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Remote Control Plane Using A Magnetic Repulsion System

Abstract: ABSTRACT: Title: Remote Control Plane Working on Magnetic Repulsion Propulsion System The repulsive-type magnetic system has been employed so far in bearing and levitation systems alone. Due to the scarcity of power generation, much modern technique must be employed for power production in this world. This work will states the new invention of producing energy from repulsive type magnetic system for propulsive units. The technique is very effective. This system uses permanent magnets to produce repulsion and this repulsive force produces a torque which drives a propeller and DC generator. The power output from the DC generator can be boosted by the voltage booster and to store in batteries or used to drive any AC loads like other electronic components in the remote control plane like servo motor and receiver device. The plane is designed to be light and strong. The gear arrangement is made up of two gears. One is larger in size and another one is smaller in size. The plane is controlled through transmitter.

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Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
28 January 2021
Publication Number
30/2022
Publication Type
INA
Invention Field
ELECTRICAL
Status
Email
hima@novelpatent.com
Parent Application

Applicants

Institute of Aeronautical Engineering
Department of ECE, Institute of Aeronautical Engineering, Dundigal Road, Hyderabad- 500043, Telangana, India.

Inventors

1. Mr.Vadupu Siva Sai Siddartha
Department of AE, Institute of Aeronautical Engineering, Dundigal Road, Hyderabad-500043, Telangana, India.
2. Mr.M V Aditya Nag
Department of ME, Institute of Aeronautical Engineering, Dundigal Road, Hyderabad-500043, Telangana, India.
3. Dr.Dussa Govardhan
Department of AE, Institute of Aeronautical Engineering, Dundigal Road, Hyderabad-500043, Telangana, India.

Specification

Claims:CLAIMS:
I / We Claim:
1. A remote control plane based on magnetic repulsive system wherein the plane is made with the fences to which the shape is occurred and further covered with the cloth to create the surface.
2. The remote control plane as claimed in claim 1, wherein the circuit includes the primary battery 11 supplies power to the small motor 12 required to generate the moment between the magnets.
3. The remote control plane as claimed in claim 1, wherein the power is transmitted from the larger gear to the smaller gear, the speed that is available at the smaller gear is relatively high the smaller gear is meshed directly which serves in transmitting power from the larger gear to the smaller gear.
4. The remote control plane as claimed in claim 1, wherein the elevator 03 and rudder 02 to both the stabilizers which are controlled by the servo motor 09 arranged under the wing. , Description:DESCRIPTION:
Field of the invention
[0001] The present invention relates to robot that mimics centipede and in particular it relates to a centicopter robot that can fly as well as move fast in the rough terrain.
Background of the invention:
[0002] Many experiments based on the generating free energy using magnet’s repulsive force, most of the applications are in bearings and machinery later it is noticed that vehicles that consume less energy frequently are considered to apply magnetic repulsive technique to increase the output from the work done.

[0003] All these experiments are carried out to generate the electricity or to extract the high amount of output energy from the existing motor. Since remote control planes or micro unmanned vehicles works with the electric brushless motor the requirement is very specific so, this is the best place to apply the magnetic repulsive technique.

[0004] In this product we are trying to use the rotational energy generated from the magnet repulsion forces to propel the plane and also to power the other requirements in it. We are building the mechanism which directly converts the repulsive forces into rotational force to power the propeller. Plane is designed to very light weight so, as to decrease the power required.
Summary of the invention
[0005] The present disclosure proposes a remote control plane working on magnetic repulsion propulsion system. The following presents a simplified summary in order to provide a basic understanding of some aspects of the claimed subject matter. This summary is not an extensive overview. It is not intended to identify key/critical elements or to delineate the scope of the claimed subject matter. Its sole purpose is to present some concepts in a simplified form as a prelude to the more detailed description that is presented later.

[0006] In order to overcome the above deficiencies of the prior art, the present disclosure is to solve the problem by providing a centicopter robot that can fly as well as move fast in the rough terrain. Using rotational energy generated from the magnet repulsion forces to propel the plane.

[0007] Magnetic lines of force spread outwards and away from each other in the space between two like magnetic poles. Hence the lines of force from each pole come together laterally, and the repulsion is caused by the centrifugal pressure in the equatorial plane of the electron-positron dipoles that make up the lines of force. Inside an electron-positron dipole the centrifugal force is merely the monopole pressure field which increases with angular acceleration. The dipoles are like rotating pump handles which screw out the pressurized vitreous electricity. If however we move beyond an electric circuit or a bar magnet in the equatorial plane of the solenoid ally aligned sea of electron-positron dipoles, the repulsive force will be attributable to the dipole field, and it should therefore take on an inverse cube law relationship just like centrifugal force on the large scale. As such, in relation to magnetic repulsion, the Biot-Savart law should more properly contain an inverse cube law relationship to the extent that it applies at all. Solenoidal field lines around an electric circuit or a bar magnet will not extend indefinitely and so it is hard to imagine that the Biot-Savart law will apply beyond that finite extent. Magnetic levitation does occur and it should not really be a mystery even if we are to accept the orthodox teaching that magnetic repulsion obeys an inverse square law.

[0008] Repulsive force is calculated by using repelling magnet calculator, the results of repelling curve and also size of magnet force is shown in below figure. The distance between the magnets is inversely proportional to the repulsive force.

[0009] When the small amount of electrical energy is used to run the motor, the motor convert electrical energy into mechanical rotational motion. The permanent magnets placed on the shaft of the motor is also rotates the speed of the motor.

[0010] The same polarity of magnets which present in the magnetic disc is rotates due to magnetic repulsion. The repulsion between the two magnets makes the rotation continuously in the magnetic disc which is coupled with the larger gear through the shaft. The gear arrangement is made up of two gears. One is larger in size and another one is smaller in size.

[0011] Both the gears are connected are meshed directly which serves in transmitting power from the larger gear to the smaller gear.

[0012] As the power is transmitted from the larger gear to the smaller gear, the speed that is available at the smaller gear is relatively high. The smaller gear is meshed directly which serves in transmitting power from the larger gear to the smaller gear.

[0013] The smaller gear is coupled with the propeller shaft which rotates the propeller of the plane with sufficient RPM.

[0014] Effective generating system which is compatible with the plane. Designing the light weight plain is important in order to decrease the power usage.

[0015] Further, objects and advantages of the present invention will be apparent from a study of the following portion of the specification, the claims, and the attached drawings.
Detailed description of drawings:
[0016] The nature and scope of the present invention will be better understood from the accompanying drawings, which are by way of illustration of a preferred embodiment and not by way of any sort of limitation. In the accompanying drawings:

[0017] FIG. 1 is a diagram depicting a schematic isometric representation of a remote control plane in accordance to an embodiment of the invention.

[0018] FIG. 2 is a diagram depicting a schematic representation of top view of a remote control plane in accordance to an embodiment of the invention.

[0019] FIG. 3 diagram depicting a schematic representation of front view of a remote control plane in accordance to an embodiment of the invention.

[0020] FIG. 4 diagram depicting a schematic representation of circuit diagram in accordance to an embodiment of the invention.

[0021] FIG. 5 is a diagram depicting a schematic representation of wireframe diagram in accordance to an embodiment of the invention.

[0022] FIG. 6 is a diagram depicting a schematic representation of open isometric view of mechanisms in accordance to an embodiment of the invention.
Detailed invention disclosure:
[0023] Various exemplary embodiments of the present disclosure will be described in reference to the accompanying drawings. Wherever possible, the same or similar reference numerals are used in the drawings and the description to refer to the same or like parts or steps.

[0024] The present disclosure has been made with a view towards solving the problem with the prior art described above, and it is an object of the present invention to provide a centicopter robot that can fly as well as move fast in the rough terrain. Using rotational energy generated from the magnet repulsion forces to propel the plane.

[0025] According to an exemplary embodiment, FIG. 1 represents a design of remote control plane, to which the concept of magnetic repulsion technique is applied. The plane is designed to be light and skinny. The major parts of the plane which supports to fly are represented, the design is a fixed wing 01 design supported by a fuselage structure 05, the fuselage structure 05 has a fuselage that is thin called boom 04, controlling is done with vertical and horizontal stabilizer 02 and 03 the magnetic repulsion system 08 is fixed at the centre of gravity of the plane and propeller 06 is connected through a shaft 07.

[0026] According to another exemplary embodiment, FIG. 2 represents the top view of the plane, where the arrangement of the magnetic repulsion system is visible, the position of the system is specified, and also the aspect ratio of the wing 01 is visible. The wing 01 is rectangle in shape and is a thin plate aerofoil mounted by the wing structure and it is given swept back shape is given to the wing, the fuselage boom 04 is fixed at the of chord of wing to which elevator 03 and rudder 02 are attached to the stabilizer with the help of the hinges, also the shaft 07 length can be visible from the gears 08 to the propeller 06.

[0027] According to another exemplary embodiment, FIG. 3 represents the front view of the plane to show the wing supports 10 and the alignment of the wing to the fuselage to attain the stability, here the propeller 06 shape is specified compared to the wing 01, wing is supported through the support 10 because of the wing loading comparatively more with the structure, alignment of the power system 08 to the plane is specified, the shaft 07 varies from the fuselage is specified, the alignment with respect to the wing height is specified to the elevator 03 and rudder 02 to both the stabilizers which are controlled by the servo motor 09 arranged under the wing, wing is given a dihedral angle to have the rolling stability.

[0028] According to another exemplary embodiment, FIG. 4 is a circuit diagram of the model. First, a primary battery 11 is supplying the power to a small motor 12 in order to generate the moment between the magnets. The motor 12 helps to rotate the magnets initially to create moment, there generates a rotational motion this is used to rotate the shaft 15 that is connected to the propeller 16. As the power is transmitted from the larger gear to the smaller gear, the speed that is available at the smaller gear is relatively high the smaller gear is meshed directly which serves in transmitting power from the larger gear to the smaller gear. Further, the rotational motion is used to power the other electronic devices like receiver 19 and servo 20 through the DC generator and secondary battery.

[0029] According to another exemplary embodiment, FIG. 5 is the wireframe of the plane design the whole plane made with the fences to which the shape is occurred and further covered with the cloth to create the surface. The wing has the borders 21 made with the metal only to shape like the aerofoil where the leading edge is 22 and the maximum bend occurs at the one-fourth of the chord length, this wing structure is rested on the fuselage design 27, the propeller is also made with the frame 25 and covered with the sheet also the stabilizers are also made of metal frame in order to reduce the weight of the plane, only the hinges are attached at the edges of the frame, control rods are attached to the frame of the control surfaces from the servo horn, here the magnetic repulsion system has two magnets 24 arrayed arrangement which is supported by the non-magnetic support 23 which carries the shaft 07 loads in the form of torque.

[0030] According to another exemplary embodiment, FIG. 6 refers to the magnetic repulsive system with two types of magnets arranged in the order to create opposite poles. There are two bearings to both the supports 35, one set of magnets are attached to the small wheel 37 and other set are attached to the big well 31. These magnets rotate the set of gears with a small gear 33 rotated by the big gear 34. As the power is transmitted from the larger gear to the smaller gear, the speed that is available at the smaller gear is relatively high. The smaller gear is meshed directly, which serves in transmitting power from the larger gear to the smaller gear. This moment is transferred to the shaft 32 which is further connected to the propeller.

[0031] Numerous advantages of the present disclosure may be apparent from the discussion above. In accordance with the present disclosure, a centicopter robot that can fly as well as move fast in the rough terrain. Using rotational energy generated from the magnet repulsion forces to propel the plane.

[0032] The generating system is compatible with the plane. The design of the light weight plain decreases the power usage.

[0033] It will readily be apparent that numerous modifications and alterations can be made to the processes described in the foregoing examples without departing from the principles underlying the invention, and all such modifications and alterations are intended to be embraced by this application.

Documents

Application Documents

# Name Date
1 202141003723-STATEMENT OF UNDERTAKING (FORM 3) [28-01-2021(online)].pdf 2021-01-28
2 202141003723-POWER OF AUTHORITY [28-01-2021(online)].pdf 2021-01-28
3 202141003723-FORM 1 [28-01-2021(online)].pdf 2021-01-28
4 202141003723-DRAWINGS [28-01-2021(online)].pdf 2021-01-28
5 202141003723-DECLARATION OF INVENTORSHIP (FORM 5) [28-01-2021(online)].pdf 2021-01-28
6 202141003723-COMPLETE SPECIFICATION [28-01-2021(online)].pdf 2021-01-28
7 202141003723-Correspondence, Form-1, Form-3, Form-5 And POA_08-02-2021.pdf 2021-02-08
8 202141003723-FORM 18 [02-11-2022(online)].pdf 2022-11-02
9 202141003723-FER.pdf 2023-01-11
10 202141003723-OTHERS [11-07-2023(online)].pdf 2023-07-11
11 202141003723-FORM-26 [11-07-2023(online)].pdf 2023-07-11
12 202141003723-FORM 3 [11-07-2023(online)].pdf 2023-07-11
13 202141003723-FER_SER_REPLY [11-07-2023(online)].pdf 2023-07-11
14 202141003723-ENDORSEMENT BY INVENTORS [11-07-2023(online)].pdf 2023-07-11
15 202141003723-DRAWING [11-07-2023(online)].pdf 2023-07-11
16 202141003723-COMPLETE SPECIFICATION [11-07-2023(online)].pdf 2023-07-11
17 202141003723-CLAIMS [11-07-2023(online)].pdf 2023-07-11
18 202141003723-ABSTRACT [11-07-2023(online)].pdf 2023-07-11
19 202141003723-FORM-8 [07-03-2024(online)].pdf 2024-03-07
20 202141003723-US(14)-HearingNotice-(HearingDate-01-09-2025).pdf 2025-08-18
21 202141003723-FORM-26 [30-08-2025(online)].pdf 2025-08-30
22 202141003723-Correspondence to notify the Controller [30-08-2025(online)].pdf 2025-08-30
23 202141003723-Written submissions and relevant documents [12-09-2025(online)].pdf 2025-09-12
24 202141003723-Proof of Right [12-09-2025(online)].pdf 2025-09-12
25 202141003723-FORM 3 [12-09-2025(online)].pdf 2025-09-12
26 202141003723-EVIDENCE FOR REGISTRATION UNDER SSI [12-09-2025(online)].pdf 2025-09-12
27 202141003723-EDUCATIONAL INSTITUTION(S) [12-09-2025(online)].pdf 2025-09-12
28 202141003723-RELEVANT DOCUMENTS [29-09-2025(online)].pdf 2025-09-29
29 202141003723-FORM 13 [29-09-2025(online)].pdf 2025-09-29
30 202141003723-Proof of Right [30-09-2025(online)].pdf 2025-09-30

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