LU93016B1 - Appareil de spécifications qui transforme l'énergie dans les gaz comprimés en un mouvement de rotation - Google Patents

Appareil de spécifications qui transforme l'énergie dans les gaz comprimés en un mouvement de rotation Download PDF

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Publication number
LU93016B1
LU93016B1 LU93016A LU93016A LU93016B1 LU 93016 B1 LU93016 B1 LU 93016B1 LU 93016 A LU93016 A LU 93016A LU 93016 A LU93016 A LU 93016A LU 93016 B1 LU93016 B1 LU 93016B1
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movements
pressure
compressed gas
oscillation
gases
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LU93016A
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French (fr)
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LU93016A1 (en
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Mustafa Dayanik
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Mustafa Dayanik
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H21/00—Gearings comprising primarily only links or levers, with or without slides
    • F16H21/10—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane
    • F16H21/16—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane for interconverting rotary motion and reciprocating motion
    • F16H21/18—Crank gearings; Eccentric gearings
    • F16H21/34—Crank gearings; Eccentric gearings with two or more connecting-rods to each crank or eccentric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G4/00—Devices for producing mechanical power from geothermal energy
    • F03G4/074—Safety arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/10—Alleged perpetua mobilia

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Energy (AREA)
  • Transmission Devices (AREA)

Description

THE SPECIFICATIONS
APPARATUS THAT TRANSFORMS THE ENERGY IN THE COMPRESSED GASES INTO ROTATIONAL MOTION
Tecnical area
This invention is aboutthe mechanical set up which makes the transformation of the existing potential energy in the compressed gases into kinetic energy without subjecting to chemical reaction.
Previous technique
Nowadays the transformation of linear force into rotational motion is made whit common, classic crankshafts. The crankshaft is an eccentric shaft and it is the element that converts the reciprocation of the pistons into rotational motion. It affects rotational motion as much as the intensity of the linear force. The crankshaft is one of the most expensive and important parts of all the machines. If the crankshaft is damaged, it is not possible to fix it and also the deformations that will appear in the manufacturing cannot be fixed later on. As for the other system; the piston that moves up and down on a center axis and this movement makes the rotational motion with the mechanism that converts into rotational motion on the same center axis via circular rail profile that continues agitational. This system facilitates the transformation of the up and down linear motion into rotational motion, but it does not add power to the rotational motion. Also there are manufacturing and installation difficulties besides the depreciation and friction losses as it is made of many elements. There is a technique, which I have its patent, with examination under the number of TR2009/07688 B. In this technique there are some problems of production and vibration that are problematic to solve. And this technique is the most ideal technological motor, appropriate for its purpose, in spite of the disadvantage of this technology that it does two jobs in one tour of rotation time in 360 degrees.
The purpose of this device
The purpose of this device is to produce a motor that works whit the pressure force of the compressed gas while converting the potential energy in these compressed gases into kinetic energy without the chemical reaction, without reducing the volume of the compressed gas which is available in its tank.
Explanations of the illustrations
The apparatus that transforms the energy in the compressed gasses into rotational motion are illustrated in the attached illustrations, which are created for the invention to reach its aim. In these illustrations, the dimensions are shown with the (t) symbol which is taken as a base to determine ideal dimensions and shapes of the apparatus, which are appropriate for its function. In accordance with this base (t) dimension, the illustrations that analyses the diagrams and orbits which are drawn about the working principle of the system;
Figure-1: Ml, M4=t/5 and M2, M5=t/5, the eccentric center connected with the M4 center is Ml. The eccentric center connected with the M5 center is M2. The distance between Ml and M2 is (2t) horizontally. Also the distance between M4 and M5 is (2t) which are the eccentric centers horizontally. When M4 and M5 centers rotate in reverse direction to each other in 90 degrees, the distance between Ml and M2 is (2t+z). The sliding length here is the sliding in the M2 center when Ml center is stable. Again, when it rotates in 270 degrees, the distance between Ml and M2 is again (2t+z). This sliding in here is the sliding distance in the Ml center when M2 center is stable. For this reason, the sliding tolerances must be applied in both centers.
Figure-2: M point, where (x) and (y) coordinates intersect, is equal to the distances of disk element (3) to M3, M4 and M5 centers and has the length of(t).
Figure-3; M point, where (x) and (y) coordinates intersect, is equal to the distances of symmetric disk element (4) to M4, M5 and M6 centers and has the length of (t).
The determination of the diagrams that are drawn simultaneously by the M3 center of the disk element (3) that moves connected with the eccentric elements (Al .5) and (A2.5) that move in the opposite direction of each other in their centers end M6 center of the symmetric disc element (4);
Figure-4; The beginning point for the infinity symbol diagram is (Bl) that will be drawn by the M3 point of disk element (3) that makes two-centered motion movement connected with the Ml and M2 eccentric rod of eccentric element (Al .5) whose rotation centers are M4 and M5. Also the beginning point for the infinity symbol diagram is B5 that will be drawn by the M6 point of symmetric disk element (4) that makes two-centered motion movement connected with the Ml and M2 eccentric rod of the eccentric element (A2.5), which is in the reverse symmetry of that.
Figure-5; When the eccentric elements (A1.5) and (A2.5), whose rotation centers are M4 and M5, rotate for the first time in 90 degrees, the disk element (3) draw Cl diagram between B1-B2 and the symmetric disk element (4) draws C5 diagram between B5-B6.
Figure-6; When the eccentric elements (Al .5) and (A2.5), whose rotation centers are M4 and M5, rotate for the second time in 90 degrees, the disk element (3) draw C2 diagram between B2-B3 and the symmetric disk element (4) draws C6 diagram between B6-B7.
Figure-7; When the eccentric elements (A1.5) and (A2.5), whose rotation centers are M4 and M5, rotate for the third time in 90 degrees, the disk element (3) draw C3 diagram between B3-B4 and the symmetric disk element (4) draws C7 diagram between B7-B8.
Figure-8; When the eccentric elements (A1.5) and (A2.5), whose rotation centers are M4 and M5, rotate for the last time in 90 degrees, the disk element (3) draw C4 diagram between B4-B1 and the symmetric disk element (4) draws C8 diagram between B8-B5.
Determining eccentric distance of the shuttle element (Al .2)
Figure-9; (B3) Point is the point where the motion diagram in 180 degrees ends. The distance between B3 and B4 points is motion diagram in 90 degrees. The eccentric center of shuttle element (A 1.2) has to be in an equal distance to (B3), which is the start point, and B4 point, is the end the diagram in 90 degrees. As the orbit of the center of shuttle element (A 1.2) is diagram, the diameter of the circle, which is tangent to the end point of the diagram from D2 point, is the eccentric sliding distance of shuttle element (A1.2). This distance is determined as (r=t/12). The position of the shuttle element (Al .2) in the D2 and M9 axis is the end of its D2 centered rotation counter clockwise, and it is the starting location of its clockwise rotation.
Figure-10; (B2) Point is the point where the motion diagram in 90 degrees ends. The distance between B2 and B3 point is the second motion diagram in 90 degrees. B4 point is the point where motion diagram in 270 degrees ends. The distance between B4 and BI point is the fourth motion diagram in 90 degrees. The intersection point of B2, B3 and B4, BI diagrams is the D3 point on axis (x). D4 point, which the circle with the diameter of (r=t 12) that is drawn from this point cuts the (x) axis, as it is equally distant from both diagrams, is the eccentric center of the shuttle element (A 1.2). The shuttle element (A 1.2) makes its two-way motions throughout the straight lines of these two diagrams.
Figure-11; (BI) Point is the beginning point of motion diagram. The distance between BI and B2 points is the motion diagram in 90 degrees. The eccentric center of shuttle element (A 1.2) has to be in an equal distance to (BI), which is the start point, and B2 point, which is the end point of the diagram in 90 degrees. As the orbit of the center of shuttle element (A 1.2) is diagram, the diameter of the circle which is tangent to the diagram’s end point from DI point, is the eccentric sliding distance of shuttle element (Al .2). This distance is determined as (r=t/l 2). The position of the shuttle element (A 1.2) in the DI and M10 axis is the end of its DI centered rotation counter clockwise, and it is the starting location of its counter clockwise rotation.
Determining the oscillation axis of the hammer (A 1.1) and oscillation boundary, Figure-12; The determined eccentric centers of shuttle element (A1.2) are DI, D2 and D4. The center of the circle which is passing these points is on the (x) axis and is Ml 1, which is the oscillation axis. The straight line that combines DI and Ml 1 points is the tip oscillation boundary counter clockwise and the straight line that combines D2 and Mil points is the tip oscillation boundary counter clockwise and it happens between these two straight lines.
The explanation of the creation of the opposing forces made by apparatus Al; Figure-13; When the center of the shuttle element (A 1.2) of the accelerating mechanic system comes to the rotation point (BI) on the diagram it has drawn, the straight line of oscillation axis, which passes the fixed and joint point (Ml 1) of the hammer element (Al. 1) that moves connected to the eccentric center of the shuttle element (Al .2) makes an angle of 15.6° with the straight line of tip oscillation axis. The system is balanced at the position when the straight line which combines the rotation point (BI) and eccentric center of the shuttle element (Al .2) makes the (v) angle in the eccentric center of the shuttle element (A1.2) with the straight line of oscillation axis of hammer element (Al. 1).
When the eccentric elements (A1.5) that move connected to the gear group (6) of the accelerating system rotate reversely to each other, they accelerate the disc element (3) clockwise and as the shuttle element (A 1.2) in its bearing with the center (M3) is connected to the hummer element (Al .1) from the eccentric center and all the distances to this points are fixed, it has to rotate around its center clockwise. While the shuttle element (A 1.2) makes this movement, load tip of eccentric center, the center of motion the point of this straight line which cuts the orbit turn into a leverage with a forge tip (k), the (v) angle widens.
Fixed (Ml 1) and jointed center of the oscillation axis of hummer element (A 1.1) which moves according to the leverage principles always be the bearing point, it changes according to the position of the other two tip oscillation distance. If its movement is counter clockwise from the tip oscillation angle clockwise; The point in the range (CK1) of 7Tangle is the force tip, it turns into a leverage which works as a tip load in the range of 15.6óangle. The pistons (16a-16b) of the apparatus (Al) are connected to (CK1) point via piston rods (17a-17b).
When apparatus is in this position, its (v) angle grows when it transmits the gas pressure force to disc element (3) which moves clockwise which the shuttle element (A 1.2) is connected. The buoyancy force rate of the leverage system created by the force that continues its rotation clockwise in its center of the shuttle element (A 1.2) is bigger than the buoyancy force rate of the leverage system created by the hammer element (Al. 1). The opposing force which is created via this technique constantly produces the compression force which is needed to compress the gases, as a feature of the system, until it completes the range of 15.6°angle. The rotation point (Bl) and these functions that are created after that accelerate the apparatus (Al), which enables it repeating exactly, symmetrically in the rotation point (B3) of the diagram where it has a range of 180° angle, the system in one tour of time for two times.
Determining the eccentric distance of the symmetric shuttle element (A2.2); Figure-14; (B8) point is the point where the motion diagram in 270 degrees ends. The distance between (B8) and (B5) points is motion diagram in 90 degrees. The eccentric center of the shuttle element (A2.2) must have equal distance to beginning (B8) and the end point (B5) of the diagram in 90 degrees. As the orbit of the shuttle element’s (A2.2) center is a diagram, the diameter of the circle which is tangent to the end point of the diagram from the (G2) point is the eccentric shifting distance of the shuttle element (A2.2). This distance is determined as (r=t/l 2). The position of the shuttle element (A2.2) in the (G2) And (N9) axis is the end of counter clockwise rotation with (G2) center, clockwise is the beginning position of the rotation.
Figure-15; (B7) point is the point where the motion diagram in 180 degrees ends. The distance between (B7) and (B8) points is the third motion diagram in 90 degrees. (B5) point is the point where the motion diagram in 360 degrees ends. The distance between (B5) and (B6) points is the first motion diagram in 90 degrees. The intersection point of (B7), (B8) and (B5), (B6) diagrams is the (G3) point on the (x) axis. As (G4) point, which cuts the (x) axis of the circle with a diameter of (r=t/12) which is drawn from the mentioned point, has equal distance to both diagrams, it is the eccentric center of the shuttle element (A2.2). The shuttle element (A2.2) makes its two-way motions throughout this diagram line.
Figure-16; The distance between (B6) and (B7) points is the second motion diagram in 90 degrees. The eccentric center of the shuttle element (A2.2) must have equal distance to the beginning point (B6) and end point (B7) of the second diagram in 90 degrees. As the orbit of the shuttle element’s (A2.2) center is a diagram, the diameter of the circle which is tangent to the end point of the diagram from the (GI) point is the eccentric shifting distance of the shuttle element (A2.2). This distance is determined as (r=t/12). The position of the shuttle element (A2.2) in the (GI) and (N10) axis is the end of clockwise rotation of the shuttle element (A2.2) with (GI) center, counter clockwise is the beginning position of the rotation.
Determining the oscillation axis of the hammer (A2.1) and oscillation boundary; Figure-17; The determined eccentric centers of shuttle element (A2.2) are (GI), (G2) and (G4). The center of the circle which is passing these points is on the (x) axis and is (N11) which is the joint oscillation center. The straight line that combines (GI) and (Nil) points is the tip oscillation boundary counter clockwise and it happens between these two straight lines.
The explanation of the creation of the opposing forces made by apparatus A2; Figure-18; When the center of the shuttle element (A2.2) of the accelerating mechanic system comes to the rotation point (B6) on the diagram it has drawn; the straight line of oscillation axis, which passes the fixed and joint point (Nil) of the hammer element (A2.1) that moves connected to the eccentric center of the shuttle element (A2.2) makes an angle of 19.4° with the straight line of tip oscillation axis. The system is balanced at the position when the straight line which combines the rotation point (B6) and eccentric center of the shuttle element (A2.2) makes the (q) angle in the eccentric center of the shuttle element (A2.2) with the straight line of oscillation axis of hammer element (A2.1).
When the eccentric elements (A2.5) that move connected to the gear group (6) of the accelerating system rotate reversely to each other, they accelerate the symmetric disc element (4) clockwise and as the shuttle element (A2.2) in its bearing with the center (M6) is connected to the hummer element (A2.1) from the eccentric center and all the distances to this points are fixed, it has to rotate around its center clockwise. While the shuttle element (A2.2) makes this movement; load tip of eccentric center, the center of motion the point of this straight line which cuts the orbit turn into a leverage with a forge tip (s), the (q) angle widens. Fixed (Ml 1) and jointed center of the oscillation axis of hummer element (A2.1) which moves according to the leverage principles always be the bearing point, it changes according to the position of the other two tip oscillation distance. If its movement is counter clockwise from the tip oscillation angle clockwise; the point in the range (CK2) of 74.6° angle is the force tip, it turns into a leverage which works as a tip load in the range of 19.4° angle. The pistons (16c-16d) of the apparatus (A2) are connected to (CK2) point via piston rods (17c-17d). When apparatus is in this position, its (q) angle grows when it transmits the gas pressure force to symmetric disc element (4) which moves clockwise which the shuttle element (A2.2) is connected. The buoyancy force rate of the leverage system created by the force that continues its rotation clockwise in its center of the shuttle element (A2.2) is bigger than the buoyancy force rate of the leverage system created by the hammer element (A2.1). the opposing force which is created via this technique constantly produces the compression force which is needed to compress the gases, as a feature of the system, until it completes the range of 19.4° angle. The rotation point (B6) and these functions that are created after that accelerate the apparatus (A2), which enables it repeating exactly, symmetrically in the rotation point (B8) of the diagram where it has a range of 180 angle, the system in one tour of time for two times. The 90° angle is formed between the acceleration start of this apparatus (A2) and the acceleration start of apparatus (Al).
Figure-19; It is the section (1-1) view of the elements of the apparatus, which produces rotational motion from the energy in the compressed gases, that are placed in the dimensions that are determine according to their functions.
Figure-20; It the position of the piston that is 15.6° distant to the tip oscillation angle in the (2-2) section of the apparatus which produces rotational motion from the energy in the compressed gases.
Figure-21; It is the position of the piston that is 19.4° distant to the tip oscillation angle in the (3-3) section of the apparatus which produces rotational motion from the energy in the compressed gases.
Figure-22; (4-4) section view of the shared gear (6) group of the apparatus which produces rotational motion from the energy in the compressed gases.
Figure-23; (5-5) section view of the apparatus which produces rotational motion from the energy in the compressed gases.
Figure-24; It is the perspective view of the hammer element (A 1.1) and (A2.1).
Figure-25; It is the perspective view of the shuttle element (A1.2) and (A2.2).
Figure-26; It is the perspective view of the disk element (3).
Figure-27; It is the perspective view of the symmetric disk element (4).
Figure-28; It is the perspective view of the eccentric element (Al .5) and (A2.5).
Figure-29; It is the plan view of the gear group (6).
Figure-30; It is the perspective view of the sliding element (Al .7) and (A2.7).
Figure-31 ; It is the perspective view of the spring element (Al .8) and (A2.8).
Figure-32; It is the perspective view of the flywheel guard (10).
Figure-33; It is the section view of the cylinder press volumes (1 la-1 lb-1 Ιοί ld) and compressed gas inlet (12a-12b-12c-12d).
Figure-34; It is the plan and section view of the pressure gas balancing channel (13a-13b-13c-13d).
Figure-35; It is the perspective view of the pressure segment element ( 15a-15b-15c-15d).
Figure-36; It is the perspective view of the piston element ( 16a-16b-16c-16d).
Figure-37; It is the plan view of the long piston rod element (17c) and (17d).
Figure-38; It is the plan view of the short piston rod element (17a) and(17b).
Figure-39; It is the section view of the pressure control valve element (14).
Explanations of the references in the illustrations, MK) Engine housing; A1.1 ) Hammer element A2.1) Hammer element A 1.2) Shuttle element A2.2) Shuttle element 3) Disk element 4) Symmetric disk element A 1.5) Eccentric element A2.5) Eccentric element 6) Gear grup A1.7) Sliding element A2.7) Sliding element A 1.8) Spring element A2.8) Spring element 9) Engine oil 10) Flywheel guard BH ) Press volumes; 11 a ) Cylinder press volume 1 lb ) Cylinder press volume 11c) Cylinder press volume lid) Cylinder press volume 12a ) Compressed gas inlet 12b ) Compressed gas inlet 12c ) Compressed gas inlet 12d ) Compressed gas inlet 13a ) Pressure gas balancing channel 13b ) Pressure gas balancing channel 13c ) Pressure gas balancing channel 13d ) Pressure gas balancing channel 14 ) Pressure control valve 15 ) Pressure segment 16 a) Piston element 16 b) Piston element 16 c) Piston element 16 d) Piston element 17 a) Piston rods 17 b) Piston rods 17 c) Piston rods 17 d) Piston rods
Explanation for the invention,
The subject of the invention is ‘the apparatus that transforms the energy in the compressed gases into rotational movement’ and this technology that Works under constant pressure, has twe main groups; engine hausing (MK) that functions as a compressed gas tank and the press volumes (BH). After placing of this mechanic setup anti-symmetrically to each other, the mechanic setup which gets the feature to be able to make four operations in one tour of time is atechnology motor that makes the transformation of the potential energy in the compressed gases without the chemical reaction. The compressed gas volume in the apparatus’s tank does not change during these processes, the energy that it produces is in direct proportion to the compressed gas pressure and it has no connection with the mass of the technological motor. The analysis of features of the two apparatuses; (Al) and (A2) in the engine housing (MK) and the press volumes (BH) of the motor which is environment friendly, tecnological and has zero emission.
Apparatus; Al
When you apply linear force to the hammer element (A 1.1) of this apparatus that functions according to the leverage principle, it makes its oscillation motion in the oscillation angle and transfers that to disk element (3) through shuttle element (Al .2) at the tip of the load. The eccentric elements (Al .5), which indirectly accelerate with this pressure force, in connection with the motion of the gear group (6) which rotate reversely to each other, make the disk element (3), which becomes active through the sliding element (A 1.7) and its motions via the spring (A 1.8). Do the two centered motion movement. While the shuttle element (A 1.2), which transfers these two motions to each other, makes the rotational motions in 90° clockwise and in 90° counter clockwise, the eccentric center completes the oscillation angle spring two times in one tour of rotation time, and its center completes diagram motion of the infinity symbol, which is formed with the two centered motion of the disk element (3), in one tour of rotation time. During this motion, the rotation and eccentric centers of the eccentric element (A 1.5) are lined one time each on a straight line, clockwise and counter clockwise. And the points, which the straight line of the axis of the hammer element (Al.l) makes 15.6° angle with the oscillation point angle two times, are the rotation points of the shuttle element (A 1.2), which makes the oscillation motions connected with the hammer element (Al.l). Before these points, the disk element (3) depends on the motions of the hammer element (Al. 1 ) in both directions and the shuttle element (Al.2) can do its two-way motions. After this point, the bearing that is the shuttle element (A 1.2), which cannot do its rotational motion back as it depends on the two centered motion movement of the disk element (3), turns into a leverage whose eccentric center functions as the tip of the load. And although a linear force is applied in the reverse direction of the ongoing oscillation motion of the hammer element (Al.l), There is another opposing force bigger than this linear force and after the shuttle element (A1.2) continues its oscillation motion in 15.6° until the oscillation point angle, when the 15.6° angle distance is opened, the eccentric element (Al .5) makes a rotational motion in 90°. This feature happens in the two rotation points, in clockwise and counter clockwise directions.
Apparatus; A2
When you apply linear force to the hammer element (A2.1) of this apparatus that functions according to the leverage principle; it makes its oscillation motion in the oscillation angle and transfers that to symmetric disk element (4) through shuttle element ( A2.2) at the tip of the load. The eccentric elements (A2.5), which indirectly accelerate with this pressure force, in connection with the motion of the gear group (6) which rotate reversely to each other, make the symmetric disk element (4), which becomes active through the sliding element (A2.7) and its motions via the spring (A2.8), do the two centered motion movement. While the shuttle element (A2.2), which transfers these two motions to each other, makes the rotational motions in 90° clockwise and in 90° counter clockwise; the eccentric center completes the oscillation angle spring two times in one tour of rotation time, and its center completes diagram motion of the infinity symbol, which is formed with the two centered motion of the symmetric disk element (4), in one tour of rotation time. During this motion, the rotation and eccentric centers of the eccentric element (A2.5) are lined one time each on a straight line, clockwise and counter clockwise. And the points, which the straight line of the axis of the hammer element (A2.1) makes 19.4° angle with the oscillation point angle two times, are the rotation points of the shuttle element (A2.2), which makes the oscillation motions connected with the hammer element (A2.1). Before these points, the symmetric disk element (4) depends on the motions of the hammer element (A2.1) in both directions and the shuttle element (A2.2) can do its two-way motions. After this point, the bearing that is the shuttle element (A2.2), which cannot do its rotational motion back as it depends on the two centered motion movement of the symmetric disk element (4), turns into a leverage whose eccentric center functions as the tip of the load. And although a linear force is applied in the reverse direction of the ongoing oscillation motion of the hammer element (A2.1), There is another opposing force bigger than this linear force and after the shuttle element (A2.2) continues its oscillation motion in 19.4° until the oscillation point angle, when the 19.4° angle distance is opened, the eccentric element (A2.5) makes a rotational motion in 90°. This feature happens in the two rotation points, in clockwise and counter clockwise directions.
Press volumes; BH
There are four cylinder press volumes (1 la-1 lb-1 lc-1 Id) in this group which also do the duty of compressed gas tank. It is a mechanical setup that has a compressed gas inlet (12a-12b-12c-12d) between each group, which forms two teams and functions as a communicating vessel; and the pressure control valves (14), which provide the gases in the pressure volumes to be compressed equally and control the compressed gas pass going to the pressure gas balancing channels (13a-13b-13c-13d); and that is connected to the hammer elements (Al. 1) and (A2.1) of the apparatus through the piston rods (17a-17b-17c-17d) of piston elements (16a-16b-16c-16d) whit pressure segment (15) within these two groups. And it is the absolute part of technological motor which provides the conversion of the energy in the compressed gases into rotational motion. The apparatus that transforms the energy in the compressed gases into rotational movement; The distance of the two rotation starting points is the rotational time in 180° which is formed in the horizontal positions, in clockwise and counter clockwise directions, of the setup apparatus (Al) which is under constant pressure and has a compressed gas tank for the engine housing (MK). Having the anti-symmetry of this, the apparatus ( A2) makes the two rotational starting points when they are in diagonal positions and the distance of these two rotational starting points is the rotational time of 180°. The system’s shift from the horizontal position into the diagonal position is the rotational time in 90°.
The four operations that is makes in one tour of time has the order of the sequential system’s compressed gas pressing periods (1 la-1 lb-1 lc-1 Id) which happens in the ranges of rotation time in 90°.
Determining the waiting times of the system according to this order; When it comes to the level of the compressed gas inlet (12a) of the pressure gas balancing cannel (13a) with the upward movement of the piston element (16a) in the cylinder press volume (11a), the piston element (16d) of the cylinder press volume (1 Id) in the anti-symmetric system completes its upward movement and when the pressure gas balancing cannel (13d) comes to the compressed gas intel (12d) level through the back rotational motion; the positions, which the pressure of the gases in the two cylinder press volumes (1 la-1 Id) are balanced, are the first and third waiting times of the system. When the upward movement of the piston element (16b) in the cylinder press volume (11b) comes to the level of pressure gas inlet (12b) of the pressure gas balancing channel (13b), the piston element (16c) of the cylinder press volume (1 lc) in the anti-symmetric system completes its upward movement and when the pressure gas balancing channel (13c) comes to the compressed gas inlet (12c) level through the back rotational motion, the positions, which the pressure of the gases in the two cylinder press volumes (1 lb-1 lc) are balanced, are the second and fourth waiting times of the system. This system makes four pressing operations and four waiting times in one four of rotation time. When rotational force is applied to flywheel guards (10) of the apparatus whose the waiting time is in the clockwise direction and horizontal position, which hurls the (Al) and (A2) engine oil and continue its momentum; the oscillation motions of the hammer element (A 1.1) push the piston element (16a) in the cylinder press volume (11a) via the piston rod (17a) and when the pressure gas balancing channel (13a) closes the compressed gas tip oscillation angle, the shuttle element (Al .2) starts to produce opposing force. The piston element (16a), Which continues its movements connected with the hummer element (Al.l), completes its oscillation motion in 15.6° although it increases the pressure of the gas that it compresses at the rate of (1x10). And when the piston element (16a), which is hurled by the effect of high pressure, comes on the compressed gas inlet (12a) again; the oscillation motions of the hammer element (A2.1) of the symmetric system push the piston element (16c) in the cylinder press volume (11c) via the piston rod (17c). And when the pressure gas balancing channel (13c) closes the compressed gas inlet (12c), when it passes the rotation point having the distance in 19.4° to the tip oscillation angle, the shuttle element (A2.2) starts to produce opposing force. The piston element (16c), which continues its motions connected whit the hummer element (A2.1), completes its oscillation motion in 19.4° although it increases the pressure of the gas that it compresses at the rate of (1x10). And when the piston element (16c), which is hurled by the effect of high pressure, comes on the compressed gas inlet (12c) again, the oscillation motions of the hummer element (Al.l) of the symmetric system push the piston element (16b) in the cylinder press volume (11 b) via the piston rod (17.b). And when it closes the compressed gas inlet (12b) of the pressure gas balancing cannel (13b), when it passes the rotation point which has the distance in 15.6° to the tip oscillation angle, the shuttle element (Al .2) starts to produce opposing force. The piston element (16b), which continues its movements connected with the hammer element (Al.l), completes its oscillation motion in 15.6° although it increases the pressure of the gas that it compresses at the rate of (1x10). And when the piston element (16b), which is hurled by the effect of high pressure, comes on the compressed gas inlet (12b) again, the oscillation motions of the hummer element (A2.1) of the symmetric system push the piston element (16d) in the cylinder press volume (lid) via the piston rod (17d). And when it close the compressed gas inlet (12d) of the pressure gas balancing channel (13d), when it passes the rotation point having the distance of 19.4° to the tip oscillation angle, the shuttle element (A2.2) starts to produce opposing force. The piston element (16d), which continues its movements connected with the hammer element (A2.1), completes its oscillation motion of 19.4° although it increases the pressure of the gas that it compresses at the rate of (1x10). And when the piston element (16d), which is hurled by the effect of high pressure, comes on the compressed gas inlet (12d) again, the technological system, which can make four operations in one tour of rotation time, is the motor technology which converts the potential energy in the compressed gasses into kinetic energy without chemical reaction.
The invention’s form of application into industry,
This technology is a motor which transforms the energy in the compressed gases into rotational motion that serves the purposes mentioned above. The apparatuses (Al and A2) in this technological motor’s engine housing (MK) works as crank shaft for converting the linear forces into rotational motion. As for the technological motor, it will used for air, land, sea and space vehicles or by combining the systems which is producing energy for the motors of these vehicles, operating with electric energy, therefore this technology with zero emission will be used in everywhere that needs energy and will be a must in the next era.

Claims (18)

1. Système de réglage mécanique dans le compartiment moteur d’un appareil qui transforme l’énergie des gaz comprimés en un mouvement de rotation, caractérisé en ce que, lorsque l’on applique une force linéaire sur les éléments de martelage (Al.l) et (A2.1), qui fonctionnent selon le principe de levier, de ces appareils, cette force est transférée à un disque (3) et à un disque symétrique (4) par le biais de navette (A 1.2) et (A2.2) ; des éléments excentriques antisymétriques (Al.5) et (A2.5), qui accélèrent avec la force de la pression, font tourner le disque (3) et le disque symétrique (4) de manière opposée l’un à l’autre en fonction des mouvements du groupe d’engrenages (6) qu’ils partagent, et deviennent actifs par le biais d’un élément coulissant (A 1.7) et de ses mouvements à l’aide d’un ressort (Al.8) et (A2.8), qui provoque un mouvement de rotation centré ; les centres excentriques des navettes (A 1.2) et (A2.2) transfèrent ces deux mouvements par le biais de leur mouvement bilatéral, et font leur angle d’oscillation ressort deux fois au cours d’une seule rotation ; de plus, les centres effectuent le mouvement de diagramme du symbole d’infini en une seule rotation ; la rotation et les centres excentriques de l’élément excentrique (A 1.5) et (A2.5) sont alignés sur une ligne droite deux fois ; et les points que la ligne droite de l’axe de l’élément de marteau (Al.l) effectue un angle de 15,6° deux fois avec l’angle du point d’oscillation sont déterminés comme les points de rotation de l’élément de navette (A 1.2) ; les centres excentriques des arbres excentriques (A 1.5) et (A2.5) possèdent une position verticale et perpendiculaire deux fois ; et les points que la ligne droite de l’axe de l’élément de marteau (A2.1) effectue un angle de 19,4° deux fois avec l’angle du point d’oscillation sont déterminés comme les points de rotation de l’élément de navette (A2.2) ; avant ces points, les éléments de navettes (A 1.2) et (A2.2) effectuent leurs mouvements dans les deux directions, après quoi le palier, qui est le centre de l’élément de navette (Al.2) et (A2.2), qui n’effectue pas la rotation vers l’arrière étant donné qu’il dépend des deux mouvements de rotation centrés du disque (3) et du disque symétrique (4), se transforme en un levier dont le centre excentrique fonctionne comme la pointe de la charge ; bien qu’une force linéaire soit appliquée de manière opposée aux mouvements d’oscillation permanents des éléments de martelage (Al.l) et (A2.1), les éléments de navettes (A 1.2) et (A2.2) créent une force opposée plus importante que cette force linéaire ; et les caractéristiques qui font que ces mouvements d’oscillation se poursuivent jusqu’à l’extrémité de la ligne droite d’oscillation et la rendent projetée se produisent dans les quatre points de rotation également.1. Mechanical adjustment system in the engine compartment of a device which converts the energy of the compressed gases into a rotational movement, characterized in that, when a linear force is applied to the hammering elements (Al.l ) and (A2.1), which operate according to the lever principle, of these devices, this force is transferred to a disc (3) and a symmetrical disc (4) via shuttle (A 1.2) and (A2). .2); antisymmetric eccentric elements (Al.5) and (A2.5), which accelerate with the force of the pressure, rotate the disc (3) and the symmetrical disk (4) in opposition to each other. according to the movements of the gear group (6) which they share, and become active by means of a sliding element (A 1.7) and its movements by means of a spring (Al.8) and ( A2.8), which causes a rotational movement centered; the eccentric shuttle centers (A 1.2) and (A2.2) transfer these two movements through their bilateral movement, and make their oscillation angle spring twice during a single rotation; in addition, the centers perform the movement of the infinite symbol diagram in a single rotation; the rotation and the eccentric centers of the eccentric element (A 1.5) and (A2.5) are aligned on a straight line twice; and the points that the straight line of the axis of the hammer element (Al.l) makes an angle of 15.6 ° twice with the angle of the point of oscillation are determined as the rotation points of the shuttle element (A 1.2); the eccentric centers of the eccentric shafts (A 1.5) and (A2.5) have a vertical and perpendicular position twice; and the points that the straight line of the axis of the hammer element (A2.1) makes an angle of 19.4 ° twice with the angle of the point of oscillation are determined as the rotation points of the shuttle element (A2.2); before these points, the shuttle elements (A 1.2) and (A2.2) move in both directions, after which the bearing, which is the center of the shuttle element (Al.2) and (A2. 2), which does not rotate backwards since it depends on the two centered rotational movements of the disc (3) and the symmetrical disc (4), is transformed into a lever whose eccentric center functions as the tip of the load; although a linear force is applied in opposition to the permanent oscillation movements of the hammering elements (A1.1) and (A2.1), the shuttle elements (A 1.2) and (A2.2) create a force opposite more important than this linear force; and the characteristics that make these oscillation movements continue to the end of the straight line of oscillation and make it projected occur in the four points of rotation as well. 2. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon la revendication 1, caractérisé en ce qu’il comprend les éléments de martelage (Al.l) et (A2.1) qui fonctionnent selon le principe de levier, il transfère vers le disque (3) et le disque symétrique (4) par le biais des éléments de navettes (A 1.2) et (A2.2) à la pointe de la charge qui convertissent les forces linéaires en mouvement d’oscillation.2. Apparatus for converting the energy of compressed gases into rotational movement according to claim 1, characterized in that it comprises the hammering elements (Al.l) and (A2.1) which operate according to the lever principle. , it transfers to the disc (3) and the symmetrical disc (4) through shuttle elements (A 1.2) and (A2.2) at the tip of the load that convert the linear forces into oscillation motion. 3. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 2, caractérisé en ce que, après les mouvements dépendants des éléments de navettes excentriques (Al.2) et (A2.2), sur les éléments de martelage (Al.l) et (A2.1), il produit une force opposée lorsqu’il dépend des deux mouvements centrés du disque (3) et du disque symétrique (4).3. Apparatus for converting the energy of compressed gas into rotational movement according to claims 1 and 2, characterized in that after the dependent movements of the eccentric shuttle elements (Al.2) and (A2.2), on the hammering elements (Al.l) and (A2.1), it produces an opposite force when it depends on the two centered movements of the disc (3) and the symmetrical disc (4). 4. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 3, caractérisé en ce que le disque (3) et le disque symétrique (4) qui fonctionnent de manière antisymétrique l’un par rapport à l’autre font que le système exécutent quatre opérations en un seul tour de temps par le biais de la force de la pression renvoyée par l’élément de navette (Al.2) et (A2.2), par le biais des deux mouvements centrés des éléments excentriques (Al.5) et (A2.5) en fonction de leurs mouvements dans la position antisymétrique.Apparatus for converting the compressed gas energy into rotational motion according to claims 1 and 3, characterized in that the disk (3) and the symmetrical disc (4) which operate in an antisymmetric manner with respect to the other means that the system performs four operations in a single lapse of time through the force of the pressure returned by the shuttle element (Al.2) and (A2.2), through both movements centered eccentric elements (Al.5) and (A2.5) according to their movements in the antisymmetric position. 5. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 4, caractérisé en ce que les éléments excentriques (Al.5) et (A2.5), dans une direction opposée l’un à l’autre, effectuent leur mouvement de rotation grâce à un groupe d’engrenages (6) qui sont leurs éléments partagés et font que le disque (3) et le disque symétrique (4) effectuent deux mouvements centrés.5. Apparatus for converting the energy of compressed gases in rotational motion according to claims 1 and 4, characterized in that the eccentric elements (Al.5) and (A2.5), in a direction opposite to each other. the other, perform their rotational movement through a group of gears (6) which are their shared elements and make the disc (3) and the symmetrical disk (4) perform two movements centered. 6. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 5, caractérisé en ce que son groupe d’engrenages (6) possède quatre éléments en contact, et en ce qu’il permet aux éléments excentriques (Al.5) et (A2.5), qui sont dans une position antisymétrique l’un par rapport à l’autre dans leurs engrenages des deux côtés, de tourner dans une direction opposée.6. Apparatus for converting the compressed gas energy into rotational motion according to claims 1 and 5, characterized in that its gear group (6) has four elements in contact, and in that it allows the elements eccentric (Al.5) and (A2.5), which are in an antisymmetric position relative to each other in their gears on both sides, to rotate in an opposite direction. 7. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1, 4 et 5, caractérisé en ce que le système utilise les éléments coulissants (Al.7) et (A2.7), le disque (3) et le disque symétrique (4) et les éléments excentriques (Al.5) et (A2.5).7. Apparatus for converting the energy of compressed gases into rotational motion according to claims 1, 4 and 5, characterized in that the system uses the sliding elements (Al.7) and (A2.7), the disc ( 3) and the symmetrical disk (4) and the eccentric elements (Al.5) and (A2.5). 8. Appareil de transformation de l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 4, caractérisé en ce que les éléments coulissants (A 1.8) et (A2.8) rendent les deux mouvements centrés des disques (3) et du disque symétrique (4) actifs.8. Apparatus for converting compressed gas energy into rotational movement according to claims 1 and 4, characterized in that the sliding elements (A 1.8) and (A2.8) make the two movements centered discs (3) and symmetrical disk (4) active. 9. Technologie mécanique composée de deux principaux groupes de compartiment moteur (MK) et de volumes de compression (BH), qui peut effectuer quatre opérations en un tour de temps lors du placement symétrique et antisymétrique de certains éléments mécaniques dans le compartiment moteur (MK), est le moteur qui convertit l’énergie potentielle des gaz comprimés en énergie cinétique sans réaction chimique, et est caractérisée en ce que, lorsque l’on applique une force de rotation sur le volant (10), qui projette l’huile moteur (9) dans le compartiment moteur (MK) de l’appareil en position horizontale et son temps d’attente se trouve dans le sens des aiguilles d’une montre et assure le mouvement de l’appareil, les mouvements d’oscillation de l’élément de martelage (Al.l) poussent le piston (16a) avec un segment de pression (15) dans le volume de compression des cylindres (lia), via la tige à piston (17a) ; et lorsqu’il ferme l’admission de gaz comprimé (12a) du canal d’équilibrage des gaz sous pression (13a), l’élément de navette (A 1.2) qui transmet le point de rotation commence à créer une force opposée et, bien que l’élément de piston (16a) avec le segment de pression (15), qui continue ses mouvements en fonction de l’élément de martelage (Al.l), augmente la pression des gaz qu’il comprime, il continue le mouvement d’oscillation de 15,6° ; et, lorsque l’élément de piston (16a) avec le segment de pression (15), qui est projeté par l’effet de la pression élevée, vient à nouveau sur l’admission des gaz comprimés (12a), les mouvements d’oscillation de l’élément de martelage (A2.1) du système symétrique poussent l’élément de piston (16c) avec le segment de pression (15) dans le volume de compression du cylindre (lie) via la tige de piston (17c) ; et lorsqu’il ferme l’admission de gaz comprimés (12c) du canal d’équilibrage de gaz sous pression (13c), l’élément de navette (A2.2) qui transmet le point de rotation commence à produire une force opposée ; et, bien que le piston (16c) avec le segment de pression (15), qui continue ses mouvements en fonction de l’élément de martelage (A2.1), augmente la pression des gaz qu’il comprime, il poursuit le mouvement d’oscillation de 19,4° ; et lorsque le piston (16c) avec le segment de pression (15), qui est projeté par la pression élevée, vient sur l’admission de gaz comprimés (12c) à nouveau, les mouvements d’oscillation de l’élément de martelage (Al.l) du système symétrique poussent le piston (16c) avec le segment de pression (15) dans le volume de compression des cylindres (11b) via la tige de piston (17b) ; et lorsqu’il ferme l’admission de gaz comprimés (12b) du canal d’équilibrage des gaz sous pression (13b), l’élément de navette (Al.2) qui transmet le point de rotation commence à produire une force opposée ; et, bien que le piston (16b) avec le segment de pression (15), qui poursuit ses mouvements en fonction de l’élément de martelage (Al.l), augmente la pression des gaz qu’il comprime, il poursuit le mouvement d’oscillation de 15,6° ; et lorsque le piston (16b) avec le segment de pression (15), qui est projeté par l’effet de la pression élevée, vient à nouveau sur l’admission des gaz comprimés (12b), les mouvements d’oscillation de l’élément de martelage (A2.1) du système symétrique poussent le piston (16d) avec le segment de pression (15) dans le volume de compression des cylindres (1 ld) via la tige de piston ( 17d) ; et lorsqu’il ferme l’admission de gaz comprimés (12d) du canal d’équilibrage des gaz sous pression ( 13d), l’élément de navette (A2.2) qui transmet le point de rotation commence à produire une force opposée ; et, bien que le piston (16d) avec le segment de pression (15), qui poursuit ses mouvements en fonction de l’élément de martelage (A2.1), augmente la pression des gaz qu’il comprime, il poursuit le mouvement d’oscillation de 19,4° ; et lorsque le piston (16d) avec le segment de pression (15), qui est projeté par l’effet de la pression élevée, vient à nouveau sur l’admission de gaz comprimés ( 12d), cette technologie, qui convertit l’énergie potentielle des gaz comprimés en énergie cinétique sans réaction chimique, est un moteur qui est commandé par la soupape de régulation de la pression (14) pour le fonctionnement rapide ou lent du système technologique qui peut effectuer quatre opérations en un tour de temps.9. Mechanical technology consisting of two main engine compartment groups (MK) and compression volumes (BH), which can perform four operations in a single lap of time during the symmetrical and antisymmetric placement of certain mechanical elements in the engine compartment (MK ), is the motor that converts the potential energy of compressed gases into kinetic energy without chemical reaction, and is characterized in that, when a rotating force is applied to the flywheel (10), which projects the engine oil (9) in the motor compartment (MK) of the device in horizontal position and its waiting time is in the direction of clockwise and ensures the movement of the device, the oscillating movements of the hammering element (Al.l) pushing the piston (16a) with a pressure segment (15) in the compression volume of the cylinders (11a), via the piston rod (17a); and when closing the compressed gas inlet (12a) of the pressurized gas balancing channel (13a), the shuttle element (A 1.2) which transmits the point of rotation starts to create an opposite force and, although the piston element (16a) with the pressure segment (15), which continues its movements according to the hammering element (Al.l), increases the pressure of the gases that it compresses, it continues the oscillation motion of 15.6 °; and, when the piston member (16a) with the pressure segment (15), which is projected by the effect of the high pressure, comes again on the admission of the compressed gases (12a), the movements of oscillation of the hammer element (A2.1) of the symmetrical system push the piston member (16c) with the pressure segment (15) into the cylinder compression volume (lie) via the piston rod (17c) ; and when closing the compressed gas inlet (12c) of the pressurized gas balancing channel (13c), the shuttle element (A2.2) which transmits the point of rotation begins to produce an opposite force; and, although the piston (16c) with the pressure segment (15), which continues its movements according to the hammering element (A2.1), increases the pressure of the gases it compresses, it continues the movement oscillation 19.4 °; and when the piston (16c) with the pressure segment (15), which is projected by the high pressure, comes on the compressed gas inlet (12c) again, the oscillating movements of the hammering element ( Al.l) of the symmetrical system push the piston (16c) with the pressure segment (15) into the compression volume of the cylinders (11b) via the piston rod (17b); and when closing the compressed gas inlet (12b) of the pressurized gas balancing channel (13b), the shuttle element (Al.2) which transmits the point of rotation begins to produce an opposite force; and, although the piston (16b) with the pressure segment (15), which continues its movements according to the hammering element (Al.l), increases the pressure of the gases it compresses, it continues the movement oscillation 15.6 °; and when the piston (16b) with the pressure segment (15), which is projected by the effect of the high pressure, comes again on the admission of the compressed gases (12b), the oscillation movements of the hammering element (A2.1) of the symmetrical system push the piston (16d) with the pressure segment (15) into the compression volume of the cylinders (1 ld) via the piston rod (17d); and when closing the compressed gas inlet (12d) of the pressurized gas balancing channel (13d), the shuttle element (A2.2) which transmits the point of rotation begins to produce an opposite force; and, although the piston (16d) with the pressure segment (15), which continues its movements according to the hammering element (A2.1), increases the pressure of the gases that it compresses, it continues the movement oscillation 19.4 °; and when the piston (16d) with the pressure segment (15), which is projected by the effect of the high pressure, comes again on the compressed gas inlet (12d), this technology, which converts the energy potential of compressed gases in kinetic energy without chemical reaction, is a motor that is controlled by the pressure regulating valve (14) for the fast or slow operation of the technological system that can perform four operations in a lapse of time. 10. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 9, caractérisé en ce que l’huile machine (9) possède un liquide qui réduit les frottements dans le compartiment moteur (MK) du système technologique.Apparatus which converts compressed gas energy into rotational movement according to claims 1 and 9, characterized in that the machine oil (9) has a liquid which reduces friction in the engine compartment (MK) of the technological system . 11. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 9, caractérisé en ce que les volants (10) poursuivent leur mouvement après que l’appareil ait accéléré.Apparatus that converts compressed gas energy into rotational movement according to claims 1 and 9, characterized in that the flywheels (10) continue their movement after the apparatus has accelerated. 12. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 9, caractérisé en ce que les tiges de piston (17a-17b-17c-17d) transfèrent les mouvements d’oscillation des éléments de martelage (Al.l) et (A2.1) vers les pistons ( 16a-16b-16c-16d).Apparatus which converts compressed gas energy into rotational movement according to claims 1 and 9, characterized in that the piston rods (17a-17b-17c-17d) transfer the oscillating movements of the hammering elements ( Al.l) and (A2.1) to the pistons (16a-16b-16c-16d). 13. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 9, caractérisé en ce que les volumes de compression des cylindres (1 la-1 lb-1 lc-1 ld) fonctionnent comme un lit pour les pistons (16a-16b-16c-16d) et assurent la formation de cellule pour la compression des gaz comprimés.13. Apparatus which converts the compressed gas energy into rotational movement according to claims 1 and 9, characterized in that the compression volumes of the cylinders (1a-1b-1c-1dc) function as a bed for the pistons (16a-16b-16c-16d) and provide cell formation for compressing compressed gases. 14. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 9, caractérisé en ce que les segments de pression (15a-15b-15c- 15d) fonctionnent comme un lit pour les pistons (16a-16b-16c-16d) et ne font pas fuir les gaz.An apparatus which converts compressed gas energy into rotational movement according to claims 1 and 9, characterized in that the pressure segments (15a-15b-15c-15d) function as a bed for the pistons (16a-16b). -16c-16d) and do not flush the gases. 15. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1, 9, 13 et 14, caractérisé en ce que ses pistons ( 16a-16b-16c-16d) sont munis de segments de pression (15a-15b-15c-15d) qui fonctionnent comme un lit et compriment les gaz dans les volumes de compression (1 la-1 lb-1 lc-1 ld) par le biais de mouvements de va-et-vient.15. Apparatus which converts the compressed gas energy into rotational movement according to claims 1, 9, 13 and 14, characterized in that its pistons (16a-16b-16c-16d) are provided with pressure segments (15a). 15b-15c-15d) which function as a bed and compress the gases in the compression volumes (1a-1 lb-1c-1dd) through reciprocating motions. 16. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1, 9 et 11, caractérisé en ce que ses canaux d’équilibrage des gaz sous pression (13a-13b-13c-13d) sont au niveau de l’admission de gaz comprimés (12a-12b-12c-12d) à 15,6° et 19,4°, et en ce qu’il possède un canal circulaire sur la surface extérieure des volumes de compression (1 la-1 lb-1 lc-1 ld) et transfère les gaz comprimés dans les deux volumes de compression (1 la-1 lb) et (1 lc-1 ld) l’un vers l’autre, avec un réservoir de communication.Apparatus which converts the compressed gas energy into rotational movement according to claims 1, 9 and 11, characterized in that its pressurized gas balancing channels (13a-13b-13c-13d) are at the level of the admission of compressed gases (12a-12b-12c-12d) at 15.6 ° and 19.4 °, and in that it has a circular channel on the outer surface of the compression volumes (1 la-1 lb) -1 lc-1 ld) and transfers the compressed gases in the two compression volumes (1 la-1 lb) and (1 lc-1 ld) to one another, with a communication tank. 17. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1 et 9, caractérisé en ce que le compartiment de son admission de gaz comprimés (12a-12b-12c-12d) est l’emplacement auquel le système se trouve sur le point de rotation à 15,6° et 19,4°, et en ce qu’il peut assurer l’entrée et la sortie des gaz comprimés sans retard.An apparatus which converts the compressed gas energy into rotational movement according to claims 1 and 9, characterized in that the compartment of its compressed gas inlet (12a-12b-12c-12d) is the location at which the system is on the point of rotation at 15.6 ° and 19.4 °, and in that it can ensure the entry and exit of compressed gases without delay. 18. Appareil qui transforme l’énergie de gaz comprimés en mouvement de rotation selon les revendications 1, 9 et 13, caractérisé en ce qu’il égalise les pressions des gaz dans les volumes de compression (11 a-1 lb-1 le-1 ld) en régulant la vitesse et le débit des gaz via la soupape de régulation de la pression (14), et en ce qu’il permet au moteur technologique de fonctionner lentement ou rapidement.Apparatus which converts the compressed gas energy into rotational movement according to claims 1, 9 and 13, characterized in that it equalizes the pressures of the gases in the compression volumes (11a-1 lb-1). 1 ld) by regulating the speed and the flow of the gases via the pressure regulating valve (14), and in that it allows the technological engine to operate slowly or quickly.
LU93016A 2014-08-11 2015-07-28 Appareil de spécifications qui transforme l'énergie dans les gaz comprimés en un mouvement de rotation LU93016B1 (en)

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