• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The magnetic motor, powered, is a push system for a mobile, formed by an electromagnet (2, 3, 4, 6) to which we extend the surface of the ends of its core (3), which will increase the power of its magnetic field, which will be directed towards small magnets (5, 7), anchored to the fuselage of the mobile in question, be it an aircraft, a ship, a submarine, or, the artificial satellite in which we install them. The north magnets (7) at one end will be attracted to the south end (6) of the core (3), and, at the same time, the north magnets (5) at the other end will be repelled by the north end (4) of the core (3). This double simultaneous thrust will produce a greater or lesser movement, depending on the magnetic field of the main coil (2), to which, to increase its power, we connect, each of its turns, with other secondary coils (8), formed by a cable of the same thickness. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2614748A1
    申请号:ES201500890
    申请日:2015-12-01
    公开日:2017-06-01
    发明作者:Fco. Javier Porras Vila
    申请人:Fco. Javier Porras Vila；
    IPC主号:
    专利说明:

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    DESCRIPTION
    Magnetic motor, powered.
    Object of the invention
    The main objective of the present invention is to greatly increase the thrust power of the magnetic motor that serves as a precedent, as I have presented in another prior patent. This increase in power, will make this engine useful, to raise helicopters, artificial satellites, or airplanes vertically, and, it will also be able to push submarines well, and, large-size ships.
    Background of the invention
    The main antecedent of the invention shown today is found in my previous Patent, No. P201200861, entitled: Accelerator of artificial satellites with electroiman and shaft, in which it presented a similar system, although, much simpler, in which the magnetic field of the main coil (2) could not reach the same power that it could achieve in the present improvement. In today's invention, the thrust that the core (3, 4, 6) can be multiplied much more can be applied on the fuselage to which the magnets (5, 7) will be anchored, because the core (3) has now expanded, both upwards and downwards, at the ends (4, 6) of the core (3), which are the extension of the mild iron that, as long as its volume increases, and, also, increases the magnetic field that runs through it. The second improvement of the present invention refers to the increase in the power of the current that can be practiced in the main coil (2), while we are going to connect a few secondary coils (8) at two different points of each one of his thick turns. In this way, the current that crosses each of its turns will increase its power in its corresponding secondary coil (8), so that the power of this same current will reach the next turn with a value much greater than the one that has arrived to the previous turn. The consequence of this considerable increase in the power of the current, translates into a considerable increase in the magnetic field to be induced in the nucleus (3, 4,
    6), and, therefore, also in a considerable push towards the small magnets (5, 7) that face their ends, and, these, will push the fuselage of the aircraft to which they are fixed.
    Description of the invention
    The Magnetic Motor, powered, is a thrust system that is formed by a plug (1), to which we connect an electroiman, formed, in turn, by a main coil (2) and a core (3), to which we go to be potentiated by its two extremes (4, 6) by expanding its surface and its matter, both towards both sides, upwards and downwards. This is what is presented in figure 1. In front of each enlargement (4, 6) of the nucleus (3), we place several magnets (5, 7) of smaller size than the extensions (4, 6), whose magnetic field it will be much lower than the core (3, 4, 6) of the electroiman (2, 3). The magnets (5) of the upper zone will face their north pole to the extension (4) of the north end of the core (3). The magnets (7) of the lower zone will also face their north pole, to the extension (6) of the south end of the core (3). All these magnets (5,
    7), - as well as, the core (3) of the electroiman (2, 3, 4, 6) -, will be fixed to the fuselage of the aircraft, or, of the mobile in which they are installed. At every two different points of each turn of the main coil (2), we will connect the cable ends of other secondary coils (8), formed with a cable of a thickness similar to that of the main coil (2), or, just like yours. If the main coil cable (2) is two
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    centimeters and a half, that of the secondary coils (8) will be one centimeter and a half. Date of the invention: (29.11.15).
    Description of the figures
    Figure n ° 1: Plan view of the Magnetic Motor, enhanced, in which the position of advance of the motor of, for example, an airplane, towards the upper part of the paper sheet is defined. The figure shows a plug (1), to which the main coil (2) is connected, which has a core (3) that is powered by its two ends (4, 6), expanding its surface and its matter. In front of each extension (4, 6), other magnets (5, 7) of smaller size are placed than the core (3, 4, 6) of the electroiman (2, 3). The magnets (5) of the upper zone, face their north pole, to the extension (4) of the north end of the core (3), and, the magnets (7) of the lower zone, face their north pole, to the prolongation (6) from the south end of the nucleus (3). At each turn of the main coil (2), the ends of the cable of other secondary coils (8), formed with a cable of a thickness similar to that of the main coil (2), are connected at two different points, or, same as yours.
    Figure 1:
    1) Plug
    2) Main coil
    3) Nucleus
    4) Extension of the North end of the nucleus
    5) North Magnets
    6) Extension of the South end of the nucleus
    7) South Magnets
    8) Secondary coils
    Description of a preferred embodiment
    The magnetic motor, enhanced, is characterized by being a thrust system for all types of mobile, especially for those of greater size, while this size allows them to enable a special area to locate these engines that will generate in their great electroiman (2-6) very great powers. The operation of the mechanism described above cannot be easier. The electroiman (2, 3, 4, 6) will produce attraction to the north magnets (7) of the lower zone that face the south pole of the nucleus (3, 4). And, at the same time, it will produce repulsion towards the northern magnets (5) of the upper zone, which face the north pole of that same nucleus (3, 4). Thus, with these two simultaneous forces, - and, like the magnets (5, 7) are fixed to the fuselage of the aircraft -, these magnets (5, 7) will receive the force of the electroiman (2, 3, 4, 6) , and, they will move the fuselage of the plane, -or, of the cell phone in question-, forward, -that is, towards the upper part of the sheet where figure n ° 1 is presented. As it happens whenever they face two magnets, the magnet that will tend to move will be the one whose magnetic field is smaller than that of the other, the one that will remain fixed, so that, upon receiving the impact of the waves from the opposite pole of the other magnet, the one with the lowest magnetic field will to get away from the one with the greatest magnetic field. And, as in this case, it cannot be moved because the magnets (5, 7) are fixed to the fuselage, they will transmit to it the force that
    It makes them tend to move away. Keep in mind that it will always be better to put many small magnets (5, 7), than just one that is as large as the sum of all the small ones. It is about all the power of the magnetic field of the nucleus (3, 4, 6) being poured into each and every one of the magnets (5, 7), because, like all of them they will be fixed to the fuselage of an artificial satellite, for example, the thrust will be greater, because this fuselage will receive as many simultaneous thrusts, at points other than the fuselage, as small magnets (5, 7) we have fixed on it. The second improvement presented in this invention is to enhance the current through the main coil (2). For this purpose, we have added other secondary coils (8), formed by a cable that has the same diameter as that of the main coil (2), or, slightly smaller than yours. If the one of the main coil (2) is a cable of two and a half centimeters in diameter, the diameter of the cable of the secondary coils (8), may also have two and a half centimeters, or a centimeter and a half. The number of turns of the secondary coils (8) will be less than that of the main coil (2). With these secondary coils 15 (8), the current will increase the values of their power, both in intensity and in voltage, which will be transmitted to the same coil of the main coil (2) to which the two are connected ends of your cable. And, thus, in each turn of the main coil (2), the current will have been enhanced much more, so that the magnetic field that can be induced in the core (3, 4, 6) will also be very powerful, which 20 will result in a very powerful thrust and a very powerful simultaneous attraction to the Magnets (5, 7) that face them, which will accelerate artificial satellites, airplanes, ships, submarines, and all types of vehicles.
    权利要求:
    Claims (1)
    [1]
    1. Magnetic motor with extended core electroiman and powered coils, facing magnets, for aircraft, characterized by being a push system formed by a plug (1), to which we connect an electroiman (2, 3, 4, 6) , formed by a main coil (2) and a core (3), which we potentiate at its two ends by extending its surface and its matter sideways, both above, which forms the end (4), as below, what forms the end (6). In front of each extension of the ends (4, 6) of the nucleus (3), we place several magnets (5, 7) of smaller size than the 10 extensions (4, 6). The magnets (5) of the upper zone will face their north pole to the
    extension (4) of the north end of the nucleus (3). The magnets (7) of the lower zone will also face their north pole, to the extension (6) of the south end of the core (3). All these magnets (5, 7), - as well as the core (3) of the electroiman (2, 3, 4, 6) - will be attached to the fuselage of the aircraft. At every two different points of each turn of the main coil (2), we will connect the cable ends of other coils
    secondary (8), formed with a cable of a thickness similar to that of the main coil (2), or, just like yours.
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    同族专利:
    公开号 | 公开日
    ES2614748B1|2018-03-12|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    GB1255067A|1968-04-10|1971-11-24|Gen Lab Associates Inc|Permanent magnet alternator|
    CN201041980Y|2007-05-14|2008-03-26|刘新广|Permanent magnetic machine|
    CN102437705A|2011-11-28|2012-05-02|苏州普思自动化科技有限公司|Linear motor|
    WO2015039716A1|2013-09-19|2015-03-26|Brose Fahrzeugteile GmbH & Co. Kommanditgesellschaft, Würzburg|Electric machine|
    法律状态:
    2018-03-12| FG2A| Definitive protection|Ref document number: 2614748 Country of ref document: ES Kind code of ref document: B1 Effective date: 20180312 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201500890A|ES2614748B1|2015-12-01|2015-12-01|Magnetic motor, powered|ES201500890A| ES2614748B1|2015-12-01|2015-12-01|Magnetic motor, powered|
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