WO2017217834A1

WO2017217834A1 - Device, mechanism and machine for compressing gaseous fluids

Info

Publication number: WO2017217834A1
Application number: PCT/MX2016/000060
Authority: WO
Inventors: José Guillermo CASTRO GONZÁLEZ
Original assignee: BARRAZA SÁMANO, María Delia
Priority date: 2016-06-14
Filing date: 2016-06-14
Publication date: 2017-12-21
Also published as: MX2018013908A

Abstract

The invention relates to a device for converting inertial rotational energy in situ into linear movement with the ability to perform work, which is formed by: a kinetic part (1) having a shape and assembly that allow the centrifugal rotation thereof with at least one other identical kinetic part (1), in a centrifugal movement mechanism; a device that transmits linear movement (11) and is actuated by the kinetic part (1); and a device (12) that receives the linear movement. The invention also relates to a mechanism for compressing gaseous fluids, which comprises: at least two devices for converting inertial rotational energy in situ into linear movement with the ability to perform work, according to the present invention. The mechanism comprises: a mechanism that provides centrifugal movement to said devices; a fixed support (18) which support the devices; a tank that stores highly-pressurised air that comes from an outlet valve for pressurised air of a compression unit (12); and a power source that provides power to the mechanism providing the centrifugal movement. The invention further relates to a machine for compressing gaseous fluids, characterised in that it comprises: at least two mechanisms for compressing gaseous fluids according to the present invention; and a structure (34) that supports the devices for compressing gaseous fluids.

Description

APPARATUS, MECHANISM AND MACHINE TO COMPRESS FLUIDS

GASEOUS

TECHNICAL FIELD OF THE INVENTION

The present invention belongs to the technical field of mechanics, because it provides us with an apparatus, mechanism and machine for compressing fluids in the gaseous state, such as air.

BACKGROUND OF THE INVENTION

In the market there are currently screw compressors that suck air through two helical screws, where they manage to handle large volumes of air but at low pressures.

Also in the market we find piston compressors or pneumatic actuators, these can compress air at high pressures, but the operating costs to achieve a lot of compressed air volume are very large; The cause of the high costs in the piston compressors, is that a rotational actuator, either an electric or internal combustion engine, normally handles two heads with pneumatic actuators and, it is the rotational actuator itself that provides directly and by means of bands, arrows and gears the labor force required by pneumatic actuators.

Nowadays, the most commercial pneumatic actuators require between 4,000 or 5,000 N of force to carry out their work, the ones that require the most strength are around 7,500 Newton of force and the operating costs are expensive and the volumes of compressed air they handle are low. . That is why, in order to overcome the aforementioned drawbacks, an apparatus was developed to convert in-situ rotational inertial energy into a linear movement with the ability to perform work, which greatly exceeds the efficiency of current piston compressors. A mechanism was also developed to compress gaseous fluids using said apparatus; as well as a compressor machine that also consists of at least two mechanisms for compressing gaseous fluids according to the present invention.

BRIEF DESCRIPTION OF THE FIGURES

Figure 1 is a conventional perspective view of a kinetic part, which is part of the apparatus for converting in-situ rotational inertial energy, into a linear movement capable of performing work, of the present invention; where its cavities are observed to lodge rolling elements.

Figure 2 is a conventional perspective view of the kinetic part of the previous figure, where another of its cavities is illustrated, suitable to accommodate a fastening and suspension means.

Figure 3 is an explosive view of the two halves that make up the kinetic piece and its characteristic details are clearly observed. Figure 4 is an explosive view of the kinetic piece, where its other components are observed.

Figure 5 is an explosive view of the kinetic piece, where the arrangement of its components is observed.

Figure 6 is a conventional perspective view of the kinetic part, in an assembled condition.

Figure 7 is an explosive view of the apparatus for converting in-situ rotational inertial energy into a linear movement capable of performing work, according to the present invention.

Figure 8 is an explosive view of a mechanism for compressing gaseous fluids, comprising two apparatus for converting in-situ inertial rotational energy, in linear motion with the ability to perform work, in accordance with the present invention. Figure 9 is a conventional perspective view of a fixed support that has the ability to support two devices to convert insitu rotational inertial energy into a linear movement capable of developing work.

Figure 10 is an explosive view of a rotating support that forms part of the mechanism for compressing gaseous fluids, provided in the present invention.

Figure 11 is a conventional perspective view of the rotating support illustrated in the previous figure, in an assembled condition. Figure 12 is a top view of the mechanism for compressing gaseous fluids, where the arrangement of the two devices can be observed to convert inertial rotational energy, into a linear movement capable of performing work.

Figure 13 is a conventional perspective view of the mechanism for compressing gaseous fluids, of the present invention, in an assembled and closed condition.

Figure 14 is a longitudinal section of said mechanism for compressing gaseous fluids, in an assembled condition.

Figure 15 is a longitudinal section of a gaseous fluid compressor comprising two mechanisms for compressing gaseous fluids.

Figure 16 is a conventional perspective view of an exterior structure that supports two mechanisms for compressing gaseous fluids, to form a compressor for gaseous fluids.

Figure 17 is a conventional perspective view of a gaseous fluid compressor machine, with two mechanisms for compressing gaseous fluids, in accordance with the present invention. DETAILED DESCRIPTION OF THE INVENTION

The characteristic details of the present invention are clearly shown in the following description, accompanying figures and examples, which illustrate some of the preferred embodiments of said invention, and therefore should not be considered as limiting for the invention in question.

For a better understanding in the description of the present invention, a list (Table 1) of the components that conform to the invention in question are included, which are referenced in the included figures.

Table 1. List of the components and their references, which are part of the present invention.

Table 1. Continued ...

A. Apparatus for converting in-situ rotational Ineclal energy to linear movement with the ability to perform work.

In the first instance, the present invention relates to an apparatus for converting in-situ rotational inertial energy, to linear movement with the capacity to perform work, where said apparatus is formed of a kinetic piece (1), whose shape and assembly allows it to rotate in a centrifugal manner with at least one other kinetic part (1) equal, located and suspended equidistant from each other, in a mechanism that provides centrifugal movement.

In this example, the kinetic piece (1) is substantially oval, shaped by two halves equal to each other (see figures 3, 4 and 5) and joined together as a sandwich (see figures 1 and 2); wherein said kinetic part (1) has a first cavity (2) on one of its lateral sides, where a first rolling element (3) placed in an orthogonal plane is partially housed with respect to the central rotational axis of the mechanism that provides the centrifugal movement , and parallel to the plane of rotation of the kinetic piece itself (1); a second cavity (4) at one of its ends, where at least a second rolling element (5) is also partially housed in an orthogonal plane in relation to the central rotational axis of the mechanism that provides centrifugal movement, and parallel to the rotation plane of the kinetic piece itself (1); and a third cavity (6) on its other lateral side, where part of a suspension element (7) is housed and held, which joins said kinetic piece (1) suspended with the mechanism that gives the centrifugal movement.

The shapes and dimensions of the third cavity (6) and the suspension element (7) will be those that provide stability to the kinetic part (1); that is, they prevent the kinetic part (1) from having a rotational movement on its own longitudinal axis; therefore, the portion of the suspension medium (7) that is housed in the third cavity (6), must remain completely fixed. In this case, it was decided by a "T" shaped configuration, for the third cavity (6) and the clamping and suspension element (7).

It should be noted that the suspension means (7) must be constructed with a solid rectangular or square profile, since this shape allows sliding only in the radial direction, without tolerance of angular variation of the kinetic part (1) when they are in rotational motion .

It is important to mention that the rolling elements (3 and 5) must be attached to the kinetic part (1) in such a way that said rolling elements (3 and 5) rotate freely on their rotation axes. Therefore, the means that hold the rolling elements (3 and 5) can be conventional fastening bolts (9 and 10), which are fixed to the walls of the kinetic part (1) in a conventional manner. The representation of this kinetic piece (1) is merely illustrative, which is not a limitation for the design and construction of said piece (1), because for a person skilled in the art, there may be many other forms of design and construction , so that such designs are included in the scope of the spirit of the present invention. Likewise, the bearing elements (3 and 5) can be selected from the following group: wheels, solid tires, pneumatic tires, roller bearings, pellets, needles, balls or spheres, among others that may be useful for the purposes of the present invention.

The apparatus in question also comprises a device that transmits a linear movement (11), the configuration of which is suitable for being driven by the kinetic part (1), by direct contact with its first rolling means (3); An example of that device that transmits linear motion can be a cam (11) like the one illustrated in Figure 7.

If necessary, the kinetic part (1) may have a perimeter groove (33) in those parts of its edges that make contact with the device that transmits linear motion (11); for example at the edge of the end where not there are rolling elements; in such a way that the cam part (11), in this case, that comes to make contact with the edge of the piece (1) is introduced slightly in said perimeter groove (33), thus avoiding contact between them.

Finally, said apparatus must have a device (12) that receives the linear movement from the device (11), whereby said device that receives the linear movement (12) is in contact with said device that produces it (11), more specifically at one end of said device (11). An example of this type of device that receives linear movement (12), can be a compression unit (12) or similar, whose function is to compress fluids, preferably fluids in a gaseous state, such as air. Where said compression unit (12) is conventionally formed by a piston (16) with its respective arm (13) and its sleeve (14), where the cooling system not illustrated is integrated into the container (30).

B. Mechanism for compressing gaseous fluids.

Therefore, one of the many applications that this device could have to convert energy inertia! Rotational, in linear motion with the ability to perform work, in accordance with the present invention, is the construction of a mechanism for compressing gaseous fluids, where said mechanism comprises at least two apparatus for converting inertial energy in motion, in motion. linear with ability to perform work, described in this invention; where said apparatus are placed equidistant from each other and in a compensatory manner, see figure 12. Therefore, this mechanism for compressing gaseous fluids is part of the object of the present invention.

For this, the mechanism requires a mechanism that provides centrifugal movement to the kinetic parts (1); where said mechanism that gives the movement, can be formed of: a rotating central arrow (28), the which is attached to the arrow (39) of a conventional rotary actuator rotor (22) or other means that provide rotational movement to the central arrow (28); the union is by means of a toothed copy (37); and a rotating support (8) with a central perforation (17) that projects in a slight tubular extension (47), is inserted by means of the central perforation (17) in the central arrow (28) and is fixed by means of any suitable clamp (38) that is inserted transversely in the tubular extension (47) (like a bolt), to said arrow (28), so that by turning the central arrow (28) it also rotates the rotating support (8 ). Therefore, said rotating support (8) also comprises at least two transverse cavities (31) into which the free ends of the clamping and suspension means (7) of the kinetic parts (1) are introduced, in such a way that the rotating support (8) in turn causes the kinetic parts (1) with their respective rolling means (3 and 5) to rotate in a centrifugal manner around it; whereby said kinetic pieces (1) must be suspended to the rotating support (8) in an equidistant manner between them, and perfectly compensated, so that there is no imbalance at the time they are in their centrifugal movement. The rotating support (8) also has limbs that push the second rolling elements (5) to give greater stability to the kinetic parts (1) and reduce efforts on the sliding cover (15).

The sliding cover (15) suspends the free end of the suspension means (7) that is inside the transverse cavity (31) of the rotating support (8), whereby said sliding cover (15) is previously placed inside the cavity (31) with radial direction with respect to the rotating support (8), whereby said suspension means (7) have radial sliding inside the transverse cavities (31) of the center of the rotating support (8) but without reaching the central perforation (17), that is to say without making contact with the rotating arrow (28); b) that the kinetic pieces (1) are independent of each other. & therefore, said centrifugal parts (1) are suspended to the rotating support (8). It should be noted that it is preferred that the transverse cavity (31) and the sliding cover (15) have the quadrangular shape, to coincide with the shape of the free end of the clamping and suspension means (7) and thus give proper balance to the kinetic parts (1) when they are rotating.

An example of construction of the rotating support (8) in question can be a rotor (8) in the form of a blade, consisting of two equal pieces, obvious in the form of symmetrical blades; however, said rotating support (8) can have at least two blade-shaped ends, which make contact with the second rolling element (5) of the kinetic parts (1), this to give greater stability to said parts (1) when they are in centrifugal movement, another function of the rotating support (8) is to minimize the internal stresses that the sliding cover (15) will assume. The way of joining the two rotor parts (8) is conventionally as a sandwich; But this suggestion is to facilitate its manufacture, so there may be other ways to build it, which are also included in the protection of the present invention.

Placing in this way the kinetic parts (1) and that their sliding suspension means (7) have no contact with each other, nor are fixed to the rotating support (8), as with conventional compressors; we achieve that in this invention the torque force provided by the rotational actuator (22) is better used, since due to this, the kinetic parts (1) take advantage of their own useful centrifugal force, and therefore have greater working capacity to perform the linear displacement of the cam (11) and do so with very little energy consumed by the rotary actuator (22).

The mechanism in question also requires a fixed support (18) that supports, at least, two devices to convert in-sltu rotational inertial energy, into a linear movement capable of performing work, and allowing the kinetic pieces to be rotated ( 1), in addition to holding the cams (11) in a position that make contact with the first rolling element (3) and in turn are in contact with the conventional compression unit (12), same which receives the linear movement, and therefore takes advantage of the centrifugal force provided by the kinetic part (1) to perform the utilitarian work.

An example of this fixed support (18) is like the one illustrated in Figures 8 and 9, which is circular in shape and is configured of: a first platform (19); a second platform (20) of smaller diameter rises concentrically on one of the faces of said first platform (19); the second platform (20) has at least two peripheral hangers (21) located equidistant from each other; A ring (23) is provided on the second platform (20) and is smaller in diameter with respect to said second platform (20). The ring (23) delimits an area (24) and in the center of the area there is a perforation (27). Within the area (24) the rotating support (8) is housed, locating its perforation (17) that coincides with the perforation (27) of the fixed support (18) to be crossed by the rotating central arrow (28). The kinetic pieces (1) are suspended in the rotating support (8) equidistant from each other, within the area (24) delimited by the ring (23). Therefore, said ring (23) has at least two longitudinal grooves (25) in its lower part and located where the hangers (21) are, to place a cam (11) in each groove (25); wherein said cam (11) is suspended on the second platform (20) by means of one of its ends with a conventional pivot bolt (26) whose function is to hold the cam (11) allowing it to have angular movement; but said angular movement is controlled by a stop (40), which is placed externally of the ring (23), in the hangover (21), of the second platform (20). With the hangovers (21) on the second platform (20) it is avoided that there is friction of the cam (11) with the surface of the second platform itself (20).

The mechanism for compressing a gaseous fluid comprises a container (30) where the device receiving the linear movement is housed, in this case the compression unit (12); whereby said container (30) is fixed on the free surface of the face of the first platform (19), and in a position that facilitates the sliding of the plunger (16) with its respective arm (13), of the compression unit (12); where the jacket (14) of the compression unit is inside the container (30) and this in a conventional manner will have the appropriate cooling system included (not shown).

With the arrangement of the kinetic pieces (1) a kind of kinetic flywheel is generated, which, when in centrifugal motion, normally centrifugal and centripetal forces occur that cancel themselves; but because the centrifugal parts (1) are not fixed (but suspended) to the rotating support (8), the centrifugal force that they act before they are nullified is used, this use is due to the kinetic parts (1) they move the cams (11) that have the ability to drive the compression units (12), which compress air inside a conventional compressor and in this way the utilitarian work is carried out.

The mechanism of the present invention additionally comprises a compression unit of gaseous fluids (not shown) of lower compression capacity, in each of the compression units (12), which is connected to the filling or air supply valves of said compression unit (12), this in order to fill with new air and with the speed required to return the cam (11) in its initial position. It should also be noted that the other valve of the compression unit (12) is the pressurized air outlet valve, and this is connected to a tank (not shown) that stores the air at high pressure.

Finally, the mechanism in question comprises a cover (29) to cover the area (24) where the kinetic parts (1) suspended from the rotating support (8) are housed, whereby said cover (29) is fixed on the upper edge of the ring (23). Said cover (29) comprises a central perforation (43) so that the rotating central arrow (28) passes to interconnect to other elements, such as several apparatus for compressing gaseous fluids. With this gaseous fluid compressor mechanism, in question, one of the advantages is that the rotational actuator (22) is not the one who applies more force to the compression units (12), with this advantage it allows us to operate with ease 10 Compressor mechanisms or more, placed along the same central rotor arrow (28) and operated with the same rotary actuator (22), while the competition can only drive 2 or 3 pneumatic actuators; the other advantage lies in the amount of force that will be applied in the pistons (16), this can be greatly overcome, which currently drives the conventional compressors. With this device, forces of up to 15,000 N or greater can be applied easily.

It is obvious to note that the mechanism that provides the rotating movement must have conventional elements to allow the central rotating arrow (28) to freely rotate on its own longitudinal axis. For example, a first radial bearing (41) is placed between the edge of the bore (27), of the fixed support (18), and the central arrow (28) to give the free rotating movement to said central arrow (28). Another example of bearing elements, is to place in the lower part of the first platform (19), of the fixed support (18), next to the central arrow (28), and a first bearing container (42) that contains in its inside an axial and radial bearing (not illustrated) to prevent said arrow (28) from sliding linearly on its own longitudinal axis. In the upper or outer part of the cover (29) of the fixed support (18), next to the free end of the central arrow (28) a second axial and radial bearing container (44) is held, which, like the first container (42), has axial and radial bearings that suspend the central arrow (28) at the opposite end of the toothed copy (37), thus preventing the central rotor arrow (28) from sliding in the direction of its central axis.

Therefore, the mechanism of the present invention requires an electric power source (not shown) to feed the rotary actuator (22) and that it provides the rotary movement to the rotating central arrow (28), which in turn, it rotates the rotating support (8), and this in turn provides centrifugal movement to the kinetic pieces (1), which, each, give a linear (angular) movement to the device that provides the linear movement (11 ) and this in turn gives linear movement to the compression unit (12) which in turn will compress a high pressure gaseous fluid.

An example of this rotational actuator (22) may be a conventional electric motor itself that provides the appropriate rpm for each mechanism design.

With the realization of this apparatus to convert in situ rotational inertial energy, into linear motion with the ability to perform a job; and of this mechanism for compressing gaseous fluids, in accordance with the present patent application, the way has been achieved to considerably increase the efficiency of current compressors and lower the cost in the production of large volumes compressed air at high pressure.

The compressed air inside a large tank has the capacity to provide useful mechanical energy, it does so by moving pistons of larger diameters, which provide greater utilitarian forces to the outside, and these can be used in the propulsion of vehicles, mobiles, industrial machines and hydropneumatic, etc.

C. Compressing machine for gaseous fluids.

Another object of the present invention is the construction of a more complex mechanism for compressing a gaseous fluid, which we will call a gaseous fluid compressor, where said machine comprises at least two mechanisms for compressing gaseous fluids, as described in the present invention To build a gas fluid compressor, an external stator support structure (34) is required, and at least two mechanisms for compressing gaseous fluids, such as the detailed description of this invention, so that the size and number of compartments of said external stator structure (34) will depend on the number of mechanisms to include. In this case, the construction of a compressor machine with two mechanisms for compressing gaseous fluids is exemplified, figures 15, 16 and 17.

In this case, the machine comprises a structure (34) as shown in Figure 16, which has 8 vertical supports (35) distributed equidistant from each other, delimiting an interior area where 4 horizontal transverse supports (32, 36, 45 and 46) separated from each other, enough to form three compartments where a mechanism for compressing fluids is placed, in each of the upper compartments, since in the lower compartment the rotational actuator (22) is placed with its arrow (39) and the toothed copy (37) that joins them with the central rotating arrow (28). In the center of the horizontal transverse supports (32) there is a perforation (not illustrated) so that the central arrow (28) passes and reaches the upper horizontal support (46). The first bearing container (42) is placed at the point where it crosses the central arrow (28) of the horizontal support (36), which is where a first fluid compressor mechanism is to be placed on said support (36); The second bearing container (44) is placed at the point where the arrow (28) of the horizontal support (46) arrives.

A second mechanism for compressing gaseous fluids is placed on the horizontal support (45); whereby the central arrow (28) crosses both devices through their respective perforations (17 and 43); and at the point where the central arrow (28) passes, a third bearing container (not shown) is placed which contains only a radial bearing. This is an illustrative example of how to build the machine with various mechanisms to compress gaseous fluids, whose shapes, dimensions, arrangements of the apparatus, materials, etc., can be in any other way as desired.

Claims

1. A device to convert inertia energy in situ! rotational, with linear movement with the capacity to perform work, said device is characterized in that it comprises: a kinetic piece (1), whose shape and assembly allows it to rotate centrifugally with, at least, another identical kinetic piece (1), located and suspended equidistantly from each other, in a mechanism that provides them with centrifugal movement; The kinetic piece (1) in turn comprises:

a) a first cavity (2) in one of its lateral sides;

b) a first rolling element (3) is partially housed in the first cavity (2), placed in an orthogonal plane with respect to the central axis of rotation of the mechanism that provides the centrifugal movement, and parallel to the plane of rotation of the piece itself kinetics (1);

c) a second cavity (4) at one of its ends; d) at least one second rolling element (5) is partially housed in the second cavity (4), placed in an orthogonal plane in relation to the central axis of rotation of the mechanism that provides the centrifugal movement, and parallel to the plane of rotation of the kinetic piece itself (1);

e) a third cavity (6) on its other lateral side; and f) part of a fastening and suspension element (7) is housed and held in the third cavity (6), while the other part is inserted into the mechanism that gives the rotary movement, to attach in a suspended manner to said kinetic part. (1) with such mechanism;

a device that transmits linear movement (11), whose configuration is suitable to be activated by the kinetic part (1), through direct contact with the first rolling means (3); and iii) a device (12) that receives the linear movement coming from the device that transmits linear movement (11), whereby the device that receives the linear movement (12) is in contact with the device (11), more specifically in one of the ends of the device (11).

2. The apparatus of the preceding claim, wherein the kinetic piece (1) is substantially oval, configured by two halves equal to each other and joined together like a sandwich.

3. The apparatus according to claim 1, where the shape and dimensions of the third cavity (6) and the fastening and suspension element (7) will be those that provide stability to the kinetic part (1), to prevent the kinetic piece (1) tends to have rotary movement about its own longitudinal axis, therefore, the portion of the suspension means (7) remains fixed in the third cavity (6).

4. The apparatus of the preceding claim, wherein the third cavity (6) and the suspension element (7) have a "T"-shaped configuration.

5. The apparatus according to the previous claim, where the fastening and suspension means (7) is constructed with a solid rectangular or square profile, since this shape allows sliding only in the radial direction, without tolerance for angular variation of the kinetic piece (1) when it is in centrifugal motion.

6. The apparatus as claimed in claim 1, wherein the rolling elements (3 and 5) must be attached to the kinetic part (1) in such a way that said rolling elements (3 and 5) rotate freely on their axes. rotation; where the means that hold the rolling elements (3 and 5) are holding bolts (9 and 10), which are fixed to the walls of the kinetic part (1).

7. The apparatus according to the preceding claim, wherein the rolling elements (3 and 5) are selected from the following group: wheels, solid tires, pneumatic tires, roller bearings, pellets, needles, balls and spheres.

8. The apparatus according to claim 1, characterized in that the kinetic part (1) further comprises a perimeter groove (33) in those parts of its edges that could make contact with the device that transmits linear movement (11), to avoid contact between them.

9. The apparatus according to claims 1 and 8, wherein the device that transmits linear movement (11) is a cam.

10. The apparatus according to claim 1, wherein the device that receives the linear movement is a gaseous fluid compression unit (12).

11. The apparatus of the preceding claim, where the compression unit (12) is made up of a piston (16) with its respective arm (13) and its sleeve (14).

12. A mechanism for compressing gaseous fluids, characterized in that it comprises: i) at least two devices to convert in situ rotational inertial energy into linear motion with the capacity to perform work, in accordance with any of the preceding claims; where said devices are placed equitably from each other;

ii) a mechanism that provides centrifugal movement to the kinetic parts (1) of the devices to convert inertial energy in situ rotational, in linear motion with the capacity to do work;

iii) a fixed support (18) that supports the devices to convert in-situ rotational inertial energy into linear movement with the capacity to perform work;

iv) a lower capacity gas fluid compression unit, in each of the gas compression units (12), which is connected to the filling or air supply valves of said compression units (12), to fill with air with the required speed and return the device that transmits linear movement (11) to its initial position;

v) a tank that stores the high-pressure air that comes from the pressurized air outlet valve of the compression unit (12); and

vi) an energy source provides energy to the mechanism that provides centrifugal motion.

13. The mechanism of the preceding claim, wherein the mechanism that provides centrifugal movement to the kinetic parts (1), comprises: i) a rotating central arrow (28);

ii) a rotating support (8) activated by the central arrow (28); where said support (8) has a central perforation (17) that projects into a slight tubular extension (47), to be inserted and fixed in the rotating central arrow (28) by means of a fastening means (38) that is inserted transversely in the tubular extension (47); said rotating support (8) also comprises at least two transverse cavities (31) equidistant from each other, into which the free ends of the suspension means (7) of the kinetic parts (1) are introduced; and also has at least two ends to push the second rolling element (5); iii) a sliding sleeve (15) is inserted into each transverse cavity (31) to suspend the free end of the suspension means (7) that remains inside the transverse cavity (31), from the rotating support (8), thereby which, said suspension means (7) have radial sliding within the transverse cavities (31) of the center of the rotating support (8), but without making contact with the central rotating arrow (28);

iv) a rotational actuator rotor (22) provides rotary movement to the central shaft (28); and

v) a toothed copy (37) connects the central rotating arrow (28) with the arrow (39) of the actuator rotor (22).

14. The mechanism of the preceding claim, where the rotating support (8) is a rotor in the shape of a blade, made up of two equal pieces joined together like a sandwich.

15. The mechanism of claim 13 and 14, where the transverse cavity (31) and the sleeve (15) have a quadrangular shape, to coincide with the shape of the free end of the fastening and suspension means (7) and thus give proper balance to the kinetic parts (1) when they are rotating centrifugally.

16. The mechanism of claim 12, wherein the fixed support (18) comprises: i) a first platform (19);

ii) a second platform (20) of smaller diameter rises concentrically on one of the faces of the first platform (19); the second platform (20) has at least two peripheral recesses (21) located equidistant between them;

iii) a ring (23) is provided on the second platform (20) and is of smaller diameter than the second platform (20), to delimit a area (24) in the center of which there is a perforation (27); The rotating support (8) is housed within the area (24), locating its perforation (17) that coincides with the perforation (27) of the fixed support (18), to be crossed by the rotating central arrow (28); and the kinetic pieces (1) that are suspended in the rotating support (8) located equidistant from each other; said ring (23) has at least two longitudinal slots (25) in its lower part and located where the undercuts (21) are, to place a cam (11) in each slot (25);

iv) a pivot bolt (26) suspends the cam (11) on the second platform (20), through one of the ends of said cam (11), whereby the cam has angular movement;

v) a stop (40) controls the angular movement of the cam (11), so it is placed externally of the ring (23) in the recess (21) of the second platform (20);

vi) a container (30) where the device that receives the linear movement is housed, in this case the compression unit (12); therefore said container (30) is fixed on the free surface of the face of the first platform (19), and in a position that facilitates the sliding of the plunger (16) with its respective arm (13), of the unit. compression (12); and

vii) a cover (29) with a central perforation (43), to cover the area (24) where the kinetic parts (1) suspended from the rotating support (8) are housed, so said cover (29) is fixed in the upper edge of the ring (23).

17. The mechanism according to claims 12, 13 and 16, wherein the mechanism providing the rotary movement comprises bearing means to allow the rotating central shaft (28) to rotate freely about its own axis.

18. The mechanism of the previous claim, where the bearing means are: a first radial bearing (41) placed between the edge of the perforation (27), of the fixed support (18), and the central rotating arrow (28); a first bearing container (42) containing a radial bearing and an axial bearing, is placed at the bottom of the first platform (19), of the fixed support (18), next to the central rotating shaft (28); and a second bearing container (44), like the first container (42), is placed on the top of the cover (29) of the fixed support (18), next to the central arrow (28), to help the rotation of such central arrow (28) and keeping it suspended by its opposite end to the toothed copy (37).

19. A gaseous fluid compression machine, characterized in that it comprises: i) at least two mechanisms for compressing gaseous fluids, in accordance with any of claims 12 to 18; and ii) an external stator support structure (34), configured to support at least two mechanisms for compressing gaseous fluids.

20. The machine of the preceding claim, wherein the stator support structure (34) comprises: i) vertical supports (35) distributed radially and equidistantly from each other, delimiting an interior area where they are fixed;

ii) at least three horizontal transverse supports separated from each other, enough to form compartments where a mechanism to compress fluids is placed, in each of the upper compartments, since the rotational actuator (22) is placed in the lower compartment with its arrow (39) and the toothed copy (37) that joins the arrow (39) of the actuator (22) with the central rotating arrow (28); iii) a perforation is provided in the center of the horizontal transverse supports so that the central rotating arrow (28) passes through and reaches the upper horizontal support (46);

iv) a first bearing container (42) is placed at the point where the central arrow (28) of the horizontal support (36) crosses, which is where a first fluid compression mechanism is going to be placed on said support (36); and

v) a second bearing container (44) is placed at the point where the arrow (28) of the horizontal support (46) reaches.

21. The machine of the preceding claim, characterized in that it comprises a third bearing container, which contains only a radial bearing, and is placed in the lower part of the platform (19) of the second mechanism for compressing gaseous fluids, together with the central arrow (28).