CN108657413A - It floats row levitation device and its application method - Google Patents

It floats row levitation device and its application method Download PDF

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Publication number
CN108657413A
CN108657413A CN201810382399.2A CN201810382399A CN108657413A CN 108657413 A CN108657413 A CN 108657413A CN 201810382399 A CN201810382399 A CN 201810382399A CN 108657413 A CN108657413 A CN 108657413A
Authority
CN
China
Prior art keywords
row
fire balloon
floats
nacelle
photovoltaic
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
CN201810382399.2A
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Chinese (zh)
Inventor
杨京广
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhengzhou Air Port Iot Technology Co Ltd
Original Assignee
Zhengzhou Air Port Iot Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhengzhou Air Port Iot Technology Co Ltd filed Critical Zhengzhou Air Port Iot Technology Co Ltd
Priority to CN201810382399.2A priority Critical patent/CN108657413A/en
Publication of CN108657413A publication Critical patent/CN108657413A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons
    • B64B1/42Construction or attachment of stabilising surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/40Balloons
    • B64B1/46Balloons associated with apparatus to cause bursting
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Wind Motors (AREA)

Abstract

The present invention provides float row levitation device and its application method, including photovoltaic panel, fixed fin, horizontal stabilizer, sealing device, connecting rope, nacelle device and fire balloon, and photovoltaic panel is arranged on the top of fire balloon;Fixed fin is arranged in the upper and lower position of fire balloon right part;The front and back position in fire balloon right part is arranged in horizontal stabilizer;Sealing device is arranged in the lower part of fire balloon;Nacelle device is mounted on the lower part of fire balloon by connecting rope.The present invention can in the air float the longer time, and row, mobility are flexible, landing is stablized, save fuel, the luggage that floats in the air good to the instrumentation protection on device is set, and the setting of photovoltaic panel extends the cruise duration of device;The setting of power motor, the control in direction when realization device control is floated;The setting of movable pulley, equipment is slided when landing, and landing is stablized;The setting of damping device, the stability of equipment when landing avoid when landing because vibration damages equipment.

Description

It floats row levitation device and its application method
Technical field
The invention belongs to boat technical fields of floaing, more particularly to float row levitation device and its application method.
Background technology
The existing aerial row levitation device that floats has hydrogen balloon, helium balloon, fire balloon, by lighter-than-air gas, generates Buoyancy, the object that can be floated up, in addition electric appliance and mechanical device of ascending to heaven, and become motor-driven and controllable.
For example:Hydrogen balloon generally has rubber hydrogen ball, plastic foil hydrogen balloon and several, smaller hydrogen of cloth coating hydrogen balloon Balloon, be currently chiefly used in toy for children or it is celebrating let use fly away, larger hydrogen balloon is also hydrogen drifted by wind for the Advertisement wall scroll that floats Ball, meteorology is upper to detect high-altitude with hydrogen balloon, and military affairs are upper to set up communication antenna or granting leaflet with hydrogen balloon, when earthquake generation, it Disaster area situation shooting can be carried out by unmanned to the investigation of a disaster area situation.Again for example:High-altitude helium for shooting flies Row device, can be stopped in the air with the long period, and comprehensive, far and near distance shooting monitoring is carried out to a city, a piece of mountain forest.
Fire balloon is floated relative to hydrogen balloon, the continuity in the air of helium balloon energy longer time, fire balloon plus electric appliance and Ascend to heaven after mechanical device, the capable time of floaing in the air is longer, when use electric appliance with machinery when, generally require to it is related to this this The power supply of kind electronic device power supply, and supply unit weight is big, power consumption is fast, can shorten fire balloon and float in the air the capable time.
Following luggage that floats, which is set, may be used antigravity technology and magnetic levitation technology, but these current technologies are also in theory On or laboratory in, civilian magnetic levitation technology can't be applied in practice.
WeiLai Technology needs, using now ripe technology, a series of row products that float to be designed, to adapt to people in the air Daily life, therefore, invention it is a kind of can longer time float in the air row, mobility flexibly, landing it is stable, energy saving, to device On the good aerial luggage that floats of instrumentation protection set and be very necessary.
Invention content
In order to solve the above technical problem, the present invention provides row levitation device and its application methods of floaing, and can exist the longer time Aerial float row, mobility are flexible, landing is stablized, save fuel, to the good luggage that floats in the air of instrumentation protection on device It sets, existing problems and faulty state is set to solve the existing air luggage that floats.
In order to achieve the above object, the utility model of sheet uses following technical scheme.
Float row levitation device, including photovoltaic panel, fixed fin, horizontal stabilizer, sealing device, connecting rope, hanging basket dress It sets and fire balloon, the photovoltaic panel is arranged on the top of fire balloon;The fixed fin is arranged in fire balloon right part Upper and lower position;The front and back position in fire balloon right part is arranged in the horizontal stabilizer;The sealing device is arranged in hot gas The lower part of ball;The nacelle device is mounted on the lower part of fire balloon by connecting rope;The nacelle device includes firn-jet head, Combustion furnace, cartridge, supporting rack, power slurry, rudder, connecting plate, power motor, movable pulley, accumulator, wireless telecommunications dress It sets, control box, damping device, fuel cartridge, instrument place position, fuel valve and hot photoelectromotive force structure, firn-jet head welding On the top of combustion furnace;The combustion furnace is welded on the top of nacelle device by supporting rack;The connecting plate setting exists The right lower quadrant of nacelle device;The rudder is mounted on the top of connecting plate;The power motor is arranged in nacelle device Right part;The damping device bolt is mounted on the lower part of nacelle device;The movable pulley bolt is mounted on damping device Lower part;The wireless communication apparatus is mounted on the lower part of nacelle device;The accumulator bolt is mounted on wireless telecommunications The top of device;The control box bolt is mounted on the top of accumulator;The fuel cartridge is fixed on a left side for nacelle device Lower part;The instrument place position is arranged in the left side of fuel cartridge;The fuel valve is mounted on fuel cartridge by cartridge Top;The combustion furnace is attached with fuel valve by cartridge;The hot photoelectromotive force structure setting is filled in hanging basket The upper right quarter set.
Preferably, the damping device includes mounting hole, spring shell, spring, spring lever and tire mounting hole, described Mounting hole be arranged on the top of spring shell;The tire mounting hole is arranged in the lower part of spring lever;The spring lever The inside of spring shell is mounted on by spring.
The sealing device 4 includes diaphragm seal, closing device, electromagnet sealing strip, temperature sensor;Each diaphragm seal is mutual It is combined into a positive round, after energization, closing device makes diaphragm seal be in level, and it is close that the connection side between each is equipped with electromagnet Strip of paper used for sealing, the adjacent side polarity of electromagnet sealing strip are opposite;After power-off, no longer mutual attracting, the weight of diaphragm seal of electromagnet sealing strip Amount makes diaphragm seal be in plumbness with closing device.
Temperature sensor installation is vertically mounted on the frame of sealing device, is stretched into temperature fire balloon, to sealing device Signal transmission power-off and be powered.
Preferably, the photovoltaic panel specifically uses flexible photovoltaic plate, is advantageously implemented hot light complementation power supply.
Preferably, the fire balloon specifically uses terylene ball.
Preferably, the power motor specifically uses vacuum cup high-speed electric expreess locomotive.
Preferably, the movable pulley specifically uses vacuum wheel.
Preferably, the damping device specifically uses air-fuel mixture damping device.
Preferably, the fuel valve specifically uses solenoid valve.
Preferably, the hot photoelectromotive force structure includes photovoltaic charger, accumulator group, shell and photovoltaic controller, The photovoltaic charger is embedded in the middle and upper part of shell;The accumulator group is embedded in the middle and lower part of shell;The light Volt controller is embedded in the centre position of shell.
Preferably, the photovoltaic panel is electrically connected with photovoltaic charger;The photovoltaic charger respectively with storage Battery pack and photovoltaic controller are attached;The accumulator group is electrically connected with accumulator;The wireless telecommunications Device, photovoltaic controller and fuel valve are electrically connected with control box respectively.
The present invention provides float row levitation device and its application method, and capable of in the air floaing the longer time, row, mobility are flexible, drop It falls and stablizes, saves fuel, the good aerial luggage that floats of instrumentation protection on device is set, floatd row with solving existing air Problems present in device and faulty state.Meanwhile beneficial effects of the present invention are:
1. in the present invention, the setting of the photovoltaic panel and the setting of sealing device are conducive to extend the cruise duration of device.It is complete At some special work, some places at a distance are reached.
2. in the present invention, the setting of the power motor is advantageously implemented the control in direction when device control is floated.
3. in the present invention, the setting of the movable pulley, equipment is slided when being conducive to landing, landing is stablized.
4. in the present invention, the setting of the damping device is conducive to the stability of equipment when landing, when avoiding landing Because vibration damages equipment.
5. in the present invention, the setting of the fuel valve is advantageously implemented remote control device lifting.
6. in the present invention, the setting of the instrument place position is conducive to preferably place instrument, avoids the damage of equipment It ruins.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention.
Fig. 2 is the structural schematic diagram of the nacelle device of the present invention.
Fig. 3 is the structural schematic diagram of the damping device of the present invention.
Fig. 4 is the structural schematic diagram of the hot photoelectromotive force structure of the present invention.
Fig. 5 is the sealing device schematic diagram of the present invention.
In figure:
1, photovoltaic panel;2, fixed fin;3, horizontal stabilizer;4, sealing device;41, diaphragm seal;42, closing device;43, electric Magnet sealing strip;44, temperature sensor;5, connecting rope;6, nacelle device;601, firn-jet head;602, combustion furnace;603, fuel Pipe;604, supporting rack;605, power is starched;606, rudder;607, connecting plate;608, power motor;609, movable pulley;610, it stores Battery;611, wireless communication apparatus;612, control box;613, damping device;6131, mounting hole;6132, spring shell;6133、 Spring;6134, spring lever;6135, tire mounting hole;614, fuel cartridge;615, instrument place position;616, fuel valve;617, hot Photoelectromotive force structure;6171, photovoltaic charger;6172, accumulator group;6173, shell;6174, photovoltaic controller;7, hot gas Ball.
Specific implementation mode
The present invention is described further below in conjunction with attached drawing:
Embodiment:
As shown in attached drawing 1 to attached drawing 4
The present invention provides float row levitation device, including photovoltaic panel 1, fixed fin 2, horizontal stabilizer 3, sealing device 4, connection Rope 5, nacelle device 6 and fire balloon 7, the photovoltaic panel 1 are arranged on the top of fire balloon 7;The fixed fin 2 is arranged In the upper and lower position of 7 right part of fire balloon;The front and back position in 7 right part of fire balloon is arranged in the horizontal stabilizer 3;Described is close Seal apparatus 4 is arranged in the lower part of fire balloon 7;The nacelle device 6 is mounted on the lower part of fire balloon 7 by connecting rope 5;It is described Nacelle device 6 include firn-jet head 601, combustion furnace 602, cartridge 603, supporting rack 604, power slurry 605, rudder 606, even Fishplate bar 607, power motor 608, movable pulley 609, accumulator 610, wireless communication apparatus 611, control box 612, damping device 613, fuel cartridge 614, instrument place position 615, fuel valve 616 and hot photoelectromotive force structure 617, the firn-jet head 601 weld On the top of combustion furnace 602;The combustion furnace 602 is welded on the top of nacelle device 6 by supporting rack 604;The company The right lower quadrant in nacelle device 6 is arranged in fishplate bar 607;The rudder 606 is mounted on the top of connecting plate 607;Described is dynamic The right part in nacelle device 6 is arranged in force motor 608;613 bolt of damping device is mounted on the lower part of nacelle device 6;Institute 609 bolt of movable pulley stated is mounted on the lower part of damping device 613;The wireless communication apparatus 611 is mounted on nacelle device 6 Lower part;610 bolt of accumulator is mounted on the top of wireless communication apparatus 611;612 bolt of the control box installation On the top of accumulator 610;The fuel cartridge 614 is fixed on the lower left quarter of nacelle device 6;The instrument place position 615 It is arranged in the left side of fuel cartridge 614;The fuel valve 616 is mounted on the top of fuel cartridge 614 by cartridge 603;It is described Combustion furnace 602 be attached by cartridge 603 with fuel valve 616;The hot photoelectromotive force structure 617 is arranged in hanging basket The upper right quarter of device 6.
In above-described embodiment, specifically, the damping device 613 includes mounting hole 6131, spring shell 6132, spring 6133, spring lever 6134 and tire mounting hole 6135, the mounting hole 6131 are arranged on the top of spring shell 6132;It is described Tire mounting hole 6135 be arranged in the lower part of spring lever 6134;The spring lever 6134 is mounted on spring by spring 6133 The inside of shell 6132.
In above-described embodiment, specifically, the sealing device 4, including diaphragm seal 41, closing device 42, electromagnet sealing Item 43, temperature sensor 44;Diaphragm seal 41 has six, is combined with each other into a positive round, and after energization, closing device 42 makes diaphragm seal The 41 connection side between level, each is equipped with electromagnet sealing strip 43, the adjacent side polarity phase of electromagnet sealing strip 43 Instead, close attracting after contact, that is to say, that the mouth into hot gas is just sealed;After power-off, electromagnet sealing strip 43 is no longer mutually Mutually attracting, the weight of diaphragm seal 41 makes diaphragm seal 41 be in plumbness with closing device 42, that is to say, that into hot gas mouth just It opens.
The installation of temperature sensor 44 is vertically mounted on the frame of sealing device 4, is stretched into temperature fire balloon 7, with detection Air themperature in fire balloon, within the temperature range of setting, to the signal of sealing device 4 transmission power-off and energization.
Electromagnet sealing strip 43 is formed by being enclosed with electronic coil in flexible material, and flexible material is with flexible material in polarity Opposite electronic coil it is attracting under, be in close contact, play sealing function.
In above-described embodiment, specifically, the photovoltaic panel 1 specifically uses flexible photovoltaic plate, it is mutual to be advantageously implemented hot light Mend power supply.
In above-described embodiment, specifically, the fire balloon 7 specifically uses terylene ball.
In above-described embodiment, specifically, the power motor 608 specifically uses vacuum cup high-speed electric expreess locomotive.
In above-described embodiment, specifically, the movable pulley 609 specifically uses vacuum wheel.
In above-described embodiment, specifically, the damping device 613 specifically uses air-fuel mixture damping device.
In above-described embodiment, specifically, the fuel valve 616 specifically uses solenoid valve.
In above-described embodiment, specifically, the hot photoelectromotive force structure 617 includes photovoltaic charger 6171, accumulator Group 6172, shell 6173 and photovoltaic controller 6174, the photovoltaic charger 6171 are embedded in the middle and upper part of shell 6173;Institute The accumulator group 6172 stated is embedded in the middle and lower part of shell 6173;The photovoltaic controller 6174 is embedded in shell 6173 Between position.
In above-described embodiment, specifically, the photovoltaic panel 1 is electrically connected with photovoltaic charger 6171;Described Photovoltaic charger 6171 is attached with accumulator group 6172 and photovoltaic controller 6174 respectively;The accumulator group 6172 with Accumulator 610 is electrically connected;The wireless communication apparatus 611, photovoltaic controller 6174 and fuel valve 616 respectively with control Box 612 processed is electrically connected.
Operation principle
In the present invention, firn-jet head 601 is lighted, the size of 601 fire of firn-jet head is controlled by fuel valve 616, is risen to control Highly, power slurry 605 is driven by power motor 608, equipment realizes the movement of controllable direction, passes through 606 side of progress of rudder To control, landing and sliding is carried out by movable pulley 609, buffering absorbing is realized to equipment by damping device 613 when landing, is led to The collection of energy of photovoltaic panel 1 and the hot gas heat preservation of sealing device 4 are crossed, the aerial residence time is extended.
Using technical solutions according to the invention or those skilled in the art under the inspiration of technical solution of the present invention, Similar technical solution is designed, and reaches above-mentioned technique effect, is to fall into protection scope of the present invention.

Claims (10)

1. float row levitation device, which is characterized in that it includes photovoltaic panel(1), fixed fin(2), horizontal stabilizer(3), close Seal apparatus(4), connecting rope(5), nacelle device(6)And fire balloon(7), the photovoltaic panel(1)It is arranged in fire balloon(7)It is upper Portion;The fixed fin(2)It is arranged in fire balloon(7)The upper and lower position of right part;The horizontal stabilizer(3)Setting exists Fire balloon(7)The front and back position of right part;The sealing device(4)It is arranged in fire balloon(7)Lower part;The nacelle device (6)Pass through connecting rope(5)Mounted on fire balloon(7)Lower part;The nacelle device(6)Including firn-jet head(601), combustion furnace (602), cartridge(603), supporting rack(604), power slurry(605), rudder(606), connecting plate(607), power motor (608), movable pulley(609), accumulator(610), wireless communication apparatus(611), control box(612), damping device(613), combustion Gas tank(614), instrument place position(615), fuel valve 616 and hot photoelectromotive force structure 617, the firn-jet head(601)Welding In combustion furnace(602)Top;The combustion furnace(602)Pass through supporting rack(604)It is welded on nacelle device(6)Top; The connecting plate(607)It is arranged in nacelle device(6)Right lower quadrant;The rudder(606)Mounted on connecting plate(607) Top;The power motor(608)It is arranged in nacelle device(6)Right part;The damping device(613)Bolt is installed In nacelle device(6)Lower part;The movable pulley(609)Bolt is mounted on damping device(613)Lower part;Described is wireless Communication device(611)Mounted on nacelle device(6)Lower part;The accumulator(610)Bolt is mounted on wireless communication apparatus (611)Top;The control box(612)Bolt is mounted on accumulator(610)Top;The fuel cartridge(614)Gu It is scheduled on nacelle device(6)Lower left quarter;The instrument place position(615)It is arranged in fuel cartridge(614)Left side;The combustion Expect valve(616)Pass through cartridge(603)Mounted on fuel cartridge(614)Top;The combustion furnace(602)With fuel valve (616)Pass through cartridge(603)It is attached;The upper right quarter in nacelle device 6 is arranged in the hot photoelectromotive force structure 617.
2. the row levitation device as described in claim 1 that floats, which is characterized in that the damping device(613)Including mounting hole (6131), spring shell(6132), spring(6133), spring lever(6134)With tire mounting hole(6135), the mounting hole (6131)It is arranged in spring shell(6132)Top;The tire mounting hole(6135)It is arranged in spring lever(6134)Under Portion;The spring lever(6134)Pass through spring(6133)Mounted on spring shell(6132)Inside.
3. the row levitation device as described in claim 1 that floats, which is characterized in that the sealing device(4), including diaphragm seal (41), closing device(42), electromagnet sealing strip(43), temperature sensor(44);Each diaphragm seal(41)It is combined with each other into one A positive round, after energization, closing device(42)Make diaphragm seal(41)In level, it is close that the connection side between each is equipped with electromagnet Strip of paper used for sealing(43), electromagnet sealing strip(43)Adjacent side polarity is opposite;After power-off, electromagnet sealing strip(43)No longer mutual phase It inhales, diaphragm seal(41)Weight and closing device(42)Make diaphragm seal(41)In plumbness;Temperature sensor(44)Installation It is vertically mounted on sealing device(4)Frame on, stretch into temperature fire balloon(7)In, to sealing device(4)Transmission power-off and energization Signal.
4. the row levitation device as described in claim 1 that floats, which is characterized in that the fire balloon(7)Terylene ball is specifically used, The photovoltaic panel(1)Specifically use flexible photovoltaic plate.
5. the row levitation device as described in claim 1 that floats, which is characterized in that the power motor(608)It is specific to use very Empty cup high-speed electric expreess locomotive.
6. the row levitation device as described in claim 1 that floats, which is characterized in that the movable pulley(609)Specifically use vacuum Wheel.
7. the row levitation device as described in claim 1 that floats, which is characterized in that the damping device(613)It is specific to use oil Gas mixing damping device.
8. the row levitation device as described in claim 1 that floats, which is characterized in that the fuel valve(616)Specifically use electromagnetism Valve.
9. the row levitation device as described in claim 1 that floats, which is characterized in that the hot photoelectromotive force structure(617)Including Photovoltaic charger(6171), accumulator group(6172), shell(6173)And photovoltaic controller(6174), the photovoltaic charger (6171)It is embedded in shell(6173)Middle and upper part;The accumulator group(6172)It is embedded in shell(6173)Middle and lower part; The photovoltaic controller(6174)It is embedded in shell(6173)Centre position, the photovoltaic panel(1)With photovoltaic charger (6171)It is electrically connected;The photovoltaic charger(6171)Respectively with accumulator group(6172)And photovoltaic controller (6174)It is attached;The accumulator group(6172)With accumulator(610)It is electrically connected;The wireless telecommunications dress It sets(611), photovoltaic controller(6174)And fuel valve(616)Respectively with control box(612)It is electrically connected.
10. the application method of the row levitation device as described in claim 1 that floats, which is characterized in that by firn-jet head(601)It lights, Pass through fuel valve(616)Control firn-jet head(601)The size of fire passes through power motor to control lifting height(608)It drives Power is starched(605), equipment realize controllable direction movement, pass through rudder(606)Into the control of line direction, pass through movable pulley (609)Landing and sliding is carried out, when landing passes through damping device(613)Buffering absorbing is realized to equipment, passes through photovoltaic panel(1)Energy Amount is collected and sealing device(4)Hot gas heat preservation, extend the aerial residence time.
CN201810382399.2A 2018-04-26 2018-04-26 It floats row levitation device and its application method Withdrawn CN108657413A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810382399.2A CN108657413A (en) 2018-04-26 2018-04-26 It floats row levitation device and its application method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810382399.2A CN108657413A (en) 2018-04-26 2018-04-26 It floats row levitation device and its application method

Publications (1)

Publication Number Publication Date
CN108657413A true CN108657413A (en) 2018-10-16

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810382399.2A Withdrawn CN108657413A (en) 2018-04-26 2018-04-26 It floats row levitation device and its application method

Country Status (1)

Country Link
CN (1) CN108657413A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110707993A (en) * 2019-10-26 2020-01-17 苏师大半导体材料与设备研究院(邳州)有限公司 Floating photovoltaic power generation system
CN111895447A (en) * 2020-06-07 2020-11-06 李迎春 Ignition control system based on people number analysis

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110707993A (en) * 2019-10-26 2020-01-17 苏师大半导体材料与设备研究院(邳州)有限公司 Floating photovoltaic power generation system
CN111895447A (en) * 2020-06-07 2020-11-06 李迎春 Ignition control system based on people number analysis

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