CN106904293A - A kind of geostationary satellite platform in 2~3 meters altitudes - Google Patents
A kind of geostationary satellite platform in 2~3 meters altitudes Download PDFInfo
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- CN106904293A CN106904293A CN201710125306.3A CN201710125306A CN106904293A CN 106904293 A CN106904293 A CN 106904293A CN 201710125306 A CN201710125306 A CN 201710125306A CN 106904293 A CN106904293 A CN 106904293A
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- storehouse
- magnetic valve
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- auxiliary
- platform
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
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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
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
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- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention relates to a kind of geostationary satellite platform in 2~3 meters altitudes, including main platform body, described main platform body includes the main storehouse, auxiliary storehouse and the load storehouse that are fixedly connected sequentially up and down, sheet metal of the described main storehouse, auxiliary storehouse, load storehouse by thickness less than 0.2mm is rolled into regular hexagon column, the first magnetic valve, the second magnetic valve are respectively arranged with main storehouse, auxiliary storehouse, main storehouse, auxiliary storehouse are connected external evacuator and are evacuated by the first magnetic valve, the second magnetic valve respectively, and the first magnetic valve, the second magnetic valve are electrically connected control device.Present invention employs hexagonal cylindrical and can Modularized splice main platform body, by being evacuated generation buoyancy lift on ground in advance, hover over 2~3 meters altitudes, sucking air by remote control magnetic valve carries out safe landing, and reclaim many times, possess its unique superiority and more superior cost performance, existing many homochronousness satellites can be replaced, meet the different demands of client.
Description
Technical field
The present invention relates to the Geo-synchronous flying platform in stratosphere in a kind of atmospheric thermodynamics.
Background technology
At present, the hot balloon applied both at home and abroad, fire balloon, helium balloon, hydrogen balloon, dirigible, helicopter, fixed-wing fly
The various aircraft such as machine, all in the presence of this various different degrees of potential safety hazard, and with production cost is high, technology is complicated will
Seek deficiency high.And current, aircraft is also existed cannot be in 2~3 meters altitudes in stratosphere in atmospheric thermodynamics for a long time
Hovered, multiple safety returns to defect and the problems such as bottom surface.
The concept of cheap geostationary satellite is proposed both at home and abroad.1st, 2~3 meters altitudes can be hanged in atmospheric thermodynamics stratosphere
Stop；2nd, can be kept for more than one month in same longitude, same latitude, level floating state；3rd, can many times from ground to high-altitude,
Safety is steady safely to be hovered in high-altitude, and ground, the shuttle mode that ground is reclaimed are returned to from high-altitude.
But, there is presently no the example for seeing real achievement, although in October, 2015, " number of interpreting a dream " of China is exerted oneself
The world is completed by force and is about 20 hours in the 2 meters altitudes hovering time first, during return, take and tear covering just reluctantly
Discharge helium, safe landing ground is reclaimed.Owner according to " number of interpreting a dream " claims, it is intended to same two in 2016
Carry out commercial aviation flight.But, so far, successful flight disappears again all not to receive " number of interpreting a dream " huge dirigible
Breath, it is judged that, it has 4 basic reasons to cause the plan stranded：
1st, " number of interpreting a dream " is to employ to fill helium and obtain the dirigible of main buoyancy lift, because filling helium is only flushed with hydrogen the same of gas
The buoyancy lift of the 1/4 of volume（, come to judge hydrogen be 1.0079, helium is 4.00260 for atomic weight in the periodic table of chemical element）More
It is utilized in duricrust air bag is evacuated 1/24 or so buoyancy lift.
2nd, because " number of interpreting a dream " is bulky, 10,008 kilosteres are reached, employs the multi-layer covering of costliness, therefore it is conducted oneself with dignity
Power is also huge, therefore can only produce the buoyancy lift of about half itself hovered in two meters altitudes.
3rd, second half buoyancy lift of " number of interpreting a dream ", is obtained from being produced using 6 huge electric propellers.
4th, " number of interpreting a dream " just produces main buoyancy after being filled with helium, therefore its covering is at its ground, 1/3 for being only subject to
The pressure of atmospheric pressure, but when it is raised to 2 meters altitude, its covering is but to bear 1 pressure of the atmospheric pressure for Jia 1/3
Power, so ensureing that it can impermeable be a great difficult problem in high-altitude hovering for a long time.
Can in stratosphere in atmospheric thermodynamics 2~3 meters altitudes geostationary satellite, hereinafter referred to as homochronousness satellite, its
Development prospect is immeasurable, and the various types of satellites than being currently in operation are all practical, all inexpensively, and possesses its unique superiority
More superior cost performance.
1st, homochronousness satellite is most cheap, and it is because without the expensive rocket required for all kinds of transmitting satellites to be launched
Cost, so become being dirt cheap.
2nd, homochronousness satellite, can both establish one's own system network consisting, it is also possible to after adding three current geo-stationary satellites,
Global network system can be constituted.
3rd, homochronousness satellite is all the time in certain together longitude, hovering on latitude, height, and what is be not currently in operation is various types of
The time interval blind area that the satellite of type is existed, therefore various sounding meteorological balloons can be replaced with homochronousness satellite, and as gas
As satellite and the important relay nodes of various regions meteorological observatory.Most of Beidou navigation satellite can be replaced, and as its important node, and
An accuracy for geometric progression can be mentioned, a centimetre class precision is reached, and can in the range of it non-blind area, especially in early warning management and control
Qu Shi, to various stealth targets on various skies, sea, ground, also can clearly show.Part can be replaced to communicate
Satellite, the launching tower as cheap maritime telephone, the TV for substituting various regions, as direct satellite broadcasting TV platform.Can turn into wireless
The important node of internet, mobile phone 4G, 5G network, and the transfer high ferro on the numerous and diverse various ground of current substantial amounts can be replaced
Tower, and non-blind area and big volume of passenger traffic can be easily able to.Can be as the important terminal of quantum communication, etc. and waiting for peacefully reward hair
Open up its various now also unknown various derivation function.
The content of the invention
In order to overcome deficiency of the prior art, the present invention provide one kind can in stratosphere in atmospheric thermodynamics 2~3 myriametres it is high
Aerial hovering for a long time and can free remote control on the ground, it is continuously round many times
Geostationary satellite platform.
The present invention solve its technical problem technical scheme be：
A kind of geostationary satellite platform in 2~3 meters altitudes, it is characterised in that：Including main platform body, described platform master
Body includes the main storehouse, auxiliary storehouse and the load storehouse that are fixedly connected sequentially up and down, and described main storehouse, auxiliary storehouse, load storehouse are less than by thickness
The sheet metal of 0.2mm is rolled into regular hexagon column, and the first aspirating hole, second are respectively arranged with described main storehouse, auxiliary storehouse
Aspirating hole, seals on the first described aspirating hole and sets the first magnetic valve, is sealed on the second aspirating hole and sets the second magnetic valve, institute
Main storehouse, the auxiliary storehouse stated are connected external evacuator and are evacuated by the first magnetic valve, the second magnetic valve respectively, described main storehouse
Upper end face is provided with solar panel, and battery, the Yi Jilian of electrical connection solar panel are provided with main platform body
Connect the control device of battery, described the first magnetic valve, the second magnetic valve are electrically connected described control device.
Preferably, skin-surface is coated with nanoscale graphite alkene of the thickness less than 0.04mm.
Preferably, described battery is fixedly connected between auxiliary storehouse and load storehouse, battery is set to hexagon post
Shape, battery middle setting has threeway shape jet pipe, and blower fan is respectively fixed with three pipelines of jet pipe, and described motor is electric respectively
Connection control device is provided with the first magnetic valve of control, the preferably, also include a remote control on described control device
The solenoid valve control circuit of two magnetic valves opening and closing and the wireless receiving module of connection solenoid valve control circuit, described is wireless
Receiver module receives the control signal of remote control.
Preferably, the lower end in load storehouse is fixedly connected with buffering pin.
Preferably, main platform body is connected up and down or laterally in parallel or mixing connection splicing is integral.
Main platform body is to be formed by fixedly connecting up and down by main storehouse, auxiliary storehouse, load storehouse, and main platform body can also connect up and down
Or horizontal in parallel or Hybrid connections, main storehouse, auxiliary storehouse, load storehouse are rolled into just by the sheet metal that thickness is less than 0.2mm
Hexagonal cylindrical, is coated with Graphene of the thickness less than 0.04mm outside sheet metal.
Satellite platform rises unprecedented, on ground, first passes through evacuator main storehouse, auxiliary storehouse are vacuumized respectively, is pumped into true
Sky, satellite platform global density is less than atmospheric density, produces buoyancy lift, and satellite platform rises, and uphill process is a weak deceleration
Movement locus, rises to the hovering of 2~3 meters altitudes.Load in load storehouse carries out operation.When needing to reclaim, filled by remote control
Put and opening is respectively controlled to the second magnetic valve on auxiliary storehouse, then auxiliary storehouse gradually sucks air, produce down-force, safety landing
To ground.During remote control, second magnetic valve in auxiliary storehouse can be opened, realize slow decline.In order to integrally provide electric energy to satellite,
Battery is provided between auxiliary storehouse and load storehouse, in order to adjust translation position of the satellite platform in hovering, in battery
Middle setting have a threeway shape jet pipe, connecting fan respectively in three pipelines of jet pipe then can as needed open wherein one
Individual or two blower fans, realize the translation of position or the rotation of angle.Whole satellite platform is powered by storage battery power supply, battery
Subsequent power by main storehouse upper end solar panel absorb solar energy provide.
In this satellite platform from ground uphill process, the most tranquil time window of atmosphere convection layer may be selected（Such as evening 20
O'clock to 8 o'clock of second day）.The hovering height of this satellite had both avoided busy civil aviaton 8,000~1.2 ten thousand in 2~3 meters altitudes
The air corridor of rice, also avoids the limit of the maximum height less than 2 myriametres of fixed wing aircraft, therefore be also very safe.
This satellite is ground remote control, therefore nobody is in indispensable this huge and complicated system of life support system in high-altitude
System, therefore be efficient this satellite, the inevitable outcome of low cost operation.After controlling the magnetic valve in auxiliary storehouse, main platform body will be produced down
Drop power.Ensure that the safe safety of this satellite returns to ground, return securely back to ground, and reclaim this satellite.
This satellite employs generalization, standardization, seriation, modularization this four changes design principle and is designed, and uses
Regular hexagon cylindrical shape structure ensures, can arbitrarily go here and there, in parallel, and modularization is neatly small to be combined into, in, it is greatly, huge
Various types of satellite platform is come the need for the difference for meeting various clients.
The beneficial effects of the present invention are：Present invention employs hexagonal cylindrical and can Modularized splice platform master
Body, by being evacuated generation buoyancy lift on ground in advance, hovers in 2~3 meters altitudes, is sucked by remote control magnetic valve empty
Gas carries out safe landing, and reclaims many times, possesses its unique superiority and more superior cost performance, can replace existing
Many homochronousness satellites, meet the different demands of client.
Brief description of the drawings
Fig. 1 is structural representation of the invention.
Fig. 2 is part-structure schematic diagram of the invention.
Specific embodiment
The present invention is described in further detail with reference to the accompanying drawings and detailed description.
As shown in Figure 1, 2, a kind of geostationary satellite platform in 2~3 meters altitudes, including main platform body, platform master
Body includes the main storehouse 2, auxiliary storehouse 3 and the load storehouse 4 that are fixedly connected sequentially up and down, and main storehouse, auxiliary storehouse, load storehouse are less than by thickness
The sheet metal of 0.2mm is rolled into regular hexagon column, and sheet metal surface is coated with Graphene of the thickness less than 0.04mm.It is main
The first aspirating hole, the second aspirating hole are respectively arranged with storehouse, auxiliary storehouse, are sealed on the first aspirating hole and the first magnetic valve 5, second is set
Sealed on aspirating hole and the second magnetic valve 6 is set, main storehouse, auxiliary storehouse connect external taking out by the first magnetic valve, the second magnetic valve respectively
Vacuum machine is evacuated, and main storehouse upper end face is provided with solar panel 1, is provided between auxiliary storehouse and load storehouse and electrically connected
The battery 7 of solar panel and the control device of connection battery, the first magnetic valve, the second magnetic valve are electrically connected respectively
Connect described control device.There is the jet pipe 10 of threeway shape in battery middle setting, be connected in three pipelines of jet pipe
Blower fan 11, as long as opening one or both of which blower fan, it is possible to achieve position translation or the angle rotation of satellite.
Also include a remote control, the first magnetic valve of control, the electromagnetism of the second magnetic valve opening and closing are provided with control device
The wireless receiving module of valve controling circuit and connection solenoid valve control circuit, described wireless receiving module receives remote control dress
The control signal put.The lower end for loading storehouse is fixedly connected with buffering pin 8, more firm safety when being easy to land.
Main platform body can connect up and down or laterally in parallel or mixing connection splicing is integral.
In the present invention, main platform body is to be formed by fixedly connecting about 4 by main storehouse 2, auxiliary storehouse 3, load storehouse, and main platform body is also
Can connect up and down or horizontal in parallel or Hybrid connections, the metal of main storehouse, auxiliary storehouse, load storehouse by thickness less than 0.2mm
Sheet material is rolled into regular hexagon column, and Graphene of the thickness less than 0.04mm is coated with outside sheet metal.
Satellite platform rises unprecedented, on ground, first passes through evacuator main storehouse, auxiliary storehouse are vacuumized respectively, is pumped into true
Sky, satellite platform global density is less than atmospheric density, produces buoyancy lift, and satellite platform rises, and uphill process is a weak deceleration
Movement locus, rises to the hovering of 2~3 meters altitudes.Load in load storehouse carries out operation.When needing to reclaim, filled by remote control
Put and opening is controlled to the second magnetic valve 6 on auxiliary storehouse, then auxiliary storehouse gradually sucks air, produce down-force, safety landing is real
Now it is slowly declined to ground.In order to integrally provide electric energy to satellite, battery is provided between auxiliary storehouse and load storehouse, in order to be able to
Enough, there are threeway shape jet pipe, three pipes of jet pipe in translation position of the adjustment satellite platform in hovering in the middle setting of battery
Difference connecting fan, then can as needed open wherein one or two blower fan 10 in road, realize translation or the angle of position
The rotation of degree.Whole satellite platform is powered by storage battery power supply, the subsequent power of battery by main storehouse upper end solar cell
Plate 1 absorbs solar energy and provides.
The invention has the characteristics that：
1st, with the continuous lifting of domestic and international scientific and technological level, make to be previously referred to as high-tech product, technique, be already known to market
On the common product that can buy, such as weld the ultra-thin materials of 0.2mm thickness, the Graphene of coating 0.04mm, reinforce and
Sealing technology material, the air exhauster of energy pumping high vacuum, the efficient optimal collocation of solar power generation and lithium storage battery, sealing property are complete
Beautiful magnetic valve etc., so the process materials of the application are all feasible.In the balloon of gas or helium is flushed with hydrogen, more to high-altitude,
Because air is thin, appointment produce gas leakage, and in the application due in low latitude atmospheric pressure it is larger, it is necessary to bear
Larger atmospheric pressure, and be pressurized to high-altitude and gradually reduce, it is safer on the contrary.
2nd, it is according to generally acknowledged principle in the geostationary satellite platform of 2~3 meters altitudes：In earth atmosphere circle, especially
Height is higher in stratosphere for it, and atmospheric density is smaller, when the deadweight for having individual container（Including its load）With the proportion of volume and
There is ＜=＞ in the volume weight of the air of equal height, these three situations, will show on this container, shows buoyance lift
Power, hovering, down-force these three states after the deadweight of used vessel is filled with the hydrogen or helium for filling with load, can produce floating,
Hovering, declines the addition rule that three kinds of results Jia 1 equal to 2 by appellation 1.If, after the air for pumping same amount in duricrust air bag,
Also above-mentioned three kinds of floatings, hovering, the result of decline can be produced.Also the subtraction rule axiom for subtracting 1 equal to 2 by appellation 3.It is of the invention
2~3 meters altitudes can for a long time be hovered in stratosphere in earth atmosphere circle, also can be steady, the ground round many times of safety.
Hovered to high-altitude on ground.The application this be that to apply subtraction rule be foundation.
3rd, main storehouse, auxiliary storehouse are evacuated in advance using ground evacuator to produce the main buoyancy lift of this satellite, are driven
This satellite floats to the hovering requirement specified highly.When needing it to fall back to ground, as long as the electromagnetism in auxiliary storehouse is opened in remote control
Valve, it is sucked the air around it will produce.
4th, in this satellite transit journey, the requirement of environmentally friendly highest standard no pollution zero-emission is reached.
5th, the present invention it is safer, this satellite be in process of being hovered from ground to high-altitude, because with highly it is higher, air is close
The thinner restraining factors of degree.Therefore this satellite uphill process is the motion mark of a weak deceleration.And this satellite is relied on from floating state
The magnetic valve in auxiliary storehouse sucks neighbouring air to control, and is also a weak acceleration, the movement locus of approximate uniform motion.Namely
Say will not security incident.Both made to occur in that accident in main storehouse, auxiliary storehouse, such as and when aerolite and guided missile run through, will not also produce
The possibility of combustion explosion, because not possessing three big key elements of burning.Comburant oxidizer --- --- oxygen, higher than burning-point
Temperature, also can safety drop to ground come.
6th, in this satellite from ground uphill process, the most tranquil time window of atmosphere convection layer may be selected（Such as at 20 points in evening
To 8 o'clock of second day）.The hovering height of this satellite had both avoided the myriametre of busy civil aviaton 8,000~1.2 in 2~3 meters altitudes
Air corridor, also avoid the limit of the maximum height less than 2 myriametres of fixed wing aircraft, therefore be also very safe.
7th, because the covering in main storehouse 2 and auxiliary storehouse 3 is welded using 0.2 millimeter of sheet metal.Coat again less than 0.04
Nano material --- --- Graphene of millimeter, therefore its covering only has 0.24 mm of thickness, this guarantees main storehouse 2, auxiliary storehouse 3 from
Weight, reaches the most light limit, and obtains the buoyancy lift of maximum, and ensure that structural strength.
8th, this satellite is ground remote control, therefore nobody is in indispensable this huge and complicated system of life support system in high-altitude
System, therefore be efficient this satellite, the inevitable outcome of low cost operation.Down-force will be produced.Ensure that the safe safety of this satellite is returned to
Ground, returns securely back to ground, and reclaim this satellite.
9th, there can be enough electric energy can use to ensure this satellite, can use the general of ground at ground, before rising
Charging Chinese toon, battery sufficient electrical energy, when this satellite is raised to 2~3 meters altitudes and hovers, the sun generate electricity and can during the day,
The electric energy of maximum can most be obtained.
10th, in order to ensure the effect of the slight hysteresis quality that this satellite is produced in earth rotation, thus employ three it is small-sized
Assembling finely tunes the position of the displacement of this satellite in diverse location.
11st, because main platform body uses hexagonal body, this satellite can in any combination, series, parallel or connection in series-parallel
Mode.
This satellite employs generalization, standardization, seriation, modularization this four changes design principle and is designed, and uses
Regular hexagon cylindrical shape structure ensures, can arbitrarily go here and there, in parallel, and unitization is neatly small to be combined into, in, it is greatly, huge
Various types of satellite platform is come the need for the difference for meeting various clients.
Present invention employs hexagonal cylindrical and can Modularized splice main platform body, by being pumped into very on ground in advance
Sky produces buoyancy lift, hovers in 2~3 meters altitudes, and sucking air by remote control magnetic valve carries out safe landing, and countless
Secondary recovery, possesses its unique superiority and more superior cost performance, can replace existing many homochronousness satellites, meets client
Different demands.
Claims (6)
1. a kind of geostationary satellite platform in 2~3 meters altitudes, it is characterised in that：Including main platform body, described platform
Main body includes the main storehouse, auxiliary storehouse and the load storehouse that are fixedly connected sequentially up and down, and described main storehouse, auxiliary storehouse, load storehouse are small by thickness
Regular hexagon column is rolled into the sheet metal of 0.2mm, the first aspirating hole, are respectively arranged with described main storehouse, auxiliary storehouse
Two aspirating holes, seal on the first described aspirating hole and set the first magnetic valve, are sealed on the second aspirating hole and set the second magnetic valve,
Described main storehouse, auxiliary storehouse is connected external evacuator and is evacuated by the first magnetic valve, the second magnetic valve respectively, described master
Storehouse upper end face is provided with solar panel, be provided with main platform body electrical connection solar panel battery and
The control device of battery is connected, described the first magnetic valve, the second magnetic valve are electrically connected described control device.
2. a kind of geostationary satellite platform in 2~3 meters altitudes according to claim 1, it is characterised in that：It is described
Sheet metal surface be coated with thickness less than 0.04mm nanoscale graphite alkene.
3. a kind of geostationary satellite platform in 2~3 meters altitudes according to claim 2, it is characterised in that：It is described
Battery be fixedly connected on auxiliary storehouse and load storehouse between, battery is set to hexagonal cylindrical, and battery middle setting has three
Logical shape jet pipe, blower fan is respectively fixed with three pipelines of jet pipe, and described motor is electrically connected control device.
4. a kind of geostationary satellite platform in 2~3 meters altitudes according to claim 3, it is characterised in that：Also wrap
A remote control is included, the first magnetic valve of control, the solenoid valve control of the second magnetic valve opening and closing are provided with described control device
The wireless receiving module of circuit and connection solenoid valve control circuit, described wireless receiving module receives the control of remote control
Signal processed.
5. a kind of geostationary satellite platform in 2~3 meters altitudes according to claim 4, it is characterised in that：It is described
The lower end in load storehouse be fixedly connected with buffering pin.
6. a kind of geostationary satellite platform in 2~3 meters altitudes according to claim 5, it is characterised in that：It is described
Main platform body connect up and down or laterally in parallel or mixing connection splicing is integral.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710125306.3A CN106904293A (en) | 2017-03-04 | 2017-03-04 | A kind of geostationary satellite platform in 2~3 meters altitudes |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710125306.3A CN106904293A (en) | 2017-03-04 | 2017-03-04 | A kind of geostationary satellite platform in 2~3 meters altitudes |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110572118A (en) * | 2019-07-30 | 2019-12-13 | 中国科学院光电研究院 | circulating energy power supply system suitable for high-altitude balloon |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US20110127382A1 (en) * | 2009-12-01 | 2011-06-02 | Im Sunstar | Sky/space elevators |
| CN202389603U (en) * | 2011-11-25 | 2012-08-22 | 马建兵 | Multifunctional near-earth space station |
| CN202966650U (en) * | 2012-10-10 | 2013-06-05 | 杨贻方 | Vacuum airship |
| CN105383677A (en) * | 2015-11-24 | 2016-03-09 | 郭鹏 | Long-acting vacuum chamber satellite |
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2017
- 2017-03-04 CN CN201710125306.3A patent/CN106904293A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110127382A1 (en) * | 2009-12-01 | 2011-06-02 | Im Sunstar | Sky/space elevators |
| CN202389603U (en) * | 2011-11-25 | 2012-08-22 | 马建兵 | Multifunctional near-earth space station |
| CN202966650U (en) * | 2012-10-10 | 2013-06-05 | 杨贻方 | Vacuum airship |
| CN105383677A (en) * | 2015-11-24 | 2016-03-09 | 郭鹏 | Long-acting vacuum chamber satellite |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110572118A (en) * | 2019-07-30 | 2019-12-13 | 中国科学院光电研究院 | circulating energy power supply system suitable for high-altitude balloon |
| CN110572118B (en) * | 2019-07-30 | 2021-10-29 | 中国科学院光电研究院 | Circulating energy power supply system suitable for high-altitude balloon |
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