WO2017217834A1 - Appareil, mécanisme et machine pour comprimer des fluides gazeux - Google Patents

Appareil, mécanisme et machine pour comprimer des fluides gazeux Download PDF

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Publication number
WO2017217834A1
WO2017217834A1 PCT/MX2016/000060 MX2016000060W WO2017217834A1 WO 2017217834 A1 WO2017217834 A1 WO 2017217834A1 MX 2016000060 W MX2016000060 W MX 2016000060W WO 2017217834 A1 WO2017217834 A1 WO 2017217834A1
Authority
WO
WIPO (PCT)
Prior art keywords
kinetic
arrow
central
support
rotating
Prior art date
Application number
PCT/MX2016/000060
Other languages
English (en)
Spanish (es)
Inventor
José Guillermo CASTRO GONZÁLEZ
Original Assignee
BARRAZA SÁMANO, María Delia
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BARRAZA SÁMANO, María Delia filed Critical BARRAZA SÁMANO, María Delia
Priority to PCT/MX2016/000060 priority Critical patent/WO2017217834A1/fr
Priority to MX2018013908A priority patent/MX2018013908A/es
Publication of WO2017217834A1 publication Critical patent/WO2017217834A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/02—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having two cylinders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/12—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B9/00—Piston machines or pumps characterised by the driving or driven means to or from their working members
    • F04B9/02—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical
    • F04B9/04—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical the means being cams, eccentrics or pin-and-slot mechanisms

Definitions

  • 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.
  • 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.
  • 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.
  • 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.
  • 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).
  • 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 .
  • 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.
  • 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);
  • a device that transmits linear motion can be a cam (11) like the one illustrated in Figure 7.
  • 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.
  • 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).
  • a device (12) 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.
  • 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).
  • 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 ).
  • 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).
  • 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.
  • 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.
  • 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).
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • This rotational actuator (22) may be a conventional electric motor itself that provides the appropriate rpm for each mechanism design.
  • 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.
  • 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
  • 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.
  • the construction of a compressor machine with two mechanisms for compressing gaseous fluids is exemplified, figures 15, 16 and 17.
  • 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.

Abstract

L'invention concerne un appareil destiné à la conversion in situ d'énergie inertielle rotationnelle en mouvement linéaire permettant de réaliser un travail, constitué par : une pièce cinétique (1), dont la forme et l'ensemble lui permettent de tourner de manière centrifuge avec au moins une autre pièce cinétique (1) identique, dans un mécanisme à mouvement centrifuge; un dispositif transmettant le mouvement linéaire (11), actionné par la pièce cinétique (1); et un dispositif (12) recevant le mouvement linéaire. L'invention concerne également un mécanisme destiné à comprimer des fluides gazeux, comprenant : au moins deux appareils pour la conversion in situ d'énergie inertielle rotationnelle en mouvement linéaire permettant de réaliser un travail, selon la présente invention; un mécanisme imprimant un mouvement centrifuge auxdits appareils; un support fixe (18) qui soutient lesdits appareils; un réservoir permettant de stocker l'air haute pression provenant de la valve de sortie d'air sous pression de l'unité de compression (12); et une source d'énergie fournissant de l'énergie au mécanisme qui imprime le mouvement centrifuge. L'invention se rapporte en outre à une machine de compression de fluides gazeux, comprenant : au moins deux mécanismes de compression de fluides gazeux, selon la présente invention; et une structure (34) qui soutient les appareils de compression de fluides gazeux.
PCT/MX2016/000060 2016-06-14 2016-06-14 Appareil, mécanisme et machine pour comprimer des fluides gazeux WO2017217834A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PCT/MX2016/000060 WO2017217834A1 (fr) 2016-06-14 2016-06-14 Appareil, mécanisme et machine pour comprimer des fluides gazeux
MX2018013908A MX2018013908A (es) 2016-06-14 2016-06-14 Aparato, mecanismo y máquina para comprimir fluídos gaseosos.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/MX2016/000060 WO2017217834A1 (fr) 2016-06-14 2016-06-14 Appareil, mécanisme et machine pour comprimer des fluides gazeux

Publications (1)

Publication Number Publication Date
WO2017217834A1 true WO2017217834A1 (fr) 2017-12-21

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Application Number Title Priority Date Filing Date
PCT/MX2016/000060 WO2017217834A1 (fr) 2016-06-14 2016-06-14 Appareil, mécanisme et machine pour comprimer des fluides gazeux

Country Status (2)

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MX (1) MX2018013908A (fr)
WO (1) WO2017217834A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019164386A1 (fr) * 2018-02-22 2019-08-29 BARRAZA SÁMANO, María Delia Volant d'inertie, unité et système mécanico-cinétiques qui exploitent la force centrifuge du volant d'inertie
WO2021162539A1 (fr) * 2020-02-11 2021-08-19 Castro Gonzalez Jose Guillermo Masses inertielles et volant d'inertie libérant une force centrifuge, pour systèmes mécaniques cinétiques

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000019096A1 (fr) * 1998-09-29 2000-04-06 Pressel Hans Georg G Systeme de compresseur d'air
US20030072654A1 (en) * 2001-10-12 2003-04-17 Pressel Hans-Georg G. Shuttle piston assembly with dynamic valve
US20070251379A1 (en) * 2004-05-21 2007-11-01 Lund Morten A Air Compression Apparatus and Method of Use
WO2009086051A2 (fr) * 2007-12-21 2009-07-09 Carleton Life Support Systems Inc. Compresseur radial à came et ensembles compresseurs à cames
US20150198185A1 (en) * 2011-10-18 2015-07-16 Lightsail Energy, Inc. Compressed gas energy storage system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000019096A1 (fr) * 1998-09-29 2000-04-06 Pressel Hans Georg G Systeme de compresseur d'air
US20030072654A1 (en) * 2001-10-12 2003-04-17 Pressel Hans-Georg G. Shuttle piston assembly with dynamic valve
US20070251379A1 (en) * 2004-05-21 2007-11-01 Lund Morten A Air Compression Apparatus and Method of Use
WO2009086051A2 (fr) * 2007-12-21 2009-07-09 Carleton Life Support Systems Inc. Compresseur radial à came et ensembles compresseurs à cames
US20150198185A1 (en) * 2011-10-18 2015-07-16 Lightsail Energy, Inc. Compressed gas energy storage system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019164386A1 (fr) * 2018-02-22 2019-08-29 BARRAZA SÁMANO, María Delia Volant d'inertie, unité et système mécanico-cinétiques qui exploitent la force centrifuge du volant d'inertie
WO2021162539A1 (fr) * 2020-02-11 2021-08-19 Castro Gonzalez Jose Guillermo Masses inertielles et volant d'inertie libérant une force centrifuge, pour systèmes mécaniques cinétiques

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