WO2014183230A1 - Appareil électromagnétique de réduction de pression et de propulsion à air/fluide - Google Patents

Appareil électromagnétique de réduction de pression et de propulsion à air/fluide Download PDF

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Publication number
WO2014183230A1
WO2014183230A1 PCT/CN2013/000575 CN2013000575W WO2014183230A1 WO 2014183230 A1 WO2014183230 A1 WO 2014183230A1 CN 2013000575 W CN2013000575 W CN 2013000575W WO 2014183230 A1 WO2014183230 A1 WO 2014183230A1
Authority
WO
WIPO (PCT)
Prior art keywords
electrodes
magnet
propulsion device
lift
gas fluid
Prior art date
Application number
PCT/CN2013/000575
Other languages
English (en)
Chinese (zh)
Inventor
贾龙
Original Assignee
Jia Long
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jia Long filed Critical Jia Long
Priority to PCT/CN2013/000575 priority Critical patent/WO2014183230A1/fr
Publication of WO2014183230A1 publication Critical patent/WO2014183230A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/001—Flying saucers

Definitions

  • the present invention relates to a fluid decompression and propulsion device, and more particularly to an electromagnetic gas fluid depressurization and propulsion device. Background technique
  • an object of the present invention is to provide an electromagnetic gas fluid decompression and propulsion device which is simple in structure, good in lift effect, high in safety, and capable of accelerating decompression and propulsion of a gas fluid.
  • An electromagnetic gas fluid decompression and propulsion device which comprises: a lift bottom plate, a pair of electrodes, a magnet, two or more laser sources and several laser reflections
  • the lower surface of the lifting bottom plate is connected to the magnet, one end of the lifting bottom plate is located on the magnet, and the other end extends outside the magnet in the direction of air flow; and two sides of the upper surface of the lifting bottom plate are respectively disposed
  • the electrodes, the relative positions of the lift bottom plate, the two electrodes and the magnet are fixed; the two electrodes are correspondingly provided with a plurality of small holes, and the plurality of multi-layer lasers emitted by the laser sources pass through the small holes. Reciprocating through the reflector between the two electrodes.
  • the electric field formed between the two electrodes and the lift floor are both perpendicular to the axis of the magnet.
  • Each of the reflectors is made of copper or silver.
  • a barrier plate is respectively added to the upper portions of the two electrodes.
  • the magnet adopts one of a solenoid type conduction cooled superconducting magnet and a neodymium iron boron permanent magnet Strong magnet.
  • the two electrodes are respectively connected to the positive and negative electrodes of the electromagnetic gas fluid decompression and the external power supply of the propulsion device, and the voltage of the electromagnetic fluid is controlled to be decompressed and the propulsion device is generated by adjusting the voltage between the two electrodes.
  • the present invention has the following advantages due to the above technical solution: 1.
  • the present invention is composed of a lifting bottom plate, a magnet, an electrode and a reflector, and one end of the lifting bottom plate is disposed on the magnet, and the other end extends to the outside of the magnet, and the structure is simple. And can effectively improve the lift of the lift floor.
  • a plurality of multi-layer laser beams emitted by the respective laser sources pass through a plurality of small holes corresponding to the two electrodes, and then reciprocally penetrate between the electrodes to increase the electromagnetic force.
  • the height of the area In the prior art, an ionosphere produced by a single laser is used, which is thin and does not produce sufficient lift.
  • the present invention is made of copper or silver for each reflector, and wires are connected between the reflectors and the electrodes to reduce the contact resistance between the plasma channel of the laser beam and the electrodes, thereby increasing the conductivity and thereby increasing the lift. . 4.
  • the invention uses the laser emitted by the laser source to ionize the air between the two electrodes, thereby forming an air plasma, and has no greenhouse gas emission, thereby being environmentally friendly and safe to use. Therefore, the purpose of accelerating decompression and propulsion of the electromagnetic gas fluid of the object is achieved.
  • the invention can be widely applied in the fields of aviation (especially low-altitude flight), fire rescue and recreation.
  • Figure 1 is a schematic view of the overall structure of the present invention
  • FIG. 2 is a schematic view showing the effect of obtaining lift of the lift floor of the present invention
  • Figure 3 is a schematic view showing the action area of the electromagnetic force on the lift floor of the present invention.
  • Figure 4 is a schematic diagram showing the rise of force generated by the use of a plurality of laser sources in accordance with H/L;
  • FIG. 5 is a schematic diagram of a curve of a lift force generated by a plurality of laser sources according to the present invention as a function of electromagnetic force density, wherein the curve with a circle is a schematic diagram of an air flow velocity curve accelerated after ionization, and the curve with a square shape is lift with electromagnetic Schematic diagram of the change in force density;
  • Figure 6 is a schematic view showing the structure of the present invention after adding a barrier plate over the two electrodes;
  • Figure 7 is a schematic view showing the relationship between the lift density and the length of the electromagnetic force applied to the electrode of the present invention, wherein the square curve is Schematic diagram of the velocity profile of the airflow accelerated after ionization; the curve with a circle is a schematic diagram of the curve after the barrier is added; the curve with a triangle It is a schematic diagram of the curve without the barrier. Best mode for carrying out the invention
  • the present invention utilizes air plasma to generate lift and propulsion under the action of an electromagnetic field, which includes a lift base plate 1, a pair of electrodes 2, a magnet 3, two or more laser sources 4, and a plurality of laser reflections.
  • an electromagnetic field which includes a lift base plate 1, a pair of electrodes 2, a magnet 3, two or more laser sources 4, and a plurality of laser reflections.
  • Device 5 includes a lift base plate 1, a pair of electrodes 2, a magnet 3, two or more laser sources 4, and a plurality of laser reflections.
  • the lower surface of the lift base plate 1 is connected to the magnet 3, and one end of the lift base plate 1 is located on the magnet 3, and the other end extends in the flow direction of the air to the outside of the magnet 3 to increase the lift.
  • An electrode 2 is disposed on each side of the upper surface of the lift base plate 1. The electric field formed between the two electrodes 2 and the lift base plate 1 are perpendicular to the axis of the magnet 3, and the relative positions of the lift base plate 1, the two electrodes 2 and the magnet 3 during operation The fixed remains the same.
  • a plurality of small holes 6 are respectively formed on the two electrodes 2, and a plurality of multi-layer laser beams emitted from the laser sources 4 pass through the small holes 6, and are reciprocally penetrated between the two electrodes 2 via the reflector 5, so that the two electrodes 2 are interposed therebetween.
  • the air continues to ionize, generating an air plasma to form an electromagnetic force.
  • the lift base plate 1 of the present invention can be effectively increased in lift force as compared with the lift floor of the prior art.
  • the electromagnetic force density F x 1000000 N/m 3
  • the length of the electromagnetic force acting region 40 ⁇
  • the pressure on the upper surface of the lift base plate 1 (as shown in Fig. 2, where the dark solid line is the pressure curve of the upper surface of the lift base plate 1) is lower than The lower surface (as shown in Fig. 2, wherein the light solid line is the pressure curve of the lower surface of the lift base plate 1); and the absolute value F1 of the static pressure integral in the range of 0 to 0. 074 m is greater than 0. 074 ⁇ ! ⁇ 0.
  • the absolute value of the static pressure integral in the range of lm F2 the difference between Fl and F2 is the lift obtained by the lift base plate 1. Therefore, extending the length of the lift base plate 1 can effectively increase the lift.
  • the present invention uses two or more laser sources 4, a plurality of multi-layer laser beams emitted from the plurality of laser sources 4 reciprocally pass between the two electrodes 2, which can effectively increase the height and density of the electromagnetic force acting region, thereby effectively The lift of the lift floor 1 is increased.
  • the lift of the force plate 1 is increased.
  • the lift is 3090 ⁇ / ⁇ 1 2 .
  • the length of the electromagnetic force acting region is 40 legs, as the electromagnetic force density increases,
  • the maximum velocity V max of the airflow accelerated after the air ionization increases, and the lift of the lift floor 1 also increases.
  • each of the reflectors 5 is made of copper or silver. Since the central portion of the plasma channel generated by the laser has the highest conductivity, when the laser beam emitted from the laser source 4 passes through the small hole 6 in the electrode 2, only the outer edge of the plasma channel is in contact with the electrode 2, so that the contact resistance is large. . Therefore, each of the reflectors 5 of the present invention is connected to the electrode 2 by a wire to reduce the contact resistance between the plasma beam plasma channel and the electrode.
  • a barrier plate 7 is further added to the upper portions of the two electrodes 2 to increase the lift.
  • the height H of the electromagnetic force acting region is 40 mm
  • the 3D calculation results of the addition-resistive separator 7 and the non-blocking separator 7 were compared. It can be seen that the maximum speed increases with the increase of the length of the electromagnetic force acting region! ⁇ ; when the ratio of the length of the electromagnetic force acting region!
  • ⁇ to the length L of the base plate 1 / L is greater than 0.3, the lift density of the resistive baffle 7 is greater than Without the barrier plate 7, and as the increase, the difference gradually increases; in the interval [0.3, 0.6], the lift density changes slowly; when less than or equal to 0.3, the barrier is not added The lift is slightly larger than the lift of the baffle plate 7.
  • the magnet 3 employs a solenoid-type conduction-cooled superconducting magnet to generate a magnetic field B in the axial direction (as shown in Fig. 1); the magnet 3 can also use other strong magnets such as neodymium-boron-boron permanent magnets.
  • the two electrodes 2 are respectively connected to the positive and negative electrodes of the electromagnetic gas fluid decompression and external power supply of the propulsion apparatus of the present invention, thereby forming an electric field J (shown in Fig. 1). Further, by adjusting the level of the voltage between the electrodes 2, the electromagnetic gas fluid decompression of the present invention and the magnitude of the lift and thrust generated by the propulsion device can be controlled.
  • the electromagnetic gas fluid decompression and propulsion device of the present invention may be disposed at any position in the atmosphere.
  • the air between the two electrodes 2 is ionized by the laser light emitted from the laser source 4 under atmospheric pressure to form an air plasma, and the electric field generated between the two electrodes 2 and Under the action of the magnetic field B perpendicular thereto, the electromagnetic force in the F direction can be generated. Therefore, the air plasma is accelerated by the action of the electromagnetic force F, and the accelerated motion of the air will cause The pressure on the surface of the lift base plate 1 is lowered, and the gas on the other side is not affected by the electromagnetic force, and the pressure is maintained. Therefore, a pressure difference is formed between the upper and lower sides of the lift floor 1, thereby generating electromagnetic lift, and the electromagnetic gas fluid decompression and propulsion device of the present invention are suspended. At the same time, the accelerated flow of air can also generate thrust, thereby facilitating the decompression of the electromagnetic gas fluid of the present invention and the advancement of the propulsion device.

Abstract

La présente invention concerne un appareil électromagnétique de réduction de pression et de propulsion à air/fluide, caractérisé en ce qu'il comprend une plaque de fond à force de levage, une paire d'électrodes, un aimant, plus de deux sources de laser et une pluralité de réflecteurs de laser. Une surface inférieure de la plaque de fond à force de levage est reliée à l'aimant. Une extrémité de la plaque de fond à force de levage est disposée sur l'aimant, et son autre extrémité s'étend à l'extérieur de l'aimant dans la direction d'un flux d'air entrant. Les deux électrodes sont respectivement agencées des deux côtés d'une surface supérieure de la plaque de fond à force de levage. Une position relative de la plaque de fond à force de levage, des deux électrodes et de l'aimant est fixe. Une pluralité de petits orifices est ménagée sur les deux électrodes. Plusieurs faisceaux laser multi-couches émis par chaque source de laser traversent les petits orifices, et sont transmis entre les deux électrodes en va-et-vient entre les réflecteurs. Du fait qu'il comprend la plaque de fond à force de levage, l'aimant, les électrodes et les réflecteurs, qu'une extrémité de la plaque de fond à force de levage est agencée sur l'aimant et que l'autre extrémité s'étend à l'extérieur de l'aimant, l'appareil selon l'invention présente une structure simple et améliore de manière efficace la force de levage de la plaque de fond à force de levage. La présente invention a un vaste champ d'application dans des domaines tels que l'aéronautique, la lutte contre l'incendie, les loisirs, etc.
PCT/CN2013/000575 2013-05-14 2013-05-14 Appareil électromagnétique de réduction de pression et de propulsion à air/fluide WO2014183230A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2013/000575 WO2014183230A1 (fr) 2013-05-14 2013-05-14 Appareil électromagnétique de réduction de pression et de propulsion à air/fluide

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2013/000575 WO2014183230A1 (fr) 2013-05-14 2013-05-14 Appareil électromagnétique de réduction de pression et de propulsion à air/fluide

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WO2014183230A1 true WO2014183230A1 (fr) 2014-11-20

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101381005A (zh) * 2008-10-23 2009-03-11 上海交通大学 多级式离子射流装置与方法
US20100243816A1 (en) * 2003-05-06 2010-09-30 Gary Richard Gochnour Aircraft also called a spacecraft, an aerospace craft, or a submersible craft
CN102139763A (zh) * 2011-01-30 2011-08-03 贾龙 一种电磁气流体减压及推进装置
CN102745331A (zh) * 2012-06-26 2012-10-24 贾龙 一种电磁气流体减压及推进装置
CN103085969A (zh) * 2013-02-06 2013-05-08 贾龙 一种电磁气流体减压、推进及升力装置

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100243816A1 (en) * 2003-05-06 2010-09-30 Gary Richard Gochnour Aircraft also called a spacecraft, an aerospace craft, or a submersible craft
CN101381005A (zh) * 2008-10-23 2009-03-11 上海交通大学 多级式离子射流装置与方法
CN102139763A (zh) * 2011-01-30 2011-08-03 贾龙 一种电磁气流体减压及推进装置
CN102745331A (zh) * 2012-06-26 2012-10-24 贾龙 一种电磁气流体减压及推进装置
CN103085969A (zh) * 2013-02-06 2013-05-08 贾龙 一种电磁气流体减压、推进及升力装置

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