CN208412174U - A kind of fuel cell-powered unmanned plane launching platform - Google Patents
A kind of fuel cell-powered unmanned plane launching platform Download PDFInfo
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- CN208412174U CN208412174U CN201820913710.7U CN201820913710U CN208412174U CN 208412174 U CN208412174 U CN 208412174U CN 201820913710 U CN201820913710 U CN 201820913710U CN 208412174 U CN208412174 U CN 208412174U
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- unmanned plane
- air
- nitrogen
- fuel cell
- launching platform
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Abstract
The utility model relates to a kind of fuel cell-powered unmanned plane launching platforms, including unmanned plane launching platform and UAV system, the UAV system is fixed on unmanned plane launching platform by electromagnetic drive fixing lock, dynamical system is equipped in the unmanned plane launching platform, air supply system, nitrogen supply (NS) system, operating system, communication system and control system, the control system and control dynamical system, air supply system, nitrogen supply (NS) system, operating system and communication system connection, the UAV system is connect by air fast interface with air supply system, it is connect by nitrogen fast interface with nitrogen supply (NS) system.The unmanned plane takes off the platform of guarantee, it is mainly used for system detection and activation before fuel cell-driven UAV system is taken off, ensure that UAV system is let fly away in the case where state qualification, the safety of fuel cell-driven UAV system and its reliability of power-supply system can be promoted.
Description
Technical field
The utility model relates to unmanned plane launching platform technical field, in particular to a kind of fuel cell-powered unmanned plane
Launching platform.
Background technique
Today's society, with the rapid development of science and technology, intelligence machine are widely used in people's lives, now, nothing
People, which drives an airplane, to be widely used in the projects such as aerophotography, resource investigation, delivering disaster relief supplies, air patrol, with winged
The UAV of the universalness of machine attitude control system and space technology, all size progresses into commercial market.
Utility model content
Take off the platform of guarantee the purpose of the utility model is to provide a kind of unmanned plane, be mainly used for fuel cell-driven without
Man-machine system take off before system detection and activation, it is ensured that UAV system state qualification in the case where let fly away, can be promoted
The safety of fuel cell-driven UAV system and its reliability of power-supply system.
The technical solution of the utility model is as follows:
A kind of fuel cell-powered unmanned plane launching platform, including unmanned plane launching platform and UAV system, institute
It states UAV system to be fixed on unmanned plane launching platform by electromagnetic drive fixing lock, be equipped in the unmanned plane launching platform
Dynamical system, air supply system, nitrogen supply (NS) system, operating system, communication system and control system, the control system
It is connect with control dynamical system, air supply system, nitrogen supply (NS) system, operating system and communication system, the unmanned plane
System is connect by air fast interface with air supply system, is connect by nitrogen fast interface with nitrogen supply (NS) system.
As one of technological improvement, the dynamical system includes built-in fuel cell system and built-in lithium battery packet,
The built-in control system of the built-in fuel cell system and built-in lithium battery packet and unmanned plane launching platform forms hybrid power
Power supply circuit, and connect with control system.
As one of technological improvement, the air supply system includes air filter, air pump, gas-liquid mixed
Device, atomizer and water tank, air pump connect air filter, pump discharge access air and liquid mixer, be then connected to take off it is flat
Air fast interface on countertop, atomizer entrance are connected to water tank, and atomizer exit is connect with the collateral mouth of air and liquid mixer.
As one of technological improvement, the nitrogen supply (NS) system includes nitrogen cylinder, pressure reducing valve, the adjusting of nitrogen flow electricity
Valve, atomizer, air and liquid mixer and water tank, nitrogen cylinder accesses nitrogen flow electricity regulating valve after connecting pressure reducing valve, with being followed by
Enter the nitrogen fast interface that air and liquid mixer is then connected on launching platform top surface, atomizer entrance is connected to water tank, atomizer
Outlet is connect with the collateral mouth of air and liquid mixer.
As one of technological improvement, the operating system include UAV system status indicator lamp, total power switch,
Air loop atomizer switch, nitrogen circuit atomizer switch, air pump speed-regulating switch, nitrogen flow regulating switch, Electronic Negative
Adjusting knob, liquid crystal display and buzzer are carried, they are arranged in unmanned plane launching platform outer surface, UAV system state
Indicator light, liquid crystal display and buzzer are connect with control system, air loop atomizer switch and nitrogen circuit atomizer
Switch is connect with atomizer, and air pump speed-regulating switch is connected with air pump, and nitrogen flow regulating switch and nitrogen flow electricity are adjusted
Valve is connected, and electronic load adjusting knob is connected with electronic load.
As one of technological improvement, the control system is master board, and master board connects electromagnetism separation connection
Device, lithium battery pack, electronic load, air pump, nitrogen Electromagnetic Flow regulating valve, status indicator lamp, alarm buzzer, electromagnetic drive
Fixing lock, atomizer, display screen and communication system, for power transmission, transformation, distribution, control, information acquisition process and
It is communicated with each device.
As one of technological improvement, the communication system is wireless data sending/receiving module, is arranged in unmanned plane
Inside launching platform, unmanned plane launching platform outer surface is equipped with wireless data transceiving port, for realizing master board and nobody
The communication of machine system, and realize the communication of master board and third party's information process unit.
As one of technological improvement, nitrogen cylinder inflating port, the inflating port are provided on the launching platform top surface
It is connected to through check valve with nitrogen cylinder.
As one of technological improvement, water tank filler, the water storage are additionally provided on the launching platform top surface
Tank filler is connected to the water tank built in platform.
Compared with prior art, the utility model has the following beneficial effects:
1, unmanned plane launching platform is mainly used for system detection and work before fuel cell-driven UAV system is taken off
Change, it is ensured that UAV system is let fly away in the case where state qualification, unmanned plane launching platform and UAV system gas, electric power,
The connection of signal improves the safety of fuel cell-driven UAV system and its reliability of power-supply system；
2, one piece of lithium battery built in unmanned plane launching platform and unmanned plane fuel cell pass through the built-in control electricity of launching platform
Road plate forms hybrid power power supply circuit, i.e., also functions to the effect of protection fuel cell simultaneously as startup power supply；
3, adjustable electronic load built in unmanned plane launching platform, operating temperature, membrane electrode interface state in fuel cell
When being all not up to best, phase step type heavy load is easy to draw cell voltage to very low, causes to damage to battery.Built-in adjustable electronic
Load realizes that during avoiding fuel cell start-up, best effort is had not yet been reached in battery to the gradually loading procedure of fuel cell
State just bears to be large current discharge, so that battery has the process for being gradually warmed up and adjusting interface state, plays battery oneself
Activation；
4, unmanned plane launching platform built in air pump, air filter, atomizer, water tank.Air pump and air filtration
Device connection, and be connected to by platform Quick air interface with unmanned plane fuel cell system air side, it can be to fuel battery air
Lateral electrode carries out the water removal of atm number purging, dedusting；It can also be extracted in water tank and be deposited by the atomizer on air pump gas passage
The deionized water of storage carries out ultrasonic atomizatio to air humidification, the air of humidification fuel cell membrane electrode is started before pre- work
Change, prevent membrane electrode dehydration, reduce the internal resistance of cell, nitrogen cylinder built in unmanned plane launching platform passes through the quick nitrogen interface of platform
It is connected to unmanned plane fuel cell system hydrogen gas side, atm number purging water removal can be carried out to fuel cell hydrogen lateral electrode；It can also
The deionized water stored in water tank is extracted by the atomizer on nitrogen gas channel and carries out ultrasonic atomizatio to nitrogen humidification, is increased
Wet nitrogen fuel cell membrane electrode is started before pre-activate, prevent membrane electrode dehydration, reduce the internal resistance of cell.
5, unmanned plane launching platform is provided with the cable data acquisition port being connected with control panel and wireless data transceiving
Port can be connect with Unmanned Aerial Vehicle Data output port by data line or obtain data by the wireless transmission port of unmanned plane；
It include voltage, electric current, temperature, rotation speed of the fan and the unmanned plane oneself state parameter etc. of fuel cell in the data of transmission.Control
Plate carries out processing analysis to received data, judges to fuel cell and unmanned state, if there is cell voltage is too low, electric
It flows through situations such as big, temperature is excessively high, unmanned plane failure to occur then to show fault parameter in liquid crystal display, indicator light red is dodged
It is bright, and buzzer long time of alarm, unmanned plane do not enter take-off process, wait artificial treatment；If fuel cell and unmanned plane
In good condition, then ready in liquid crystal display screen display system, indicator light green length is bright, and the short ring prompt of buzzer, nothing
Man-machine to enter state to be flown, electromagnetic drive fixing lock and electromagnetism separate connector are powered on unlock automatically and are detached from, can be operated
Fly.
Detailed description of the invention:
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the utility model unmanned plane launching platform appearance southwest normal axomometric drawing；
Fig. 2 is the utility model unmanned plane launching platform appearance northeast normal axomometric drawing；
Fig. 3 is southwestern normal axomometric drawing inside the utility model unmanned plane launching platform；
Fig. 4 is northeast normal axomometric drawing inside the utility model unmanned plane launching platform；
Fig. 5 takes off for the utility model ensures that platform air supplies flow diagram；
Fig. 6 takes off for the utility model ensures that platform nitrogen supplies flow diagram；
Fig. 7 takes off for the utility model and ensures platform built-in lithium battery packet and unmanned plane fuel cell hybrid power supply line
Diagram is intended to；
Fig. 8 takes off for the utility model and ensures that platform master board connect topological structure schematic diagram with each device；
Wherein, 1, UAV system；2, unmanned plane launching platform；3, status indicator lamp；4, total power switch；5, air returns
Road atomizer switch；6, nitrogen circuit atomizer switchs；7, air pump speed-regulating switch；8, nitrogen flow regulating switch；9, electronics
Load regulation knob；10, liquid crystal display；11, buzzer；12, electromagnetic drive fixing lock；13, air fast interface；14, nitrogen
Gas fast interface；15, wireless data transceiving port；16 nitrogen cylinder inflating ports；17, water tank filler；18, master board；19,
Electronic load；20, replaceable air filter；21, air pump；22, air and liquid mixer；23, atomizer；24, lithium battery pack；
25, air and liquid mixer；26, nitrogen cylinder；27, nitrogen flow electricity regulating valve；28, pressure reducing valve；29, atomizer；30, water tank；31,
Electromagnetism separate connector.
Specific embodiment
Illustrate the embodiments of the present invention below by way of specific specific example, those skilled in the art can be by this theory
Content disclosed by bright book understands other advantages and effect of the utility model easily.
As shown in Figures 1 to 8, a kind of fuel cell-powered unmanned plane launching platform, including UAV system 1 and nothing
Man-machine launching platform 2, UAV system are fixed on unmanned plane launching platform by electromagnetic drive fixing lock 12, and unmanned plane takes off
Dynamical system, air supply system, nitrogen supply (NS) system, operating system, communication system and control system, control are equipped in platform
System processed is connect with control dynamical system, air supply system, nitrogen supply (NS) system, operating system and communication system, nobody
Machine system is connect by air fast interface 13 with air supply system, is connected by nitrogen fast interface 14 and nitrogen supply (NS) system
It connects.
Dynamical system includes built-in fuel cell system and built-in lithium battery packet 24, built-in fuel cell system and built-in lithium
Battery pack 24 and the built-in control system of unmanned plane launching platform form hybrid power power supply circuit, and connect with control system.
Air supply system includes air filter 20, air pump 21, air and liquid mixer 22, atomizer 23 and water tank
30, air pump 21 connects air filter 20, and pump discharge accesses air and liquid mixer 22, the sky being then connected on launching platform top surface
Gas fast interface 13,23 entrance of atomizer are connected to water tank 30, and the outlet of atomizer 23 is connect with the collateral mouth of air and liquid mixer 22.
Nitrogen supply (NS) system includes that nitrogen cylinder 26, pressure reducing valve 28, nitrogen flow electricity regulating valve 27, atomizer 29, gas-liquid are mixed
Clutch 25 and water tank 30, nitrogen cylinder 26 access nitrogen flow electricity regulating valve 27 after connecting pressure reducing valve 28, then access gas-liquid
Mixer 25 is then connected to the nitrogen fast interface 14 on launching platform top surface, and 29 entrance of atomizer is connected to water tank 30, atomization
The outlet of device 29 is connect with the collateral mouth of air and liquid mixer 25.
Operating system includes UAV system status indicator lamp 3, total power switch 4, air loop atomizer switch 5, nitrogen
Air circuit atomizer switch 6, air pump speed-regulating switch 7, nitrogen flow regulating switch 8, electronic load adjusting knob 9, liquid crystal
Display screen 10 and buzzer 11, they are arranged in unmanned plane launching platform outer surface, status indicator lamp 3, the liquid of UAV system
Crystal display screen 10 and buzzer 11 are connect with control system, air loop atomizer switch 5 and nitrogen circuit atomizer switch 6
It is connect with atomizer 29, air pump speed-regulating switch 7 is connected with air pump 21, nitrogen flow regulating switch 8 and nitrogen flow electricity tune
It saves valve 27 to be connected, electronic load adjusting knob 9 is connected with electronic load 19.
Control system is master board 18, and master board 18 connects electromagnetism separate connector 31, lithium battery pack 24, Electronic Negative
Carry 19, air pump 21, nitrogen Electromagnetic Flow regulating valve 27, status indicator lamp 3, buzzer 11, electromagnetic drive fixing lock 12, atomization
Device 23, liquid crystal display 10 and communication system, for power transmission, transformation, distribution, control, information acquisition process and with
Each device communication.
Communication system is wireless data sending/receiving module, is arranged inside unmanned plane launching platform, unmanned plane takes off flat
Platform outer surface is equipped with wireless data transceiving port 15, for realizing the communication of master board and UAV system, and realizes master
The communication of control panel and third party's information process unit.
It is provided with nitrogen cylinder inflating port 16 on launching platform top surface, the nitrogen cylinder inflating port 16 is through check valve and nitrogen cylinder
26 connections；Water tank filler 17, the water tank filler 17 and the storage built in platform are additionally provided on launching platform top surface
Water pot 30 is connected to.
Unmanned plane launching platform 2 is mainly used for system detection and activation before fuel cell-driven UAV system 1 is taken off,
Ensure UAV system state qualification in the case where let fly away, can be promoted fuel cell-driven UAV system safety and
The reliability of its power-supply system.UAV system 1 is fixed on plane on unmanned plane launching platform by electromagnetic drive fixing lock 12,
Anti- sliding stop and malfunction, UAV system state-detection is qualified, then electromagnetic drive fixing lock 12 automatically opens.UAV system
1 is connected to by the air fast interface on unmanned plane launching platform 2 with the realization of nitrogen fast interface with the gas circuit of platform；Pass through electricity
The realization of Magneto separate connector 31 is connect with the electrical and wire signal of launching platform.The gas of air fast interface access passes through nothing
Threeway electromagnetic switching valve built in man-machine system accesses fuel battery negative pole；The gas of nitrogen fast interface access passes through unmanned plane system
Built-in threeway electromagnetic switching valve of uniting accesses anode of fuel cell, can be purged respectively to fuel cell cathode and anode, be humidified work
Change.UAV system fuel cells output end, controller output end are taken off by electromagnetism separate connector 31 with unmanned plane flat
Master board 18 is connected in platform, and control platform can read in fuel cell condition parameter and drone status parameter, including voltage,
Electric current, temperature, humidity, rotation speed of the fan, attitude angle etc. can also send control command to UAV system.Unmanned plane takes off flat
Platform 2 is additionally provided with wireless data transceiving port 15, also may be implemented with UAV system and external information processing without line number
According to communication.
Unmanned plane launching platform 2 is built-in with master board 18, electronic load 19, lithium battery pack 24, as shown in fig. 7, lithium is electric
Pond is wrapped 24 and is all connect from the fuel cell that UAV system accesses with master board 18, and two pole of ideal in master board is passed through
Pipe anti-reversing charging circuit realizes hybrid power supply in parallel, provides electric power for the electricity consumptions device such as electronic load, pump, valve.When fuel electricity
Pond is in good condition, and being higher than lithium battery pack in operating point end voltage, then fuel cell undertakes whole electric power output；Work as fuel cell
When the situations such as material supply is insufficient, load becomes larger suddenly, battery status is bad occur, decline in operating point fuel cell end voltage
To the then the two shared electric power output of lithium battery pack end voltage, lithium battery plays the role of the peak load protection fuel cell that disappears.
Replaceable air filter 20, air pump 21, air and liquid mixer 22, atomization are provided in unmanned plane launching platform 2
Device 23, water tank 30, several persons form fuel battery negative pole and purge humidification activation circuit, as shown in Figure 5.Air pump 21 is through filter
Air after suction filter pumps out the fast quick access of air that gas access air and liquid mixer 22 is then connected on launching platform top surface
Mouth 13,23 entrance of atomizer are connected to water tank 30, and outlet is connect with the collateral mouth of air and liquid mixer 22.Starting atomizer 23 then can be with
Air and liquid mixer 22 is sprayed into after extracting deionized water ultrasonic atomization in water tank 30, realization is pumped into air to air pump and adds
It is wet.Similarly, nitrogen cylinder 26, pressure reducing valve 28, nitrogen flow electricity regulating valve 27, atomizer are additionally provided in unmanned plane launching platform 2
29, air and liquid mixer 25 form anode of fuel cell purging humidification activation circuit with water tank 30, as shown in Figure 6 together.Nitrogen
High pressure nitrogen in bottle 26 accesses nitrogen flow electricity regulating valve 27 after pressure reducing valve 28 is reduced to low pressure, and the nitrogen after adjusting flow velocity connects
Enter the nitrogen fast interface 14 that air and liquid mixer 25 is then connected on launching platform top surface, 29 entrance of atomizer is connected to water tank
30, outlet is connect with the collateral mouth of air and liquid mixer 25.It is super that starting atomizer 29 can then extract deionized water from water tank 30
Air and liquid mixer 25 is sprayed into after sound wave atomization, realizes the humidification to anode of fuel cell purge circuit nitrogen.Launching platform top surface
On nitrogen cylinder inflating port 16 is installed, be connected to through check valve threeway with nitrogen cylinder, can be directly to built-in nitrogen by this inflating port
Gas cylinder is inflated.Water tank 30 can supplement deionization by the water tank filler 17 being placed on launching platform top surface
Water.
2 upper surface of unmanned plane launching platform is equipped with UAV system status indicator lamp 3, and front panel is opened configured with general supply
Close 4, air loop atomizer switch 5, nitrogen circuit atomizer switch 6, air pump speed-regulating switch 7, nitrogen flow regulating switch
8, electronic load adjusting knob 9, liquid crystal display 10, buzzer 11.Status indicator lamp 3 has colour change function, when unmanned plane system
System detection qualification can let the long green of then status indicator lamp 3 fly away and show, the short ring of buzzer 11 prompt, and on liquid crystal display 10
Prompt system is in good condition, and system readiness can let information fly away；When UAV system detects faulty then status indicator lamp 3
Red flashing display, police is warned in the sudden strain of a muscle of buzzer 11, and shows fault code on liquid crystal display 10.Air loop atomizer is opened
It closes 5 and shuts down ultrasonic ultrasonic delay line memory for opening with nitrogen circuit atomizer switch 6, realize the humidification to air or nitrogen.Air
Pump speed-regulating switch 7 is connected with air pump 21, for the starting and speed regulation to air pump；Nitrogen flow regulating switch 8 and nitrogen stream
Electric regulating valve 27 is measured to be connected, for nitrogen circuit open and flow velocity is adjusted；Electronic load adjusting knob and 19 phase of electronic load
Even, for adjusting the electric current, voltage or power of electronic load, to simulate the load behavior of UAV system built-in power.Liquid crystal
Display screen 10 can show fuel cell condition parameter and drone status parameter, voltage, electric current including fuel cell, temperature
Degree, humidity, rotation speed of the fan；The voltage of built-in lithium battery, electric current, temperature；Attitude angle, comprehensive state, the fault code of unmanned plane
Etc. information.
Unmanned plane launching platform 2 by built-in master board 18 realize with the connection of each electricity consumption device, play power transmission,
Transformation, distribution, control, the acquisition process of information and the function with the communication of each device.The topological structure being connect with each device such as Fig. 8
It is shown.Master board 18 can from UAV system, electronic load, wireless data sending/receiving module carry out data acquisition or
Order is executed to the transmission of these devices, UAV system and its built-in fuel cell condition are sentenced according to collected data
Reading processing, and corresponding information is sent to display screen, status indicator lamp, buzzer by treated.Wireless data sending/receiving
Master board and the communication of UAV system may be implemented in block, and master board and third party's information process unit also may be implemented
Communication.
The course of work of unmanned plane launching platform are as follows:
Fuel cell-driven UAV system is reliably fixed on unmanned plane launching platform by electromagnetic drive fixing lock
Plane.Fuel battery air built in UAV system and hydrogen inlet triple valve are switched to external input interface, pass through flexibility
Hose, connection fuel battery air side and the air fast interface ensured on platform that takes off, hydrogen gas side and taking off ensure on platform
Nitrogen fast interface；Output electricity consumption Magneto separate connector and guarantee of taking off in UAV system are connected by multi-core cable harness
Electromagnetism separate connector on platform, to realize UAV system and the take off gas for ensureing platform, electricity, information communication.
It the gas for ensureing platform and is electrically connected with taking off:
Launching platform total power switch is opened, self-test starting, which is taken off, ensures platform；Air pump speed-regulating switch is opened, is adjusted empty
Gas velocity carries out 1~15min of purging to battery air side, then opens air loop atomizer switch, starts atomizer,
1~15min is purged under air humidification state, after, air pump and atomizer are shut down, fuel cell air inlet triple valve is cut
Internal gas supply end is changed to, the connection of external hose and fuel battery air side is disconnected.Nitrogen flow regulating switch is opened, nitrogen is adjusted
Gas velocity carries out 1~15min of purging to battery hydrogen gas side, then opens nitrogen circuit atomizer switch, starts atomizer,
1~15min is purged under nitrogen humidification state, after, shut down nitrogen and atomizer, the switching of fuel cell hydrogen inlet three-way valve
To internal hydrogen end, the connection of external hose and fuel cell hydrogen gas side is disconnected.And it opens UAV system and carries high pressure hydrogen
Valve makes fuel cell have fan-out capability.Air and nitrogen connection can synchronize progress.
Set constant current or constant power mode for electronic load, by electronic load adjusting knob incrementally increase electric current or
Power.The voltage for increasing fuel cell during loading journey cannot be below setting voltage, this process is until fuel cell reaches pre-
30~180S is stablized in the fully loaded output of setting, and electronic load power consumption is adjusted to be 0, is switched to unmanned plane pre-actuated state.It takes off flat
Platform control panel reads fuel cell and unmanned plane parameter, judges fuel cell and drone status, shows shape in liquid crystal display
State parameter or fault code.Fault parameter, the flashing of indicator light red, and buzzer are shown in liquid crystal display if failure
Long time of alarm, unmanned plane do not enter take-off process, wait artificial treatment.If fuel cell and drone status are good,
Liquid crystal display screen display system is ready, and indicator light green length is bright, and the short ring prompt of buzzer, electromagnetism separation fixing lock are beaten
It opens, electromagnetism separate connector is opened, and unmanned plane enters state to be flown, and be can be operated and is taken off.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (9)
1. a kind of fuel cell-powered unmanned plane launching platform, it is characterised in that: including unmanned plane launching platform and nobody
Machine system, the UAV system are fixed on unmanned plane launching platform by electromagnetic drive fixing lock, and the unmanned plane takes off
Dynamical system, air supply system, nitrogen supply (NS) system, operating system, communication system and control system, institute are equipped in platform
Control system is stated to connect with control dynamical system, air supply system, nitrogen supply (NS) system, operating system and communication system,
The UAV system is connect by air fast interface with air supply system, and nitrogen fast interface and nitrogen supply (NS) system are passed through
System connection.
2. the fuel cell-powered unmanned plane launching platform of one kind according to claim 1, it is characterised in that: the power
System includes built-in fuel cell system and built-in lithium battery packet, the built-in fuel cell system and built-in lithium battery packet and nothing
The built-in control system of man-machine launching platform forms hybrid power power supply circuit, and connect with control system.
3. the fuel cell-powered unmanned plane launching platform of one kind according to claim 2, it is characterised in that: the air
Supply system includes air filter, air pump, gas-liquid mixed gas, atomizer and water tank, and air pump connects air filtration
Device, pump discharge access air and liquid mixer, the air fast interface being then connected on launching platform top surface, the connection storage of atomizer entrance
Water pot, atomizer exit are connect with the collateral mouth of air and liquid mixer.
4. the fuel cell-powered unmanned plane launching platform of one kind according to claim 3, it is characterised in that: the nitrogen
Supply system includes nitrogen cylinder, pressure reducing valve, nitrogen flow electricity regulating valve, atomizer, air and liquid mixer and water tank, nitrogen cylinder
Nitrogen flow electricity regulating valve is accessed after connecting pressure reducing valve, air and liquid mixer is then accessed and is then connected to the nitrogen on launching platform top surface
Gas fast interface, atomizer entrance are connected to water tank, and atomizer exit is connect with the collateral mouth of air and liquid mixer.
5. the fuel cell-powered unmanned plane launching platform of one kind according to claim 4, it is characterised in that: the operation
System includes UAV system status indicator lamp, total power switch, air loop atomizer switchs, nitrogen circuit atomizer is opened
Pass, air pump speed-regulating switch, nitrogen flow regulating switch, electronic load adjusting knob, liquid crystal display and buzzer, they
Setting is in unmanned plane launching platform outer surface, UAV system status indicator lamp, liquid crystal display and buzzer and control system
It unites and connects, air loop atomizer switch and nitrogen circuit atomizer switch are connect with atomizer, air pump speed-regulating switch and sky
Air pump is connected, and nitrogen flow regulating switch is connected with nitrogen flow electricity regulating valve, electronic load adjusting knob and electronic load phase
Even.
6. the fuel cell-powered unmanned plane launching platform of one kind according to claim 5, it is characterised in that: the control
System is master board, and master board connects electromagnetism separate connector, lithium battery pack, electronic load, air pump, nitrogen electromagnetic current
Adjustable valve, status indicator lamp, alarm buzzer, electromagnetic drive fixing lock, atomizer, display screen and communication system, are used for
Power transmission, transformation, distribution, control, information acquisition process and with each device communicate.
7. the fuel cell-powered unmanned plane launching platform of one kind according to claim 6, it is characterised in that: the communication
System is wireless data sending/receiving module, is arranged inside unmanned plane launching platform, unmanned plane launching platform outer surface is equipped with
Master board and third party for realizing the communication of master board and UAV system, and are realized in wireless data transceiving port
The communication of information process unit.
8. the fuel cell-powered unmanned plane launching platform of one kind according to claim 7, it is characterised in that: described to take off
Nitrogen cylinder inflating port is provided on platform top surface, the inflating port is connected to through check valve with nitrogen cylinder.
9. the fuel cell-powered unmanned plane launching platform of one kind according to claim 8, it is characterised in that: described to take off
Water tank filler is additionally provided on platform top surface, the water tank filler is connected to the water tank built in platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820913710.7U CN208412174U (en) | 2018-06-13 | 2018-06-13 | A kind of fuel cell-powered unmanned plane launching platform |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201820913710.7U CN208412174U (en) | 2018-06-13 | 2018-06-13 | A kind of fuel cell-powered unmanned plane launching platform |
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| CN208412174U true CN208412174U (en) | 2019-01-22 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108725823A (en) * | 2018-06-13 | 2018-11-02 | 杭州氢航科技有限公司 | A kind of fuel cell-powered unmanned plane launching platform |
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2018
- 2018-06-13 CN CN201820913710.7U patent/CN208412174U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108725823A (en) * | 2018-06-13 | 2018-11-02 | 杭州氢航科技有限公司 | A kind of fuel cell-powered unmanned plane launching platform |
| CN108725823B (en) * | 2018-06-13 | 2024-04-09 | 浙江氢航科技有限公司 | Unmanned aerial vehicle take-off platform powered by fuel cell |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: No. 15, general aviation industrial park, LEIDIAN Town, Deqing County, Huzhou City, Zhejiang Province (Moganshan national high tech Zone) Patentee after: Zhejiang Hydrogen Technology Co., Ltd Address before: 310000 13, 3, 301, Yangcheng Road, fengyao industrial area, Yuhang, Hangzhou, Zhejiang. Patentee before: Hangzhou hydrogen Navigation Technology Co., Ltd. |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190122 Termination date: 20210613 |