GASES INTO ROTATIONAL MOTIO

DESCRIPTION

Technical area;

This invention is about the mechanical set up which transforms existing potential energy in compressed gases into kinetic energy without subjecting the gases to a chemical reaction.

Previous technique;

Nowadays the transformation of linear force into rotational motion is made with common, classic crankshafts. The crankshaft is an eccentric shaft and it is the element that converts the reciprocation o 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 machines. If the crankshaft is damaged, it is not possible to fix it and also the deformations that will appear in the manufaeturing cannot be fixed later on. As for the other system; the piston moves up and down on a centre axis and this movement makes the rotational motio with the mechanism that converts into rotational motion on the same centre axis via a circular rail profile. This system facilitates the transfonnation of the up and down linear motion into rotational motion, but it does not add power to the rotational motion. Also ther are manufacturing and installation difficulties besides the depreciation and f iction losses as it is made of many elements. There is a technique, which I have its patent, reference numbe 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, appropriat for its purpose, in spite of the disadvantage of this technology that it does two strokes in one rotation of 360 degrees.

The purpose of this device; The purpose of this device is to produce a zero emission ecologic motor that works while converting the potential energy in the compressed gases into kinetic energy without the chemical reaction and without decreasing the compressed gas volume available in the tank however oil seals in the gear group (6) shaft which transmit the rotation motion of the system to the outside of the engine housing (MK) can not achieve the compressed gas pressure at the intended level, adding a pressure gas tank is necessary for the system to operate or the mechanical system must be completely designed includin a closed engine housing (KM ).

Explanations of the illustrations

The apparatus that transforms the energy in the compressed gasses into rotational motion is 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 take 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 centre connected with the M4 centre is Ml . The eccentric centre connected wdth the M5 centre is M2. The distance between Ml and M2 is (2t) horizontally. Also the distance betwee M4 and M5 is (2t) which are the eccentric centres horizontally. Moreover, as the distance between Ml and M2 is (2t+z), when M4 and M5 centres rotate in reverse direction to each other in 90 degrees, we used a sliding bearing (7) which complies with the bidirectional motions in the joints that contact with the eccentric elements (Al .5 and A2.5) of the disk elements (3 and 4) which were designed in accordance with these conditions. Because of this design, the diagram, which is drawn by the centres of the socket of the shuttle elements (A1.2 and A2.2) of the disk elements (3 and 4), becomes deformed and the system could not reach its aim because of this. To solve this problem; we used jointed connecting rods (3a and 4a) which are linked via a bearing instead of sliding bearings (A 1.7 and A2.7) in the rotating shafts of the eccentric elements (Al.Sa and A2.5a), we prevented the formation of the deformation for the function and we made the mechanical design of the system reach its aim.

Figure-2- M point, where X and Y coordinates intersect, is equal to the distance of the jointed connecting rod element (3 a) to M3, M4 and M5 centres and has the length of (t). Figure-3; M point, where X and Y coordinates intersect, is equal to the distances of the symmetric jointed connecting rod element (4a) to M4, M5 and M6 centres and has the length of (t). Determining the diagrams that are drawn simultaneously by the M3 centre of the jointed connecting rod element (3a) that moves connected with the eccentric elements (Al .Sa) and (A2.5a) that move in the opposite direction of each other in their centres with M6 centre of the symmetric jointed connecting rod element (4a);

Figure-4— The beginning point for the infinity symbol diagram is B 1 that will be drawn by the M3 point of the jointed connecting rod element (3 a) that makes two-centred motion movement connected with the Ml and M2 eccentric rod of eccentric element (ALSa) whose rotation centres are M4 and MS. Also the beginning point for the infinity symbol diagram is B5 that will be drawn by the M6 point of symmetric jointed connecting rod element (4a) that makes two- centred movement motion connected with the Ml and M2 eccentric rod of the eccentric element (A2.5a), which is in symmetry. Figure-S— When the eccentric elements (Al .Sa) and (A2.5a), whose rotatio centres are M4 and M5, rotate for the first time in 90 degrees, the jointed connecting rod element (3a) draw CI diagram between B1-B2 and the symmetric jointed connecting rod element (4a) draws C5 diagram between B5- B6.

Figure-6— Whe the eccentric elements (Al.Sa) and (A2.5a), whose rotation centres are M4 and MS, rotate for the second time in 90 degrees, the jointed connecting rod element (3 a) draw C2 diagram between B2-B3 and the symmetric jointed connecting rod element (4a) draws C6 diagram between B6- B7.

Figure-7— Whe the eccentric elements (Al .Sa) and (A2.5a), whose rotation centres are M4 and MS, rotate for the third time in 90 degrees, the jointed connecting rod element (3 a) draw C3 diagram between B3-B4 and the symmetric jointed connecting rod element (4a) draws C7 diagram between B7- B8, Figure-8— When the eccentric elements (Al.Sa) and (A2.5a), whose rotation centres are M4 and 5, rotate for the last time i 90 degrees, the jointed connecting rod element (3 a) draw C4 diagram between B4-B1 and the symmetric jointed connecting rod element (4a) draws C8 diagram between B8- B5,

Determining the eccentric distance of the shuttle element (A 1.2);

Figure~9™ B3 point is the point where the motion diagram in 180 degrees ends. The distance between B3 and B4 points is the motion diagram i 90 degrees. The eccentric centre of shuttle element (A 1.2) has to be in an equal distance to B3, which is the start point, and B4 point, is th end the diagram in 90 degrees. As the orbit of the centre of shuttle element (A 1.2) is diagram, the diameter of the circle , whi ch is tangent to the end point of the diagram from D2 point, i s the eccentric slidin distance of shuttle element (A 1.2). This distance is detennined as (r=t 12). The position of the shuttle element (A1.2) in the D2 and M9 axis is the end of Its D2 centred 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 betwee B4 and B l point is the fourth motion diagram in 90 degrees. The intersection point of B2, B3 and B4, Bl diagrams is the D3 point o X axis. 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 centre of the shuttle element (Al .2). The shuttle element (A l .2) makes its two- way motions throughout the straight lines of these two diagrams.

Figure-11- Bl point is the beginning point of motion diagram. The distance between Bl and B2 points is the motion diagram i 90 degrees. The eccentric centre of shuttle element (A 1.2) has to be in an equal distance to B l, which is the start point, and B2 point, which is the end point of the diagram in 90 degrees. As the orbit of the centre of shuttle element (Al .2) is diagram, the diameter of the circle which is tangent to the diagram's end point from Dl 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 (A 1.2) in the Dl and M10 axis is the end of D l centred rotation of the shuttle element (Al .2) counter clockwise, and it is the starting location of its counter clockwise rotation. Determining the oscillation axis of the hammer (A L ib), and oscillation boundary;

Figure- 12- The determined eccentric centres of shuttle element (AL2) are Dl _r D2 and D4. The centre of the circle which is passing these points is on the X axis and is Mi l, which is the oscillation joint axis. The straight line that combines D2 and Ml 1 points is the tip oscillation boundary clockwise and the straight line that combines Dl and Mi l 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 A 1 ; Figure- 13— When the centre of the shuttle element (A 1.2) of the accelerating mechanic system comes to the rotation point B l on the diagram, the straight line of oscillation axis, which passes the fixed and joint point (Ml 1) of the hammer element (A L ib) that move connected to the eccentric centre of the shuttle element (AL2), makes an angle of 14.4° with the straight line of tip oscillation axis, The system is balanced at the position when the straight line which starts from eccentric centre of the shuttle element (AL2) and passes the rotation point Bl and makes the V angle in the eccentric centre of the shuttle element (A 1.2) with the straight line of oscillation axis of hammer element (A L ib). When the eccentric elements (A 1.5b) that move connected to the gear group (6) of the accelerating system, rotate reversely to each other, they accelerate the jointed connecting rod element (3a) clockwise and as the shuttle element (AL2) in its bearing with the centre M3 is connected to the hummer element (A Lib) from the eccentric centre and all the distances to this points are fixed, it has to rotate around its centre clockwise. While the shuttle element (AL2) makes this movement, load tip of eccentric centre, the centre of support and the point of this straight line which cuts the orbit turn into a leverage with a force tip , the V angle widens. Fixed Ml 1 jointed centre of oscillation axis of hammer element (Al. lb), which moves according to the leverage principles, always be the support point, the other two tip oscillation distance changes according to thei position. If its movement is counter clockwise from the tip oscillation angle clockwise; CKl point in the range of 78.9° angle is the force tip. If it is in the range of 14.4° angle, it turns into a leverage which works as a tip load. The pistons (16a- 16b) of the apparatus (Al) are connected to CKl point via piston rods (17a- 17b). When the apparatus (Al) is in this position, its V angle grows when it transmits the gas pressure force to the jointed connecting rod element (3a) which moves clockwise, and which the shuttle element (Al .2) is connected to, therefore the system becomes unbalanced. When the shuttle element (A1.2) of the unbalanced system turns into a leverage while it is turning around its centre clockwise. The buoyancy force is bigger than the buoyanc force of th hammer element (Al . lb). 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 l4.4°angle.The rotation point Bl and these functions that are created after that, 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, accelerate the system twice in one rotation.

Determining the eccentric distance of the 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 the motion diagram in 90 degrees. The eccentric centre of the shuttle element (A2.2) must have an equal distance to B8 the beginnin point and B5 the end point of the diagram in 90 degrees. As the orbit of the shuttle element's (A2.2) centre 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 12). The position of the shuttle element (A2. ) in the G2 and N9 axis is the end of counter clockwis rotation with G2 centre and 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 betwee 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, is an equal distance to both diagrams, it is the eccentric centre of the shuttle element (A2.2). The shuttle element (A2.2) makes its two-way motions throughout these two diagram lines.

Figure- 16- the distance betwee B6 and B7 points is the second motion diagram in 90 degrees. The eccentric centre of the shuttle element (A2.2) must have an equal distance to the beginning point B6 and the end point B7 of the second diagram in 90 degrees. As the orbit of the shuttle element's (A2.2) centre is a diagram, the diameter of the circle which is tangent to the end point of the diagram from the Gl 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 01 and NIO axis is the end of the clockwise rotation of the shuttle element (A2.2) with Gl centre and counter clockwise is the beginning position of the rotation.

Determining the oscillation axis of the hammer (A2.1b) and oscillation boundary;

Figure- 17- The determined eccentric centres of shuttle element (A2.2) are: Gl, G2 and G4. The centre of the circle which is passing these points is on the X axis and is Ni l which is the joint oscillation centre. The straight line that combines Gl and Nl 1 points is the tip oscillation boundary clockwise and the straight line that combines G2 and Nl 1 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 it comes to the rotation point B6 on the diagram that was drawn by the centre of the shuttle element (A2.2) of the accelerating mechanic system; the straight line of oscillation axis, which passes the fixed and joint point Nl 1 of the hammer element (A2.1b) that moves connected to the eccentric centre of the shuttle element (A2.2) makes an angle of 15.3° with the straight line of tip oscillation axis. The system is balanced at the position when the straight line which starts from the eccentric centre of the shuttle element (A2.2) and passes from the rotation point B6 makes the Q angle with the straight line of oscillation axis of the hammer element (A2.1b) in the eccentric centre of the shuttle element (A2.2). When the eccentric elements (A2,5a), which move connected to the gear group (6) of the accelerating system, rotate reversely to each other; they accelerate the symmetric jointed connecting rod element (4a) clockwise and as the shuttle element (A2.2) in its socket with the centre M6 is connected to the hammer element (A2.1b) through the eccentric centre and all the distances to these points are fixed, it has to rotate around its centr clockwise. While the shuttle element (A2.2) makes this movement, whe the load ti of eccentric centre, the centre of the support and the point of this straight line which cuts the orbit, turns into leverage with a forge tip S, the Q angle widens. Fixed Nl 1 jointed centre of the oscillation axis of hammer element (A2.1b) which moves according to the leverage principles always be the support point, the other two tip oscillatio distances change according to their position. If its movement is counter clockwise from th tip oscillation angle clockwise; the CK2 point in the range of 76.8° angle is the force tip, if it is in the range of 15.3° angle, it turns into a leverage which works as a tip load. The pistons (16e- 16d) of the apparatus (A2) are connected to CK2 point via piston rods (1 Tend). When the apparatus (A2) is in this position, the Q angle grows when it transmits the gas pressure force to the symmetric joint connecting rod element (4a) which moves clockwise and which the shuttle element (A2.2) depends on and the system becomes unbalanced. The unbalanced system's shuttle element (A2.2) turns into a leverage while it turns around its centre clockwise. The buoyancy force is bigger than the one that is created by the hammer element (A2.1b). 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 15.3° angle. The rotation point B6 and these functions that are performed after that, the apparatus (A2), which enables it to repeat exactly, symmetrically in the rotation point B8 of the diagram where it has a range of 180° angle, accelerates the system twice in one rotation. It is range of 90° angle between the acceleration start of apparatus A2 and the acceleration start of apparatus Al .

Figure- 19- It is the section (1-1) view of the elements, which are placed in the measurements that are determined according to their functions, of the technology that produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK).

Figure-2G~ It is the section (2-2) view of the elements, which are placed in the measurements that are determined according to their functions, of the technology that produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK).

Figure-21- It is the section (3-3) view of the technology, which produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK).

Figure- 22- It is the section (4-4) view of the technology, which produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK),

Figure-23- It is the section (5-5) view of the technology, which produces rotational motion from the energy withi the compressed gases, in the closed engine housing (KMK). Figure-24- It is the section (6-6) view of the technology, whic produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK).

Figure-25- It is the section (7-7) view of the technology, which produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK).

Figure-26- It is the section (8-8) view of the technology, which produces rotational motion from the energy within the compressed gases, in the closed engine housing (KMK).

Figure-27— It is the perspective view of the hammer element (Al.lb) and (A 1.2 b).

Figure-28— It is the perspective view of the hammer element (A2.1b) and (A2.2b).

Figure-29- It is the perspective view of the shuttle element (A1.2) and (A2.2). Figure-30- It is the perspective view of the j ointed connecting rod element (3 a). Figure-31- It is the perspective view of the symmetric jointed connecting rod element (4a).

Figure-32- It is the perspective view of the eccentric element (Al .Sa) and (A2.5a).

Figure-33~ It is the plan view of the gear group (6).

Figure-34- It is the perspective view of the shaft element (7a).

Figure-35- It is the view of the alternator elements (8a).

Figure-36- It is the perspective view of the flywheel element (9a).

Figure-37- It is the plan view of the starter motor (10a).

Figure-38- It is the section view of the cylinder element (1 la-1 lb-11 c-1 Id).

Figure-39~ It is the section view of the pressure balancing channel (13a-13b-

13c- 13 d).

Figure-40- It is the section view of the pressure control valve element (14).

Figure-41- It is the perspective of the compression ring element (15a-15b-15c- 15d).

Figure-42- It is the perspective of the piston elements (16a-16b-1 c-1 d).

Figure-43- It is the plan view of the long piston rod element (17c) and (1 d). Figure-43- It is the plan view of the short piston rod element (17a) and (17b). Explanations of the references in the illustrations;

KMK) Closed engine housing,

A 1.1 b) Hammer element A 1.2 b) Hammer element

A2, lb) Hammer element

A2.2b) Hammer element

AI .2) Shuttle element

A2.2) Shuttle element

3a) Jointed connecting rod element

4a) Symmetric jointed connecting rod element A 1.5 a) Eccentric element

A2,5a) Eccentric element

6) Gear group

7a) Shaft element

8 a) Alternator

9a) Flywheel element

10a) Starter motor

BH) Press volumes;

1 l a) Cylinder press volume

I l b) Cylinder press volume

I I c) Cylinder press volume

l id) Cylinder press volume

12a) Compressed gas inlet

12b) Compressed gas inlet

12c) Compressed gas inlet

12d) Compressed gas inlet

13 a) Pressure gas balancing channel

13 b) Pressur gas balancing channel

13 c) Pressure gas balancing channel

13 d) Pressure gas balancing channel

14) Pressure control valve

15a) Compression ring

15b) Compression ring

15 c) Compression ring

15d) Compression ring

16 a) Piston element

16 b) Piston element

16 c) Pisto element

16 d) Piston element 17 a) Piston rods

17 b) Piston rods

1 c) Piston rods

17 d) Pi ston 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 the mechanical set up can do fou strokes i one tour throug the mechanical elements of this technology by placing the press volumes (BH) in the engine housing (MK) that works as compressed gas tank and the other elements anti-symmetrically and symmetrically to each other, this technology can transform the potential energy in the compressed gases into kinetic energy without a chemical reaction, as the oil seals in the shaft element that transmits the rotation motion, produced by this technology, outside both sides of the engine housing (MK) will leak the applied pressure; it was necessary to solve the issue throug a design for the closed engine housing (KMK) which covers the mechanical system completely. For this reason, the starter motor (10a) and alternator (8a) elements are included within this closed engine housing (KMK).

The analysis of variable technical features of the apparatus Al and A2 in the closed engine housing (KMK) and the press volumes (BH); Apparatus; Al

Shuttle element (Al .2), the essential part of this technology, depends on the disk element (3) in its movements and it needs to work extremely sensitively. When the disk element (3) i the existing design makes its two-centred motion movement, it is connected to the eccentric elements (A1.5 and A2.5) through the sliding bearing (A1.7 which moves with the bidirectional friction tolerance in the rotation centre. The diagram drawn by the rotation centre of the shuttle element (A1.2) that moves in connection with the disk element (3) which achieves two-centred motion movement along with the acceleration of the technological system, become deformed on both sides and the system can not reach its aim. For this reason, we designed the jointed connecting rod element (3 a) with a ball bearing in accordance with the technological purpose of the technology and we revised the design of the eccentric elements (A 1,5 and A2.5) and hammer elements (A Lib and A 1.2b) which depends on that (3a) and we made the apparatus function according to its purpose. When the hammer element (ALlb and A 1.2b) of this apparatus accelerate with a linear force, it makes its oscillatio motion within the range of oscillation angle of 93.3° approximately and transfers it to the jointed connecting rod element (3a) as a pressure force. The jointed connecting rod (3a) becomes unbalanced with this pressure force and makes the eccentric elements (A1.5a and A2.5a) turn reversely to each other. There are alternator (8a) and flywheel elements (9a) at the tips of the shaft element (7a) in the gear group (6) which gets this reverse rotation motion done. When the starter motor (10a) accelerates through the flywheel element (9a) and when the eccentric elements (A 1.5a and A2.5 ) move reversely to each other, this apparatus makes the jointed connecting rod element (3a) do the two-centred motion movement and the shuttle element (AL2), which depends on it, and transfers this motion into oscillation movement. When the hammer element (ALlb and AL2b) that does the oscillation movement makes about 14.4° angle with the oscillation tip angle of the axis straight line; the point (B l and B3) on the diagram of eternity symbol drawn by the rotation centre of the shuttle element (AL2) are the rotation points of the shuttle elements (A 1.2). After these points, the centre support which is the centre of the shuttle element (A 1.2) that can not do its return movement as it depends o the two centred motion movement of the jointed connecting rod element (3a) turns into a leverage that works as a tip of the load for the eccentric centre. And even if a linear force is applied reversely with the ongoing oscillation movement of the hammer element (ALlb and AL2b), a bigger opposing force comes out. And the shuttle element (A 1.2) is drifted after going on its oscillation motio which is about 14.4° until the oscillation tip angle and makes the eccentric element (Al .Sa and A2.5a) complete its rotational movement. This feature happens in the two rotation points, in clockwise and counter clockwise directions.

Apparatus; A2

Shuttle element (A2.2), the essential part of this technology, depends o the disk element (4) in its movements and it needs to work extremely sensitively. Whe the disk element (4) in the existing design makes its two-centred motion movement, it is connected to the eccentric elements (Al .5 and A2.5) through the sliding bearing (A 1.7) hic moves with the bidirectional friction tolerance in the rotation centre. The diagram drawn by the rotation centre of the shuttle element (AL2) that moves in connection with the disk element (3) which achieves two-centred motion movement along with the acceleration of the technological system, become deformed on both sides and the system can not reach its aim. For this reason, we designed the symmetric jointed connecting rod element (4a) with a ball bearing in accordance with the technological purpose of the technology and we revised the design of the eccentric elements (Al.Sa and A2,5a) and hammer elements (A2. l b and A2.2b) which depends on that (4a) and we made the apparatus function according to its purpose. When the hammer element (A2Jb and A2.2b) of this apparatus accelerate with a linear force, it makes its oscillation motion within the range of oscillation angl of 92.1° approximately and transfers it to the symmetric jointed connecting rod element (4a) as a pressure force. The symmetric jointed connecting rod (4a) becomes unbalanced with this pressure force and makes the eccentric elements (Al .Sa and A2.5a) turn reversely to each other. There are alternator (8a) and flywheel elements (9a) at the tips of the shaft element (7a) in the gear group (6) which gets this reverse rotation motion done. When the starter motor (10a) accelerates through the flywheel element (9a) and when the eccentric elements (Al.Sa and A2.5a) move reversely to each other, this apparatus makes the symmetric jointed connecting rod element (4a) do the two-centred motion movement and the shuttle element (A2.2), which depends on it, and transfers this motion into oscillation movement. When the hammer element (A2.1b and A2.2b) that does the oscillation movement makes about 15.3° angle with the oscillation tip angle of the axis straight line; the point (B6 and B8) on the diagram of eternity symbol drawn by the rotation centre of the shuttle element (A2.2) are the rotation points of the shuttle elements (A2.2). After these points, the centre support which is the centre of the shuttle element (A2.2) that can not do its return movement as it depends on the two centred motion movement o the symmetric jointed connecting rod element (4a) turns into a leverage that works as a tip of the load for the eccentric centre and even if a linear force is applied reversely with the ongoing oscillation movement of the hammer element (A2J b and A2.2b), a bigger opposing force comes out and the shuttle element (A2.2) is drifted after going on its oscillation motion which is about 1.5.3° until the oscillation tip angle and makes the eccentric element (Al .5a and A2.5a) complete its rotational movement. This feature happens in the two rotation points, in clockwise and counter clockwise directions. Press volumes; BH

There are two groups of cylinder press volumes in this group which also do the duty of compressed gas tank (11 a- l ib) and (1 1c- l id). Whe you apply rotational force through the starter motor (10a) to the flywheel element (9a) that continues its momentum of the apparatus (Al and A2) which are i horizontal position including waiting time clockwise; the oscillation motions of the hammer element (ALlb) pushes the piston element (1 a) inside the cylinder press volume (1 1a) through pisto rods (17a) and closes the compressed gas inlet (12a) of the pressure gas balancing channel (13a) and later on, the shuttle element (A 1.2) passes the rotation point with a distance of 14.4° to the oscillation angle and starts to produce opposing force. The piston element (16a) that goes on its motions depending on the hammer element (ALlb) and (A 1.2b), despite gas pressure that it compresses increases, completes its oscillation motion of 14.4° and when the piston element (1 a), drifted by the effect of the high pressure, comes on the compressed gas inlet (12a) again; the oscillation motions of the hammer element (A2.1b) and (A2.2b) of the symmetric system push the piston element (16c) inside the cylinder press volume (l ie) through piston rods (17c) and closes the compressed gas inlet (12c) of the pressure gas balancin channel (13c) and later on, the shuttle element (A2.2) passes the rotation point with a distance of 15.3° to the oscillation angle starts to produce opposing force. The pisto element (16c) that goes on its motions depending on the hammer element (A2.1b) and (A2.2b), despite gas pressure that it compresses increases, completes its oscillation motion of 15.3° and when the piston element (16c), drifted by the effect of the high pressure, comes on the compressed gas inlet (12c) again; the oscillation motions of the hammer element (ALlb) and (AL2b) of the symmetric system push the piston element (16b) inside the cylinder press volume (l i b) through piston rods (17b) and closes the compressed gas inlet (12b) of the pressure gas balancing channel (13b) and later on, the shuttle element (Al ,2) passes the rotation point with a distance of 14.4° to the oscillation angle and starts to produce opposing force.

The piston element (16b) that goes on its motions depending on the hammer element (ALlb) and (AL2b), despite gas pressure that it compresses increases, completes its oscillation motion of 1.4.4° and when the piston element (16b), drifted by the effect of the high pressure, comes on the compressed gas inlet (12b) again, the oscillation motions of the hammer element (A2.1b) and (A2.2b) of the symmetric system push the piston element (1 d) inside the cylinder press volume (l id) through piston rods (17d) and closes the compressed gas inlet (12d) of the pressure gas balancing channel (13 d) and later on, the shuttle element (A2.2) passes the rotation point with a distance of 15.3° to the oscillation angle and starts to produce opposing force. The piston element (16d) that goes on its motions depending on the hammer element (A2.1b) and (A2 2b), despite gas pressure that it compresses increases, completes its oscillation motion of 15.3°. When the piston element (16d), drifted by the effect of high pressure, comes on the compressed gas inlet (12d) again, this technology can make four strokes in one rotation and the system is an engine that transforms the potential energy in the compressed gases into kinetic energy without a chemical reaction.

The invention's form of application into industry

This technology is an engine which transforms the energy in the compressed gases into rotational motion that serves for the purposes mentioned above; the apparatuses (Al and A2) i this technological motor's closed engine housing ( MK) work as a crank shaft for converting the linear forces into rotational motion. The technological engine will be used as an e ergy producer for the engines of the air, land, sea and space vehicles that work with electrical energy and in every area that needs energy, therefore this zero emission technology will be a must in the next era.