Field of the Invention
This invention relates to an intelligent device for producing propulsive force.
Background of the Invention
US20090183951A1: Disclosed herein are two separate processes that do not require a propellant and do not produce an equal and opposite reaction against any external form of matter in the Local Inertial Reference Frame and do not violate Newton's Laws in the Universal Reference Frame. The first process produces horizontal motion, relies on the earth's gravitational field as an external force, and has been successfully tested. The second process produces vertical motion and relies only on the aether. It has been successfully tested considering the effect of the earth's gravity. The two processes referenced above are examples of converting the rotary motion of a spinning rotor into unidirectional linear motion. Due to the law of conservation of angular momentum, the first process is normally considered not possible, but with the proper use of an external field (for example, gravity) and the phenomenon of precession, it becomes possible. A clear distinction is made between a simple rotor and a gyroscope which is a far more complex device.
US7900874B2: Disclosed herein are two separate processes that do not require a propellant and do not produce an equal and opposite reaction against any external form of matter in the Local Inertial Reference Frame and do not violate Newton's Laws in the Universal Reference Frame. The first process produces horizontal motion, relies on the earth's gravitational field as an external force, and has been successfully tested. The second process produces vertical motion and relies only on the aether. It has been successfully tested considering the effect of the earth's gravity. Due to the law of conservation of angular momentum, the first process is normally considered not possible, but with the proper use of an external field (for example, gravity) and the phenomenon of precession, it becomes possible. A clear distinction is made between a simple rotor and a gyroscope which is a far more complex device.
US20050109138A1: An inertial thrust drive (10) comprising a centrifugal thrust generator (12) that comprises a first motor (14); with a weighted arm (16) comprising a radial arm (18) and a weight (20); a platform (22), a second motor (24); the entire assembly mounted on a thrust mount (26). The motor (14) rotates the weighted arm (16) in a counterclockwise rotational direction (30) to generate unbalanced centrifugal forces in its plane of rotation. The centrifugal thrust generator (12) is supported by the platform (22). The platform (22) rotates the thrust generator (12) in a clockwise direction of rotation (32) opposite to the arm (16) rotational direction (30). Both, the first motor (14) and the second motor (24) rotate about a common central axis (34). To generate a directional propulsion force (36), the weighted arm (16) generates unbalanced centrifugal forces in its plane of rotation; and the platform (22) rotates the thrust generator (12) in the opposite direction to maintain the arm (16) pointing in the same direction. The synergy of superimposing the rotational energy of the platform (22) on the thrust generator (12) generates a directional propulsion force (36). The propulsion force (36) vector is useful as a source of thrust for propellant less propulsion.
US3653269A: Unidirectional thrust and consequent unidirectional motion are achieved by rotating thrust-producing units in a circular orbit. The thrust producing units involve weights or masses which are caused to accelerate in the direction of the orbital travel during all or a portion of the one-half of the orbital travel which is away from the direction of the desired thrust. The reaction to this acceleration occurs and manifests itself at an orbital location-i.e., away from the axis of rotation-and provides the unidirectional thrust. During the one-half of the orbital travel which is toward the direction of the desired thrust there either is no such acceleration or the reaction to such acceleration is directly transferred to the axis of rotation, and consequently in either case no reaction is manifested at an orbital location. Hence, there is no thrust in the direction opposite that desired.
None of the prior art indicates above either alone or in combination with one another disclose what the present invention has disclosed. Present invention is produces thrust without using any kind of liquid or solid propellant. It produces thrust by using electrical power only and the power-to-thrust ratio of the system is greater than that of the ion propulsion systems.
SUMMARY OF THE INVENTION
This summary is provided to introduce a selection of concepts, in a simplified format, that are further described in the detailed description of the invention.
This summary is neither intended to identify key or essential inventive concepts of the invention and nor is it intended for determining the scope of the invention.
To further clarify advantages and features of the present invention, a more particular description of the invention will be rendered by reference to specific embodiments thereof, which is illustrated in the appended drawings. It is appreciated that these drawings depict only typical embodiments of the invention and are therefore not to be considered limiting of its scope. The invention will be described and explained with additional specificity and detail with the accompanying drawings.
Fig. 1, shows a single rotor system in which 100a,100b, and 100c are permanent Magnets. The electric motor (103) rotates the shaft (102) which has a permanent magnet (101) connected to it. The magnet (101) is attracted to magnets 100a,100b, and 100c. The electric motor (103) rotates the shaft (102) and during the rotations, the magnet (101) gets attracted to the other three magnets 100a,100b, and 100c at three stages during this rotation of the rotor the angular momentum of the rotor (102) get transformed into linear momentum which moves the whole system (104) in one direction (105).
Fig. 2, shows a double-rotor system which is more stable than the single-rotor system shown in fig. 1. In fig. 2 the rotor (108) and (109) both are coupled with each other and both rotates at the same time. The rotor (108) rotates clockwise and the rotor (109) rotates counterclockwise. The current ion propulsion system which is being used in space crafts and satellites provides thrust by using gas as a propellant which after some time gets depleted and the thrust produced by the ion propulsion system is significantly small. The current invention produces thrust without using any kind of liquid or solid propellant. It produces thrust by using electrical power only and the power-to-thrust ratio of the system is greater than that of the ion propulsion systems.
BRIEF DESCRIPTION OF THE DRAWINGS
The illustrated embodiments of the subject matter will be understood by reference to the drawings, wherein like parts are designated by like numerals throughout. The following description is intended only by way of example, and simply illustrates certain selected embodiments of devices, systems, and methods that are consistent with the subject matter as claimed herein, wherein:
The device is a magnetic-based system that produces a uni-directional force in one direction without using any type of solid or liquid propellant.
Fig. 1, shows a single rotor system in which 100a,100b, and 100c are permanent Magnets. The electric motor (103) rotates the shaft (102) which has a permanent magnet (101) connected to it. The magnet (101) is attracted to magnets 100a,100b, and 100c. The electric motor (103) rotates the shaft (102) and during the rotations, the magnet (101) gets attracted to the other three magnets 100a,100b, and 100c at three stages during this rotation of the rotor the angular momentum of the rotor (102) get transformed into linear momentum which moves the whole system (104) in one direction (105).
Fig. 2, shows a double-rotor system which is more stable than the single-rotor system shown in fig. 1. In fig. 2 the rotor (108) and (109) both are coupled with each other and both rotates at the same time. The rotor (108) rotates clockwise and the rotor (109) rotates counterclockwise.
The figures depict embodiments of the present subject matter for the purposes of illustration only. A person skilled in the art will easily recognize from the following description that alternative embodiments of the structures and methods illustrated herein may be employed without departing from the principles of the disclosure described herein.
DETAILED DESCRIPTION OF THE INVENTION
The detailed description of various exemplary embodiments of the disclosure is described herein with reference to the accompanying drawings. It should be noted that the embodiments are described herein in such details as to clearly communicate the disclosure. However, the amount of details provided herein is not intended to limit the anticipated variations of embodiments; on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the scope of the present disclosure as defined by the appended claims.
It is also to be understood that various arrangements may be devised that, although not explicitly described or shown herein, embody the principles of the present disclosure. Moreover, all statements herein reciting principles, aspects, and embodiments of the present disclosure, as well as specific examples, are intended to encompass equivalents thereof.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments. As used herein, the singular forms “a",” “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises,” “comprising,” “includes” and/or “including,” when used herein, specify the presence of stated features, integers, steps, operations, elements and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components and/or groups thereof.
It should also be noted that in some alternative implementations, the functions/acts noted may occur out of the order noted in the figures. For example, two figures shown in succession may, in fact, be executed concurrently or may sometimes be executed in the reverse order, depending upon the functionality/acts involved.
In addition, the descriptions of "first", "second", “third”, and the like in the present invention are used for the purpose of description only, and are not to be construed as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" and "second" may include at least one of the features, either explicitly or implicitly.
Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which example embodiments belong. It will be further understood that terms, e.g., those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
These and other advantages of the present subject matter would be described in greater detail with reference to the following figures. It should be noted that the description merely illustrates the principles of the present subject matter. It will thus be appreciated that those skilled in the art will be able to devise various arrangements that, although not explicitly described herein, embody the principles of the present subject matter and is included within its scope.
Fig. 1, shows a single rotor system in which 100a,100b, and 100c are permanent magnets. The electric motor (103) rotates the shaft (102) which has a permanent magnet (101) connected to it. The magnet (101) is attracted to magnets 100a,100b, and 100c. The electric motor (103) rotates the shaft (102) and during the rotations, the magnet (101) gets attracted to the other three magnets 100a,100b, and 100c at three stages during this rotation of the rotor the angular momentum of the rotor (102) get transformed into linear momentum which moves the whole system (104) in one direction (105).
Fig. 2, shows a double-rotor system which is more stable than the single-rotor system shown in fig. 1. In fig. 2 the rotor (108) and (109) both are coupled with each other and both rotates at the same time. The rotor (108) rotates clockwise and the rotor (109) rotates counterclockwise. The current ion propulsion system which is being used in space crafts and satellites provides thrust by using gas as a propellant which after some time gets depleted and the thrust produced by the ion propulsion system is significantly small. The current invention produces thrust without using any kind of liquid or solid propellant. It produces thrust by using electrical power only and the power-to-thrust ratio of the system is greater than that of the ion propulsion systems.
Best Method of working:
• Unlike any other kind of propulsion system, the device did not need any type of propellant to Produce thrust.
• The device uses only electrical power to produce thrust.
• The overall weight of the device is very much less than compared to any other kind of propulsion system. The weight of the given system is 450 grams which are far less than any present ion propulsion engine. For example, the weight of the DS1’s ion engine is around 490 kilograms.

We Claims:

1. Intelligent device for producing a propulsive force system is comprised of the magnet (101), shaft (102), electric motor (103), the whole system (104), one direction (105), the rotor (108), and (109).
2. The system as claimed in claim 1, wherein which is consist of the electric motor (103) rotates the shaft (102) which has a permanent magnet (101) connected to it.
3. The system as claimed in claim 1, wherein the electric motor (103) rotates the shaft (102) and during the rotations, the magnet (101) gets attracted to the other three magnets 100a,100b, and 100c at three stages during this rotation of the rotor the angular momentum of the rotor (102) get transformed into linear momentum which moves the whole system (104) in one direction (105).
4. The system as claimed in claim 1, wherein which is consist of the rotor (108) and (109) both are coupled with each other and rotate at the same time.
5. The system as claimed in claim 1, wherein consists of a rotor (108) rotating clockwise and a rotor (109) rotating counterclockwise.