Dynamic propulsion device
The Dynamic Propulsion Device, featuring a rotor and rotating arms, addresses the limitation of traditional propulsion systems by enabling independent movement without environmental dependence or mass ejection, achieving efficient forward thrust.
Patent Information
- Application Number
- PCT/TR2024/050932
- Authority / Receiving Office
- WO · WO
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2024-08-08
- Publication Date
- 2025-02-13
AI Technical Summary
Existing propulsion systems require a solid surface or fluid environment to generate thrust, limiting their ability to move independently of their surroundings without ejecting mass.
The Dynamic Propulsion Device utilizes a rotor and arms that rotate around their respective axes, generating forward thrust by the backward movement of the arms, allowing the system to move independently of environmental conditions.
This solution enables vehicles equipped with the Dynamic Propulsion Device to move forward without needing a solid surface or fluid environment, and without ejecting mass, thereby overcoming the limitations of traditional propulsion systems.
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Abstract
Description
[0001] DYNAMIC PROPULSION DEVICE
[0002] Technical Field of the Invention
[0003] This invention relates to obtaining thrust force by utilizing circular motion.
[0004] State of the Art
[0005] Currently, thrust force is generated using wheels, tracks, propellers, jet engines, and rockets. In wheeled and tracked vehicles, movement is achieved through the friction between the wheel or track and the ground. In floating vehicles, movement is facilitated by the backward propulsion of fluid using a propeller. In propeller-driven aircraft, the vehicle moves as a result of the pressure difference generated on both sides of the propeller’s rotation plane due to the rotation of the propeller. In jet- powered vehicles and rockets, the vehicle moves as a result of high-speed fluid being ejected backward by the engine.
[0006] A wheeled or tracked vehicle cannot move without a surface, such as a road or a solid surface, for the wheel or track to rub against. For a propeller-driven vehicle to move, it must either be in a fluid or semi-submerged in another fluid. Jet-powered vehicles also need a fluid in the movement environment to move.
[0007] Rockets do not require any fluid or matter in the movement environment to move; however, to generate thrust force, they must eject a large portion of their mass at very high speed from the rear, thus requiring a very high amount of fuel.
[0008] To enable a vehicle to move independently of the environment, i.e., without needing any fluid or solid matter in the movement environment, the invention named “Rotary Propulsion Device” has been developed.
[0009] Technical Problems the Invention Aims to Solve
[0010] The aim is to develop a propulsion system that can move independently of the environment and ground without using rockets. The propulsion system is intended to move without needing to eject mass from the rear.
[0011] DESCRIPTIONS OF THE FIGURES
[0012] Figure 1 ) Front view of the rotor.
[0013] Figure 2) Isometric view of the rotor.
[0014] Figure 3) Side view of the mass.
[0015] Figure 4) Isometric view of the mass.
[0016] Figure 5) Side view of the dynamic propulsion device (Rotor at 0 degrees).
[0017] Figure 6) Isometric view of the dynamic propulsion device (Rotor at 0 degrees).
[0018] Figure 7) Side view of the dynamic propulsion device (Rotor at 90 degrees). Figure 8) Isometric view of the dynamic propulsion device (Rotor at 90 degrees). Figure 9) Side view of the dynamic propulsion device (Rotor at 180 degrees).
[0019] Figure 10) Isometric view of the dynamic propulsion device (Rotor at 180 degrees). Figure 11 ) Side view of the dynamic propulsion device (Rotor at 270 degrees).
[0020] Figure 12) Isometric view of the dynamic propulsion device (Rotor at 270 degrees). Figure 13) Top view of the dynamic propulsion device (Rotor at 0 degrees).
[0021] Figure 14) Top view of the dynamic propulsion device (Rotor at 90 degrees).
[0022] Figure 15) Top view of the dynamic propulsion device (Rotor at 180 degrees).
[0023] Figure 16) Top view of the dynamic propulsion device (Rotor at 270 degrees).
[0024] EXPLANATIONS OF THE REFERENCES IN THE FIGURES
[0025] 1 ) Rotor.
[0026] 2) Rotor shaft.
[0027] 3) Rotor mounting axis.
[0028] 4) Arm.
[0029] 5) Arm mounting axis.
[0030] Y) Direction of movement.
[0031] R) Rotor axis.
[0032] K) Arm axis.
[0033] DESCRIPTION OF THE INVENTION
[0034] The dynamic propulsion device consists of a rotor (1 ), arms (4) mounted in such a way that the rotor shaft (2) and the arm mounting axis (5) coincide to allow the rotor (1 ) to rotate around the rotor axis ®. The rotor (1 ) can be mounted on any vehicle from the rotor mounting axis (3) to enable movement.
[0035] The dynamic propulsion device can include multiple arms (4).
[0036] The rotor axis ® is perpendicular to the direction of movement (H), and the arm axis (K) is perpendicular to the rotor axis ®.
[0037] The rotor (1 ) rotates around the rotor axis ®, and the arms (4) rotate around the arm axis (K).
[0038] In this document:
[0039] The term “YR plane” refers to the intersecting plane passing through the direction of movement (Y) and the rotor axis ®.
[0040] The term “RK plane” refers to the intersecting plane passing through the rotor axis ® and the arm axis (K).
[0041] The term “System” refers to the dynamic propulsion device.
[0042] The term “Forward” refers to the desired direction of movement of the dynamic propulsion device. The term “Backward” refers to the opposite direction of the desired movement of the dynamic propulsion device.
[0043] In this document, the rotor (1 ) rotates clockwise, and the angular velocity of the rotor (1 ) and the arms (4) is the same. However, the angular velocity of the arms (4) can be higher than the angular velocity of the rotor.
[0044] When the Dynamic Propulsion Device First Starts Moving; (Figure - 5, Figure - 6)
[0045] 1 . The arms (4) should be positioned such that the center of gravity of the total mass of the arms is at the intersection point of the arm axis (K) and the rotor axis ®.
[0046] 2. The arms (4) should be positioned so that the center of gravity of each arm (4) coincides with the RK plane. This positioning ensures that half of the total mass of the arms (4) is on one side of the arm axis (K) and the other half is on the other side of the arm axis (K).
[0047] 3. The initial movement plane of the arms (4) should be the YR plane.
[0048] 4. All arms (4) should start rotating in the opposite direction of the movement direction (Y). At the same time, the rotor (1 ) should also start rotating.
[0049] Here, the arms (4) below the arm axis (K) will rotate clockwise, and the arms (4) above the arm axis (K) will rotate counterclockwise.
[0050] The rotation of the rotor (1 ) and the arms (4) around their respective axes can be achieved by any method. The rotor (1 ) and the arms (4) should continuously rotate around their respective axes.
[0051] The Operating Principle of the Dynamic Propulsion Device is Explained Below.
[0052] Here, the rotation direction of the rotor (1 ) is clockwise.
[0053] 1 . Initially, the rotor (1 ) is positioned such that the arm axis (K) is perpendicular to the intersecting plane passing through the movement direction (Y) and the rotor axis ® (Figure - 5, Figure - 6).
[0054] 2. Initially, the arms (4) should be positioned such that the center of gravity of the total mass of the arms is at the intersection point of the arm axis (K) and the rotor axis ® (Figure - 5, Figure - 6).
[0055] 3. As the rotor (1 ) starts to rotate, the arms (4) begin to rotate in the opposite direction of the movement direction (4). The angular velocity of the rotor (1 ) and the arms (4) is the same.
[0056] 4. The backward movement of the arms (4) applies forward thrust to the system.
[0057] 5. When the rotor (1 ) moves 90 degrees, the arms (4) will have rotated 90 degrees (Figure-7, Figure-8). 6. When the rotor (1 ) moves 180 degrees, the arms (4) will have rotated 180 degrees (Figure-9, Figure-10). In this case, the arms (4) will have changed their initial positions by 180 degrees (Figure-9, Figure-10). The movement of the arms (4) after this position will again be backward and will apply forward thrust to the system.
[0058] 7. When the rotor (1 ) rotates 270 degrees, the position of the arms (4) will be as shown in Figure-11 and Figure-12. The position of the arms (1) is the same as the position they took after rotating 90 degrees from the initial position of the rotor (1 ).
[0059] 8. When the rotor (1 ) rotates 360 degrees, the rotor and the arms will return to the same position as the initial position (Figure-5, Figure-6).
[0060] 9. The entire process will repeat from step 5.
[0061] 10. When the rotor (1 ) is at 0 degrees and 180 degrees, the arms (4) move backward parallel to the plane intersecting the movement direction (Y) and the rotor axis ®, thus producing forward thrust for the system.
[0062] 11 .As the rotor (1 ) rotates around the rotor axis ®, the change in the distance of the center of mass of the arms (4) from the rotor axis (1 ) and the rotation of the arms (4) around the rotor axis ® will not generate a backward thrust force large enough to hinder the forward movement of the system.
[0063] The system consists of a rotor (1 ) rotating around the rotor axis ®, which is perpendicular to the direction of movement (Y), and arms (4) rotating around the arm axis (K). The angular velocity of the arms (4) can be the same as or greater than the angular velocity of the rotor (1 ).
[0064] The arms (4) are positioned on the rotor shaft (2) such that the total center of mass of the arms is on the arm axis (K), and the initial movement of the arms (4) is in the backward direction.
[0065] By mounting two Dynamic thrust devices with rotors (1 ) rotating in opposite directions on the same vehicle, the resultant forces parallel to the arm axis (K) generated by the rotation of the rotor (1 ) and the arms (4) are reduced to zero.
Claims
CLAIMS1. The invention is a Dynamic thrust device, consisting of a rotor (1 ) and an arm (4) mounted such that the rotor shaft (2) and the arm mounting axis (5) coincide, allowing the rotor (1 ) to rotate around the rotor axis ®. The rotor (1) is mounted on any vehicle from the rotor mounting axis (3) to enable its movement.
2. The Dynamic thrust device mentioned in Claim 1 , characterized by the arms (4) being positioned such that the center of mass of the total mass of the arms is at the intersection point of the arm axis (K) and the rotor axis ®.
3. The Dynamic thrust device mentioned in Claims 1 and 2, characterized by the arms (4) being positioned such that the center of mass of each arm (4) coincides with the RK plane, and the initial movement plane of the arms (4) is the YR plane.
4. The Dynamic thrust device mentioned in Claims 1 , 2, and 3, characterized by all the arms (4) starting to rotate in the opposite direction of the movement direction (Y) and the rotor (1 ) starting to rotate simultaneously.
5. The Dynamic thrust device mentioned in Claims 1 , 2, 3, and 4, characterized by the angular velocity of the arms (4) being the same as or higher than the angular velocity of the rotor (1 ).6
Citation Information
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