CN115571380A - Stress wave static working medium propelling device and method - Google Patents
Stress wave static working medium propelling device and method Download PDFInfo
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- CN115571380A CN115571380A CN202211112927.5A CN202211112927A CN115571380A CN 115571380 A CN115571380 A CN 115571380A CN 202211112927 A CN202211112927 A CN 202211112927A CN 115571380 A CN115571380 A CN 115571380A
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- working medium
- solar photovoltaic
- propeller
- stress wave
- anode
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- 238000000034 method Methods 0.000 title claims abstract description 21
- 230000003068 static effect Effects 0.000 title claims abstract description 21
- 239000003380 propellant Substances 0.000 claims abstract description 23
- 150000002500 ions Chemical class 0.000 claims abstract description 21
- 230000001133 acceleration Effects 0.000 claims abstract description 20
- 230000005672 electromagnetic field Effects 0.000 claims abstract description 10
- 229910052724 xenon Inorganic materials 0.000 claims abstract description 10
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 claims abstract description 10
- 238000010894 electron beam technology Methods 0.000 claims abstract description 7
- 239000011261 inert gas Substances 0.000 claims description 8
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 6
- 230000005684 electric field Effects 0.000 claims description 6
- 239000000126 substance Substances 0.000 claims description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 3
- 229910052786 argon Inorganic materials 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 3
- 238000005421 electrostatic potential Methods 0.000 claims description 3
- 239000001307 helium Substances 0.000 claims description 3
- 229910052734 helium Inorganic materials 0.000 claims description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 3
- 239000001257 hydrogen Substances 0.000 claims description 3
- 229910052739 hydrogen Inorganic materials 0.000 claims description 3
- 229910052743 krypton Inorganic materials 0.000 claims description 3
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 239000000446 fuel Substances 0.000 abstract description 9
- 238000002679 ablation Methods 0.000 description 5
- 230000002349 favourable effect Effects 0.000 description 3
- 241001529251 Gallinago gallinago Species 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 108010066057 cabin-1 Proteins 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/405—Ion or plasma engines
Abstract
The invention discloses a stress wave static working medium propelling device and a method, and the device comprises a working medium cabin, a propelling device, a telescopic device, solar photovoltaic panels, an anode charged panel and an accelerating channel, wherein the working medium propelling device is installed at one end of the working medium cabin, the interior of the working medium propelling device is communicated with the interior of the working medium cabin, a jet orifice is arranged at the top of the propelling device and communicated with the propelling device, the solar photovoltaic panels are arranged outside the propelling device, two solar photovoltaic panels are arranged, one ends of the two solar photovoltaic panels are connected with one end of the telescopic device, electron beams in high-speed annular motion are used for sniping a propellant working medium near an anode, the working medium is ionized after violent collision, ions of the propeller working medium generate axial acceleration under the action of an electromagnetic field, and are finally ejected at high speed to generate thrust to form plasma jet, the device can be driven to propel by only a small amount of xenon, and the used fuel only accounts for 10 percent of the traditional propeller.
Description
Technical Field
The invention relates to the technical field of propulsion devices and methods, in particular to a stress wave static working medium propulsion device and a method.
Background
Through retrieval, patent one, chinese patent No. CN207843350U discloses a stress wave static working medium propulsion device, and relates to a stress wave static working medium propulsion device, the stress wave static working medium propulsion method is to utilize the difference of the speed of stress wave propagation of the internal stress medium of the propulsion device and/or the difference of the propagation distance of stress wave propagation of the propulsion device, so that the propulsion device generates different acting forces in two opposite directions, thereby pushing the propulsion device to move towards one direction. The stress wave static working medium propulsion device has small energy loss, low cost, little pollution or basically no pollution;
through retrieval, patent two, chinese patent No. CN208431118U discloses an externally constrained discharge channel and a solid ablation pulsed electric thruster, wherein, an externally constrained discharge channel is applied to a solid ablation pulsed electric thruster, and the externally constrained discharge channel includes: a conductive anode; a conductive cathode, a gap being left between the conductive anode and the conductive cathode; and the restraint piece is provided with a restraint surface, the restraint piece, the conductive anode and the conductive cathode enclose a discharge channel with two open ends, the restraint surface faces the inside of the discharge channel, and the restraint piece is made of an insulating material resistant to arc ablation. The technical scheme of the invention has the advantages of improving the uniformity of the ablation end face of the working medium and improving the thermopneumatic efficiency of the neutral macromolecular ablation product.
The above patents suffer from the following disadvantages:
1. the device is propelled by an external working medium in the using process, so that the device can generate power, and can only carry more propelling working media in order to be used for a long time, and the energy consumed by the propeller can be increased by carrying more propelling working media;
2. when the device is used, the specific impulse is small, so that the same amount of fuel generates less power, and the fuel cannot be fully used.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides a stress wave static working medium propelling device and a method, which solve the problems in the background art.
(II) technical scheme
In order to achieve the purpose, the invention is realized by the following technical scheme: the static working medium propelling device comprises a working medium bin, a propelling device, a telescopic device, a solar photovoltaic panel, an anode charged panel and an accelerating channel, wherein the working medium propelling device is installed at one end of the working medium bin, the inside of the working medium propelling device is communicated with the inside of the working medium bin, a jet orifice is arranged at the top of the propelling device and is communicated with the propelling device, two solar photovoltaic panels are arranged outside the propelling device, one ends of the two solar photovoltaic panels are connected with one end of the telescopic device, the accelerating channel is arranged at the top of the propelling device, the anode charged panel is arranged at the bottom of the accelerating channel, a coil is arranged on the outer side of the accelerating channel, an axial magnetic field is arranged in the middle of the accelerating channel, and an electron emission gun is arranged on one side of the accelerating channel.
Preferably, the filling medium in the working medium cabin is inert gas, and the inert gas is xenon.
Preferably, the jet orifices are distributed at the top of the working medium propeller at regular intervals in an annular shape, one end of each jet orifice is located inside the accelerating channel, the surface of the anode charged plate at the bottom of the accelerating channel is provided with a hole groove, the jet orifices are arranged inside the hole grooves, and the molded surfaces of the jet orifices are in a conical shape or a bell shape.
Preferably, the number of the solar photovoltaic panels is two, the two solar photovoltaic panels are of a folding structure, and the solar photovoltaic panels are electrically connected with the electron emission guns.
Preferably, an inner magnetic core is arranged inside the axial magnetic field, a radial magnetic field is formed inside the acceleration channel by the inner magnetic core and the coil inside the axial magnetic field, and the anode live plate is applied with high-voltage electricity through a power supply device to form an axial acceleration electric field in the acceleration channel.
Preferably, the steps are as follows:
the method comprises the following steps: the accelerating channel stably releases electrons through the cathode of the electron emission gun 9, the current formed by the electrons spirally accelerates and falls to the anode under the action of Lorentz force of a ring-shaped magnetic field, the electrons emitted from the cathode are captured by a crossed electromagnetic field, and after being captured, the electrons can perform angular drift in a discharge area, wherein the angular drift is the result of the action of a crossed radial magnetic field and an axial electric field;
step two: the medium is conveyed by distributing and conveying the medium in the working medium cabin 1 through the working medium propelling device 2, and the difference between the flow rate of the propellant in the region with high propellant flow rate and the flow rate of the propellant in the region with low propellant flow rate is adjusted to be 10 percent, so that the medium is conveyed to the channel 10 through the jet orifice 7;
step three: ionizing to form an accelerating channel of the annular discharge space to ionize the propellant medium flowing into the discharge space to generate ions, sniping the sprayed propellant working medium near the anode by the electron beam in high-speed annular motion, and ionizing the working medium after violent collision;
step four: generating thrust, wherein ions of the working medium of the propeller generate axial acceleration under the action of an electromagnetic field and are finally ejected at high speed to generate thrust to form plasma jet;
step five: the working substance ion plume is neutralized, and the ions pick up electrons and neutralize the light beam when leaving, and leave the propeller in a high-speed state to form power.
Preferably, the electric propulsion working medium in the working medium bin in the second step is a simple substance or a mixture of xenon, argon, krypton, helium and hydrogen.
Preferably, in step one, the impeller accelerates the ions to a high velocity using an electrostatic potential, the negative attractive charge being provided by the electron plasma at the open end of the impeller, and a potential of 150 to 800 volts being applied between the anode and cathode of the impeller in such a way that the central portion of the impeller forms the magnetic pole of the electromagnet.
(III) advantageous effects
The invention provides a stress wave static working medium propelling device and a method. The method has the following beneficial effects:
(1) According to the stress wave static working medium propelling device and method, through the mutual combination of all parts, electrons are stably released through a cathode of an electron emission gun, currents formed by the electrons spirally accelerate and fall to an anode under the action of an annular magnetic field, media in a working medium bin are distributed and conveyed through the working medium propelling device, electron beams in high-speed annular motion snipe an ejected propellant working medium near the anode to ionize the working medium after violent collision, ions of the working medium of the propeller generate axial acceleration under the action of the electromagnetic field and are ejected at high speed finally to generate thrust to form plasma jet, the device can be driven to push only by a small amount of xenon, the used fuel only accounts for 10% of that of a traditional propeller, and the device can be continuously conveyed with electric power through a solar photovoltaic panel, so that the carried fuel is favorably reduced.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a front view of the present invention;
FIG. 3 is a top view of the present invention;
FIG. 4 is a schematic view of an electron emission gun according to the present invention;
FIG. 5 is a schematic view of a coil structure according to the present invention;
fig. 6 is a graph of the operating characteristics of the anode layer type with respect to the magnetic flux density B of the present invention.
In the figure, 1-working medium cabin, 2-working medium propeller, 3-telescoping device, 4-solar photovoltaic panel, 5-anode charged panel, 6-coil, 7-jet orifice, 8-axial magnetic field, 9-electron emission gun, 10-accelerating channel.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, an embodiment of the invention provides a technical solution: a stress wave static working medium propulsion device and a method thereof comprise a working medium bin 1, a propulsion device 2, a telescopic device 3, a solar photovoltaic panel 4, an anode charged panel 5 and an accelerating channel 10, wherein the working medium propulsion device 2 is installed at one end of the working medium bin 1, the interior of the working medium propulsion device 2 is communicated with the interior of the working medium bin 1, a jet orifice 7 is arranged at the top of the propulsion device 2, the jet orifice 7 is communicated with the propulsion device 2, the solar photovoltaic panel 4 is arranged outside the propulsion device 2, the number of the solar photovoltaic panels 4 is two, one end of each of the two solar photovoltaic panels 4 is connected with one end of the telescopic device 3, the accelerating channel 10 is arranged at the top of the propulsion device 2, the anode charged panel 5 is arranged at the bottom of the accelerating channel 10, a coil 6 is arranged outside the accelerating channel 10, an axial magnetic field 8 is arranged in the middle of the accelerating channel 10, an electron emission gun 9 is arranged on one side of the acceleration channel 10, electrons are stably released through a cathode of the electron emission gun 9, current formed by the electrons spirally accelerates and falls to the anode charged plate 5 under the action of an annular magnetic field, the medium in the working medium bin 1 is distributed and conveyed through the propulsion device 2, the ejected propellant working medium is snipped near the anode to ionize the working medium after violent collision, ions of the working medium of the propeller generate axial acceleration under the action of an electromagnetic field and are ejected at high speed finally to generate thrust to form plasma jet, the device can be driven to be pushed only by a small amount of xenon, the used fuel only accounts for 10% of the traditional propeller, and the device can be continuously conveyed with electric power through the solar photovoltaic panel, so that the carried fuel is reduced.
The working medium bin 1 is filled with inert gas which is xenon, the inert gas is easy to ionize, the atomic number is high, and the inert gas is also inert gas and has low corrosivity.
The jet orifices 7 are distributed at the top of the working medium propeller 2 in an annular equidistant regular shape, one end of each jet orifice 7 is located inside the accelerating channel 10, the surface of the anode live plate 5 at the bottom of the accelerating channel 10 is provided with a hole groove, the jet orifices 7 are arranged inside the hole grooves, the molded surface of each jet orifice 7 is conical or bell-shaped, the jet orifices 7 are beneficial to electron beams in high-speed annular motion, and the propellant working medium sprayed out is snipped near the anode.
The solar photovoltaic panel 4 is equipped with two, two the solar photovoltaic panel 4 is beta structure, solar photovoltaic panel 4 and electron emission rifle 9 electric connection are favorable to providing the electric energy for the device through solar photovoltaic panel 4 to be favorable to the holding device can produce the magnetic field, thereby keep power.
The inner magnetic core is arranged inside the axial magnetic field 8, a radial magnetic field is formed inside the acceleration channel 10 by the inner magnetic core and the coil inside the axial magnetic field 8, high-voltage electricity is applied to the anode charged plate 5 through a power supply device to form an axial acceleration electric field in the acceleration channel 10, and the radial magnetic field of the acceleration channel 10 is favorable for ions to generate axial acceleration.
The steps are as follows:
the method comprises the following steps: the accelerating channel stably releases electrons through the cathode of the electron emission gun 9, the current formed by the electrons spirally accelerates and falls to the anode under the action of Lorentz force of a ring-shaped magnetic field, the electrons emitted from the cathode are captured by a crossed electromagnetic field, and after being captured, the electrons can perform angular drift in a discharge area, wherein the angular drift is the result of the action of a crossed radial magnetic field and an axial electric field;
step two: the medium is conveyed, the medium in the working medium bin 1 is distributed and conveyed through the working medium propelling device 2, and the difference between the flow rate of the propellant in the region with high propellant flow rate and the flow rate of the propellant in the region with low propellant flow rate is adjusted to be 10%, so that the medium is conveyed to the channel 10 through the jet orifice 7;
step three: ionizing to form an accelerating channel of an annular discharge space so as to ionize propellant media flowing into the discharge space to generate ions, wherein the high-speed annularly moving electron beams snipe the sprayed propellant working medium near the anode and ionize the working medium after violent collision;
step four: generating thrust, wherein ions of the working medium of the propeller generate axial acceleration under the action of an electromagnetic field and are finally ejected at high speed to generate thrust to form plasma jet;
step five: the working medium ion plume is neutralized, and when the ions leave, the ions pick up electrons and neutralize the light beam, and leave the propeller in a high-speed state to form power.
And in the second step, the electric propulsion working medium in the working medium bin 1 is a simple substance or a mixture of xenon, argon, krypton, helium and hydrogen.
In the first step, the propeller accelerates ions to high speed by using electrostatic potential, the negative attraction charge is provided by the electron plasma at the opening end of the propeller, and 150-800V of electric potential is applied between the anode and the cathode of the propeller, so that the central part of the propeller forms the magnetic pole of the electromagnet.
When the device is used, electrons are stably released through a cathode of an electron emission gun 9, current formed by the electrons spirally accelerates to fall to an anode charged plate 5 under the action of an annular magnetic field, a medium in a working medium bin 1 is distributed and conveyed through a working medium propeller 2, high-speed electron beams circularly move, propellant working media sprayed from a spray opening 7 are snipped near an anode, the working media are ionized after violent collision, ions of the working medium of the propeller generate axial acceleration under the action of the electromagnetic field and are finally sprayed out at high speed to generate thrust to form plasma jet, the device can be driven to push only by a small amount of xenon, the used fuel only accounts for 10% of that of the traditional propeller, the device can be continuously conveyed with electric power through a solar photovoltaic plate 4, the carried fuel can be reduced, the solar photovoltaic plate 4 can be unfolded through a telescopic device 3, electric energy can be provided for the device through the solar photovoltaic plate 4, the device can be kept to generate the magnetic field, and power can be kept.
The invention relates to a working medium cabin 1, a working medium propeller 2, a telescopic device 3, a solar photovoltaic panel 4, an anode charged panel 5, a coil 6, a jet orifice 7, an axial magnetic field 8, an electron emission gun 9 and an acceleration channel 10, wherein the parts are all universal standard parts or parts known by technicians in the field, and the structure and the principle of the parts can be known by technicians in the field through technical manuals or conventional experimental methods.
While there have been shown and described what are at present considered the fundamental principles and essential features of the invention and its advantages, it will be apparent to those skilled in the art that the invention is not limited to the details of the foregoing exemplary embodiments, but is capable of other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (8)
1. A stress wave static working medium propulsion device is characterized in that: including working medium storehouse (1), advancing device (2), telescoping device (3), solar photovoltaic board (4), positive pole charged plate (5) and with higher speed passageway (10), working medium advancing device (2) are installed to working medium storehouse (1) one end, working medium advancing device (2) inside and working medium storehouse (1) inside intercommunication, advancing device (2) top is equipped with jet (7), jet (7) and advancing device (2) intercommunication, advancing device (2) outside is equipped with solar photovoltaic board (4), solar photovoltaic board (4) are equipped with two, two solar photovoltaic board (4) one end is connected with telescoping device (3) one end, advancing device (2) top is equipped with passageway (10) with higher speed, passageway (10) bottom is equipped with positive pole charged plate (5) with higher speed, passageway (10) outside is equipped with coil (6) with higher speed, passageway (10) middle part is equipped with axial magnetic field (8) with higher speed, passageway (10) one side is equipped with electron emission gun (9) with higher speed.
2. The stress wave static working medium propulsion device according to claim 1, characterized in that: the working medium bin (1) is filled with inert gas, and the inert gas is xenon.
3. The stress wave static working medium propulsion device according to claim 2, characterized in that: the jet orifices (7) are distributed at the top of the working medium propeller (2) in an annular equidistant regular shape, one end of each jet orifice (7) is located inside the accelerating channel (10), the surface of the anode live plate (5) at the bottom of the accelerating channel (10) is provided with a hole groove, the jet orifices (7) are arranged inside the hole grooves, and the molded surface of each jet orifice (7) is conical or bell-shaped.
4. The stress wave static working medium propulsion device and method according to claim 1, characterized in that: the solar photovoltaic panel (4) is provided with two, two the solar photovoltaic panel (4) is beta structure, solar photovoltaic panel (4) and electron emission rifle (9) electric connection.
5. The stress wave static working medium propulsion device according to claim 4, characterized in that: an inner magnetic core is arranged inside the axial magnetic field (8), a radial magnetic field is formed inside the acceleration channel (10) by the inner magnetic core and the coil inside the axial magnetic field (8), and a high-voltage electricity is applied to the anode charged plate (5) through a power supply device to form an axial acceleration electric field in the acceleration channel (10).
6. The method for propelling a stress wave static working medium according to any one of claims 1 to 5, characterized by the steps of:
the method comprises the following steps: the accelerating channel stably releases electrons through a cathode of the electron emission gun (9), current formed by the electrons spirally accelerates and falls to the anode under the action of Lorentz force of an annular magnetic field, the electrons emitted from the cathode are captured by a crossed electromagnetic field, and after the electrons are captured, the electrons are subjected to angular drift in a discharge area, and the angular drift is a result of the action of a crossed radial magnetic field and an axial electric field;
step two: the medium is conveyed, the medium in the working medium bin (1) is distributed and conveyed through the working medium propelling device (2), the difference between the flow rate of the propellant in the area with the high propellant flow rate and the flow rate of the propellant in the area with the low propellant flow rate is adjusted to be 10%, and therefore the medium is conveyed to the channel (10) through the jet orifice (7);
step three: ionizing to form an accelerating channel of the annular discharge space to ionize the propellant medium flowing into the discharge space to generate ions, sniping the sprayed propellant working medium near the anode by the electron beam in high-speed annular motion, and ionizing the working medium after violent collision;
step four: generating thrust, wherein ions of the working medium of the propeller generate axial acceleration under the action of an electromagnetic field and are finally ejected at high speed to generate thrust to form plasma jet;
step five: the working substance ion plume is neutralized, and the ions pick up electrons and neutralize the light beam when leaving, and leave the propeller in a high-speed state to form power.
7. The method for propelling the stress wave static working medium according to claim 6, wherein the method comprises the following steps: and in the second step, the electric propulsion working medium in the working medium bin (1) is a simple substance or a mixture of xenon, argon, krypton, helium and hydrogen.
8. The method for propelling the stress wave static working medium according to claim 6, wherein the method comprises the following steps: in the first step, the propeller accelerates ions to high speed by using electrostatic potential, the negative attraction charge is provided by the electron plasma at the opening end of the propeller, and 150-800V of electric potential is applied between the anode and the cathode of the propeller, so that the central part of the propeller forms the magnetic pole of the electromagnet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211112927.5A CN115571380A (en) | 2022-09-13 | 2022-09-13 | Stress wave static working medium propelling device and method |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211112927.5A CN115571380A (en) | 2022-09-13 | 2022-09-13 | Stress wave static working medium propelling device and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115571380A true CN115571380A (en) | 2023-01-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211112927.5A Pending CN115571380A (en) | 2022-09-13 | 2022-09-13 | Stress wave static working medium propelling device and method |
Country Status (1)
| Country | Link |
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| CN (1) | CN115571380A (en) |
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- 2022-09-13 CN CN202211112927.5A patent/CN115571380A/en active Pending
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