Patent Application
20160004250
The present invention relates generally to satellites or unmanned aircrafts, and more particularly, to magnetic satellites or unmanned aircrafts.
The present invention describes a magnetic satellite or unmanned aircraft, which carriers electric charges and cruises according to earth's magnetic fields. Traditional satellites only follow earth's gravitational fields, and do not respond to earth's magnetic fields.
The following presents a simplified summary in order to provide a basic understanding of one or more aspects of the invention. This summary is not an extensive overview of the invention, and is neither intended to identify key or critical elements of the invention, nor to delineate the scope thereof Rather, the primary purpose of the summary is to present some concepts of the invention in a simplified form as a prelude to the more detailed description that is presented later.
The present invention provides a magnetic satellite or unmanned aircraft which carriers electric charges to react with earth's magnetic fields and generate a centripetal force. The motion of the satellite follows this electromagnetic field generated centripetal force, instead of the gravitational force which guides a traditional satellite. S the result of this magnetic force, this new satellite may fly man times faster than a traditional gravitational satellite. The speed of the magnetic satellite can be adjusted by the electric charges. The speed of a traditional gravitational satellite is much lower, can not be adjusted, and is determined only by the altitude of the satellite.
To the accomplishment of the foregoing and related ends, the invention comprises the features hereinafter fully described and particularly pointed out in the claims. The following description and the annexed drawings set forth in detail certain illustrative aspects and implementations of the invention. These are indicative, however, of but a few of the various ways in which the principles of the invention may be employed. Other objects, advantages and novel features of the invention will become apparent from the following detailed description of the invention when considered in conjunction with the drawings.
The present invention will now be described with respect to the accompanying drawings in which like numbered elements represent like parts. The figures provided herewith and the accompanying description of the figures are merely provided for illustrative purposes. One of ordinary skill in the art should realize, based on the instant description, other implementations and methods for fabricating the devices and structures illustrated in the figures and in the following description.
When electric charges move in a magnetic field, according the electromagnetic theories, a magnetic force is generated. The direction of the magnetic force is perpendicular to both the magnetic field and the moving direction of the electric charges. The magnitude of the magnetic force is proportional to the speed of the moving charges and the magnetic field strength, as well as the amount of electric charges.
A satellite which carries electric charges can fly according to the magnetic force generated by the reaction of the electric field from the electric charges and earth's magnetic fields. By following this magnetic force, a magnetic satellite can fly many times faster than a traditional gravitational satellite, up to the speed of light. A traditional gravitational satellite moves much slower, and can not change the speed without changing the altitude. The speed of a magnetic satellite can be adjusted by changing the electric charges carried by the satellite.
The control center, or the main body of the satellite, is sustained by an array of electric charge carrying devices. These charge carrying devices react with earth's magnetic fields and supply the centripetal forces necessary to guide the magnetic satellite.
Electric charges can leak if they are in contact with air, water, moisture, or other substances. In order to prevent the charges from leaking, a layer of insulator surrounds the electric charges, which are typically stored in metal surfaces.
The electric field from the electric charges can not go through metals. By adjusting the electric fields, the magnetic force can be adjusted. In order to adjust the amount of electric charges, an outside layer is programmed to provide different sizes of metal surfaces, as these metal surfaces can block the electric fields from the charges.
Although the invention has been shown and described with respect to a certain aspect or various aspects, it is obvious that equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. In particular regard to the various functions performed by the above described components (assemblies, devices, circuits, etc.), the terms (including a reference to a “means”) used to describe such components are intended to correspond, unless otherwise indicated, to any component which performs the specified function of the described component (i.e., that is functionally equivalent), even though not structurally equivalent to the disclosed structure which performs the function in the herein illustrated exemplary embodiments of the invention. In addition, while a particular feature of the invention may have been disclosed with respect to only one of several aspects of the invention, such feature may be combined with one or more other features of the other aspects as may be desired and advantageous for any given or particular application. Furthermore, to the extent that the term “includes” is used in either the detailed description or the claims, such term is intended to be inclusive in a manner similar to the term “comprising.”
