Patent Publication Number: US-2021194391-A1

Title: Power generating apparatus

Description:
BACKGROUND OF THE INVENTION 
     Field of the Invention 
     The present invention relates to a power generating apparatus for obtaining a force to repulse the gravitational force. 
     Description of the Related Art 
     Conventionally, there have been proposed a number of such apparatuses as flying bodies loaded with an engine for propelling themselves vertically or horizontally in a 3-D space, rockets, which injects the fuel downward for obtaining a propelling force (motive power), and submarines, which utilize rotation of a screw as a propelling force for moving themselves in water. Such propelling forces provide motive power for moving mobile bodies, and they have been obtained by using gasoline, a solid fuel, or the like. 
     In addition, there has been another proposal, in which, within a magnetic field, supplied hydrogen is caused to emit electrons at one gas diffusion electrode (the fuel electrode) to produce hydrogen ions, which are then moved to the other gas diffusion electrode (the air electrode) in sea water, being an electrolytic solution, to generate electric energy, and an electric current is caused to flow between both electrodes to thereby move the sea water on the basis of Fleming&#39;s left-hand rule for obtaining a propelling force through the utilization of a reaction force of the sea water (refer to second to fourth pages and FIG. 1 in Patent Document 1, for example). 
     Patent Document 1: Japanese Unexamined Patent Application Publication No. 1998-297589 
     However, any of the above-mentioned conventional technologies for obtaining a propelling force consumes a large quantity of energy, and cannot always be said to be preferable from the viewpoint of ecology on a global scale, and the like. In addition, fossil fuels are running out year by year. 
     In addition, the apparatus as disclosed in Patent Document 1 have disadvantages that it requires such components as chambers for accommodating gases, such as hydrogen gas, thereby the scale of the apparatus being increased, and hydrogen gas must be handled with great care due to its combustibility, and the like. 
     The present invention has been made in view of the above-mentioned problems that are associated with the conventional technologies, and is intended to provide a power generating apparatus for obtaining a force to repulse the gravitational force. 
     SUMMARY OF THE INVENTION 
     In order to achieve the above purpose, the power generating apparatus of the present invention includes:
         a magnetic field generation part, generating a magnetic field, and   an electromagnetic wave irradiation part, irradiating an electromagnetic wave on a gravitational wave within the magnetic field, having been generated.       

     Herein, it is preferable that the electromagnetic wave irradiation part irradiate the electromagnetic wave in parallel or substantially in parallel with the gravitational wave at the center or in a vicinity of the center of the magnetic field, having been generated by the magnetic field generation part. 
     In addition, the magnetic field generation part can be configured such that it generates a magnetic field when an electric current is caused to flow through a coil, being formed by winding an electric wire around a non-magnetic material cylindrical member, or can be configured such that it is formed of a cylindrical magnet. 
     Further, the magnetic field generation part can be configured such that it causes an electric current to generate a magnetic field after the coil having been brought into a superconducting state. 
     With the power generating apparatus according to the present invention, a force repulsive to the gravitational force can be obtained. In addition, it is capable of realizing a mobile body that is moved with a force repulsive to the gravitational force. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         FIG. 1  is a configuration drawing schematically exemplifying a power generating apparatus; 
         FIG. 2  is a configuration drawing schematically exemplifying a power part of the power generating apparatus; 
         FIG. 3  is a configuration drawing exemplifying a mobile body, being equipped with the power generating apparatus; 
         FIG. 4  is a configuration drawing exemplifying a mobile body in another embodiment; 
         FIG. 5  is a configuration drawing exemplifying a balance, having been used for measurement; 
         FIG. 6  is an explanation drawing exemplifying a measuring instrument with an electromagnetic coil; 
         FIG. 7  is an explanation diagram exemplifying a configuration of a part of an electrical system; 
         FIG. 8  is an explanation diagram exemplifying a configuration of a part of an electrical system; 
         FIG. 9  is an explanation drawing exemplifying a measuring instrument with magnets; 
         FIG. 10  is an explanation drawing exemplifying another measuring instrument with magnets; 
         FIG. 11  is an explanation drawing for a hypothesis; 
         FIG. 12  is a configuration drawing schematically exemplifying a variant of the power generating apparatus; and 
         FIG. 13  is a configuration drawing schematically exemplifying another variant of the power generating apparatus. 
     
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     Hereinbelow, embodiments representing the present invention will be explained with reference to the drawings. However, the embodiments, being explained hereinafter, are one example, and the present invention is not limited to these embodiments. 
     &lt;Setting of Hypotheses&gt; 
     At present, since the real identity of gravitational wave itself has not been clarified, the present invention sets the following two hypotheses to configure a power generating apparatus  10  for repelling the universal gravitation. In other words, the hypothesis 1 assumes that “the gravitational wave is an electromagnetic wave”, and the hypothesis 2 assumes that “the gravitational wave is based on the structure of “proton” and “neutron”. 
       FIG. 11  is an explanation drawing for these two hypotheses. The structure of a “proton” or a “neutron”, constituting an atomic nucleus, is as shown in  FIG. 11 . In other words, at the center of a “proton” or a “neutron”, there is a spot where an electric current (a) is heavily oscillated vertically. In accordance with the oscillation of the electric current (a), a magnetic field (b) is generated outside of the electric current (a). Actually, with the electric current (a) being moved, a magnetic field (b) is generated, the magnetic field (b) regenerating an electric current (a), and further, a magnetic field (b) being generated to regenerate an electric current (a). In this way, in the inside of a “proton” or a “neutron”, an electric current is repetitively produced. 
     Fundamentally, if the space is a free space, existence of an electric current (a) generates a magnetic field (b), and with such a thing being repeated, an electric field (d), a magnetic field (c), an electric field (e), and a magnetic field (f) are generated, thereby an electromagnetic wave being delivered, however, the inside of a “proton” or a “neutron” provides an extremely narrow space, compared to the free space, and thus only the generation of an electric current (a) and a magnetic field (b) will be repeated. 
     In addition, around the magnetic field (b), a number of electric fields (d) are generated, but the electric fields (d) repulse one another, thereby the intensity of the resulting electric field (d) is extremely low. Accordingly, the electromagnetic wave (g), which is delivered as a combined wave of the electric field (d), and the magnetic, field (c), the electric field (e), and the magnetic field (f), following the electric field (d), has an extremely low intensity. Such electromagnetic wave (g) acts as a “gravitational wave”. 
     If a “proton” or a “neutron” in such a state is subjected to an electromagnetic wave (h) from the outside, the “proton” or the “neutron” will be excited to thereby obtain a longer life. Whether the region of the “proton” or the “neutron” covers only the electric current (a) and the magnetic field (b), or it also covers the electric field (d) and the magnetic field (c), or further the electric field (e) and the magnetic field (f) is unclear with the above-mentioned hypotheses. 
     &lt;Configuration of Power Generating Apparatus  10 &gt; 
       FIG. 1  is a configuration drawing for the power generating apparatus  10 . The power generating apparatus  10  has a columnar magnet  20 , an electromagnetic wave irradiation device  30 , an electromagnetic wave irradiation part  31 , an electromagnetic wave irradiation device power supply  40  and controller  50 , and an electromagnetic wave irradiation device wiring  41 . In the present embodiment, the columnar magnet  20  corresponds to one example of the “magnetic field generation part” of the present invention, the electromagnetic wave irradiation part  31  corresponds to one example of the “electromagnetic wave irradiation part” of the present invention. 
     The columnar magnet  20  is, for example, a cylindrical magnet, being hollow as a whole, with the upper half providing an N-pole (or an S-pole), while the lower half an S-pole (or an N-pole). In addition, at a middle location in a vertical direction of a hollow part of the columnar magnet  20 , the electromagnetic wave irradiation part  31  of the electromagnetic wave irradiation device  30  is disposed. 
     The electromagnetic wave irradiation device  30  is connected to the electromagnetic wave irradiation device power supply  40  and controller  50  by means of the electromagnetic wave irradiation device wiring  41 . In addition, from the electromagnetic wave irradiation part  31 , an electromagnetic wave is irradiated in parallel or substantially in parallel with a magnetic field, being generated by the columnar magnet  20 , and the electromagnetic wave irradiation part  31  is subjected to a gravitational wave. In  FIG. 1 , the generation of a magnetic field using the columnar magnet  20  as one example is explained, however, if the magnetic field generated is in parallel or substantially parallel with the gravitational wave, either of the N magnetic field and the S magnetic field may be used. 
     Electromagnetic waves to be irradiated from the electromagnetic wave irradiation device  30  include electric waves (electromagnetic waves for communications, observation, and the like), far-infrared rays, visible light rays, ultraviolet rays, X-rays, gamma rays, and various laser rays. In the later-described Example, an ultraviolet ray is used as one example of electromagnetic wave. 
     &lt;Operating Principle of Power Generating Apparatus  10 &gt; 
     The hypothesis  1 , having been set above, assumes that the “gravitational wave” is an electromagnetic wave. When an electromagnetic wave, being, irradiated from the electromagnetic wave irradiation part  31  as an artificially prepared wave, is collided with a gravitational wave (an electromagnetic wave) within the magnetic field of either the N-pole or the S-pole in the columnar magnet  20 , the respective electromagnetic waves are deformed into the same shape of wave by the magnetic field. 
     Herein, the statement of “are deformed into the same shape of wave” means that both of the gravitational wave and the electromagnetic wave, which has been irradiated from the electromagnetic wave irradiation part  31 , are transformed into the same oscillation mode of wave. In the state in which both the gravitational wave and the electromagnetic wave have been transformed into the same oscillation mode of wave, a repulsive force is generated between both waves. Herein, the action of transformation supports the hypothesis of “the gravitational wave is an electromagnetic force”, which is given above under the heading of “Setting of hypotheses”. Further, with an electromagnetic wave, there exist the N magnetic field and the S magnetic field in an alternative manner. 
     From these, it can be considered that both of the gravitational wave and the electromagnetic wave, which has been irradiated from the electromagnetic wave irradiation part  31 , are of the same oscillation mode, although they are different from each other in oscillation frequency. When those electromagnetic waves having the same oscillation mode are each passed through the S-pole in  FIG. 1 , the S waveform of the electromagnetic wave is reduced, being subjected to a repulsive force of the S magnetic field of the magnet. The N waveform of the electromagnetic wave is enlarged, being provided with an attractive force of the S magnetic field of the magnet. With both the enlarged N waveform of the gravitational wave and that of the electromagnetic wave being collided with each other, a repulsive force is produced. In case where there is given no magnetic field of a magnet, since the S waveform and the N waveform of an electromagnetic wave are of the same oscillation mode, either repulsion or attraction will not be caused. 
     Embodiment 1 
       FIG. 2  is a configuration drawing of a power part  11  as another form of power part in the power generating apparatus  10 . In the power part  11 , a coil is wound around the outer periphery of a non-magnetic material cylinder  21 , being made of a non-magnetic material, to thereby provide a superconducting coil unit  22 . Both ends of the coil are connected to a superconducting coil power supply  23  by means of a superconducting coil wiring  24 . The coil is brought into a superconducting state with a superconducting coil cooling device  25 . 
     The electromagnetic wave irradiation device power supply  40  and controller  50  is connected to the electromagnetic wave irradiation device  30  by means of an electromagnetic wave irradiation device wiring  41 . The electromagnetic wave irradiation device  30  is disposed at an intermediate location in the vertical direction in the inside of the non-magnetic material cylinder  21  in order to place it in the central portion of the magnetic field. The present embodiment is characterized in that, in order to provide a stronger magnet, the “magnetic field generation part” of the present invention is constituted by the superconducting coil unit  22 . 
       FIG. 3  is a configuration drawing of a mobile body  100 , being equipped with the power part  11  (i.e., power generating apparatus) shown in  FIG. 2 . The mobile body  100  shown in  FIG. 3  is provided with the power part  11  in the central portion of a dome-shaped airframe  101 . In the lower portion of the airframe  101 , there is provided a machine room  102 . In the machine room  102 , fuel, a power supply, an airframe controlling part, various types of controlling devices, and the like, are provided, for example. Further, in the upper portion of the machine room  102 , there is provided a crew residence space  103 . 
     The airframe  101  is provided with three arms  104 , which are arranged at equal angles in a plain view. In the respective arms  104 , an airframe posture controlling part  105  is provided. The airframe posture controlling part  105  is comprised of, for example, a small-sized propulsion device, being capable of controlling the posture, a wheel, and the like. 
     The power part  11  (i.e., the power generating apparatus) generates power high enough to repulse the gravitational wave to lift the airframe  101 . When the electromagnetic wave irradiation device in the power part  11  (see  FIG. 2 ) is oriented to the top of the airframe  101 , the lower side of the airframe  101  is provided as a repulsing side of the airframe  101  to allow it to be moved upward. Herein, the gravitational wave not always arrives at from a definite direction, and thus the mobile body  100  is configured such that, by controlling the power part  11  and the airframe posture controlling part  105 , the power can be generated in a desired direction to move the airframe  101  in that direction. 
     &lt;&lt;Operation of Mobile Body  100 &gt;&gt; 
     With the superconducting coil cooling device  25 , being provided in the machine room  102  (see  FIG. 2 , the superconducting coil unit  22  (see  FIG. 2 ) is cooled. Thereafter, by energizing the superconducting coil unit  22 , a powerful magnetic field is obtained. With the electromagnetic wave irradiation device power supply  40  and controller  50  (see  FIG. 2 ), an electromagnetic wave is irradiated from the electromagnetic wave irradiation device  30  (see  FIG. 2 ). Thereby, the power part  11  functions to generate power. Through the operation of the airframe posture controlling part  105  and the electromagnetic wave irradiation device power supply  40  and controller  50  (see  FIG. 2 ), the airframe  101  is lifted and propelled. 
     Embodiment 2 
       FIG. 4  is a configuration drawing of a mobile body  110  in Embodiment  2 . With the mobile body  110  shown in  FIG. 4 , there is disposed another form of power part in a machine room  112  in the lower portion of a dome-shaped airframe  111 . In the above-described Embodiment 1, power is generated only by the power part  11 , however, the present Embodiment 2 is characterized in that, as power part, there are provided amain power part  12  and a sub-power part  13 . In  FIG. 4 , for example, four sub-power parts  13  are provided, a single superconducting coil  26  being provided in correspondence with these four sub-power parts  13 . 
     With this form of power part, a plurality of sub-power parts  13  are provided, the magnetic field being generated by the superconducting coil  26 , whereby more powerful motive power can be generated. Moreover, a single superconducting coil  26  is provided for a plurality of sub-power parts  13 , thereby the total weight being reduced. Needless to say, the mobile body  110  may be configured such that each sub-power part  13  is provided with a superconducting coil  26 . 
     Herein, the gravitational wave arrives at not only from a single direction, but also from every direction, and therefore, on the earth, it is felt that the gravitational wave arrives at from one&#39;s feet, however, actually, a composite of the “gravitational waves”, having arrived at from every direction, is felt as the force of gravity in the vertical direction. In other words, if the airframe  111  is on the earth, it is subjected to the gravitational wave from every direction thereunder. Then, by receiving the gravitational wave from every direction under the airframe  111  with a wide area to irradiate an electromagnetic wave over a wide area, higher power can be obtained. The airframe  111  can be configured such that the direction of propulsion can be controlled through the control of the main power part  12  and the sub-power parts  13 . 
     EXAMPLE 
     &lt;Details of Experiment and Measurement&gt; 
     Next, the details of the experiment and measurement that have provided a ground for the present invention will be explained. 
     &lt;&lt;Structure of Balance  200 , Which Was Used for Measurement&gt;&gt; 
       FIG. 5  is a configuration drawing of a balance  200 , which was used for measurement. With the balance  200 , a post  202  is provided to stand on a base  201 , and at the upper end of the post  202 , a scale plate  203 , being graduated, is fixed. 
     In addition, in a portion above the middle of the post  202 , there is provided a balance arm receiving blade  205 , serving as a fulcrum for the right and left weights of a balance arm  204 . In this way, the balance arm  204  is formed symmetric. In the central portion in a longitudinal direction of the balance arm  204 , there are provided a supporting plate  206 , being made of metal, for supporting the balance arm receiving blade  205 , and a pointer  207 . The balance arm  204  is formed of a square timber. 
     At one end of the balance arm  204  (the left end in  FIG. 5 ), there is provided a receiving plate  208  for a supporting blade  210   a , being given in a measuring instrument suspension part  210 , being made of metal. In addition, at the other end of the balance arm  204  (the right end in  FIG. 5 ), there is provided a receiving sliding plate  209  for a supporting blade  211   a , being given in a weight suspension part  211 , being made of metal. The measuring instrument suspension part  210  is provided at one end of the balance arm  204 , while the weight suspension part  211  is provided at the other end of the balance arm  204 . 
     In the measuring instrument suspension part  210 , the supporting blade  210   a  therefor is provided, and also in the weight suspension part  211 , the supporting blade  211   a  therefor is provided. The supporting blade  210   a  for the measuring instrument suspension part  210  is set on the receiving plate  208 . On the other hand, the supporting blade  211   a  for the weight suspension part  211  is set on the receiving sliding plate  209 . Further, the edge of the supporting blade  210   a  for the measuring instrument suspension part  210 , and that of the supporting blade  211   a  for the weight suspension part  211  serve as a fulcrum for the measuring instrument suspension part  210  and the weight suspension part  211 , respectively. 
     The position of the measuring instrument suspension part  210  is fixed. The weight suspension part  211  has a structure, allowing it to be moved on a receiving sliding plate  209 , thus being configured so as to allow adjustment of the balance with the weight of a measuring instrument. With the balance arm  204 , there are marked graduations by dividing the length, ranging from the central point thereof to the location where the supporting blade  210   a  for the measuring instrument suspension part  210  is fixed, into ten equal parts, for example. The graduations serve to roughly know the loss in weight of a coin, the weight thereof being previously known, that will be produced as a result of repulsion against the gravitational force by the coin at the time of measurement. 
     Further, in the lower portion of the balance arm  204  at one end thereof, there is provided a hanging metal fitting  212  for suspending a measuring instrument therefrom, while, in the lower.portion of the balance arm  204  at the other end thereof, there is provided a hanging metal fitting  213  for suspending a weight therefrom. The balance  200 , which was used, was specifically 595 mm wide and 660 mm high. 
     &lt;&lt;Operation of Balance  200 &gt;&gt; 
     First, the measuring instrument is suspended from the hanging metal fitting  212 . Then, the weight is suspended from the hanging metal fitting  213 . The weight suspension part  211  is moved to strike a balance with the measuring instrument. Balancing is performed in such a way that the pointer  207  is stopped at the center of the graduations of the scale plate  203 . Herein, for easier balancing, a coin is placed on the balance arm  204  before sliding the weight suspension part  211  in the extending direction of the balance arm  204 . At this time, if the coin is placed at the center of the graduations, it is convenient to obtain a rough estimate of the “loss in weight” that will be caused at the time of measurement. Once a balance has been struck, the measuring instrument is energized for making a measurement operation. 
     &lt;&lt;Measuring Instrument  300  with Electromagnetic Coil&gt;&gt; 
       FIG. 6  is an explanation drawing for a measuring instrument  300  with an electromagnetic coil. The measuring instrument  300  is provided with a suspending ring  301  at the upper end thereof for suspending it from the hanging metal fitting  212  for the measuring instrument (see  FIG. 5 ), and from the suspending ring  301 , an electromagnet suspending plate  302  is suspended by means of three suspending strings  303 . From the electromagnet suspending plate  302 , an electromagnetic coil  310  is suspended with the use of three suspending strings  304 . Herein, the electromagnetic coil  310  is disposed substantially horizontally such that the axis thereof is positioned vertically. 
     The electromagnetic coil  310  is formed by winding an electric wire around a flanged cylinder  311 , being made of a non-magnetic material, by a desired number of turns. Both ends of the electromagnetic coil  310  are connected to an electromagnetic coil power supply  312  through an electromagnetic coil wiring  313 . 
     The electromagnetic wave irradiation device  30  is suspended from an electromagnetic wave irradiation device suspending plate  306  by means of three suspending strings  305 . At the center of the electromagnetic wave irradiation device suspending plate  306 , a position adjusting screw  307  having a prescribed length (60 mm) is provided to stand. The position adjusting screw  307  is passed through the center of the electromagnet suspending plate  302 , being screwed with a position adjusting nut  308 , being provided at the center of the same. 
     By adjusting the tightening position of the position adjusting nut  308 , the positional relationship in a vertical direction between the electromagnetic coil  310  and the electromagnetic wave irradiation device  30  can be adjusted. In addition, the electromagnetic wave irradiation device  30  is connected to the electromagnetic wave irradiation device power supply  40  and controller  50  by the electromagnetic wave irradiation device wiring  41 , whereby the intensity, and the like, of the electromagnetic wave, being irradiated from the electromagnetic wave irradiation device  30 , can be operation-controlled. 
     Next, the main components of the measuring instrument  300  will be explained in detail. In  FIG. 6 , the flanged cylinder  311 , being made of a non-magnetic material, is manufactured specifically from a plywood of 3 mm in thickness, the cylinder inside diameter being 51 mm, and the winding width being 60 mm. The electromagnetic coil  310  is formed by winding an enameled electric wire of 0.8 mm in diameter around the flanged cylinder  311 , being made of a non-magnetic material, by 1300 turns. 
     The electromagnetic coil  310  has a winding width of 60 mm, and thus the central portion of the magnetic field is provided at a location 30 mm above the lower end of the flanged cylinder  311 , made of a non-magnetic material, where the electromagnetic wave irradiation device  30  is disposed. In addition, the electromagnetic coil wiring  313  is an electric wire, being prepared by peeling off a coating of an IV electric wire having a thickness of 0.5 sq, and annealing it. Herein, the “sq” is an index for indicating the thickness of a wire, which is defined by JIS. 
     The electromagnetic wave irradiation device  30  is specifically a 32-lamp type black light, emitting ultraviolet light. This 32-lamp type black light is operated with three size-D batteries, being connected in series. By turning on or off a switch, being provided for the electromagnetic wave irradiation device power supply  40  and controller  50 , the 32-lamp type black light is lighted or extinguished. 
       FIG. 7  and  FIG. 8  are diagrams showing a part of the electrical system.  FIG. 7  shows the electrical connection between the electromagnetic coil power supply  312  and the electromagnetic coil  310 . In  FIG. 7 , a transformer T transforms a voltage of 100V AC into a voltage of 48V AC. On the secondary side of the transformer T, a resistor R having a resistance of 1 ohm is connected in series, and a capacitor C 1  is connected in parallel. The capacitor C 1  is composed by connecting  30  capacitors having a capacitance of 470 μF in parallel with one another. 
     To the right end of the resister R, a switch S is connected. To the switch S, one end of the electromagnetic coil  310  is connected through an ammeter A. The other end of the electromagnetic coil  310  is connected to the secondary side of the transformer T. In addition, to the electromagnetic coil  310 , a capacitor C 2  is connected in parallel, and a voltmeter V is connected in parallel. Through the on-off operation of the switch S, whether or not an electric current is to be caused to flow through the electromagnetic coil  310  can be selected. As one example, when a DC voltage of 48.5 V was applied, an electric current of 3.3 A was measured. 
       FIG. 8  is a diagram showing the electrical connection between the electromagnetic wave irradiation device power supply  40  and controller  50  and the electromagnetic wave irradiation device  30 . The electromagnetic wave irradiation device power supply  40  and controller  50 , and the electromagnetic wave irradiation device  30  are mutually connected by the electromagnetic wave irradiation device wiring  41 . As the electromagnetic wave irradiation device power wiring  41 , an electric wire with very small diameter for communications is used. The controller  50  is provided with a switch S. By operating this switch S, the controller  50  can control supply of an electric current from the electromagnetic wave irradiation device power supply  40 , which is a DC power supply. 
     In addition, the electromagnetic wave irradiation device  30  has aplurality of LEDs (L 1 , L 2 , L 3 , and . . . ), irradiating ultraviolet light, as the electromagnetic wave irradiation part  31 , and alight emitting diode controlling part  32  for lighting control of these diodes. When the switch S is turned on, the light emitting diode controlling part  32  lights all the LEDs (L 1 , L 2 , L 3 , and . . . ) by means of its LED driving function. As a result of this, ultraviolet light is irradiated as an electromagnetic wave in parallel or substantially in parallel with the gravitational wave. 
     &lt;&lt;Measuring Instruments  300 A and  300 B with Magnets&gt;&gt; 
       FIG. 9  and  FIG. 10  are explanation drawings of measuring instruments  300 A and  300 B with magnets, respectively. The measuring instrument  300 A in  FIG. 9  is provided with a suspending ring  301  at the upper end thereof for suspending it from the hanging metal fitting  212  of the balance  200  (see  FIG. 5 ), and from the suspending ring  301 , a magnet suspending plate  302  is suspended by means of three suspending strings  303 . From the magnet suspending plate  302 , two ring-shaped magnets  321  and  322  are suspended with the use of three suspending strings  304 . Herein, the two ring-shaped magnets  321  and  322  are disposed one upon another substantially horizontally such that the respective axes thereof are positioned vertically. 
     In addition, as with the measuring instrument  300  shown in  FIG. 6 , the electromagnetic wave irradiation device  30  is suspended from an electromagnetic wave irradiation device suspending plate  306  with the use of three suspending strings  305 : At the center of the electromagnetic wave irradiation device suspending plate  306 , a position adjusting screw  307  having a prescribed length (60 mm) is provided to stand. The position adjusting screw  307  is passed through the center of the magnet suspending plate  302 , being screwed with a position adjusting nut  308 , being provided at the center of the same. 
     By adjusting the tightening position of the position adjusting nut  308 , the positional relationship in a vertical direction between the two magnets  321  and  322  and the electromagnetic wave irradiation device  30  can be adjusted. The two magnets  321  and  322  are arranged in such a way that there are provided “an N-pole, an S-pole, an N-pole, and an S-pole” from the top. The magnets  321  and  322  can be configured simply by superposing two ring-shaped magnets one upon another. 
     The measuring instrument  300  A shown in  FIG. 9  and the measuring instrument  30 . 0  B shown in  FIG. 10  differ from each other only in that the former uses two magnets  321  and  322 , while the latter using four ring-shaped magnets  321 ,  322 ,  323 , and  324 , and except for the number of magnets used, they have the same configuration. In the configuration shown in  FIG. 10 , the four magnets  321 ,  322 ,  323 , and  324  are arranged in such a way that there are provided “an N-pole, an S-pole, an N-pole, an S-pole, an N-pole, an S-pole, an N-pole, and an S-pole” from the top. Also in this case, the magnets  321 ,  322 ,  323 , and  324  can be configured simply by superposing four ring-shaped magnets one upon another. 
     Next, the main components of the measuring instruments  300 A and  300 B will be explained in detail. The magnets  321  and  322  are formed of two ring-shaped magnets. The specific dimensions of each magnet are 90 mm in outside diameter, 50 mm in inside diameter, and 16 mm in thickness. Likewise, the magnets  323  and  324  are ring-shaped magnets, and the specific dimensions of each magnet are 90 mm in outside diameter, 50 mm in inside diameter, and 16 mm in thickness. 
     The electromagnetic wave irradiation device  30  is the same device as described above, using a 32-lamp type black light to irradiate ultraviolet light. The electromagnetic wave irradiation device power supply  40  and controller  50  shown in  FIG. 9  and  FIG. 10  is also the same as described above, being provided with three size-D batteries for operating the 32-lamp type black light, and a switch. According to the on-off control of this switch, the on-off operation of electromagnetic wave irradiation from the electromagnetic wave irradiation device is performed. In addition, the electromagnetic wave irradiation device wiring  41  is formed of an electric wire with very small diameter for communications. 
     &lt;Points of Attention That Was Paid in Making Measurement&gt; 
     Prior to describing the setup for measurement and the steps for measurement operation using the measuring instruments  300 ,  300 A, and  300 B (hereinafter, to be abbreviated to the “measuring instrument  300 , and the like”), the points of attention that was paid in performing a measurement will be described. In performing a measurement, regardless of whether the measuring instrument  300  with the electromagnetic coil  310  shown in  FIG. 6 , the measuring instruments  300 A with the magnets  321  and  322  shown in  FIG. 9  (hereinafter, the magnets  321  and  322  to be abbreviated to “the magnet  321 , and the like”), or the measuring instruments  300 B with the magnets  321 ,  322 ,  323 , and  324  shown in  FIG. 10  (hereinafter, the magnets  321 ,  322 ,  323 , and  324  to be abbreviated to “the magnet  321 , and the like”) was used, the measurement was performed, attention having been paid to the following points. 
     Point of attention 1: Since the influence of the terrestrial magnetism is unavoidable except in a special room, when setting the electromagnetic coil  310 , or the magnet  321 , and the like, being used in the measuring instrument  300 , or the like, the “N-pole” must be placed on the upper side in the northern hemisphere. Contrarily, on the southern hemisphere, the “S-pole” must be placed on the upper side. 
     Point of attention 2: If, in the measurement place, there is a piece of equipment that may generate a magnetic field, the measuring instrument must be separated away therefrom by a distance of as 3 to 4 m. This is because the measurement is affected by an attractive force or repulsive force, having been produced by the magnetic field of the measuring instrument  300 , or the like. 
     Point of attention 3: If, in the measurement place, there is a magnetic substance, the measuring instrument must be separated away therefrom by a distance as large as 3 to 4 m. This is because the influence of an attractive force, having been produced by the magnetism of the measuring instrument  300 , or the like, makes it difficult to perform a highly accurate measurement. 
     Point of attention 4: Measurement must be performed in a place without winds. This is because the repulsive force of the gravitational wave that is to be detected is small, thereby the influence of a wind making it difficult to make a measurement. 
     Point of attention 5: The electromagnetic wave irradiation device  30  must be positioned such that the irradiation point of the electromagnetic wave is at the center or in a vicinity of the center of the magnetic field. This is because, in both the measurement with the electromagnetic coil  310  shown in  FIG. 6  and the measurement with the magnet  321 , and the like, shown in  FIG. 9  and  FIG. 10 , in case where the irradiation point of the electromagnetic wave is located at the center of the measuring magnetic field, a maximum force of repulsion to the gravitational wave is generated. 
     Point of attention 6: The current consumption by the electromagnetic wave irradiation device  30  is unexpectedly large, and therefore three new D-sized batteries must be used for measurement. In the measurement, having been performed, the initial energizing electric current was 880 mA. Thereafter, the electric current was gradually reduced, and in the vicinity of 600 mA, it was so reduced that measuring the force of repulsion to the gravitational wave was impossible. Supplying of power to the electromagnetic wave irradiation device  30  must be controlled on the basis of the supplied current rather than on the supplied voltage. In other words, measurement must be performed while taking care of the value indicated by the ammeter. 
     Point of attention 7: Electrical wiring must be performed by using a method with which the wiring resistance can be held to a minimum. 
     Point of attention 8: When the measurement is to be performed by using both of the electromagnetic coil  310  shown in  FIG. 6  and the magnet  321 , and the like, shown in  FIG. 9  or  FIG. 10 , the measurement must be started from the measurement with the electromagnetic coil  310 . By energizing the electromagnetic coil  310 , it is made possible to measure the degree of the influences as mentioned in the above Points of attention 1, 2, and 3. 
     Point of attention 9: It must be noted that, since the present measuring instrument  300 , and the like, are for an extremely small scale of experiment, and particularly they do not use an optimum electromagnetic wave, the force of repulsion to the gravitational wave that is to be measured is of an extremely small amount. 
     &lt;Setup for Measurement, and Steps for Measuring Operation&gt; 
     &lt;&lt;Setup for Measurement&gt;&gt; 
     To the hanging metal fitting  213  of the balance arm  204  in the balance  200  shown in  FIG. 5 , a stone weight is fixed. On the other hand, to the hanging metal fitting  212  of the balance arm  204 , the measuring instrument  300  with the electromagnetic coil  310  shown in  FIG. 6 , or the measuring instrument  300 A or  300 B with the magnet  321 , and the like, shown in  FIG. 9  or  FIG. 10 , respectively, which is to be repulsed by the gravitational wave, is fixed. If both the measurement with the electromagnetic coil  310  shown in  FIG. 6  and the measurement with the magnet  321 , and the like, are to be performed, it is desirable that the measuring instrument  300  with the electromagnetic coil  310  be used first for measurement. At this time, check must be made to be sure that the requirements as given in the above Points of attention 1, 2, and 3 are met. 
     &lt;&lt;Steps for Measuring Operation&gt;&gt; 
     Step 1: First, in a non-current carrying state, while confirming the position of the pointer  207  of the balance  200  on the scale, the measuring instrument  300  in  FIG. 6 , the measuring instrument  300 A in  FIG. 9 , or the measuring instrument  300 B in  FIG. 10  is balanced with the weight. The positions of the measuring instrument  300  in  FIG. 6 , the measuring instrument  300 A in  FIG. 9 , or the measuring instrument  300 B in  FIG. 10  are kept fixed. In  FIG. 5 , the weight suspension part  211  is moved to strike a balance between the balance arms  204 . The oscillation of the pointer  207  is stopped at the middle point of the graduations in  FIG. 5 . In order to finally stop the oscillation of the pointer  207 , a coin (preferably a 1-yen coin), for example, is moved on the balance arm  204  in an appropriate manner. 
     Step 2: In case where the measuring instrument  300  with the electromagnetic coil  310  shown in  FIG. 6  is used, when the operation at Step 1 has been completed, an electric current is caused to flow from the electromagnetic coil power supply  312  to the electromagnetic coil  310  in  FIG. 6 . The flow of such electric current will cause the pointer  207  to be deflected under the influence as mentioned in the above Points of attention 1, 2, and 3. The position of the pointer after having been deflected is matched to the middle point of the graduations. If the deflection of the pointer  207  has exceeded 0.3 mm, the location for measurement is shifted to another one. 
     Step 3: Then, the measurement operation is started after the oscillation of the pointer  207  having been stopped. In case where the measuring instrument  300  with the electromagnetic coil  310  shown in  FIG. 6  is used, either of the electromagnetic coil  310  or the electromagnetic wave irradiation device  30  may be first energized, or both may be energized simultaneously. Measurement using the measuring instrument  300  with the electromagnetic coil  310  must be carried out with care being taken not to cause the electromagnetic coil  310  to be overheated. When the measuring instrument  300 A or  300 B with the magnet  321 , and the like, shown in  FIG. 9  or  FIG. 10 , respectively, is used for making a measurement, after the oscillation of the pointer  207  having been stopped, the electromagnetic wave irradiation device  30  shown in  FIG. 9  or  FIG. 10  is energized. 
     Step 4: As a result of the energization, the pointer is slightly deflected, and thus careful observation is required. In a measurement, having been made using the measuring instrument  300  with the electromagnetic coil  310  shown in  FIG. 6 , an estimated amount of “loss in weight” of 3 to 4 mg was given. In making a measurement, when the pointer  207  is at an extreme right position, the electromagnetic wave irradiation device  30  is caused to start its operation, while when the pointer  207  is at an extreme left position, the electromagnetic wave irradiation device  30  is caused to stop its operation. By repeating this, the loss in weight can be grasped. Further, the position of the electromagnetic wave irradiation device  30  can have a subtle effect on the measurement, thus frequent adjustment thereof being required. 
     &lt;Results of Measurement&gt; 
     The measurements, having been made using the measuring instrument  300 A or  300 B with the magnet  321 , and the like, shown in  FIG. 9  or  FIG. 10 , respectively, exhibited an estimated amount of loss in weight of 5 to 7 mg when ultraviolet light was irradiated from the electromagnetic wave irradiation device  30  to a vicinity of the center of the magnet  321 , and the like. When the number of magnets was one, no loss in weight was detected, and the number of magnets was four, the total mass of the magnets  321 , and the like, and the weight was too large to obtain an estimated value of loss in weight. 
     &lt;Matters to be Considered&gt; 
     With the method which was used in the Example at this time, superposing the magnet  321 , and the like, upon one another for making a measurement, the state of magnetic field within the columnar magnet  321 , and the like, is unclear, and there is a possibility that the same magnetic field as expected at the beginning could not have been generated. In future, it is desirable to conduct an experiment using a powerful magnetic field, and a variety of electromagnetic waves in a single columnar magnetic field. 
     &lt;Conclusion&gt; 
     As described above, by generating a magnetic field using the columnar magnet  321 , and the like, or the electromagnetic coil  310  (the magnetic field generation part), and causing the electromagnetic wave irradiation part  31  to irradiate an electromagnetic wave in parallel or substantially in parallel with the gravitational wave at the center or in a vicinity of the magnetic field, having been generated, it is possible to obtain power repulsive to the gravitational force. 
     As a result of this, it is possible to realize a power generating apparatus  10 , which offers a variety of advantages, such as being small-sized, energy saving, and ecology friendly. Further, it is made possible to realize a variety of mobile bodies  100  and  110 , which are moved with power, being generated by the power generating apparatus  10  of the present invention. 
     &lt;Variant 1&gt; 
     As a variant 1 of the above-described power generating apparatus  10 , a power generating apparatus  10 A as stated below can be considered. As shown in  FIG. 12 , the basic configuration of the power generating apparatus  10 A is the same as that of the power generating apparatus  10 , however, with the power generating apparatus  10 A, the position where the electromagnetic wave irradiation device  30  is disposed in the hollow portion of the columnar magnet  20  is displaced to slightly above the middle in a vertical direction. 
     In this way, by raising the position of the electromagnetic wave irradiation part  31  upward, the gravitational wave from under in  FIG. 12  is deformed by the S-pole in the magnetic field of the columnar magnet  20 . On the other hand, the electromagnetic wave, having been emitted from the electromagnetic wave irradiation part  31  is deformed by the N-pole. Thereby, the gravitational wave, having been deformed by the S-pole, and the electromagnetic wave, having been deformed by the N-pole, will produce a phenomenon of attraction in the central portion of the magnetic field. 
     &lt;Variant 2&gt; 
     In addition, as a variant 2 of the above-described power generating apparatus  10 , a power generating apparatus  10 B as stated below can be considered. As shown in  FIG. 13 , the basic configuration of the power generating apparatus  10 B is the same as that of the power generating apparatus  10 , however, with the power generating apparatus  10 B, a cover and reflection plate above the electromagnetic wave irradiation part  31  (see  FIG. 1 ), which is provided for the power generating apparatus  10 , is eliminated. 
     Thereby, the electromagnetic wave irradiation part  31  irradiates an electromagnetic wave both in a downward direction and an upward direction in  FIG. 13  with respect to the magnetic field. With such a structure, an attractive force and a repulsive force can be obtained simultaneously. Since the gravitational wave arrives at the magnet from every spatial direction, it can be considered that the power generating apparatus  10 B is effective especially when used in the outer space. 
     Heretofore, the embodiments of the present invention have been described with reference to the drawings, however, the specific configuration is not limited to that of these embodiments as described above, and various changes and modifications may be included in the present invention, so long as they do not depart from the spirit and scope thereof. Each of the power generating apparatus  10  related to the above-described embodiments, the power generating apparatus  10 A related to the variant 1, and the power generating apparatus  10 B related to the variant 2 may be used with an appropriate alteration being provided therefor. 
     For example, the geometry of the magnet  321 , and the like, is not limited to a columnar shape, and an object around which the coil is to be wound is not limited to a cylindrical one, but may be a hollow non-magnetic material having an n-polygonal cross-section (where n is an integral number). In addition, various parameters, such as the length of the magnet  321 , and the like, the number of magnets of the magnet  321 , and the like, the number of turns of the coil, and the length of the coil, may be appropriately altered. 
     Further, the electromagnetic wave, being irradiated by the electromagnetic wave irradiation part  31 , is not limited to “light”, such as ultraviolet light, infrared light, and visible light, and may be an “electric wave”, such as a microwave, and a millimetric wave. In this case, the electromagnetic wave irradiation part  31  may be configured to oscillate an electromagnetic wave with the use of a magnetron, a GUNN diode, or the like. 
     INDUSTRIAL APPLICABILITY 
     The present invention can be widely utilized for a variety of power generating apparatuses. In addition, by using a plurality of power generating apparatuses, a large-sized mobile body can be created.