CN206302215U - Near space aerostatics and its energy resource system - Google Patents
Near space aerostatics and its energy resource system Download PDFInfo
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- CN206302215U CN206302215U CN201621448589.2U CN201621448589U CN206302215U CN 206302215 U CN206302215 U CN 206302215U CN 201621448589 U CN201621448589 U CN 201621448589U CN 206302215 U CN206302215 U CN 206302215U
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- 238000006243 chemical reaction Methods 0.000 claims abstract description 44
- 238000004146 energy storage Methods 0.000 claims description 48
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- 239000002775 capsule Substances 0.000 claims description 2
- 230000005540 biological transmission Effects 0.000 description 13
- 238000010586 diagram Methods 0.000 description 11
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- 230000002411 adverse Effects 0.000 description 2
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Abstract
The utility model discloses a kind of near space aerostatics and its energy resource system.Wherein, near space aerostatics includes：Utricule and the gondola being articulated in below utricule, are provided with electrical equipment at the top of the inside of gondola and/or the outside of gondola and/or utricule, energy resource system is provided with the top of the inside of gondola and/or utricule, wherein, energy resource system includes：Supply unit, for exporting the first electric energy；First conversion equipment, is connected with supply unit, for the first electric energy to be converted into the first electromagnetic wave；First dispensing device, is connected with the first conversion equipment, for sending the first electromagnetic wave to electrical equipment, wherein, the first electromagnetic wave is converted to the first electric energy by electrical equipment.The energy resource system that the utility model solves near space aerostatics of the prior art occurs the technical problem of the phenomenon of cable winds by cable for electrical equipment is powered, easily.
Description
Technical field
The utility model is related near space aerostatics field, in particular to a kind of near space aerostatics and its
Energy resource system.
Background technology
The energy resource system of existing near space aerostatics is used by the every electronic instrument in conductor cable and inside, motor etc.
Electric equipment is connected, to realize the purpose of power supply.Including the connection of electrical equipment in energy resource system and gondola, energy resource system with
Connection of utricule top electrical equipment etc..Because aerostatics electrical equipment species and number are various, numerous and diverse power cable is easy
Appearance such as knots, mutually tangles at the situation, increases the confusion degree and danger coefficient of system entirety.Additionally, when using in gondola
When energy resource system is powered to the electrical appliance at the top of utricule, because near space aerostatics average physique is huge, this cable length
More than 50 meters fly away larger adverse effect can be let near space aerostatics.
For near space aerostatics of the prior art energy resource system by cable for electrical equipment is powered, easily go out
The problem of the phenomenon of existing cable winds, not yet proposes effective solution at present.
Utility model content
The utility model embodiment provides a kind of near space aerostatics and its energy resource system, at least to solve existing skill
The energy resource system of the near space aerostatics in art occurs the phenomenon of cable winds by cable for electrical equipment is powered, easily
Technical problem.
According to the one side of the utility model embodiment, there is provided a kind of energy resource system of near space aerostatics, bag
Include：Near space aerostatics includes：Utricule and the gondola being articulated in below utricule, the inside of gondola and/or the outside of gondola and/
Or electrical equipment is provided with the top of utricule, energy resource system is provided with the top of the inside of gondola and/or utricule, wherein, the energy
System includes：Supply unit, for exporting the first electric energy；First conversion equipment, is connected with supply unit, for by the first electric energy
Be converted to the first electromagnetic wave；First dispensing device, is connected with the first conversion equipment, is set for sending the first electromagnetic wave to electricity consumption
It is standby, wherein, the first electromagnetic wave is converted to the first electric energy by electrical equipment.
Further, supply unit includes：Energy-storage battery module and solar module, energy-storage battery module are arranged on
The inside of gondola, solar module is arranged on the top of utricule.
Further, solar module includes：Solar cell, for output current；Controller for solar, and too
Positive energy battery connection, for being modulated to electric current, obtains the first electric energy.
Further, solar module also includes：Second conversion equipment, is connected with controller for solar, for inciting somebody to action
First electric energy is converted to the second electromagnetic wave；Second dispensing device, is connected with the second conversion equipment, for sending the second electromagnetic wave.
Further, energy-storage battery module includes：Reception device, for receiving the second electromagnetic wave；3rd conversion equipment, with
Reception device is connected, for the second electromagnetic wave to be converted into the first electric energy；Energy-storage battery, is connected with the 3rd conversion equipment, is used for
Store the first electric energy.
According to the another aspect of the utility model embodiment, a kind of near space aerostatics is additionally provided, including：Close on sky
Between aerostatics include：Utricule and the gondola being articulated in below utricule, wherein, near space aerostatics also includes：Claim 1 to
The energy resource system of the near space aerostatics of any one in 5, is arranged at the inside of gondola and/or the top of utricule, for inciting somebody to action
Electric energy is converted to electromagnetic wave；Electrical equipment, has correspondence with the energy resource system of near space aerostatics, is arranged at gondola
The outside and/or the top of utricule of internal and/or gondola, for converting electromagnetic waves into electric energy.
Further, electrical equipment includes：First receiving device, the energy resource system for receiving near space aerostatics is sent out
The electromagnetic wave for sending；First conversion equipment, is connected with reception device, for converting electromagnetic waves into electric energy；Electricity consumption instrument, with first
Conversion equipment is connected.
Further, electrical equipment is arranged at the inside of gondola and/or the top of utricule.
Further, electrical equipment includes：Second reception device, the energy resource system for receiving near space aerostatics is sent out
The electromagnetic wave for sending；Second conversion equipment, is connected with reception device, for converting electromagnetic waves into electric energy；Motor, with the second conversion
Device is connected.
Further, electrical equipment is arranged at the outside of gondola.
In the utility model embodiment, the energy resource system of near space aerostatics can include：Supply unit, first turn
Changing device and the first dispensing device, supply unit output the first electric energy to the first conversion equipment, the first conversion equipment are electric by first
The first electromagnetic wave can be converted into, and be radiated the first electromagnetic wave outside to electrical equipment by the first dispensing device, electrical equipment will
First electromagnetic wave is converted to the first electric energy, so as to realize the wireless power transmission between energy resource system and electrical equipment, eliminates energy
Power cable between origin system and each electrical equipment, solves the energy resource system of near space aerostatics of the prior art
By cable for electrical equipment is powered, easily there is the technical problem of the phenomenon of cable winds.Therefore, by the utility model
The scheme of embodiment offer is provided, can be reached and be improve the overall security of near space aerostatics, improve near space floating
Device let fly away or Mission Success rate effect.
Brief description of the drawings
Accompanying drawing described herein is used for providing being further understood to of the present utility model, constitutes the part of the application,
Schematic description and description of the present utility model is used to explain the utility model, does not constitute to of the present utility model improper
Limit.In the accompanying drawings：
Fig. 1 is a kind of schematic diagram of the energy resource system of the near space aerostatics according to the utility model embodiment；
Fig. 2 is the solar module and energy storage electricity of a kind of near space aerostatics according to the utility model embodiment
The schematic diagram of the wireless power transmission of pond module；
Fig. 3 is a kind of schematic diagram of the near space aerostatics according to the utility model embodiment；
Fig. 4 is the schematic diagram of a kind of optional near space aerostatics according to the utility model embodiment；And
Fig. 5 is the schematic diagram of the optional near space aerostatics of another kind according to the utility model embodiment.
Wherein, above-mentioned accompanying drawing is marked including the following drawings：
21st, solar cell；23rd, controller for solar；25th, wireless power transmitter；27th, radio energy receiver；29、
Energy-storage battery；51st, gondola；53rd, utricule；55th, energy module；57th, electrical equipment module.
Specific embodiment
In order that those skilled in the art more fully understand the utility model scheme, below in conjunction with the utility model reality
The accompanying drawing in example is applied, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described
Embodiment is only the embodiment of the utility model part, rather than whole embodiments.Based on the reality in the utility model
Example is applied, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made all should
When the scope for belonging to the utility model protection.
It should be noted that term " first " in specification and claims of the present utility model and above-mentioned accompanying drawing,
" second " etc. is for distinguishing similar object, without for describing specific order or precedence.It should be appreciated that so
The data for using can be exchanged in the appropriate case, so that embodiment of the present utility model described herein can be with except at this
In diagram or description those beyond order implement.Additionally, term " comprising " and " having " and their any deformation, meaning
Figure is that covering is non-exclusive to be included, for example, contain a series of system of units, product or equipment to be not necessarily limited to clearly arrange
Those units for going out, but may include other units do not list clearly or intrinsic for these products or equipment.
First, description below is carried out to the technical term occurred in the utility model embodiment：
Near space：Near space typically refers to the spatial domain at the km of earth's surface 20~100, spatial domain below we lead to
Frequently referred to " sky ", the spatial domain above it is exactly " space " that we say usually.Near space region includes：Atmospheric advection layer
Most of region of (12~50 kms of height), middle atmosphere region (50~80 kms of height) and partial ionization layer region
(60~100 kms of height).
Near space aerostatics：Aerostatics refers to aircraft that proportion is lighter than air, being gone up to the air by atmospheric buoyancy force, can be with
It is divided into captive balloon and dirigible, near space aerostatics refers to can be with long-term suspension in the aerostatics of near space.
Embodiment 1
According to the utility model embodiment, there is provided a kind of embodiment of the energy resource system of near space aerostatics.
Optionally, near space aerostatics includes：Utricule and the gondola being articulated in below utricule, the inside of gondola and/or
Electrical equipment is provided with the top of the outside of gondola and/or utricule, energy system is provided with the top of the inside of gondola and/or utricule
System.
Specifically, near space aerostatics can include a spherical utricule, it is filled with for bringing aerostatics in utricule
The gas of buoyancy, is mounted with a gondola below utricule, be provided near space aerostatics various electronic instruments and
Motor, electronic instrument can be arranged in gondola as needed, it is also possible to which, installed in utricule top, motor may be mounted at utricule
Top, it is also possible to outside gondola, it is ensured that near space aerostatics is suspended near space.
Fig. 1 is a kind of schematic diagram of the energy resource system of the near space aerostatics according to the utility model embodiment, such as Fig. 1
Shown, the energy resource system includes：
Supply unit 11, for exporting the first electric energy.
Specifically, above-mentioned supply unit 11 can be mounted in the energy-storage battery module in gondola, or it is arranged on
Solar module around utricule top.
First conversion equipment 13, is connected with supply unit 11, for the first electric energy to be converted into the first electromagnetic wave.
Specifically, the first above-mentioned conversion equipment 13 can be the radio energy change-over circuit in wireless power transmitter,
Radio energy change-over circuit can be made up of oscillator and power amplifier.
First dispensing device 15, is connected with the first conversion equipment 13, for sending the first electromagnetic wave to electrical equipment, its
In, the first electromagnetic wave is converted to the first electric energy by electrical equipment.
Specifically, the first above-mentioned dispensing device 15 can be the radio energy transmitting antenna in wireless power transmitter.
In a kind of optional scheme, energy resource system can (including radio energy turns by power supply and wireless power transmitter
Change circuit and radio energy transmitting antenna) constitute, it is when the electrical equipment installed near space aerostatics is powered in power supply
Wait, the electric energy that power supply is exported can be converted into electromagnetic wave outside radiation by wireless power transmitter, and electrical equipment is receiving energy
After the electromagnetic wave that origin system sends, electromagnetic wave can be converted into electric energy, complete power supply process.
According to the utility model above-described embodiment, the energy resource system of near space aerostatics can include：Supply unit 11,
First conversion equipment 13 and the first dispensing device 15, supply unit 11 export the first electric energy to the first conversion equipment 13, first turn
First electric energy is converted into the first electromagnetic wave by changing device 13, and is radiated the first electromagnetic wave outside to use by the first dispensing device 15
First electromagnetic wave is converted to the first electric energy by electric equipment, electrical equipment, wireless between energy resource system and electrical equipment so as to realize
Electric energy is transmitted, and eliminates the power cable between energy resource system and each electrical equipment, is solved and of the prior art is closed on sky
Between the energy resource system of aerostatics occur the technical problem of the phenomenon of cable winds for electrical equipment is powered, easily by cable.Cause
This, the scheme provided by the utility model above-described embodiment can reach and improve the overall safety of near space aerostatics
Property, improve near space aerostatics let fly away or Mission Success rate effect.
Optionally, in the utility model above-described embodiment, supply unit 11 includes：Energy-storage battery module and solar-electricity
Pond module, energy-storage battery module is arranged on the inside of gondola, and solar module is arranged on the top of utricule.
Specifically, above-mentioned energy-storage battery module can be high-energy-density energy-storage battery module.
In a kind of optional scheme, solar module and high-energy-density can be carried near space aerostatics
Energy-storage battery module, solar module is lies generally adjacent to the utricule top of space aerostatics, high-energy-density energy storage electricity
Pond module is lies generally adjacent to inside the gondola of space aerostatics.When daylight intensity is stronger, near space aerostatics
The solar module of installation can directly be powered by wireless power transmitter to each electrical equipment, and illumination was strong on that night
When degree is weaker, the high-energy-density energy-storage battery module installed near space aerostatics can also be by wireless power transmitter
Directly powered to each electrical equipment.
Optionally, in the utility model above-described embodiment, solar module includes：
Solar cell, for output current.
Controller for solar, is connected with solar cell, for being modulated to electric current, obtains the first electric energy.
In a kind of optional scheme, the solar module installed near space aerostatics can include multiple too
Positive energy battery, and the controller for solar being connected with each solar cell, when daylight intensity is stronger, near space
On aerostatics install multiple solar cells produce electric current, the electric current for collecting by the same modulation of controller for solar, then via
Wireless power transmitter is converted into electromagnetic wave, and to external radiation.
Optionally, in the utility model above-described embodiment, solar module also includes：
Second conversion equipment, is connected with controller for solar, for the first electric energy to be converted into the second electromagnetic wave.
Specifically, during the second above-mentioned conversion equipment can be the wireless power transmitter installed in solar module
Radio energy change-over circuit, radio energy change-over circuit can be made up of oscillator and power amplifier.
Second dispensing device, is connected with the second conversion equipment, for sending the second electromagnetic wave.
Specifically, during the second above-mentioned dispensing device can be the wireless power transmitter installed in solar module
Radio energy transmitting antenna.
In a kind of optional scheme, the solar module installed near space aerostatics can also export electric energy
It is energy-storage battery module for power supply, solar module can include multiple solar cells, is connected with each solar cell
Controller for solar, the wireless power transmitter being connected with controller for solar, when daylight intensity is stronger, closes on sky
Between multiple solar cells for installing on aerostatics produce electric current, the electric current for collecting is by the same modulation of controller for solar, then passes through
Electromagnetic wave is converted into by wireless power transmitter, and high-energy-density energy-storage battery module is given to external radiation.
Optionally, in the utility model above-described embodiment, energy-storage battery module includes：
Reception device, for receiving the second electromagnetic wave.
Specifically, above-mentioned reception device can be wireless in the radio energy receiver installed in energy-storage battery module
Electric energy reception antenna.
3rd conversion equipment, is connected with reception device, for the second electromagnetic wave to be converted into the first electric energy.
Specifically, during the 3rd above-mentioned conversion equipment can be the radio energy receiver installed in energy-storage battery module
Radio energy change-over circuit, radio energy change-over circuit can be made up of oscillator and power amplifier.
Energy-storage battery, is connected with the 3rd conversion equipment, for storing the first electric energy.
Specifically, above-mentioned energy-storage battery can be high-energy-density energy-storage battery.
In a kind of optional scheme, energy-storage battery module can include radio energy receiver and high-energy-density energy storage
Battery, when daylight intensity is stronger, the multiple solar cells installed near space aerostatics produce electric current, collect
Electric current is by the same modulation of controller for solar, then is converted into electromagnetic wave via wireless power transmitter, and to external radiation to high energy
Metric density energy-storage battery module, high-energy-density energy-storage battery module is turned by the electromagnetic wave that radio energy receiver is launched
Change electric energy into, then power storage is entered in energy-storage battery.
Herein it should be noted that being all equipped with solar array on many near space aerostatics of the prior art
With high-energy-density energy-storage battery, the former is usually located at aerostatics utricule top, and the latter is usually located inside gondola, between the two
Electric energy transmission cable length easily winding accident will occur more than 40 meters during letting fly away, cause to let failure fly away or task is lost
Lose.
Fig. 2 is the solar module and energy storage electricity of a kind of near space aerostatics according to the utility model embodiment
The schematic diagram of the wireless power transmission of pond module, as shown in Fig. 2 the system is by solar module, energy-storage battery module group
Into solar module includes solar cell 21, controller for solar 23, wireless power transmitter 25；Energy-storage battery mould
Block includes energy-storage battery 29, radio energy receiver 27.When daylight intensity is stronger, the solar energy of near space aerostatics
Battery 21 produces electric current, and the electric current for collecting is by the uniform modulation of controller for solar 23, then is changed via wireless power transmitter 25
Into electromagnetic wave, and to external radiation；Energy-storage battery module is converted into electricity by the electromagnetic wave that radio energy receiver 27 is launched
Can, then power storage is entered in energy-storage battery 29.
By such scheme, there is provided the radio energy transmission system between a kind of solar energy and energy-storage battery, solar energy is allowed
The electric current that cell power generation is produced is transmitted to energy-storage battery in the form of an electromagnetic wave, such that it is able to cancel transmission cable, is solved existing
Have between the solar module in technology and energy-storage battery module and connected by transmission cable, near space vehicle
Let the problem of larger adverse effect fly away.And once and for all solves difficult wiring, winding that each cable is likely to occur etc.
Problem, substantially increases the overall security of aircraft.
Embodiment 2
According to the utility model embodiment, there is provided a kind of embodiment of near space aerostatics.
Optionally, near space aerostatics includes：Utricule and the gondola being articulated in below utricule.
Specifically, near space aerostatics can include a spherical utricule, it is filled with for bringing aerostatics in utricule
The gas of buoyancy, is mounted with a gondola below utricule, be provided near space aerostatics various electronic instruments and
Motor, electronic instrument can be arranged in gondola as needed, it is also possible to which, installed in utricule top, motor may be mounted at utricule
Top, it is also possible to outside gondola, it is ensured that near space aerostatics is suspended near space.
Fig. 3 is a kind of schematic diagram of the near space aerostatics according to the utility model embodiment, as shown in figure 3, this faces
Near space aerostatics includes：
The energy resource system 31 of the near space aerostatics of any one in embodiment 1, is arranged inside and/or the capsule of gondola
The top of body, for converting electrical energy into electromagnetic wave.
Electrical equipment 33, has correspondence with the energy resource system 31 of near space aerostatics, is arranged at the inside of gondola
And/or the outside and/or the top of utricule of gondola, for converting electromagnetic waves into electric energy.
Specifically, between energy resource system 31 and electrical equipment 33 electric energy can be transmitted by electromagnetic wave.
Energy resource system 31 and electrical equipment 33, energy can be installed in a kind of optional scheme, near space aerostatics
Origin system 31 can include the solar module on the utricule top for being mounted adjacent to space aerostatics and be mounted adjacent to sky
Between aerostatics gondola inside energy-storage battery module, electrical equipment 33 can include being mounted adjacent to the gondola of space aerostatics
Internal electricity consumption instrument, the electricity consumption instrument being mounted adjacent at the top of the utricule of space aerostatics and is mounted adjacent to space floating
Motor outside the gondola of device.Energy resource system 31 can be changed the electric energy needed for electrical equipment 33 by wireless power transmitter
Into electromagnetic wave outside radiation, the electromagnetic wave conversion that electrical equipment 33 can be sent energy resource system 31 by radio energy receiver
Into electric energy, so as to realize the wireless power transmission between power supply and electrical equipment.
According to the utility model above-described embodiment, near space aerostatics can include：Energy resource system 31 and electrical equipment
33, the electric energy of output can be converted to electromagnetic wave and be sent to electrical equipment 33 by energy resource system 31, and electrical equipment 33 will can connect
The electromagnetic wave for receiving is converted to electric energy, so as to realize the wireless power transmission between energy resource system and electrical equipment, eliminates the energy
Power cable between system and each electrical equipment, the energy resource system for solving near space aerostatics of the prior art leads to
Cross the technical problem that cable occurs the phenomenon of cable winds for electrical equipment is powered, easily.Therefore, it is above-mentioned by the utility model
The scheme that embodiment is provided, can reach and improve the overall security of near space aerostatics, improve near space aerostatics
Let fly away or Mission Success rate effect.
Optionally, in the utility model above-described embodiment, electrical equipment 33 includes：
First receiving device, the electromagnetic wave that the energy resource system 31 for receiving near space aerostatics sends.
Specifically, above-mentioned first receiving device can be the nothing in the radio energy receiver of installation in electrical equipment 33
Line electric energy reception antenna.
First conversion equipment, is connected with reception device, for converting electromagnetic waves into electric energy.
Specifically, the first above-mentioned conversion equipment can be the nothing in the radio energy receiver of installation in electrical equipment 33
Line electrical energy conversion circuit, radio energy change-over circuit can be made up of oscillator and power amplifier.
Electricity consumption instrument, is connected with the first conversion equipment.
Optionally, in the utility model above-described embodiment, electrical equipment 33 is arranged inside and/or the utricule of gondola
Top.
In a kind of optional scheme, energy resource system 31 and electrical equipment are provided with the gondola of near space aerostatics
33, energy resource system 31 can include energy-storage battery module and wireless power transmitter, and electrical equipment 33 can include radio energy
Receiver and electricity consumption instrument.When energy-storage battery module in gondola is powered to electricity consumption instrument, can be by wireless power transmitter
Electric energy needed for electrical equipment 33 is converted into electromagnetic wave outside radiation, electricity consumption instrument can be by radio energy receiver by electricity
The electromagnetic wave that source sends is converted into electric energy, so as to realize the wireless power transmission between energy resource system and electrical equipment.
In another optional scheme, energy resource system 31, near space are provided with the gondola of near space aerostatics
The utricule top of aerostatics is provided with electrical equipment 33, and energy resource system 31 can include that energy-storage battery module and radio energy are launched
Device, electrical equipment 33 can include radio energy receiver and electricity consumption instrument.Energy-storage battery module in gondola is to electricity consumption instrument
During power supply, the electric energy needed for electrical equipment 33 can be converted into by electromagnetic wave outside by wireless power transmitter and radiated, electricity consumption
The electromagnetic wave that power supply sends can be converted into electric energy by instrument by radio energy receiver, so as to realize energy resource system and electricity consumption
The wireless power transmission of equipment room.
Optionally, in the utility model above-described embodiment, electrical equipment 33 includes：
Second reception device, the electromagnetic wave that the energy resource system 31 for receiving near space aerostatics sends.
Specifically, the second above-mentioned reception device can be the nothing in the radio energy receiver of installation in electrical equipment 33
Line electric energy reception antenna.
Second conversion equipment, is connected with reception device, for converting electromagnetic waves into electric energy.
Specifically, the second above-mentioned conversion equipment can be the nothing in the radio energy receiver of installation in electrical equipment 33
Line electrical energy conversion circuit, radio energy change-over circuit can be made up of oscillator and power amplifier.
Motor, is connected with the second conversion equipment.
Optionally, in the utility model above-described embodiment, electrical equipment 33 is arranged at the outside of gondola.
In a kind of optional scheme, energy resource system 31 is provided with the gondola of near space aerostatics, near space is floated
Electrical equipment 33 is provided with outside the gondola of pocket, energy resource system 31 can include energy-storage battery module and wireless power transmitter,
Electrical equipment 33 can include radio energy receiver and motor.When energy-storage battery module in gondola is powered to motor, can be with
The electric energy needed for electrical equipment 33 is converted into electromagnetic wave outside by wireless power transmitter to radiate, motor can be by wireless
The electromagnetic wave that power supply sends is converted into electric energy by electric energy receiver, so as to realize the radio energy between energy resource system and electrical equipment
Transmission.
Fig. 4 is the schematic diagram of a kind of optional near space aerostatics according to the utility model embodiment, with energy system
As a example by system and electrical equipment are arranged in the gondola of near space aerostatics, a kind of preferred embodiment of the utility model is entered
Row is described in detail, as shown in figure 4, including energy module, each electrical equipment module etc. in the gondola of near space aerostatics.Its
Middle energy module includes power supply 41, wireless power transmitter 25；Electrical equipment module includes electrical equipment 33, and radio energy is received
Device 27, when the power supply 41 in gondola is powered to electrical equipment 33, by wireless power transmitter 25 by needed for electrical equipment 33
Electric energy is converted into electromagnetic wave outside radiation, and electrical equipment 33 is turned by the electromagnetic wave that radio energy receiver 27 sends power supply 41
Electric energy is changed into, so as to realize the wireless power transmission between power supply 41 and electrical equipment 33.
Fig. 5 is the schematic diagram of the optional near space aerostatics of another kind according to the utility model embodiment, with the energy
System and it is layer adjacent in the gondola of space aerostatics, the utricule top that electrical equipment is layer adjacent to space aerostatics is
Example, is described in detail, as shown in figure 5, the gondola 51 of near space aerostatics to a kind of preferred embodiment of the utility model
Inside include energy module 55, the top of utricule 53 includes each electrical equipment module 57.Wherein, energy module 55 includes power supply,
Wireless power transmitter；Electrical equipment module 57 includes electrical equipment, and radio energy receiver, the power supply in gondola sets to electricity consumption
During available electricity, the electric energy needed for electrical equipment is converted into by electromagnetic wave outside by wireless power transmitter and is radiated, electrical equipment
The electromagnetic wave that power supply sends is converted into by electric energy by radio energy receiver, it is wireless between power supply and electrical equipment so as to realize
Electric energy is transmitted.
By such scheme, by being wirelessly transferred for electric energy, energy resource system and each use near space vehicle are eliminated
Power cable between electric equipment, including 1 service cable from proximity space aerostatics utricule top-to-bottom gondola, a labor is forever
The problems such as difficult wiring, winding that each cable is likely to occur is solved to ease, simultaneously as not using power cable and reducing whole
The quality of individual aerostatics, substantially increases the overall security of aircraft.
Herein also, it should be noted that electric energy is spread to surrounding by the form of electromagnetic wave, what electrical equipment was received
Electric energy is portion of energy, and the energy not received is melt into air with electromagnetic wave.Therefore electric energy must be reduced wirelessly to pass
The defeated proportion of goods damageds.
Above-mentioned the utility model embodiment sequence number is for illustration only, and the quality of embodiment is not represented.
In above-described embodiment of the present utility model, the description to each embodiment all emphasizes particularly on different fields, in certain embodiment
Without the part described in detail, the associated description of other embodiment is may refer to.
The above is only preferred embodiment of the present utility model, it is noted that for the ordinary skill people of the art
For member, on the premise of the utility model principle is not departed from, some improvements and modifications can also be made, these improvements and modifications
Also should be regarded as protection domain of the present utility model.
Claims (10)
1. a kind of energy resource system of near space aerostatics, it is characterised in that the near space aerostatics includes：Utricule and extension
The gondola below the utricule is connected on, is set at the top of the outside and/or the utricule of the inside of the gondola and/or the gondola
Electrical equipment is equipped with, the energy resource system is provided with the top of the inside of the gondola and/or the utricule, wherein, the energy
Origin system includes：
Supply unit, for exporting the first electric energy；
First conversion equipment, is connected with the supply unit, for first electric energy to be converted into the first electromagnetic wave；
First dispensing device, is connected with first conversion equipment, for sending first electromagnetic wave to the electrical equipment,
Wherein, first electromagnetic wave is converted to first electric energy by the electrical equipment.
2. system according to claim 1, it is characterised in that the supply unit includes：Energy-storage battery module and the sun
Energy battery module, the energy-storage battery module is arranged on the inside of the gondola, and the solar module is arranged on described
The top of utricule.
3. system according to claim 2, it is characterised in that the solar module includes：
Solar cell, for output current；
Controller for solar, is connected with the solar cell, for being modulated to the electric current, obtains first electricity
Energy.
4. system according to claim 3, it is characterised in that the solar module also includes：
Second conversion equipment, is connected with the controller for solar, for first electric energy to be converted into the second electromagnetic wave；
Second dispensing device, is connected with second conversion equipment, for sending second electromagnetic wave.
5. system according to claim 4, it is characterised in that the energy-storage battery module includes：
Reception device, for receiving second electromagnetic wave；
3rd conversion equipment, is connected with the reception device, for second electromagnetic wave to be converted into first electric energy；
Energy-storage battery, is connected with the 3rd conversion equipment, for storing first electric energy.
6. a kind of near space aerostatics, it is characterised in that the near space aerostatics includes：Utricule and it is articulated in the capsule
Gondola below body, wherein, the near space aerostatics also includes：
The energy resource system of the near space aerostatics in claim 1 to 5 described in any one, is arranged at the inside of the gondola
And/or the top of the utricule, for converting electrical energy into electromagnetic wave；
Electrical equipment, has correspondence with the energy resource system of the near space aerostatics, is arranged at the inside of the gondola
And/or the outside and/or the top of the utricule of the gondola, for the electromagnetic wave to be converted into the electric energy.
7. near space aerostatics according to claim 6, it is characterised in that the electrical equipment includes：
First receiving device, the electromagnetic wave that the energy resource system for receiving near space aerostatics sends；
First conversion equipment, is connected with the reception device, for the electromagnetic wave to be converted into the electric energy；
Electricity consumption instrument, is connected with first conversion equipment.
8. near space aerostatics according to claim 7, it is characterised in that the electrical equipment is arranged at the gondola
Inside and/or the utricule top.
9. near space aerostatics according to claim 6, it is characterised in that the electrical equipment includes：
Second reception device, the electromagnetic wave that the energy resource system for receiving near space aerostatics sends；
Second conversion equipment, is connected with the reception device, for the electromagnetic wave to be converted into the electric energy；
Motor, is connected with second conversion equipment.
10. near space aerostatics according to claim 9, it is characterised in that the electrical equipment is arranged at described hanging
The outside in cabin.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201621448589.2U CN206302215U (en) | 2016-12-27 | 2016-12-27 | Near space aerostatics and its energy resource system |
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| CN201621448589.2U CN206302215U (en) | 2016-12-27 | 2016-12-27 | Near space aerostatics and its energy resource system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108206668A (en) * | 2017-12-06 | 2018-06-26 | 苏州绿豆豆智能装备科技有限公司 | A kind of suspension column system available for Photospot solar equipment |
| CN108266905A (en) * | 2018-01-09 | 2018-07-10 | 苏州绿豆豆智能装备科技有限公司 | A kind of light gathering heat storage device |
-
2016
- 2016-12-27 CN CN201621448589.2U patent/CN206302215U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108206668A (en) * | 2017-12-06 | 2018-06-26 | 苏州绿豆豆智能装备科技有限公司 | A kind of suspension column system available for Photospot solar equipment |
| CN108266905A (en) * | 2018-01-09 | 2018-07-10 | 苏州绿豆豆智能装备科技有限公司 | A kind of light gathering heat storage device |
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Effective date of registration: 20231221 Address after: 518000 room 301-b077, building 2, No.1, Mawu Road, Baoan community, Yuanshan street, Longgang District, Shenzhen City, Guangdong Province Patentee after: SHENZHEN KUANG-CHI SPACE TECH. Co.,Ltd. Address before: 570100 building a, business incubation center, Haikou national high tech Zone, no.6, Yaogu 1st Road, Nanhai Avenue, Haikou City, Hainan Province Patentee before: HAIKOU INSTITUTE OF FUTURE TECHNOLOGY |