynamically variable compressibility and volumetric arrangement - Google Patents

Description

(Field of Invention)
The present invention consists of two rotors with one or more displacers per rotor so as to create more than one chamber between the displacers depending on the amount of displacer per rotor. Relates to a system for building compressors and rotary engines.

  The chamber changes in volume according to the degree of separation between the pistons caused by changes between the two rotors or alternatively by opposing speeds. This change in speed is a number that has a change in radio length as a characteristic that transforms the rotary motion into a vibrating motion of varying speed and vice versa, so that a regular and uniform rotary motion is transmitted. Can be generated by different types of systems. As an example of this type of mechanism, one composed of a double crankshaft integrated with a slide shaft or a rotating rod can be listed. This works in a position that integrates into the arm attached to each of the rotors and in an opposite position away from their geometric axis. This detachment allows for a change in the radial length through which the motion is transmitted, thereby allowing the rotor displacer to change the uniform motion of the double crankshaft into a changed motion of acceleration and deceleration in the rotor. Deform or vice versa. In exactly that way, systems using fixed solar gears around which planetary gears move support the shafts from their centers. These shafts are connected to the rotor arm through connecting rods that transmit movement. Another mechanism utilizes an elliptical gear connected to the rotor arm by rotating a rod.

  The new system is characterized by using two mechanisms, coupled or separated. One of them dynamically changes the distance between the displacers and the other dynamically changes the start of the inspiration and compression stages. The change of the displacer distance is obtained through a dynamic change of the distance between the drive mechanism as well as the geometric axis of the engine or compressor, at least one of which is placed on the slide rail, the spindle, It is moved by a hydraulic piston or gear system. The displacers approach each other or separate themselves, increasing or decreasing the compression rate just as proposed by the present invention.

  Other mechanisms change the volume located in the intake and compression chambers and consequently change the volume relationship with the combustion and exhaust chambers. This volume difference is performed by the separation between the specific parts of the intake-compression chamber, creating an opening that allows the passage of fluid and prevents the displacer from being sealed within the specific part. Prevent inhalation and compression of fluids.

  In this way, a constant drop in at least one of the chamber walls can be used to reduce the volume placed in a fixed manner. This can be done, for example, by enlarging the inlet of the intake (FIG. 1a), or by displacement of one or various parts of the chamber that approach or move away from the displacer operation by some mechanical system. Various methods create an opening between the chamber itself and the displacer to reduce the chamber sealing area (FIG. 1-b). This deployed volume change can be altered depending on whether the system is stalled or moving.

  The combined action of the two mechanisms allows a reduction or increase in the volume placed in the intake phase so that the compression rate of the engine or compressor is not changed in an undesired manner. Therefore, it is necessary to reduce or increase the compression rate to adapt the compression rate to the newly allowed volume. Assuming that it is desired to operate at a compression ratio of 1 to 9, the drainer in one of the chamber walls only advances and the method compresses 50% of the total volume. A drainer is used. Under these conditions, the compression ratio drops to half (1-4, 5). It may be necessary to reduce the distance between the displacers so that the compression ratio of 1-9 is reached again. In this way, a reduction in the aspirated volume is made, but at the point of having twice the volume in the combustion and exhaust chamber, the desired compression ratio will be maintained. Under these conditions, if one or more parts involved in the reduction of the intake-compression chamber are repositioned to allow a larger angle of displacer operation, the compression rate is changed again and It will increase proportionally with increasing volume.

  The movement of the chamber part may be hydraulic, mechanical or manual with a suitable electric engine. The electric engine is assisted by sensor readings of temperature, speed, torque, combustion quality, etc. and other supplied information according to a computer program with pre-established answers. In this way, there can be a change in the deployed volume in the intake and compression, coupled with this, a very change in the compression ratio of the engine or compressor can exist, for example, in the function of the engine or compressor. To optimize engine or compressor productivity.

  Thus, at high speeds, it would be possible to increase the volumetric efficiency of the system and adapt the system to different speeds.

By reducing the intake and compressed volume, in the case of a combustion engine, the dimensional relationship with the combustion and exhaust chambers changes automatically in its own time, thus achieving the process Increase the time and volume of the gas and ensure greater use of the expanded gas and better combustion of the mixture. The difference will result in increased productivity and reduction through efficient combustion of toxic residues (CO ₂ , hydrocarbons) common to poor combustion.

(Technology state and the present invention)
The energy and ambient crisis caused by low energy productivity pollution technology is the largest source of energy consumed in the compressor and engine sector with reduced environmental impact and reduced harmful emissions to a minimum. Requires new equipment to use. The use of any new renewable fuels such as biodiesel, ethanol, hydrogen, or other low-contamination fuels such as natural gas is ideal for all of those fuels, ie for each of those fuels. It requires a combustion engine that can operate efficiently at a compression rate of.

  On the other hand, the internal combustion engine (alternative or rotary) of the present invention does not operate at an ideal compression ratio for each speed-torque state. Conversely, the internal combustion engine of the present invention is tuned to avoid pre-detonation. The turbine is adapted to supply air at a pressure above atmospheric pressure, thereby obtaining good engine respiration and increasing engine volume. However, these turbine engines have the limitation of increasing their volume and are characterized by an increase in the compressibility that can be achieved without damaging the engine itself. Changing the volume arrangement of the alternative engine in various manners is a very difficult task to achieve in view of the four stages of intake / compression / combustion / exhaust in sequence within the same cylinder. In an Otto cycle, four stages occur in the same cylinder as if they occur at two timings or points in time.

On the other hand, alternative engines generally have to open the 60-degree release valve in advance before the final course, with the intention to promote the exhaust gas so that the exhaust gas is not blocked by the exhaust gas. To reduce the combustion gas pressure by nearly 20%. Combustion of the mixture is an alternative engine that cannot have a larger volume combustion cylinder that can make better use and efficient completion of combustion expansion in such a way that it does not produce high index pollutant residues Also harmed by the geometry. Filter catalysts have been developed to attenuate the effects of poor fuel combustion and eliminate some hydrocarbons, CO _2, etc., which in addition to high cost and short use time, effectively releases pollutant gases. Does not solve.

  On the other hand, through electronic pre-programming, “flexible” engines have been developed that change power supply and ignition parameters according to sensor readings and adjust the parameters to different types of fuel. Although the electronics make the combustion engine flexible, it is not possible to understand very different types of compressed fuels (eg diesel and gasoline), and even if you see that the compression ratio remains fixed, those compressed fuels Neither of these can provide good productivity and is suitable for fuels that require low compression.

  The dynamic change of the deployed volume during the intake and compression stages, along with the dynamic change of compressibility, combustion of larger volumes than the intake-compression chamber and the use of an exhaust chamber, offers an interesting solution. In the case of an internal combustion engine, it uses a specific compression rate for each one of the different fuels, in addition to the use of different fuels in an optimized manner, as well as the use of higher energy and the toxic residues from combustion. A significant reduction will be possible.

  The change in compressibility while the engine is functioning at different revolutions per minute can be attributed to information sent by different sensors (operating temperature, torque, fuel type, mixture richness, combustion efficiency, etc.). Taking into account will allow the best use of different fuels without the risk of premature abnormal combustion. The present invention also allows for changes in the position of the inlet and outlet relative to the position of the displacer. This is possible through a change in the angular position of the solar gear relative to the planetary gear when using the planetary system. This new system also allows for the incorporation of a much more efficient power supply turbine mode, which is now not limited in performance due to the dynamically variable compression ratio increase. Finally, we reduced the intake-compression chamber and created a space in which the gaseous fuel and preheated mixture were homogenized before being compressed. This ensures better conditions for complete and faster combustion, and complete and faster combustion will result in larger and cleaner energy efficiency. If the system is used for a compressor, the system allows compression at different rates and volumes at which it operates. For example, in the case of refrigerator compressors controlled today by thermostats or expensive systems with variable speed, the system allows efficient control of the required temperature, changes the rate and / or volume placed, This will reduce energy consumption and increase the service life of the electric engine without forcing a continuous stop and start which increases energy consumption and decreases the service life of the equipment as in the use of a thermostat.

Several types of compressors and rotary engines have been invented based on the movement of two rotors, each having at least one piston and moving at varying or opposing speeds. This speed change movement is basically performed through different mechanisms listed below.
1) Planetary gear system 2) System with elliptical gear 3) System with sliding rod 4) System with rotating rod

  All of them exhibit an established eccentricity relationship and, when using a planetary mechanism, exhibit a fixed concentric relationship with respect to the geometric axis of the engine. Based on the use of planetary gears, a number of rotary engines with a mechanism of relative speed change between the two rotors have been idealized. All of them have a fixed solar gear around which at least two planetary gears in opposite positions rotate. The gears support an axis away from the center, and the center articulates itself to the rotor arm through a rotating rod that is a transmission of movement. The reduction relationship between solar gear and planetary gear is determined by the quality of the displacer that supports each rotor, one to one when one displacer supports each rotor, and two displacers Is 2 to 1 when supporting one rotor, and so on. The relative position and the distance of the center of the planetary gear of the shaft and the length of the rod and rotor arm coupled to transmit the movement are relative to each other between the rotor and the rotor displacer. The change in speed.

  The coupling axis away from the center of the planetary gear, when rotating around the solar gear, approaches the solar gear or away from the solar gear, changing the radius at which the motion is transmitted, and having a specific relationship and position. It causes a change in speed, including even the retention of one of the rotors.

  The planetary system operated in a concentric form with respect to the engine shaft and was always planned to meet the concepts of simplicity, strength and final smaller machine dimensions. In this way, the solar gear was tightly coupled onto the engine carcass and concentric with its geometric axis. The present invention proposes to keep the planetary mechanism of the engine or compressor dynamically at a distance so as to change the compression ratio. In order to be able to separate the geometric axes using one or more displacers per rotor, the present invention is based on the number of displacers per rotor between the arm and the rotor. Suggest the use of gear reduction.

  This type of reduction is achieved by the double crankshaft joined to the rotor arm by a slide element that moves itself from the slide element of the crankshaft or by a double crankshaft joined to the arm by a rotating rod that transmits the motion. It should also be applied when a crankshaft is used. Both mechanisms generate a speed vibration at 360 degrees each, which works when there is a need for a 180 degree cycle, as in the case of a rotor each supporting two displacers. Both mechanisms require a reduction gear with one or more displacers per rotor during operation.

(Invention)
A new engine with the traditional advantages that a rotary engine offers over an alternative engine: smaller dimensions, less movable parts, less vibration, less weight, less production cost, more advantages Presents a significant reduction in the quality and quantity of toxic residues resulting from the use of greater energy and combustion. This is possible for various reasons:

  1. For this innovative system, it is possible to have a combustion chamber with a larger volume than the intake-compression chamber, which allows better use of fluid pressure and combustion during the expansion or combustion phase To do.

  2. This innovative system allows for a change in configuration that reduces fuel consummation, resulting in no polluting and adapting the deployed volume in a programmed manner to the vehicle's needs. Ensure better energy efficiency for each speed-torque situation, in the case of engines and equipment, in the case of compressors, in order to operate in the best possible manner.

  3. With this innovative system, it is possible to both change the distance between the geometric axis of the engine and the geometric axis of the operating mechanism during operation. This makes it possible to vary the compression ratio, corresponding to the need for torque and speed and the increase or decrease (arrangement) of the deployed volume, corresponding to the type of fuel in use. The result is a compression rate close to the ideal compression rate for each situation of combustion, resulting in better combustion with better toxic residues and ultimately using more energy than the current engine Will be obtained.

  4). With this innovative system, the angular relationship between solar and planetary gears can be changed, allowing more efficient control of the position of the displacer relative to the chamber and intake and exhaust ports and spark plugs, Allow the displacer to produce the best for speed, deployed volume, torque required for the engine, fuel type, etc. by changing the placement at different moments of operation.

  In one preferred realization, the present invention provides for different variations of motion between the rotor and its displacer, along with the control of the distance between the displacers, in addition to the possibility of using other speed change mechanisms. Two substantial changes are proposed that create a new and more versatile drive mechanism that allows the establishment of a relationship together or separately.

  The first modification consists of separating the planetary gear system of the engine. This controls the distance between the displacers coupled to the rotor by changing the distance between both geometric axes when some of the engine's planetary gear systems are in motion. It will be possible.

  Doing the above created a new mechanism governed by two systems of altered movement. One was created by a planetary mechanism, and another was created by the separation of the engine or compressor geometric axis and the movement mechanism coupled by a connecting rod.

  These two speed change mechanism combination types use different fuels such as gasoline, ethanol, gas with different combustion times, different torque and speed regime, relative position between different pistons, Changing the parameters of the motions of multiple rotors and their respective displacers according to the requirements of the best engine operating at different intake, compression, combustion and exhaust speeds during which the same compression ratio is maintained Will enable. This will allow for the completeness of the motion mechanism modified at different stages to use greater energy and reduce combustion pollutant residues.

  However, when more than one displacer is activated per rotor, the traditional planetary system that requires the use of a planetary gear with a diameter proportional to the solar gear is modified according to the amount of displacer supported by the rotor. Thus, it may be possible to combine the above two mechanisms. In the case of two displacers per rotor, the planetary system was designed to operate with a planetary gear having a diameter half that of the solar gear. As such, the planetary system generates two different speed change cycles for each turn made around a fixed solar gear. Separating this set of geometric axes, coupled by connecting rods that transmit motion to the rotor arm of the engine geometric axis, will generate separate speed change cycles, each operating at 360 degrees. Let's go. Both working together inevitably generate different unbalanced movements between the rotors. The mechanism of the present invention has an equal diameter between the planetary gear and the solar gear, in one preferred realization, in such a way as to produce only one 360 degree cycle that matches the cycle caused by the rod system. The reason why the unique planetary gear system is proposed is as described above. When two displacers are used per rotor, the new system places half the number of tooth gears on the axis of each rotor arm by reducing gears from two to one, It is proposed to mediate both movements by placing a gear with double the amount of teeth in each rotor that transforms a 360 degree change cycle into two 180 degree cycles.

  If more displacers are used per rotor, this reduction is proportional to the number of displacers used per rotor, from 3 to 1 for 3 displacers per rotor, 4 displays Sir decreases from 4 to 1, and so on.

  In one preferred implementation of the invention, the novel system is based on a spindle, hydraulic, pneumatic or geared system, headed by a computer that is suitably powered by sensors. A dual crankshaft that supports a solar gear shaft and planetary gear fixed on a bearing that can be moved on a rail or slide shaft is placed. And so change the distance between the geometric axis of the double crankshaft and the engine's geometric axis so that it rotates around the solar gear and change the distance between the displacers and thereby compressibility It is possible to change.

  In one preferred realization, the system of the present invention for the construction of compressors and rotary engines can be used in a fixed or variable manner to prevent inhalation or compression of fluid in the area of a particular part of the chamber. Offering the possibility of changing the volume placed by placing multiple displacers in a particular part. At the start of inspiration-compression, at least a portion of the chamber may be spindle, hydraulic, pneumatic or pneumatic so that this arrangement forms or closes the opening between the displacer and the chamber while allowing fluid flow. It is moved in a sliding manner by a gear system.

  Increasing the inhaled volume will automatically increase the compression rate at the risk of pre-detonation in certain conditions, for example if the degree of displacer separation is not changed. . This is a technology that can be conceived separately from the mechanism that allows the arrangement of the chambers to be changed so as to change the arranged volume and the mechanism that enables the compression ratio to be changed. This is why it is impossible.

  Changing the distance between the geometric axes will change the compression ratio to be maintained, eg, the same engine compression ratio that can be maintained by stopping or operating the engine.

  In one preferred implementation of the invention, the above operations can be controlled by a computerized system. The computerized system works with changes in volume arranged taking into account speed, torque, fuel used, temperature, fuel type, as never achieved by current combustion engine technology, It will dictate the necessary changes to the use of better, more efficient and clean energy.

  The present invention further presents in one of its preferred realizations a novel mechanism capable of changing the relative position of the displacer with respect to the chamber and its inlet and outlet and the spark plug. . The mechanism is a solar on a shaft that can be moved and fixed to a different position so as to change the relative position of each planetary gear shaft and a plurality of planetary gears attached to a connecting rod that transmits movement. Consists of arranging gears. The mechanism also changes the relative position of the displacer relative to the fixed chamber with its inlet and outlet by changing the position of the solar gear shaft.

By coupling the shaft to any mechanical system capable of moving the solar gear by a suitable engine or changing the relative position of the chamber,
It would be possible to perform the above adjustment during engine operation. The above adjustments can be undoubtedly operated by electronic devices programmed in association with the data sent by the sensors in order to properly position the solar gear with the intention of improving the function of the mechanism.

  The present invention, in one preferred implementation, provides a system for the construction of compressors and rotary engines having different volume arrangements between the intake and compression chambers and the combustion and exhaust chambers. The relationship between the volume of the intake and compression chambers and the compression and exhaust chambers can be fixed or variable.

  In another preferred realization of the present invention, the speed change can be varied with varying length features in which a regular and uniform conversion of rotational motion to oscillating motion or vice versa is transmitted or received. Can be generated by a type of mechanism. An example of such a system is a pair with sliding or rotating rods operating in opposing positions, joined to an arm attached to each of the rotors and spaced from their geometric axes. Mention may be made of a system constituted by a heavy crankshaft. This distance allows for a change in the length of the radius to which the motion is transmitted, thereby allowing the continuous motion of the double crankshaft to change in a modified acceleration and deceleration motion. The distance is then stopped by a slide mechanism that stops the displacer in the rotor or vice versa and is moved by a spindle, hydraulic, pneumatic piston or gear system using any of the aforementioned mechanisms. Characterized by the fact that the compression ratio can be changed dynamically by changing the distance between the geometric axes. Connecting rods that transmit movement are joined directly when the rotor supports only one displacer each (FIG. 3) and / or when operated by more than one displacer per rotor. It will be mediated by gear reduction (FIGS. 1 and 2).

  In another preferred realization, the movement mechanism operates with a double crankshaft, which supports two gears having the same number of teeth connected by a chain. A plurality of axes away from the center of the planetary gear are joined to the rotor arm by connecting rotating rods that transmit movement. The gear reduction proportional to the number of displacers applies when each rotor supports one or more displacers.

  In another preferred realization of the system of the invention, the same is used for the construction of all different types of fluids, internal combustion engines, thermal, hydraulic or pneumatic pumps and compressors.

  1-a and 1-b are views of the front part of the engine (left side) and its motion mechanism (right side), drawn separately to facilitate understanding thereof. The engine includes two rotors each having a pair of displacers (2) and (5) moving inside the chamber (1), two openings of an intake port (26) and an exhaust port (25), It has a drainer at the start point (23) of the intake air that restricts the operation of the displacer. In one aspect, the portion of the chamber (24) joined to the outer ring (1) placed on the fixed outer wall of the chamber driven by the hydraulic piston (22) is shown in FIG. Closed and opened in FIG. The hydraulic device (22) opens the chamber part and forms a groove that inhibits the operation of the displacer (2, 5), reducing 50% of the volume to be placed and compressed in the compression and suction chamber (34) While increasing the relative volume of the combustion-exhaust chamber (35) by a factor of two. The combustion chamber in which the spark plug (32) is present is operated with a compression ratio (27) of 9 to 1 in FIG. 1-a, to compensate for the reduction in volume placed to maintain the same compression ratio. It changes in half by the displacer approaching at 1-b. This change is made by dynamically changing the distance between the shafts (33) between the engine (left figure) and the motion mechanism (right figure).

  The movement mechanism is a double crankshaft (15) that supports two planetary gears (12, 13) moving on a fixed solar gear (14). The rotating rods (8, 9) transmit the movement of the inner and outer rotor arms (6, 7). These arms are rotated by half the amount of gear (30, 31) installed on the rotor (28, 29) so as to change the cycle speed range of 360 degrees to two cycles of 180 degrees each. Connected to the child. Therefore, for every 180 degree arrangement of the double crankshaft, four faces of the Otto cycle are generated. Intake-compression always operates in the engine part (34) and combustion-exhaust always operates in the engine part (35). In FIG. 1-b, it is observed that the chamber (35) has twice the volume compared to the intake-compression chamber (34), allowing a better use of the combustion gases. In FIG. 1-b, an expansion of the part (23) of the chamber is observed where the air and fuel mixture is heated and homogenized before being compressed.

  FIG. 2 shows a perspective view of the same engine as shown in the previous figures. FIG. 3 shows a cross-section in a superior view of a compressor with two rotors. The inner rotor (3) and the outer rotor (4) each form a gap (23) that inhibits or does not inhibit the operation of the displacer (2, 5), so that when necessary A display that operates in a fixed outer ring (1) that supports a portion (24) of the chamber that is driven by a hydraulic mechanism (22) in a sliding manner to dynamically change the volume deployed. Sir (5, 2). The rotor (3, 4) is driven by a rotating rod (8, 9) by means of a shaft (10, 11) attached to them away from the center of the planetary gear rotating around a fixed solar gear (14). It is attached to the arms (6, 7) joined to the planetary gears (12, 13).

  The planetary gears (12, 13) are gears that can be moved by the electric engine (21) for the purpose of changing the relative position of the displacer (5, 2) with respect to the camera (1) when necessary. Supported by a double crankshaft (15) rotating around a solar gear shaft (18) supporting (19).

  The entire speed change mechanism is moved on the rail (16) by the hydraulic mechanism (17), thereby changing the distance between the double crankshaft with planetary system and the shafts of the compressor, thereby compressing It appears to be rigidly attached to the bearing system (20) which can remove or approximate the displacer (2,5) by changing the rate.

  FIG. 4 shows the front part of the compressor with two rotors, each supporting a displacer (2, 5) moving counterclockwise towards the chamber (1). The chamber (1) is divided into two chambers, one for intake and the other for compression. The two mechanisms that are moved by the hydraulic piston (22) of the chamber part (24) can be seen, one (23) open and the other closed. In FIG. 4-a, chamber inhalation (26) through the opening begins while compression in the other chambers begins. Fig. 4-b is an intermediate state, in Fig. 4-c the maximum compression of the chamber between the two displacers contacts the exhaust (25), but the displacer (5) is still in the intake-compression The operation has not started.

It is a figure of the engine front part (left side) and its movement mechanism (right side). It is a figure of the engine front part (left side) and its movement mechanism (right side). FIG. 2 shows a perspective view of the same engine as shown in FIGS. 1-a and 1-b. Figure 2 shows a cross section in a comprehensive view of a compressor with two rotors. Figure 3 shows the front part of a compressor with two rotors supporting a displacer (2, 5) moving counterclockwise towards the chamber (1). Figure 3 shows the front part of a compressor with two rotors supporting a displacer (2, 5) moving counterclockwise towards the chamber (1). Figure 3 shows the front part of a compressor with two rotors supporting a displacer (2, 5) moving counterclockwise towards the chamber (1).

DESCRIPTION OF SYMBOLS 1 Outer ring of chamber 2 Displacer of outer rotor 3 Internal rotor 4 External rotor 5 Displacer of inner rotor 6 Rotor of outer arm 7 Rotor of inner arm 8 Rotating rod of outer rotor 9 Internal rotor Rotating rod 10 External planetary gear shaft 11 Internal planetary gear shaft 12 External planetary gear 13 Internal planetary gear 13 Internal planetary gear 14 Solar gear 15 Double crankshaft 16 Planetary mechanism chute 17 Hydraulic mechanism 18 Solar gear shaft 19 Gear for moving solar gear 20 External rotation Rotating rod of child set 21 Slide mechanism of moving mechanism 22 Hydraulic mechanism of outer ring of chamber 23 Groove of intake-compression chamber 24 Portion of outer ring of chamber 25 Exhaust port 26 Intake port 27 Maximum compression ratio 28 Larger of inner rotor Gear 29 larger than outer rotor Intake of the distance 34 the chamber between the larger gear 32 spark plug 33 geometric axis of the smaller gear 31 outside the rotor arm of the gear 30 inside the rotor arms - exhaust compressed portion 35 Chamber - combustion portion

Claims (11)

With two rotors with at least one displacer, each moving inside an annular surface at varying speeds opposite each other, creating a chamber between them that alternately changes their volume A system for the construction of rotary engines and compressors,
The distance between the displacers as well as the area of the chamber in which inspiration and compression act can be changed dynamically in order to change the volume and compression rate arranged separately or together. ,system. By moving at least a portion of the surface of the chamber and creating a groove that prevents the displacer's intake and compression action, at least one portion of the intake and compression chamber is changed in a fixed or variable manner. Thus, the well-sealed part is monitored manually or by a computerized system and by a suitable mechanical, hydraulic or electrical system in which the entire set is inactive or in operation The system of claim 1, wherein the system can be moved.   Fixed solar gear that integrates the rotor arm by a sliding element integrated into the rotor arm or by a double crankshaft attached to the rotor arm by a connecting rod or by a connecting rod that transmits the movement It has a mechanism with different changes in speed of the double crankshaft type, either by a planetary gear that moves around or by an elliptical gear added to the rotor arm that integrates the rotor arm with a rod that transmits the movement. The system according to claim 1, wherein the system can be constructed as follows. The geometric axis of the compressor or engine can be spaced from the geometric axis of the mechanism that allows a change in speed relative to both rotors so that the rotor is at rest Or dynamically moving at least one part on the rail or slide shaft through a working spindle, mechanical, hydraulic, pneumatic or electrical system, temperature sensor, speed, torque, combustion quality, arranged volume 4. The method according to claim 1 or 3, characterized in that the objective is to change the distance between the displacers, thereby changing the minimum volume of the chamber created between them. system. At least two planetary gears attached to the power shaft are constructed with a movement changing mechanism with a fixed solar gear that moves around, each one of said gears by a connecting rod that transmits the movement of the rotor arm A system for supporting an axis away from the integrated center,
Has a solar gear and the same number of teeth planetary gear is fixed, the rotor from the two when supporting the two of displacer respectively to one, from the three when the rotor supporting the three displacer one wherein the arms of the rotor are integrated to them by reduction by gears to the, to the number of displacer supporting each rotor system of claim 1, 3 or 4.   The geometric axis of the speed planetary mechanism can be spaced from the geometric axis of the engine, at least one of which is placed on a track or slide axis and moved by a system with a spindle, piston or gear. System according to any of the preceding claims, characterized in that it is controlled manually or by an engine and controlled by a computerized system.   It can be built with a double crankshaft that supports two gears connected by a chain, a shaft spaced from the center of the gear is integrated into the rotor arm by a rotating rod that transmits the movement The system according to claim 1 or 4, characterized in that: The relative position of the satellite gear with respect to the solar gear, thereby changing the angle of the solar gear to change the relative position of the rotor and its displacer with respect to the inlet and outlet and the ignition point of the chamber. 6. System according to claim 3 or 5 , characterized in that it can be arranged angularly.   9. The chamber according to claim 1, wherein the chamber, the displacer and the rotor can have dimensions and geometries that can be varied greatly, with or without sealed parts. The system described in.   System according to any of the preceding claims, characterized in that it can be operated by a turbine that increases the flow of intake air, thereby increasing its volumetric capacity.   Different types of compressors or engines, regardless of whether they are pneumatic internal combustion, injection and / or lift systems driven by the pressure of various fluids heated before or during operation by the use of various fluids or fuels System according to any of the preceding claims, characterized in that it can be applied in whole or in part to construction.

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