JPS61501219A - propulsion device - Google Patents

Abstract

(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Detailed description of the invention] Linear propulsion using molecular energy technical analysis of invention The present invention relates to linear propulsion 1'C of a vehicle in air or water, A novel method and novel propulsion device for performing propulsion work using thermal energy of fluid This is what we believe in.

Background technology of the invention In the applicant's opinion, the present invention is a basic invention and makes reference to related prior art. For a clearer explanation, the idea underlying the present invention and the current physical method The relationship with the rules is shown in the text below.

Fluids are composed of molecules that retain kinetic energy through constant motion. Are known. The pressure of a fluid acting on a solid region impacts and bounces off that region. caused by molecules that If this region is stationary, molecules approaching the region Also, the average velocity and kinetic energy of the molecules bouncing off the area are theoretically constant. It is something. This state changes if the region is not stationary. That is, the areas are close When moving away from the molecules inside, the average velocity of the molecules that bounce back is small. When the region moves towards nearby molecules, the average speed of the rebounding molecules is greater than the average initial velocity of molecules in close proximity. A somewhat similar phenomenon occurs with rubber balls. It can be observed how elastic the ball bounces off a solid wall. luck of the ball Dynamic energy can be increased or decreased depending on the direction in which the wall moves. ball field In the case of molecules, the change in velocity simply changes the kinetic energy of the ball, and in the case of molecules it changes the molecular motion. Any change in dynamic energy is felt as a change in the temperature of the fluid. Therefore, the solid region When a region moves through a fluid, the temperature of the fluid increases as the molecules move further away from each other. Or it decreases on the trailing side and increases on the front or leading side moving towards the approaching molecule.

When this region moves, the molecular force is caused by the bouncing molecules and acts on the rear side. The work that feels like it is covered by energy and the heat is extracted from the rear side is performed, and the same Sometimes an area in motion acts against a similar force acting in front of it, producing heat there. to return the work performed.

Since the opposing forces caused by the fluid pressure acting on both the front and back sides are equal, the work or The net heat gain is zero if losses are ignored.

The molecular energy possessed by surrounding fluids such as air and water is equal to the above opposing forces. If it is avoided, it can be converted into useful work. From two equals like this The force formed as a result of the opposing forces is a special force that is not currently used. It has the following two special characteristics. part, a), perceivable or Appears as a force with no noticeable reaction, and therefore a reaction It appears as a force of no force, and is possessed by fluids, including surrounding fluids such as the atmosphere and water. There are two things that can be cited for having the ability to convert molecular energy into useful work.

The object of the present invention is to generate the above-mentioned special force and use it to perform the propulsion work. Energy is generated from the thermal energy of the fluid in contact with the device to cover the propulsion work. The goal is to obtain a propulsion device that pulls out the power.

According to the current prevailing view, a force with no apparent reaction is defined by Newton's third law. does not match, and the conversion of the molecular energy of the surrounding fluid into work is the second law of thermodynamics. Furthermore, the idea on which the present invention is based is inconsistent with the current laws of physics. It is clear that the purpose of the present invention can be achieved only if the above idea is not applied. The following describes the applicable physical laws and similar phenomena that occur in natural red.

When an object submerged in a fluid moves slowly horizontally, static pressure causes the object to Since the opposing forces moving at the front end are equal, the fluid is cooled at the front end and heated by the same amount at the back end. If losses are ignored, the final fluid temperature remains unchanged.

A completely different effect appears when an object moves up and down in a fluid. against fluid Due to the action of gravity, a fluid placed in a gravitational field gains its own weight, and as a result The pressure developed in the fluid decreases with decreasing distance from the center of gravity. Therefore, The pressure acting on an object immersed in a fluid is the same at the top of the object away from the center of gravity. smaller than the bottom of the. This works downward from the top @ < small pressure and upward from the bottom Two unequal pressures of greater pressure form an upper lurch. Therefore, As stated in Archimedes' principle, an object immersed in a fluid is the fluid that displaces it. is lifted by a force equal to its weight. This upward force of Archimedes It has two special properties. That is, a), the Newtonian reaction of this force is perceivable. It is not a thing or something that stands out clearly, it looks like a force with no reaction.

However, this means that every action has an equal and opposite reaction. This does not violate Newton's third law. Newton's law is that the top of an object and the bottom can be applied separately, and each part can be clearly identified. It has a molecular Newtonian reaction that is impossible. amount that bounces off each part The velocity of the child can be determined by Newton's third law. like this is the sum of two apparent rod reaction forces, such as the forces acting on the top and bottom of the above object. The apparent rod reaction force formed by static pressure is.

It appears as a force of no reaction without violating Newton's laws.

Next, the second characteristic is that the Archimedean force of this apparent rod reaction is It has the ability to directly convert the molecular energy of the submerged fluid into work. object The work done by this apparent thermal reaction force by lifting the weight of is the molecular energy of the fluid in which the object is submerged, commonly known as thermal energy. drawn from energy.

When an object rises, molecules that bounce off the bottom of the object move farther away than molecules that approach. is cooled, and molecules bouncing off the top moving against approaching molecules are heated. deer However, the force acting on the bottom is greater than the force acting on the top, so the heating occurs at the top. More molecules are cooled at the bottom than are absorbed. After all, the fluid is a circle like air or water. Work performed by an apparent thermal reaction force that converts the heat of the surrounding fluid directly into work is cooled by the heat equivalent of the amount. The proof that must be given is that energy cannot be produced. It cannot be eliminated, it can only be transformed from one form to another. This can be obtained by the law of conservation of energy.

The seemingly inert Archimedean force that lifts objects such as airships and submarines If an object suddenly disappears due to an explosion, etc., and sinks as it is or in pieces, The apparent heat that lifts an object held in the object's mass in the form of potential kinetic energy The work done by the reaction force is the heat caused by the friction of the falling object or its fragments. and the flow of air or water in the form of heat generated by the final impact of an object on the ground. Return to body.

Thermal power converts the heat extracted from the atmosphere or an open fluid such as water into useful work. Despite the generally held view that the second law of science prohibits this, It is found in nature.

To the best of Applicant's knowledge, the author did not notice or discover this apparent difference. It was the first time. The effect of this discovery cannot be refuted. By the way, the above Archimede Lifting the weight of an object by force is accomplished without expending any energy; This is in accordance with the first law of thermodynamics, and the heat generated by falling objects is created by other objects. is not converted from the energy source, which contradicts the law of conservation of energy.

In the case of the present invention, heat is extracted from the surrounding fluid, such as the atmosphere or water, and the Archimedean force is converted into useful work in the same way as is done by nature when lifting an object. Ru. This is true if the work performance force used in the present invention is formed as follows. I can give. In other words, the reaction of force can be perceived in the same way as the reaction of Archimedes' force above. The force is caused by fluid molecules bouncing off each other or from a solid wall in a way that cannot be measured. It is formed. However, the existence of a reaction that must exist according to Newton's law Currently, the velocity of molecules bouncing off solid regions or each other is equal to the action of the beam. It is mathematically proven that it can be determined by Newton's formula that can do.

The above-mentioned forces are the essence of the invention and will be reiterated, so we will not discuss their length here. The term RAF', which means ``the apparent force of unfriendly action'', is used to shorten the traditional name. will be used in the text below.

In the present invention, RAF improves thermal energy efficiency over that which can be achieved with conventional methods. linear propulsion work other than that performed by the Archimedean forces mentioned above for the purpose of achieving the utilization As it is used for the first time. RAF recognizes the special, novel and unique features of this invention. It is a sign.

Conventional IJ near propulsion, jet propulsion has a perceptible Newtonian reaction This is generated by including the thrust force in the momentum of the discharged fluid. RAF cannot sense it or has a less noticeable Newtonian reaction, the RAF-driven Near propulsion RVC lacks such reaction, and this point makes propulsion by RAF drive This is one of the most notable features of the device.

The above describes the relationship between the idea on which the present invention is based, the purpose of the present invention, and related physical laws. Having described this, the present invention will now be explained.

Disclosure of invention In summary, the present invention generates RAF and extracts heat from a fluid such as the atmosphere or water. Propulsion work is improved by utilizing the RAF's special capabilities that can be converted into useful propulsion work. solar energy in the surrounding fluid as an energy source. A new technology that makes it easier to utilize the huge amount of energy stored as heat. It provides a style IJ near propulsion device. In the present invention, the propulsion device The fluid passing through the specially shaped duct forms an RAF that allows the device to When RAF is activated, a decrease in fluid temperature is produced corresponding to the work done in RAF. .

To clearly explain the principle, I will give two examples below: perceptible reaction and non-perceptible reaction. Show the meaning of reaction.

b) A heavy object is ascended by a balloon attached to a rope. The force acting on the rope is It is created by the static pressure acting on the balloon, and this force cannot be counteracted by any kind of fixing device. The effects are designed to be imperceptible, unnoticeable, or undetectable.

Such a force is defined in this example as the Archimedean force, which is also RAF. Ru.

RAF also has the ability to extract heat from the surrounding fluid of air or water and convert it into work. The RAF performs this task while the heavy body is ascending.

), if the same weight is to be lifted by a helicopter, the reaction of the force acting on the rope is The effect is in this case perceptible in the air being pushed downwards by the rotating propeller.

This reaction can be felt and its effects can be seen. The applied force is RA It is not an F, and does not possess the capabilities of the RAF as described above. In this case, the heavy body It is lifted by the work provided by the motor of the licopter.

Both powers are the same in their action, but completely different in their nature and abilities. They are different.

The term ``duct'' has a wide range of meanings in the text and includes channels, passageways, conduits, nodules, It has the same meaning as synonyms such as cheat.

The structure of the linear propulsion device according to the present invention will be exemplified below with reference to the attached drawings. I will clarify.

Figure 1 is a longitudinal cross-sectional view taken along A-A of a propulsion device suitable for subsonic speeds; Figure 2 is a view of the same device from B-B. Figure 3 is a longitudinal sectional view taken along C-C of a propulsion device suitable for supersonic speeds, Figure 4 shows the half of the device seen from D-D, and Figure 5 shows the platform for starting propulsion. E-KK longitudinal cross-sectional view of a propulsion device equipped with a propeller, Figure 6 is a cross-sectional view of the device taken along H-HK, and Figure 7 is a W-shaped thruster for aircraft propulsion. Longitudinal cross-sectional view from G-GK of the forwarding device, Figure 8 is a view of the same device as seen from J-J, and Figure 9 shows the bow and stern propulsion devices installed. Figure 10 is a cross-sectional view of the same ship taken along line -K, and Figure 11 is a view of the wing. Viewed from the S-S of an aircraft with a propulsion system attached to the wing and housed inside the wing. A partial cross-sectional view taken along N-H, and Figure 12 is a view of the aircraft seen from M-M. .

Explanation of the propulsion device shown in FIGS. 1 and 2 When the device moves in the direction shown by arrow 5, the main The atmosphere or fluid such as water in which the installation is submerged is forced into a diffused or wide-spread duct 1 and is directed and deflected from the duct to pass through the convergent or tapered duct 2 After being deflected rearward in section 3, it is discharged.

The rear wall 4 moves around the pivot 7 and completely or partially closes the outlet area 9 of the tapered duct 2. It is placed between the side plates so that it can be closed off. This movement is carried out by a hydraulic or pneumatic device6. It is being carried out more than ever. When outlet 9 is completely closed, the velocity of the fluid injected into the ram The head increases the pressure within the device and the device acts as a brake. Suehiro form da The pressure and velocity of the fluid at the inlet 8 of the cylinder 6 are determined by the pressure and velocity of the fluid at the inlet 8 of the cylinder 6. It is controlled by the movement of the wall 4.

The ram-injected fluid of air or water through this divergent duct 1 undergoes a special process, i.e. Due to the increase in fluid pressure due to duct diffusion as well as the increase in the absolute velocity of the fluid in the duct temperature drop due to

The absolute pressure of the fluid, which determines the energy contained in the fluid, is the ram velocity of the fluid and the duct) K vs. is the difference between its relative velocity and its relative velocity, so the decrease in relative velocity in wide-ended duct 1 is This means that the fluid gains absolute velocity in the forward direction. The kinetic energy of this fluid In this configuration, the increase in can only be covered by the molecular energy of the fluid itself. do not have. This absolute velocity is already contained within the duct 1 rather than directly by the rear wall 4. is caused by a fluid that is under increasing pressure and is under increased pressure, resulting in collisions with incoming molecules. The fluid molecules in the duct that give the thrust velocity in the forward direction lose their velocity, Therefore, the fluid is cooled there and the fluid flow formed in the divergent duct 1 This increased energy is covered by the molecular energy of the fluid. As a result of this Molecular energy, also commonly known as body thermal energy, directly affects the velocity of fluid flow. Degrees as well as pressures are converted. This effect allows the device to move and push the fluid in with ram pressure. Only IIK is obtained.

As in wind cylinder experiments, fluid is blown into a stationary device with a given velocity. In this case, the absolute velocity at which the fluid flows into the device due to the decrease in the relative velocity in the wide-end duct 1 The fluid is compressed and heated if it is a gas, and the fluid is compressed and heated if it is a liquid. In that case, the velocity is converted to pressure.

The inner surface of the duct wall ((the increased pressure in the working duct 1 results in a considerable force acting in the forward direction) , and the propulsive work performed on that side results in cooling of the fluid in the duct 1. be done.

Passing through the tapered duct 2, the fluid increases its relative velocity, which in combination with the speed of the device The momentum of the fluid changes and the fluid exerts dynamic pressure on the front of the tapered duct 2. Converts momentum into propulsion. Furthermore, a change in the momentum of the fluid is brought about by the deflection tool 3. The momentum of the fluid at the outlet of the tapered duct 1 and the fluid discharged from the device The difference between the momentum and the momentum constitutes the dynamic pressure exerted on the device in the forward direction.

Momentum of the fluid is created in the duct 1 by the molecules colliding with each other, increasing the momentum of the fluid. of the equipment walls because the kinetic energy is covered by the heat extracted from the fluid. The force formed by the static pressure of the fluid acting inward and outward, as well as the thrust formed by the dynamic force. The forces create a total thrust with the characteristics of the RAF described above. Make it in the direction shown by arrow 5. The propulsion work performed by the RAF used is due to the flow of fluid passing through and surrounding the device. A fluid such as air or water that is discharged from a device made of molecular energy and surrounds it. The idea of the present invention is that it leaves the device with a corresponding temperature change and A molecule bouncing off a wall that moves away from the child loses its speed and cools down, causing it to bounce away from the nearby Molecules bouncing off walls that move toward molecules that move toward them increase their speed and become heated. all flow The body leaves the device and is cooled by the amount of propulsion work performed by the RAF.

If flow losses through the device are kept to a minimum 1, the absolute velocity of the fluid exiting the device can be approximately equal to the absolute velocity of the fluid that it had before being forced into the ram.

In particular, due to flow losses such as friction and turbulence, the fluid exiting the device is proportional to the forward direction. This kinetic energy is the work done by the RAF. This energy is considered a loss since it absorbs a portion of the energy.

The rear wall 4 can be actuated simultaneously by the cylinders 6 to adjust the overall magnitude of thrust or Adjust the thrust force separately for each tapered duct to make it more effective. be able to effectively steer the company. Tapered duct 2 is important in this propulsion device It is an element that can increase the pressure inside the expanding duct 1, and the angle of inclination is affect the performance of the system.

This device can be propelled underwater or in the air. When used in air, subsonic desirable.

The propulsion system can be modified according to individual requirements. If desired, place the device along the center line. It is also possible to configure only one tapered duct so as to divide it. Also, it is necessary If necessary, two or more tapered ducts can be connected to the equipment by configuring their wide ends to read directly into one common inlet. It is also possible to provide one. If deflection tool 3 is also required, use this as an adjustment allowance to determine the amount of fluid deflected. The magnitude of the thrust can be adjusted by increasing or decreasing the amount of force. In addition, the deflection device can be adjusted separately and the rudder and You can also get a better effect.

If necessary, the rear wall 4 can be firmly and securely connected to the side wall in the open position and tapered ducts can also be connected. Alternatively, the flow of fluid can be adjusted using a shield installed in the wide-spread duct. .

In the illustrated example of the propulsion device shown in Figures 3 and 4, this device is designed for supersonic propulsion. has been done.

It consists of a device 10 having a wide duct 11 and a tapered duct 12. This device 10 has the same design and shape as the propulsion device shown in FIG. 1, except that it has a circular shape. It is the afterlife of Noh. An inlet diffusion section 13 and an exit diffusion section 14 are installed to meet supersonic conditions. has been added. In order to minimize drag forces, a cowl 15 is also preferably added.

In this example, the tapered duct 12 has a conical shape and is formed between two conical walls. one of which forms the leading side 17 of the tapered duct 12 and the other one forms the trailing side. tail! l! l! 118 is formed.

When the propulsion device moves at ultrasonic speed in the direction of arrow 19, the air forced in by the ram pressure The air enters the duct 13 where the velocity of the air relative to the duct is equal to that of the wide duct 11. The sonic velocity is reached at the inlet and the air is compressed accordingly. Pass through wide-end duct 11 Then, the relative velocity of the air is further reduced in the same manner as described for the apparatus of FIG. Suehiro Daku The air flowing into the tapered duct 12 from the duct 11 increases its speed and reaches its minimum. It reaches the speed of sound at the exit of the cross-sectional area, and after being deflected backwards, it flows into the discharge diffusion section 14 and there. It expands further and is then discharged.

A rear wall 18 is moved by a hydraulic or pneumatic cylinder 16 to close the exit surface of the tapered duct 12. The size of the product can be changed.

In this way, the magnitude of the air flow and thrust through the device can be adjusted. or , the device is converted into an effective brake if the exit surface area is completely KMed.

In the case of the propulsion device shown in FIG. 1, the inlet diffusion section 13 and The thrust of the RAF characteristic is calculated by considering the force formed by the air pressure acting on the wall of the exit diffusion section 14. is formed.

Air flows out of the diffusion section 14 at a supersonic velocity relative to the diffusion section, and this air ideally is equal to the ram operating speed if losses are ignored, in other words its absolute speed is It is the same as the air had before the ram was activated.

In practice, due to losses, the discharged air has a relatively small absolute velocity in the forward direction.

If necessary and to meet specific requirements, the propulsion device shown in Figure 3 may be constructed of two or more circles. Consisting of conical tapered ducts placed in front and behind each other with wide ends connected to a common inlet. Can also be done.

Explanation of the propulsion device shown in FIGS. 5 and 6. This propulsion device is a propeller driven by a motor 27. 26 is provided and the deflector 22 is hinge-connected. The location and function are the same.

When the device moves in the direction of arrow 23, the ram pressurized fluid flows into the wide-end duct 25. After entering the duct 20 and passing through the tapered duct 21 and being deflected by the deflector 22 be discharged.

The devices shown in Figures 1 and 3 are in motion, and the fluid can be pushed in by ram press-fitting. The motor-driven propeller 26 is positioned so that it only generates thrust when the device is stationary. The purpose is to facilitate the generation of thrust when stationary or moving at low speed. I have it. The driving propeller provides the initial thrust to start the device, and the fluid The thrust RAF formed when the ram is compressed is large enough to take over propulsion. When the device reaches such a speed, the propeller 26 can be stopped or retracted toward the rear wall if necessary. You can

This propulsion device operates at a sufficiently high speed similar to the device described in FIG. In the RAF In this case, the magnitude of the thrust formed is such that it moves backwards and prevents it from flowing into the tapered duct 21. It is controlled by a sleeve 24 which can be partially or completely occluded. deflector 22 is hinged and this also allows the thrust to be made in mm. Steering effect if required The deflector 22 can be separately actuated to obtain .

The propulsion device shown in FIG. 5 can operate without the wide-end rod duct 25. this place In the case of a hill, the fluid entering the duct 20 which is not wide-ended increases in pressure very suddenly. End - There is no force formed by the pressure of the fluid acting on the inner wall of the large duct 25. Therefore, the forming thrust, or RAF, also decreases when compared to the end-hiro type population. Decreasing trend Despite the power, the device can be made relatively short without the wide-end duct 25. And such propulsion devices are applied to special requirements.

In all of the propulsion devices illustrated and explained above, thrust with RAP characteristics is formed, and this The thrust is when performing work, it draws energy from the fluid used to cover this work. The pumped fluid exits the t-device with a corresponding temperature drop.

If the fluid is air, the propulsion device's thrust is adjusted to increase the air evacuation rate if necessary. This can be increased by heating the air within the device.

Application of the invention in industry The propulsion devices that can be illustrated and explained in the text are vehicles that move relatively quickly in the air, such as aircraft and trains. It is also suitable for vehicles that move in or on water, such as diving crews and water vessels. However However, this device can also be used at the tip of a helicopter rotor or a rotor designed for power generation. It is also used to obtain rotational propulsion by attaching the tip (().

The invention has numerous practical applications. Some advantages intended by the applicant 7 as just an example of the many possible applications suitable for special requirements. It is shown in Figure 12 from the figure.

Figures 7 and 8 show how the propulsion system can be used to propel an aircraft. ing. The propulsion device is formed by a circular, more preferably oval, outer shell 31, the front of which A tapered dame that can be shaped into a circular or oval shape to fit the torso along with the front part of the body. form a ct. A hydraulic or pneumatic device 32 moves the outer shell 31 closer to or closer to the shoulder body. The tip formed between the fuselage and the outer shell 310 can be moved further apart. Adjust the outlet of the narrow duct to adjust the magnitude of the thrust. The exit must be completely closed. It can also be used as a brake, in which case the device acts as a brake. The lateral stability of the construct is This can suitably be achieved by four hydraulic cylinders 32.

In the configuration shown, the device is suitable for subsonic propulsion.

The device can also be used to propel submarines. In this case, at the front of the aircraft warm body The bow of the submarine is applied instead.

In Figures 9 and 10, a propulsion device is used to propel a ship. Each Depending on the requirements of the ship, the device can be mounted on the bow or stern of the ship. both structures The configuration is shown in FIGS. 9 and 10.

The propulsion device is rigidly attached to the hull at one end and forms a wide divergent duct 36 at the front of the other end. It is attached to the bow by a plate 40. A hydraulic system is installed between this plate 40. At 39, a movable wall 37 is arranged on the rigidity of a pivot 38. Wall 37 is a ship It forms a tapered duct with the body, the outlet of which can be adjusted by a hydraulic device 39; By adjusting the magnitude of the thrust and completely closing the outlet, the device can be operated during navigation. Acts as a brake on the ship. Arrow 46 indicates the direction of movement of the ship. stern smell In this case, the propulsion device is also rigidly attached to the hull by a plate 43. plate At the front between 430 there is an adjustable wall 42, and at the rear the plate tapers. It constitutes a part of the duct 41. The rate 42 is connected to the axis 4 by a hydraulic device 44. 8, thereby forming between the plate 42 and the hull. Adjust the inflow area of the wide-end duct to adjust the amount of water passing through the device. This is K The magnitude of the thrust is adjusted.

The propulsion system described in this text operates only when the ship is sailing, and the arrangement of the propeller 45 keeps the ship quiet. The propulsion device takes over propulsion at a sufficiently high speed with the purpose of starting the movement from a standstill. , stop the propeller 45 and retract it to open a passage if necessary and hide it inside the hull. can be done.

In addition, the propulsion device should be adjusted appropriately by adjusting the wall 37 or 42 on the ship side at the bow or stern. It can also be used for steering ships.

In Figures 11 and 12, the propulsion system is located in 500 fuselage fuselage units. Ru. When the aircraft moves, the air is compressed by the ram operation and pushed into the wide-end duct 51. At the end of the duct, the air is deflected laterally and discharged through a tapered duct 57. tapered shape The duct 57 is housed in the wing of the aircraft, and the rear wall 52 is connected to the hydraulic or pneumatic system M53. It can swing around the pivot 56 to open or close the outlet area of the tapered duct 57. It is configured like this. This adjusts the thrust and also completely blocks the exit. position is converted to brake. Additional propulsion equipment as shown in Figure 3 below the wing 54 is attached.

To reduce drag, a conical tail 55 is connected to the rear wall 18 as shown in FIG. It has been added. If necessary, the device 54 can be attached to the fuselage 50 or the hull of a ship or submarine. It can also be attached to.

The increased pressure of the fluid within the device due to the ram compression process acts on the object to be propelled, causing its steering. It can also be used to obtain lateral fluid jets with counteracting reactions.

In all of the propulsion devices illustrated and explained above, thrust with RAF characteristics is formed, and the Extracts the thermal energy of the fluid used in carrying out the work and covers the work carried out. However, the fluid is left behind at the rear of the device with a corresponding drop in temperature.

FIG, 3 FIG, 4 FIG, S FIG, 6

Claims (1)

[Claims] 1. A propulsion device for performing linear propulsion, which uses "apparently no reaction force". Propulsion is provided by RAF, which is defined in this description as an abbreviation, and the propulsion device is an inlet opening (8) into which the fluid enters when it moves and forces the fluid in with ram pressure; It includes a tapered duct (2, 12, 21) formed wider than the end, and the tapered duct (2, 12, 21) is formed wider than the end. The wide end of the duct is in a more forward position relative to the direction of propulsion than the narrow end. The fluid flowing from the inlet opening is deflected laterally from the line of propulsion and directed to the wide end. The momentum of the fluid flowing in and following the duct is determined by the tapered shape of the duct and the thrust of the propulsion device. This change in momentum changes along the path depending on the advancing speed, and this force is sent to the propulsion device. The linear thrust along with the force formed by the static pressure of the fluid acting on the inside and outside of the wall of the A propulsion device characterized in that the RAF is formed to carry out a forward movement. 2. It uses the molecular energy of a fluid, also commonly known as thermal energy, to accomplish work. ram-actuatedly force the fluid into a moving device in a ram-operated manner. Ram pressure is applied to this so that the fluid enters the device, and the fluid inside the device increases its pressure and moves the device. obtains velocity in the same direction as the direction and thus forms a fluid flow within the device and the effect of the fluid flow. Energy is obtained from the molecular energy of the same fluid, where the fluid is cooled accordingly. and directing said fluid flow laterally within a propulsion device. increasing the momentum of the moving device as a force; Increase the velocity of the fluid by converting pressure to velocity, the flowing fluid increases the fluid The speed at which the device moves and the motion of the device change its momentum, and this change in momentum is expressed as Molecular energy of a fluid that includes the steps of transmitting it as a force to a device that performs work How to use gi. 3. The tapered duct has a conical shape (12), with two conical shapes parallel to each other. is formed between walls (17, 18) disposed not at the exit of said tapered duct. Form an inlet wider than the mouth, so that the velocity of the fluid flowing through the tapered duct is smaller at the inlet than at the outlet, and the two conical shapes are parallel to each other. The walls (17, 18) arranged without One constitutes the leading side of the tapered duct (12) and the other constitutes the trailing side of the tapered duct (12). Claims arranged so that the inlet at the wide end is located further forward than the outlet. Propulsion device according to scope 1. 4. Wide end duct (1, 11, 25) with one end wider than the other end ), the narrow end of which constitutes said inlet opening (8), into which the propulsion device moves. When fluid is pushed in with ram pressure, the fluid enters and after passing through the wide-end duct, the fluid is pushed forward. arranged and configured to be oriented to enter the tapered duct (2, 12, 21); A propulsion device according to claim 1. 5. A wide-ended duct (11) with one end wider than the other end is The narrow end forms the opening into which the fluid enters when the propulsion device moves and forces the fluid under ram pressure. and the fluid is directed to enter said divergent duct (12) after passing through the divergent duct. 4. A propulsion device according to claim 3, wherein the propulsion device is arranged and constructed so that it can be driven by a vehicle. 6. At the outlet of the tapered duct, the momentum of the fluid flowing out from the propulsion device changes. A tapered duct (3, 22) A propulsion device according to claim 1, which diverts fluid exiting from. 7. two tapered ducts such that fluid flowing from the inlet opening enters the wide end; A propulsion device according to claim 1 provided in the above arrangement. 8. The fluid pushed in by the ram pressure enters the wide end and exits from the narrow end to form the wide-end duct. A tapered inlet duct (13) configured to enter the narrow end of (1,11,25) ), and the fluid coming out of the tapered duct (2, 12, 21) flows into the wide-angle outlet duct ( A wide-divergent outlet duct (14) configured to enter the narrow end of and exit from the wide end of the A propulsion device according to claim 4, which is adapted to supersonic propulsion by adding the following. 9. The fluid pushed in by ram pressure enters the wide end and becomes narrow. The wide end duct comes out from the end. a tapered inlet duct (1, 11, 25) configured to enter the narrow end of the 3), and the fluid coming out of the tapered duct (2, 12, 21) is connected to a wide-end outlet duct. A wide-divergent outlet duct (14) configured to enter the narrow end of the (14) and exit from the wide end. ) A propulsion device according to claim 5, which is adapted to supersonic propulsion by adding the following. 10. The magnitude of the thrust is determined by the leading wall (17) and trailing wall (18) of the tapered duct (12). By configuring the gap between the tapered and Claim 1 adjusted by changing the size of the exit area from the outlet (12). propulsion device. 11. The magnitude and direction of the thrust are adjusted by moving the tapered duct around its axis. The tapered duct (4, 37) has a tapered shape so that the size of the exit area of the duct (4, 37) can be changed. Adjustment is achieved by pivoting the walls of the duct (7, 38). Propulsion device by. 12. The magnitude and direction of the thrust are determined by the movement of the wall of the wide-end duct (42) around the axis. The end of the tapered duct can be adjusted by adjusting the size of the inlet opening of the tapered duct. Adjustment is achieved by pivoting the walls of the wide duct (42). Propulsion device by. 13. The magnitude of the thrust is determined by the deflectors (24, 34) placed within the desired duct. A propulsion device according to claim 1, which is adjusted. 14. When it comes to propulsion of a target object, propulsion is defined as ``apparent non-reaction''. RAF is an abbreviation for ``Force of Force'', and RAF is an abbreviation for ``Force of Force''. A propulsion device attached to a target object uses ram pressure to force the fluid in which the base is submerged. The propulsion device is configured such that the fluid forced into the ram enters through the narrow end. A wide divergent duct (1.11, 25) and a fluid exiting from the wide divergent duct are lateral It enters the wide end, and the wide end is the narrow end where the fluid flows out when talking about the direction of propulsion. Propulsion of a target object characterized by being placed further forward than the end. 15. The propulsion device is configured such that the front of the target object touches the trailing side wall at the rear of the tapered duct. (Figure 7), and the magnitude of the thrust is determined by the movement of the propulsion device relative to the object being propelled. The claim range is adjusted by adjusting the size of the exit area of the tapered duct. A device for propulsion of a target object according to Section 14. 16. The propulsion device is configured such that the hull of the vessel is in the direction of movement of the vessel. Forms the trailing side wall at the rear of the narrow duct (Fig. 10), and The vertical direction is determined by the movement of the forward leading wall due to the pivoting configuration of the tapered duct. Mounted on the bow of the vessel to be adjusted by adjusting the exit area of the tapered duct on both sides. Propulsion of a ship according to claim 14. 17. The propulsion device is arranged so that the hull of the vessel is on one side of the divergent and tapered ducts. The magnitude and direction of the thrust acting on the vessel are determined by the pivoting configuration of the tapered duct. Adjustment of the entrance area of the diverging duct on both sides of the ship by the movement of the wall (42) due to According to claim 14, it is mounted on the stern of a ship so as to be adjusted by the Ship propulsion. 18. The diverging ducts (51) are arranged on both sides of the body (50), and the tapered ducts (51) are disposed on both sides of the body (50). The duct (57) is placed inside the wing of the aircraft, and is designed to control the magnitude of thrust acting on the aircraft and The direction is determined by the size of the exit area of the tapered duct due to the pivot wall (52) of the tapered duct. Propulsion of an aircraft according to claim 14 adjusted by adjustment. 19. It moves by utilizing the increased pressure of the fluid in the propulsion device due to the ram pressurization of the fluid. an adjustable lateral fluid with a reaction that acts on and steers a target object Propulsion of an object according to claim 14 to obtain a jet.