WO2018084819A1

WO2018084819A1 - Fuelless engine – ufo engine

Info

Publication number: WO2018084819A1
Application number: PCT/TR2017/050224
Authority: WO
Inventors: Salman Gurbuz
Original assignee: Salman Gurbuz
Priority date: 2016-11-01
Filing date: 2017-05-29
Publication date: 2018-05-11

Abstract

This invention is related with the turbine engines which convert the potential energy to the kinetic energy and also engines which convert this force to a turning moment after obtaining linear force through pistons in a pressure chamber. Furthermore, this invention will tear down the education system in the world which knocks people down with the physic laws. They are the basic movement components which consist of the hydraulic and turbine engine and engine with piston, without fuel, the subject of the invention. Both engines enables the operation of the engine by creating linear or turning movement thanks to the movements of the piston or wedge. Preferably, there are two or more wedges corresponding to each pressure chamber. These both two hydraulic and turbine engine are ball bearing each. Because they are ball bearing they can provide driving by making bedding which can be directly applied to the shaft required.

Description

FUELLESS ENGINE - UFO ENGINE

Technical area

This invention is related with the turbine engines which convert the potential energy to the kinetic energy and also engines which convert this force to turning moment after obtaining the linear force through pistons in a pressure chamber.

Furthermore, this invention will demolish the education system which knocks people down with the physic laws.

Previous technique The engine, known in the technique and which is closest to this invention is described called as "turbine engine" described in the patent application numbered: TR2007/00244 and the inventor and the owner of the application of which is Salman Gurbuz. In the application in question a turning movement is obtained because of the high pressure and low pressure difference between the low pressure and high pressure zones which are created around a shaft by using hydraulic and pneumatic.

This invention has no relation with any system known across the world except the patent application mentioned above. This invention is a fuelless engine and used in the flying saucers.

Brief description of the invention The subject of the invention is the basic movement components consisting of the hydraulic and turbine engine and hydraulic and engine with piston, without fuel. Both engines enables that the engine operates by creating linear or turning movement thanks to the movements of the piston or wedge by using pressure. These both piston and turbine engines are special ball bearings each. Technique of the turbine engines;

When the pressure is applied inside the high pressure chamber, the pressure to the side of the wedge accumulates in the rotor. When the pressure coming to the surface S1 at the top of the wedge, the pressure coming to the surface S2 leaning on the inclined plane goes up to the plane S1 leaning on the plane, S2 would be sucked into the high pressure plane based on the inclined plane. This movement goes on like this.

The rotation power collected in the rotor pushes the wedges leaning on the inclined plan (14 units in total leaning on the inclined plane such that 7 leans on to the right and 7 leaning on to the left and similarly 14 units in total to the flat surface such that 7 leans on to the right and 7 leaning on to the left) to the low pressure chamber from the high pressure chamber. If the force in the rotor increases after sucking the wedges leaning on the inclined plane, then this is an engine; if not, it is not an engine.

The number of wedges given here is given for the model implementation of the invention. Preferably, there are two or more wedges in each pressure chamber. The measure values and number of components, included here, are given for illustration.

The result is seen in the physical analysis. After the first drive, we collect and press the lubricant leaking (goes) inside the high pressure chamber again to the engine.

Technique with the engine with piston;

There is only the high pressure chamber. A piston is pushed with a linear movement from the pressure chamber. The other piston leans on the inclined plane.

If the force increases after the piston pushed linearly sucks the piston which leans on the inclined plane inside the pressure chamber, this is increasing energy.

If the increasing force is converted into a rotation movement by means of crank method or another method, the engine is created. Furthermore, this force may be used linearly.

The result is seen in the physical analysis. Here, again the lubricant leaking inside the pressure chamber after the engine starts moving is collected and pressed inside the engine again. The energy required for this is taken from the engine's own shaft. The movement is taken from the shaft by means of a hoop and power is transferred to the battery, then hydraulic circuit by means of charging dynamo. The system feeds itself after the first drive. The same action repeats in the one with the piston too. A lot of different solutions can be produced by using this return feed, i.e. hydraulic & pneumatic methods, mechanical method. These solutions may be different based on the area of usage. What is important is that the physical analysis is correct. Similarly, as it is in the turbine engines, the shape, dimension and number of pistons may indicate infinite differences depending on the needs. The special designs can be done based on the need of the producer. In addition to this, when linear displacement is done by the inclined plane moving the piston on it, the inclined plane itself can be movable. By using the leverage techniques spring supports and hydraulic systems, by means of the hardware which serve as the inclined plane, the piston moving on the inclined plane can be made more efficient.

Description of the figures

Figure 1 - is the perspective view of the body of the fuelless engine.

Figure 2 - is the exploded perspective view of the body of the fuelless engine, the subject of the invention.

Figure 3 - is the detailed front perspective view of the wedge of the body of the fuelless engine, the subject of the invention.

Figure 4 - is the detailed back perspective view of the wedge of the body of the fuelless engine, the subject of the invention. Figure 5 - is the detailed perspective view which belongs to the rotor disc of the body of the fuelless engine, the subject of the invention.

Figure 6 - it is the perspective view of the state of the fuelless engine, where the rotor disc and wedges are combined.

Figure 7 - it is the detailed perspective view of the guidance conduit of the internal body of the fuelless engine, the subject of the invention. Figure 8 - it is the detailed perspective view of the back surface of the cell divider, forming the high and low pressure chambers of the fuelless engine, the subject of the invention.

Figure 9 - it is the detailed perspective view of the front surface of the cell divider, forming the high and low pressure chambers of the fuelless engine, the subject of the invention.

Figure 10 - it is the internal perspective view of the external body to which the cell divider of the fuelless engine, the subject of the invention, is fixed inside.

Figure 1 1 - it is the external perspective view of the external body to which the cell divider of the fuelless engine, the subject of the invention, is fixed inside.

Figure 12 - it is the cross-section view of the body of the fuelless engine, the subject of the invention.

Figure 13 - it is the hydraulic flow schematic of the fuelless engine, the subject of the invention. Figure 14 - is the figure indicating the calculations of the fuelless engine, the subject of the invention.

Figure 15 - it is the perspective view of the bearing of the linear piston of the fuelless engine, the subject of the invention.

Figure 16 - it is the perspective view of the linear piston of the fuelless engine, the subject of the invention.

Figure 17 - it is the perspective view of the piston body of the fuelless engine, the subject of the invention.

Figure 18 - it is the perspective view of the piston body of the fuelless engine, the subject of the invention. Figure 19 - It is the view of the piston calculations of the fuelless engine, the subject of the invention. Figure 20 - it is the side view of the UFO engine, obtained with the sequential application of the fuelless engine, the subject of the invention.

The parts are numbered one by one in the figures and the equivalent of these numbers is given below.

1 . Turbine engines

2. External body

3. Cell divider

4. Internal body guidance conduit

5. Rotor disc

6. Wedge

7. Conduit

8. Engines with piston

9. Piston leaning on the inclined plane

10. Linear movement piston

1 1 . Piston body

12. High pressure valve

13. Low pressure valve

Detailed description of the invention

In this project too, the lubricant volume inside the high pressure chamber is subjected to only small changes when moving too. The engine efficiency can be calculated by making physical calculations over the dimensions of the wedges (6) and pressure differences. Because as these values changes, the power which the fuelless engine (1 ) produces would indicate variability. In order to access the higher powers, it is also possible to use serial and parallel modular systems. The pressurized oil will be supplied from the entry hole which is located on the external body (2) inside the engine (1 ). The hole in question allows that all of the gap in the internal volume of the external body (2), which has a torus (ring) shape is filled with pressurized oil.

It is required that the oil, leaking inside the low pressure chamber comes again inside the engine. It is possible to provide the leaking oil cycle externally for this purpose. If required, the dimension of the parts, running on each other can be arranged such that oil leakages don't take place. By this way, the formation of lubricant leakages is prevented. In this prototype of the invention, which is the subject of the patent application, slight lubricant leakages are preferred for the system lubricating itself. Each one of the a lot of wedges (6), aligned on the rotor disc (6) moves freely and in parallel to the rotation axis on the ball bearing for not facing with friction. The basic component which limits the movements in question is the internal body guidance (4) conduit. There are flat ad angled surfaces, parallel with each other, on this component. Thanks to the surfaces in question, the fluid ensures that the wedge (6) is displaced by pressurizing one of two surfaces once every time of the fluid (6).

The internal body guidance conduit (4) beds the rotor disk (5). The steel ring next to the conduit should be ball. However steel ring was used instead of ball in this prototype of the invention. Because we don't have the means to make ball.

Physical analysis

This invention consists of 28 wedges (6) and 14 high and 14 low pressure chambers. The physical analysis is made below based on 40 atu and 1000 rpm.

If we do the physical analysis assuming that the wedges leaning on the inclined plane at the center (r=73,51 mm), then transfer to the guidance conduit;

Two wedges inside one high pressure chamber, one moves straight while the other is pulled inside the pressure chamber leaning on the inclined plane. In this project, the calculation is made according to 14 mm load way (distance).

The wedges get closer to 0,4 mm to the cell dividers. After passing 0,4 mm, go away. The dimensions which are necessary for describing the physical analysis to us as below are given. When we apply hydraulic pressure, pulling force is formed to the SR surface turning direction. (Figure 14 may be evaluated for the notation used here). This creates 6,30 cm x 40 Atu = 252 kg force. This force is gathered in the rotor. On the surfaces S1 and S2, a force, leaning on the guidance conduit, of 7,42 cm2 x 40 Atu=296,8 kg, is formed. S2 leans on the flat surface; S1 leans on the inclined plane. S2 ignored because it will be multiplied with the friction coefficient. Force gathered in the rotor

SR x 40atu x 14 (high pressure chamber) = 6,30cm2 x 40 Atu x 14 high pressure chamber = 3528kg rotating force. (All of this force produces torque.)

The force gathered in the inclined plane = S1 x 40 atu x 14 (high pressure chamber) = 4155,2kg, the force leaning on the inclined plane. The formula which is necessary for pushing the force leaning on the inclined plane to the pressure chamber; load x load way = Force x Force way.

Load way 14mm. (The length difference - movement difference in cases where it enters most and enters less to the cell dividers dividing the high and low pressure chambers).

Hypotenuse of the force way (distance). 21 ,05mm

4155,2Kg x 14mm = Force x 21 ,05 Force =4155Kg x 14 (load way) / 21 ,05 =

2763,6kg.

Total rotating force left; 3528 - 2763,6 = 764,4 Total rotating force left.

Since we do our calculation, assuming we have 1000 revolutions in the engine;

R average =73,51 mm. W=FxV

W=764,4 x 10 x 2 x 3,14 x 0,0735 x 1000 / 60 =58,8 Kw. The torque value doesn't change, even though the rotation is increased. Only the power taken would change.

Let's transfer the force to the guidance conduit;

In this system, regardless of the rotation, the torque is constant. The power calculation in the guidance conduit:

For this the 252 kg force in the rotation direction is transferred to the conduit.

252, 2Kg x 73,5mm/104mm = 178,3kg the rotation force in each chamber. Here, force x load way = force x force way used for pulling a wedge to the pressure chamber.

296,8kg x 14mm = force x 26,8 force = 155,04kg the force increasing in each chamber in the rotation direction =178,68kg - 155,04kg=23,64kg.

The rotating power increases 23,64 x 14 =330, 96kg in total.

Power calculation

W=330,96 x 10 x 2 x 3, 14 x 0, 104 x 100/60 =36Kw

Physical analyses for different dimensions; Assuming that the load way is 12mm (i.e. S1 wedge is pulled 12 mm inside the pressure chamber; the short edge in the pressure chamber extends 2 mm.)

As the load way is 12 mm; SR 1 ,2 x 4,5cm x 40Atu = 216 kg the force in the rotation direction.

As the load way is 12 mm, the hypotenuse (the force way) becomes 19.8 mm. Accordingly; I use 296,8 x 12 / 19,8 =179,9kg, the force used to pull S1 wedge inside the pressure chamber.

The rotating force, increasing in each chamber 216 - 179,9 = 36, 1 x 14 (chamber) = 505,4 kg total rotating force left.

W = 505,4 x 10 x 2 x 3,14 x 0,0735 x 1000 / 60 = 38,8Kw. If the load way is 10 mm;

SR surface 4,5Cm x 1 Cm x 40atu =180Kq The total force in the rotation direction. As the load way is 10 mm, the hypotenuse (the force way) becomes 18.62 mm. Accordingly the force used for pulling the wedge inside the pressure chamber 296,8 x 10 / 18,62mm = 159,4Kq force used.

180 - 159,4 = 20,60kg forced left The force increasing in the rotation direction, formed in each high pressure chamber.

20,60 x 14 = 288,4kg W = 288.4 x 10 x 2 x 3.14 x 0.0735 x 1000 / 60 = 22.2 Kw. the remained power

Description of the calculation

In case that the transfer of this force is done correctly, the power will go out as 58,8 kW. The pressure at the top of the S1 wedge in the engine is leaning on the inclined plane with a pressure of 296,8 kg. If this is transferred inside the conduit, because of moment thing, it will be required to use a smaller force. I don't know how to do this transfer. In case that this transfer is done correctly, this error will be eliminated. The result would be 58,8 kW again. Modular application of the invention

The turbine engines (1 ) and engines with piston (2), the subject of the invention, can be attached to each other modularly in cases where more power and rotation increasing is needed. These are respectively;

Applications for increasing revolution (UFO engine) In order to increase the rotation, the rotor of an engine will be attached to stator of another engine. By this way, the revolution of each engine will be carried by transferring on each other. As we grow the diameter of the shaft, it will be ensured that the center of the engine becomes a pipe. A conical funnel can be obtained because the diameters of the engines, in question, are different. It may be ensured that it does suction by attaching a vane to this funnel. Energy can be produced with one of the engines. A stronger pushing can be provided by heating the air sucked. With the pushing force, the UFO engine is obtained. Flying saucer is made by making a cabinet outside. It can be applied to a lot of places of any cabin. It may be ensured that the existing planes are made without fuel by changing their engines.

Applications for increasing power;

In order to increase the power, the power of each engine will be used simultaneously and over the same shaft by means of sequencing each engine on a shaft and operating all rotors and stators synchronized. By this way it may be ensured that very big powers are obtained.

Applying the fuelless engine, the subject of the invention (1 ), with piston

No detailed design was made in this engine with piston (8). It is a schematic project for proving. Normally, these pistons will be made round. Bedding of these pistons will be done by expert engineers. A lot of pistons pushing forward inside a pressure chamber and piston sucked inside the pressure chamber. What is important is the principle that the lubricant volume inside the high pressure chamber is constant or changes very little. There may be very different inclined planes. The schema here was made scaled. Again with 3 physical analysis, the invention claim is proven. In this project too, there should be only very small changes during movement in the lubricant volume inside the high pressure chamber. High volume changes should not be because this will compel the hydraulic and pneumatic circuits. In short, the hydraulic & pneumatic solution of the problem should be without needing additional energy. Because, when the volume of the linear movement piston (10) inside the pressure chamber starts decreasing, the piston leaning on the inclined plane (9) is sucked inside the pressure chamber such that the same volume increases. The piston body (1 1 ) of the piston leaning on the inclined plane (9) is a piece having an inclination parallel with the inclined plane in question. This piece will provide the pushing with the movement in the inclined plane. The angle of the inclined plane may be changed as well as the angle between the pistons, staying with an angle of 90° to each other in the embodiment of the invention shown, may be changed. It will be required that the inclined plane on which the piston leaning on the inclined plane (9) is changed accordingly with different angles in question. The pressure inside the pressure chamber is kept pressurized such that the pistons moves continuously by means of the high pressure valve (12) and isolating valve (14).

Physical analysis of the engine with piston;

Physical analysis based on 1/6cm and 100 Bars; Fi, the force pushing the linear movement piston (10) in the Figure 19 = length 80mm x Height 60mm =48cm2

The piston, leaning on the inclined plane (9) 80mm x 80mm =64cm2

Force way (hypotenuse) calculation; square of 6 + square of 8 = 100, its square root is 10Cm, the hypotenuse. Based on 10OAtu Fi 48 x 100 = 4800kg, the force for pushing forward.

The force, Fed, pressing the piston, leaning on the inclined plane, in the Figure 19, downwards 64cm 2

64cm2 x 100 = 6400kg force leaning on the inclined plane

The force used for pushing Fed, leaning on the inclined plane to pressure chamber, Load x load way = force x force way 6400Kg x 6cm / 10Cm = 3840Kg, the force used. We slide it on to the inclined plane with the force and pull inside the pressure chamber.

4800Kg - 3840Kg = 960Kq is the force remained in 1 piston.

Calculations per different load ways

If the load way is 40 mm, i.e. height of the pushing piston is 40, width 80 mm;

Pushing force 4cm x 8cm = 32cm2 at 100 Atu a pushing force of 3200kg.

The force leaning on the inclined plane doesn't change, 6400Kg.

To slide this load in the inclined plane the force way, 8,94 cm hypotenuse Accordingly; 6400 x 4 / 8,94 = 2862kg

The pushing force increasing; 3200-2862 = 338kg force increases in the rotation direction.

If the load way becomes 20 mm, i.e. the pushing piston height becomes 20 mm, width 80 mm;

The pushing force 2cm x 8cm =16cm at 10OAtCi a pushing force of 1600kg is formed.

The force leaning on the inclined plane doesn't change, 6400Kg

To slide this load in the inclined plane the force way, 8,25 cm hypotenuse

Accordingly; 6400 x 2 / 8,25 = 1551 kg The pushing force increasing; 1600 - 1551 = 49kg force increases in the rotation direction. Volume control;

Linear movement piston (10) 48cm2 x 8cm = 384cm3 volume is discharged.

Piston leaning on the inclined plane (9) piston 64cm2 x 6cm =384cm3 volume is filled. i.e. as one of the pistons leaves the pressure field, the other one fills the pressure chamber with the same speed. And, therefore, the potential energy is converted into kinetic energy. The pump doesn't press an additional lubricant inside the pressure chamber.

If the increasing linear force is converted into rotation movement by means of crank method or another method, an engine producing infinite power is created. Besides, this force can be used linearly.

The result can be seen when the analysis below is evaluated again. In this embodiment of the invention, after the engine (1 ) is started moving, the lubricant leaked inside the low pressure chamber (ABO) is collected and pressed inside the engine with piston (9). The energy required for this can be taken from its own shaft of the engine with piston (8).

The movement is also taken by pulley from the shaft in question and power is transferred to the battery, from there to the hydraulic circuit through charging dynamo. The system feeds itself after the first drive. In the application of the invention with both wedge (6) and piston, the actions in question repeat. A lot of different solutions can be produced by using this return feed, i.e. hydraulic & pneumatic methods, mechanical methods. These solutions may differ depending on the area of usage. What is important it that the physical analysis is correct.

Operation of the engine with piston (8) In order for the engine with piston (8) starts running, the isolating valve (12) in the figure 19 is closed and the high pressure valve (13) indicated in the Figure 19 is opened. When the piston moves to the last point, i.e. when the piston will return, the pressure inside the high pressure chamber is zeroed. For this, the pressure vale (13) in the figure 19 is turned off and isolating valve (12) in the figure 19 is opened and the pressure is dropped. The piston is pulled backwards and after the retraction action is completed, the open-close valve (12) is closed and the pressure valve (13) is opened. The system is operated by repeating this operation. When the pistons are retracted backwards, only the friction force is used. This is taken from the other pistons making pressure for that moment. Special apparatus making pressure and dropping pressure will be made for this.

Area of usage of this invention;

This engine is the new engine of the world. It will be beginning of a new era. It will be used everywhere, too numerous to be counted. Furthermore it is the engine of flying saucers (UFO), access to any point in the world will be very fast; the metallurgy industry will be brought to the space. The castings to be made in the environment without gravity and where there is no atmosphere pressure will be lighter and with high strength. A very big revolution will be experienced in the metallurgy and chemistry industries. It will enable that the borders in the world will be deleted and the entire world becomes a single country. There is no need for land, air and seaways. It will also be used instead of electrical engine. Life of people will be cheaper 70%.

Because this invention breaks the laws of physics, with the two scaled prototypes to be completed our invention claim, the subject of the patent application, has been proven. Furthermore, the analysis for sliding in an inclined slope from the two narrower angles each, its understandability was clarified.

The first application of the invention; "Turbine engine" Because the turbine engine project was prepared for making prototype and realization, it can be seen in detail in the figures attached. In addition to this, the invention which is the unit with piston was for proving the increase in the linear pushing force. To the dismounting and mounting details, no details were given for the physical analysis to be understood easily. Because these applications of the invention are hydraulic ball bearing, it will be designed and produced by the ball bearing industry which has the high technology. This consists of a wide scaled R&D and engineering research. What is important is the physical analysis inside the pressure chamber. The calculations in questions are not mentioned here because the dimensions of the engine (1 ) can be variable.

Because the project has zero errors and it is simple, the function of the pieces can be understood easily. The invention, in the most general sense, is the physical analysis of two wedges (6) inside a pressure chamber. There may be more than two wedges inside a pressure chamber, especially over the inclined plane. The most basic benefit of using more wedges is in the increase of the quickness of the movement and increase in the energy production.

The fuelless engine (1 ), the subject of the invention, operates with a technique converting the potential energy to the kinetic energy. Its basic principle is that by creating a force leaning on the inclined plane when hydraulic pressure is applied in the high pressure chamber, it creates a moment force to the rotation direction to the low pressure chamber from the high pressure chamber. The force we use for pulling the wedge leaning on the inclined plane to the high pressure chamber and for closing the short edge is the loss in the pushing (rotating) force. It would be seen that the rotating moment is higher compared with the rotating moment obtained with the loss in question. What is important here is the principle that the lubricant volume inside the high pressure chamber is constant or changes very little. In this engine (1 ) there is a volume change around 0,3 cm3 in each period in each high pressure chamber. In order to feed this, the nitrogen balloon (hydraulic battery) is placed with a torus (ring) shape inside the lubricant conduit with high pressure inside the external body.

The operation process of the engine was mentioned in order. First movement

In this project, as it is seen in the return feed circuit, first the engine pressurizes lubricant to the high pressure chambers and starts the engine. Return feed power

After the engine starts running, the lubricant leaked from interior of the high pressure chamber is collected and pressed again inside the engine. In order to do this, we take the movement attached to its own shaft, first we charge the battery with the charging dynamo, then we feed the electrical motor with the battery. The system may use around 1 % of the energy it produces. If there is 1 ton of lubricant leakage, a 1 kW pump may raise to 40 Atu again. It is possible to feed this system with different techniques.

Claims

1 . In order to be able to develop turbine engines (1 ) enabling potential energy to be converted into kinetic energy; a fuelless turbine engine (1 ) ; consisting of

- at least 1 wedge (6), which the lubricant pushes, the pressure of which increased by means of a high pressure nitrogen balloon (hydraulic battery), which is contained by the internal body guidance conduit (4),

- the rotor disc (6) on which the wedges (6) are aligned and

- the cell divider (3) to be used for the pressurized lubricant affecting on each wedge (6) simultaneously and separately,

characterized by inclined planes to which the wedges (6) lean on in order to create a rotating force.

2. Fuelless turbine engines (1 ) like in the claim 1 which are brought to increasing power and revolution values by being placed one in front of another and turning each other.

3. A fuelless turbine engine (1 ) like in the claim 1 , characterized with a battery which is first charged with a charging dynamo by taking movement from a sheave which is connected to the shaft; and an electrical engine, which performs the return feed of the lubricant by means of this battery in order to collect the lubricant leaking during the operation of the turbine engine (1 ) and pump it back to the turbine engine (1 ).

4. A fuelless turbine engine (1 ) like in the claim 1 , characterized with two or more wedges (6) in each pressure chamber.

5. In order to develop engines with piston (8) enabling potential energy to be converted into kinetic energy; a fuelless engine with piston (8), consisting of

- a linear piston (10) moving towards the outside during the movement of the piston (9) leaning on the inclined plane towards the inside, such that the pressure always stays constant with the movements of the piston (9) leaning on the inclined plane and the linear movement piston (10) inside a high pressure chamber (YBO),

- the linear piston (10) moving towards the inside during the movement of the piston (9) leaning on the inclined plane towards the outside, such that the pressure always stays constant with the movements of the piston (9) leaning on the inclined plane and linear movement piston (10) inside the high pressure chamber (YBO),

characterized with the piston body (1 1 ) of the piston (9) leaning on the inclined plane which leans on the inclined plane, creating the pushing force.

6. Fuelless engines with piston (8), like in the claim 5, which are brought to increasing power and revolution values by being placed one in front of another and turning each other.

7. A fuelless engine with piston (8), like in the claim 5, characterized with a battery which is first charged with a charging dynamo by taking movement from a sheave attached to the shaft; and an electrical engine, which performs the return feed of the lubricant by means of this battery in order to collect the lubricant leaking during the operation of the engine with piston (8) and pump it back to the engine with piston (8).

8. A fuelless engine (8), like in the claim 5, characterized by the lever techniques or spring supports or hydraulic systems which changes the power transmission to be used instead of inclined plane .