CN206258112U - Rotary wind type depopulated helicopter for patrolling and examining communication base station - Google Patents
Rotary wind type depopulated helicopter for patrolling and examining communication base station Download PDFInfo
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- CN206258112U CN206258112U CN201621360911.6U CN201621360911U CN206258112U CN 206258112 U CN206258112 U CN 206258112U CN 201621360911 U CN201621360911 U CN 201621360911U CN 206258112 U CN206258112 U CN 206258112U
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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
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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
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
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Abstract
The utility model discloses a kind of rotary wind type depopulated helicopter for patrolling and examining communication base station, the UAV Flight Control device of the depopulated helicopter is electrically connected with picture pick-up device of taking photo by plane, reception of wireless signals and transmitter, methanol-water recasting hydrogen and power generation module group, delivery pump, electric power controller, energy storage battery, helicopter motor, main transmission, auxiliary driving system；Picture pick-up device of taking photo by plane is used to patrol and examine communication base station, to obtain the realtime image data of communication base station, while the realtime image data is sent to ground control station by reception of wireless signals and transmitter；Methanol-water reformation hydrogen production and power generation module group are integrated with reformer and fuel cell, and the electricity that fuel cell sends is powered for helicopter motor/energy storage battery/UAV Flight Control device.The utility model capacity usage ratio and conversion ratio is high, lighter in weight, voyage is remote, cruising time is long, operating cost is low, body run in itself it is free from environmental pollution.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of rotary wind type for patrolling and examining communication base station nobody
Helicopter.
Background technology
At present, Communication in China base station has been covered to national regional, and traditional manual inspection mode has met not
The widespread demand of Modern Communication System, and the birth that unmanned plane is patrolled and examined to make to patrol and examine improved efficiency very notable, particularly nobody
Machine is patrolled and examined and is especially suitable for applying on the communication base station of the remote districts such as mountain area, waste ridge, lake, and natural calamity causes road to be received
When resistance, personnel cannot patrol and examine, these areas are with a varied topography, and manual inspection mode is expert at time-consuming many on road, and efficiency is low, nobody
Machine can play substitution effect, and visual angle is wider, be avoided that " blind spot ".
It is presently used for patrolling and examining the unmanned plane mainly rotary wind type depopulated helicopter of communication base station, rotary wind type depopulated helicopter
It is few with landing limitation, can hover and take pictures, operate flexible advantage.Currently used for patrol and examine communication base station rotary wind type nobody go straight up to
Machine has two kinds of power modes：
One kind is that its fuel consumption is very big, and fuel oil utilization ratio is relatively low as power using Aviation Fuel engine,
Therefore unmanned plane needs to carry a large amount of Aviation Fuels, and not only Aviation Fuel price is high, high cost, and causes the weight of unmanned plane
Amount is heavier, in addition it is also necessary to set the generator driven by fuel engines, is powered with to body control system, sets and generates electricity
After machine, the load of fuel engines is increased, reduce energy conversion efficiency；Also, Aviation Fuel engine operationally can
Large quantity of exhaust gas is produced, air pollution is caused, is unfavorable for environmental protection.
Another kind is to use motor as power, using rechargeable power battery group as power supply, its chargeable power
Battery pack is very heavy, and cruising time is very short, it is difficult to be applied to patrol and examine communication base station.
Utility model content
The technical problems to be solved in the utility model is directed to above-mentioned deficiency of the prior art, there is provided one kind is for patrolling and examining
The rotary wind type depopulated helicopter of communication base station, the depopulated helicopter capacity usage ratio and conversion ratio is high, lighter in weight, voyage are remote,
Cruising time is long, operating cost is low, body run in itself it is free from environmental pollution.
In order to solve the above technical problems, the technical solution of the utility model is：A kind of rotor for patrolling and examining communication base station
Formula depopulated helicopter, it is characterised in that：Including UAV Flight Control device, picture pick-up device of taking photo by plane, reception of wireless signals and transmission
Device, methanol-water recasting hydrogen and power generation module group, air feed track, methanol-water storage container, delivery pump, electric power controller, energy storage store
Battery, helicopter motor, main transmission, propeller, auxiliary driving system, tail-rotor, wherein：
The UAV Flight Control device is electrically connected with picture pick-up device of taking photo by plane, reception of wireless signals and transmitter, first
Alcohol water recasting hydrogen and power generation module group, delivery pump, electric power controller, energy storage battery, helicopter motor, main transmission, secondary biography
Dynamic system；The picture pick-up device of taking photo by plane is used to patrol and examine communication base station, to obtain the realtime image data of communication base station, together
When the realtime image data is sent to ground control station by reception of wireless signals and transmitter；
The methanol-water reformation hydrogen production and power generation module group are integrated with reformer and fuel cell, and weight is provided with the reformer
Whole room and hydrogen purification apparatus, the temperature of reformer chamber is 300-570 DEG C of temperature, and reformer chamber is provided with catalyst, first alcohol and water
The reformation hydrogen production reaction that first alcohol and water occurs in reformer chamber is obtained hydrogen-containing gas, and reformer chamber is with hydrogen purification apparatus by being connected
Pipeline is connected, and all or part of connecting line is arranged at reformer chamber, can continue to heat from weight by the high temperature of reformer chamber
The gas of whole room output；The connecting line is used as the buffering between reformer chamber and hydrogen purification apparatus so that defeated from reformer chamber
The temperature of the gas for going out is identical with the temperature of hydrogen purification apparatus or close, and hydrogen is obtained from the aerogenesis end of hydrogen purification apparatus,
It is supplied to fuel cell；The fuel cell is used for hydrogen and electrochemical reaction generation electric energy occurs with the oxygen in air；
The air feed track is used to be input into outside air, and the outside air of input is discharged through fuel cell, in fuel electricity
Chi Zhong, air electrochemical reaction is provided for fuel cell required for oxygen, and be fuel cell radiating and cooling；
The first alcohol and water raw material of liquid is stored in the methanol-water storage container, the delivery pump is used to store up methanol-water
Deposit first alcohol and water feedstock transportation in container to methanol-water reformation hydrogen production and the reformer of power generation module group；
The electric power controller is used to for the electric energy that fuel cell is exported to be converted to helicopter motor/energy storage battery/nothing
The man-machine required appropriate voltage of flight controller, the alternating current/direct current of electric current；The energy storage battery is gone straight up to for nobody
Machine is powered when starting, and is helicopter motor power supplying when helicopter motor real-time power increases rapidly；
The helicopter motor drives propeller to rotate by main transmission, is revolved by auxiliary driving system drive tail-rotor
Turn.
The methanol-water reformation hydrogen production and power generation module group at least provided with two groups, the delivery pump at least provided with two,
And methanol-water reformation hydrogen production and power generation module group match with the quantity of delivery pump.
Heat exchanger, the methyl alcohol of low temperature are provided between the delivery pump and methanol-water reformation hydrogen production and the reformer of power generation module group
With water raw material in heat exchanger, the high-temperature hydrogen exported with reformer is exchanged heat, and methyl alcohol and coolant-temperature gage are raised, vaporized, high temperature
Hydrogen temperature reduction, transfers to the fuel cell of methanol-water reformation hydrogen production and power generation module group.
The reformer is provided with electric heater, and by fuel cell-powered, the electric heater is carried the electric heater for reformer chamber
For 300-570 DEG C of temperature.
The energy storage battery includes the battery pack with some cells, battery pack information acquisition module, balanced control
Molding block, battery pack protection module；Each cell electricity in the input and battery pack of the battery pack information acquisition module
Property connection, the output end of the battery pack information acquisition module is electrically connected with the UAV Flight Control device；It is described nobody
Machine flight controller is also electrically connected with equalization control module, battery pack protection module, the equalization control module, battery pack protection
Module is also electrically connected with each cell in the battery pack respectively；The equalization control module uses passive resistance energy consumption
Balance route pattern, is balanced foundation with the cell terminal voltage in lithium battery group, and the equalization control module is according to battery
Group information acquisition module Real-time Collection to data to certain section or it is a few section cell do equilibrium treatment.
The rotary wind type depopulated helicopter also includes global positioning module, course sensing module, highly sensing module, air speed
Sensing module, flight attitude sensing module；The UAV Flight Control device is electrically connected with global positioning module, course and passes
Sense module, highly sensing module, air speed sensing module, flight attitude sensing module.The global positioning module is fixed for gps satellite
Position module or big-dipper satellite locating module；The air speed sensing module is pitot；The course sensing module navigates for three axle magnetic
To sensor；The highly sensing module is semiconductor silicon pressure resistance type pressure-altitude sensor；The flight attitude sensing module
Vertical gyroscope and detection depopulated helicopter pitching/tilt attitude angle including detection depopulated helicopter pitching/tilt attitude angle
The angular rate gyroscope of speed.
The beneficial effects of the utility model are：
（1）It is that engine and fuselage control system are powered that the utility model uses methanol-water reformation hydrogen production and power generation module group,
Mode of traditional Aviation Fuel engine as power has been abandoned in spelling, is also spelled and has been abandoned using motor and rechargeable power battery group phase
The power mode of cooperation, methanol-water low in raw material price, energy density is big, and methanol-water reformation hydrogen production and power generation module group are to first
The utilization ratio of alcohol water raw material can reach more than 99%, and methanol-water reformation hydrogen production and power generation module group own wt are also very light, because
This, rotary wind type depopulated helicopter, with a large amount of Aviation Fuels, without heavy rechargeable power battery group is installed, is only needed without prompt
The prompt methanol-water raw material with lighter, so as to significantly alleviate the weight of rotary wind type depopulated helicopter；
（2）Methanol-water reformation hydrogen production of the present utility model and power generation module group, while for helicopter motor power supplying, can be straight
It is connected in aircraft control system modules to power, thus without additionally mounted generator, reduces the load of helicopter motor；
（3）The utility model carries out reformation hydrogen production using methanol-water raw material, and by fuel cell power generation, uncontaminated gases
Produce, body runs free from environmental pollution in itself；
（4）Preferred embodiment of the present utility model uses at least two groups methanol-water reformation hydrogen productions and power generation module group, when instant work(
When rate demand is smaller, less methanol-water reformation hydrogen production power generation module group operating, when instant power demand is larger, control are controlled
The more methanol-water reformation hydrogen production power generation module group operating of system, accordingly, it is capable to greatly reduce zero load, its integrally power consumption it is smaller, methyl alcohol and
Water consumption of raw materials is relatively low, utilization rate is high, and stability and reliability is good, intelligent high；
（5）In preferred embodiment of the present utility model, the equalization control module of energy storage battery can be adopted according to battery pack information
Collection module Real-time Collection to data to certain section or it is a few section cell do equilibrium treatment, improve monomer in lithium battery group
Battery with two side terminals, using capacity and service life, and improve the flight safety of rotary wind type depopulated helicopter.
Brief description of the drawings
Fig. 1 is overall structure block diagram of the present utility model.
Fig. 2 is methanol-water reformation hydrogen production of the present utility model and power generation module group block diagram.
Fig. 3 is the overall structure block diagram of the preferred embodiment of the utility model one.
Fig. 4 is the block diagram that methanol-water reformation hydrogen production of the present utility model and power generation module group are engaged with heat exchanger.
Fig. 5 is Control system architecture block diagram of the present utility model.
Fig. 6 is the block diagram that energy storage battery of the present utility model is engaged with UAV Flight Control device.
Specific embodiment
Structural principle of the present utility model and operation principle are described in further detail below in conjunction with the accompanying drawings.
Embodiment one
As shown in Fig. 1~Fig. 6, the utility model is a kind of rotary wind type depopulated helicopter for patrolling and examining communication base station, bag
Include UAV Flight Control device 1, take photo by plane picture pick-up device 2, reception of wireless signals and transmitter 3, methanol-water recasting hydrogen and generating mould
Group 4, air feed track 5, methanol-water storage container 6, delivery pump 7, electric power controller 8, energy storage battery 9, helicopter motor 10,
Main transmission 11, propeller 12, auxiliary driving system 13, tail-rotor 14, wherein：
The UAV Flight Control device 1 be electrically connected with take photo by plane picture pick-up device 2, reception of wireless signals and transmitter 3,
Methanol-water recasting hydrogen and power generation module group 4, delivery pump 5, electric power controller 8, energy storage battery 9, helicopter motor 10, main transmission
System 11, auxiliary driving system 13；The picture pick-up device 2 of taking photo by plane is used to patrol and examine communication base station, to obtain the reality of communication base station
When view data, while the realtime image data is sent to ground control station by reception of wireless signals and transmitter 3；
The methanol-water reformation hydrogen production and power generation module group 4 are integrated with reformer 41 and fuel cell 42, the reformer 41
Reformer chamber and hydrogen purification apparatus are inside provided with, the temperature of reformer chamber is 300-570 DEG C of temperature, and the reformer chamber is provided with catalysis
, in the presence of catalyst, there is methanol decomposition reaction and the transformationreation of carbon monoxide in agent, generate hydrogen and carbon dioxide,
This is component more than, the gas solid catalytic reaction system of many reactions, and reactional equation is：(1)CH3OH→CO+2H2、(2)H2O+CO
→CO2+H2 、(3)CH3OH+H2O→CO2+3H2, the high-temperature gas mixture body based on carbon dioxide and hydrogen is obtained；Reformer chamber with
Hydrogen purification apparatus are connected by connecting line, and all or part of connecting line is arranged at reformer chamber, can pass through reformer chamber
Interior high temperature continues to heat the gas from reformer chamber output；The connecting line is used as between reformer chamber and hydrogen purification apparatus
Buffering so that the temperature from the gas of reformer chamber output is identical with the temperature of hydrogen purification apparatus or close, from hydrogen purification dress
The aerogenesis end put obtains hydrogen, is supplied to fuel cell 42；The fuel cell 42 is used for hydrogen to be occurred with the oxygen in air
Electrochemical reaction produces electric energy；In the anode of fuel cell 42：2H2→4H++4e-, H2Two protons and two electronics are split into,
Proton passes through PEM（PEM）, electronics by external loading, and enters cathode bipolar plate by positive plate, in fuel electricity
The negative electrode in pond 42：O2+4e-+4H+→2H2O, proton, electronics and O2Recombine to form H2O；
The air feed track 5 is used to be input into outside air, and the outside air of input is discharged through fuel cell 42, in fuel
In battery 42, air is the oxygen required for fuel cell 42 provides electrochemical reaction, and is the radiating and cooling of fuel cell 42；
The first alcohol and water raw material of liquid is stored in the methanol-water storage container 6, the delivery pump 7 is used for methanol-water
First alcohol and water feedstock transportation in storage container 6 to methanol-water reformation hydrogen production and power generation module group 4 reformer 41；
The electric power controller 8 is used to for the electric energy that fuel cell 41 is exported to be converted to the energy storage electric power storage of helicopter motor 10/
The required appropriate voltage of 9/ UAV Flight Control device of pond 1, the alternating current/direct current of electric current；The energy storage battery 9 is used for
Depopulated helicopter is powered when starting, and is that helicopter motor 10 is powered when the real-time power of helicopter motor 10 increases rapidly；
The helicopter motor 10 drives propeller 12 to rotate by main transmission 11, is driven by auxiliary driving system 13
Tail-rotor 14 rotates.
As shown in figure 3, the methanol-water reformation hydrogen production and power generation module group 4 are at least provided with two groups, the delivery pump 7 is at least
Two are provided with, and methanol-water reformation hydrogen production and power generation module group 4 match with the quantity of delivery pump 7.When the multigroup methanol-water of setting
When reformation hydrogen production and power generation module group, miniature methanol-water reformation hydrogen production and power generation module group preferably using power less than 500W.When
When real-time power demand is smaller, control less methanol-water reformation hydrogen production power generation module group operating, when instant power demand compared with
When big, more methanol-water reformation hydrogen production power generation module group operating is controlled.
As shown in figure 4, be provided between the reformer 41 of the delivery pump 7 and methanol-water reformation hydrogen production and power generation module group 4 changing
Hot device 43, the first alcohol and water raw material of low temperature in heat exchanger 43, with reformer 41 export high-temperature hydrogen exchanged heat, methyl alcohol and
Coolant-temperature gage is raised, vaporization, and the reduction of high-temperature hydrogen temperature transfers to the fuel cell 42 of methanol-water reformation hydrogen production and power generation module group 4.
As the preferred embodiment of reformer 41, combustion chamber is provided with reformer, the combustion chamber is used for the obtained hydrogen in part
With the oxygen combustion in outside air, for the operation of reformer 41 provides heat；As shown in figure 4, as the more excellent of reformer 41
Mode is selected, the reformer 41 is provided with electric heater, and the electric heater is powered by fuel cell 42, the electric heater is reformer chamber
300-570 DEG C of temperature is provided.
As shown in fig. 6, the energy storage battery 9 includes that the battery pack 91, battery pack information with some cells is adopted
Collection module 92, equalization control module 93, battery pack protection module 94；The input of the battery pack information acquisition module 92 and electricity
Each cell in pond group 91 is electrically connected with, output end and the unmanned plane during flying of the battery pack information acquisition module 92
Controller 1 is electrically connected with；The UAV Flight Control device 1 is also electrically connected with equalization control module 93, battery pack protection module
94, the equalization control module 93, battery pack protection module 94 are also electrical with each cell in the battery pack 91 respectively
Connection；The equalization control module 93 uses passive resistance energy consumption balance control model, with the cell end in battery pack 91
Voltage is balanced foundation, and the data that the equalization control module 93 is arrived according to the Real-time Collection of battery pack information acquisition module 92 are to certain
Section or a few section cells do equilibrium treatment.The battery pack information acquisition module includes that voltage acquisition module, temperature are adopted
Collection module, current acquisition module, read voltage, temperature, the battery set charge/discharge current information of each cell of battery pack in real time.
The battery protection module include battery overcharge circuit, overdischarge circuit, cross current circuit, short circuit current and temperature it is too high or
The circuit protected to battery pack when temperature is too low.
As shown in figure 5, the rotary wind type depopulated helicopter for being used to patrol and examine communication base station also includes global positioning module 15, boat
To sensing module 16, highly sensing module 17, air speed sensing module 18, flight attitude sensing module 19；The unmanned plane during flying
Controller 1 is electrically connected with global positioning module 15, course sensing module 16, highly sensing module 17, air speed sensing module
18th, flight attitude sensing module 19.Preferably, the global positioning module 15 is that gps satellite locating module or big-dipper satellite are fixed
Position module；The air speed sensing module 16 is pitot；The course sensing module 17 is three axle magnetic course transmitters；The height
Degree sensing module 18 is semiconductor silicon pressure resistance type pressure-altitude sensor；The flight attitude sensing module 19 includes detecting nobody
The vertical gyroscope of helicopter pitching/tilt attitude angle and the angular speed of detection depopulated helicopter pitching/tilt attitude angular rate
Gyroscope.
Embodiment two
In the above-mentioned technical solutions, the flight controlling party for patrolling and examining the rotary wind type depopulated helicopter of communication base station
Method, including following job step：
A. start rotary wind type depopulated helicopter, be UAV Flight Control device, first by energy storage battery in start-up course
Alcohol water reformation hydrogen production power generation module group and delivery pump are powered；After the startup of methanol-water reformation hydrogen production power generation module group, by methanol-water weight
Whole preparing hydrogen, generating power module is UAV Flight Control device, delivery pump and helicopter motor power supplying, and for energy storage battery charges；
B. rotary wind type depopulated helicopter target spatial domain, in flight course, methanol-water is reformed and made by electric power controller
It is required appropriate that the electric energy of hydrogen power generation module group output is converted to helicopter motor/energy storage battery/UAV Flight Control device
Alternating current/the direct current of voltage, electric current, when helicopter motor real-time power increases rapidly, energy storage battery and methanol-water weight
Whole preparing hydrogen, generating power module is together helicopter motor power supplying；
C. communication base station is patrolled and examined, picture pick-up device of taking photo by plane is patrolled and examined communication base station, obtains the realtime graphic of communication base station
Data, while the realtime image data is sent to ground control station by reception of wireless signals and transmitter, work is patrolled and examined in completion
Industry.
Preferably, at least provided with two groups, helicopter motor is worked for the methanol-water reformation hydrogen production and power generation module group
Cheng Zhong, UAV Flight Control device is fed back to by real-time power demand；UAV Flight Control device is according to real-time power demand
Amount information controls an appropriate number of methanol-water reformation hydrogen production power generation module group operating, and controls methanol-water Storing and conveying device to operating
Methanol-water reformation hydrogen production power generation module group conveying methanol-water raw material；When instant power demand is smaller, less methyl alcohol is controlled
Water reformation hydrogen production power generation module group is operated, and when instant power demand is larger, controls more methanol-water reformation hydrogen production generating mould
Group operating.
Preferably, the flight control method for patrolling and examining the rotary wind type depopulated helicopter of communication base station, its feature exists
In：
A. rotary wind type depopulated helicopter is in flight course, ground control station by reception of wireless signals and transmitter to
UAV Flight Control device sends control instruction；Correspondingly, UAV Flight Control device passes through reception of wireless signals and transmitter
Earthward control station sends communication base station image data information；
B. in flight course, UAV Flight Control device gathers global positioning module to rotary wind type depopulated helicopter respectively
Latitude and longitude information, the course information of course sensing module, the unmanned plane elevation information of highly sensing module, air speed sensing module
The unmanned plane during flying attitude information of unmanned plane during flying velocity information, flight attitude sensing module；
C. UAV Flight Control device collects latitude and longitude information, course information, unmanned plane elevation information, unmanned plane during flying
After velocity information, unmanned plane during flying attitude information, by controlling helicopter motor, main transmission and auxiliary driving system come real
Now turning, lifting, hovering and the adjustment of the speed of a ship or plane, and instant control information is fed back into ground control station.
The above, is only the utility model better embodiment, it is every according to the technical solution of the utility model to
On implementation method any trickle amendment, equivalent variations and the modification made, belong to the scope of technical solutions of the utility model
It is interior.
Claims (7)
1. it is used to patrol and examine the rotary wind type depopulated helicopter of communication base station, it is characterised in that：Including UAV Flight Control device, take photo by plane
Picture pick-up device, reception of wireless signals and transmitter, methanol-water recasting hydrogen and power generation module group, air feed track, methanol-water storage are held
Device, delivery pump, electric power controller, energy storage battery, helicopter motor, main transmission, propeller, auxiliary driving system, tail-rotor,
Wherein：
The UAV Flight Control device is electrically connected with picture pick-up device of taking photo by plane, reception of wireless signals and transmitter, methanol-water
Recasting hydrogen and power generation module group, delivery pump, electric power controller, energy storage battery, helicopter motor, main transmission, auxiliary driving system
System；The picture pick-up device of taking photo by plane is used to patrol and examine communication base station, to obtain the realtime image data of communication base station, while will
The realtime image data is sent to ground control station by reception of wireless signals and transmitter；
The methanol-water reformation hydrogen production and power generation module group are integrated with reformer and fuel cell, and reformer chamber is provided with the reformer
And hydrogen purification apparatus, the temperature of reformer chamber is 300-570 DEG C of temperature, and reformer chamber is provided with catalyst, and first alcohol and water is in weight
The reformation hydrogen production reaction of whole indoor generation first alcohol and water is obtained hydrogen-containing gas, and reformer chamber passes through connecting line with hydrogen purification apparatus
Connection, all or part of connecting line is arranged at reformer chamber, can continue to heat from reformer chamber by the high temperature of reformer chamber
The gas of output；The connecting line is used as the buffering between reformer chamber and hydrogen purification apparatus so that from reformer chamber output
The temperature of gas is identical with the temperature of hydrogen purification apparatus or close, and hydrogen is obtained from the aerogenesis end of hydrogen purification apparatus, supply
To fuel cell；The fuel cell is used for hydrogen and electrochemical reaction generation electric energy occurs with the oxygen in air；
The air feed track is used to be input into outside air, and the outside air of input is discharged through fuel cell, in a fuel cell,
Air electrochemical reaction is provided for fuel cell required for oxygen, and be fuel cell radiating and cooling；
The first alcohol and water raw material of liquid is stored in the methanol-water storage container, the delivery pump is used to for methanol-water to store appearance
First alcohol and water feedstock transportation in device is to methanol-water reformation hydrogen production and the reformer of power generation module group；
The electric power controller is used to for the electric energy that fuel cell is exported to be converted to helicopter motor/energy storage battery/unmanned plane
Alternating current/the direct current of the required appropriate voltage of flight controller, electric current；The energy storage battery is opened for depopulated helicopter
Powered when dynamic, and be helicopter motor power supplying when helicopter motor real-time power increases rapidly；
The helicopter motor drives propeller to rotate by main transmission, is rotated by auxiliary driving system drive tail-rotor.
2. the rotary wind type depopulated helicopter for patrolling and examining communication base station according to claim 1, it is characterised in that：The first
, at least provided with two groups, the delivery pump is at least provided with two, and methanol-water is reformed and made for alcohol water reformation hydrogen production and power generation module group
Hydrogen and power generation module group match with the quantity of delivery pump.
3. the rotary wind type depopulated helicopter for patrolling and examining communication base station according to claim 1, it is characterised in that：It is described defeated
Send and heat exchanger is provided between pump and methanol-water reformation hydrogen production and the reformer of power generation module group, the first alcohol and water raw material of low temperature is in heat exchange
In device, the high-temperature hydrogen exported with reformer is exchanged heat, and methyl alcohol and coolant-temperature gage are raised, vaporized, and the reduction of high-temperature hydrogen temperature is defeated
To methanol-water reformation hydrogen production and the fuel cell of power generation module group.
4. the rotary wind type depopulated helicopter for patrolling and examining communication base station according to claim 1, it is characterised in that：It is described heavy
Whole device is provided with electric heater, and by fuel cell-powered, the electric heater provides 300-570 DEG C of temperature to the electric heater for reformer chamber
Degree.
5. the rotary wind type depopulated helicopter for patrolling and examining communication base station according to claim 1, it is characterised in that：The storage
Energy storage device includes that the battery pack with some cells, battery pack information acquisition module, equalization control module, battery pack are protected
Shield module；The input of the battery pack information acquisition module is electrically connected with each cell in battery pack, the battery
The output end of group information acquisition module is electrically connected with the UAV Flight Control device；The UAV Flight Control device is also electric
Property connection equalization control module, battery pack protection module, the equalization control module, battery pack protection module also respectively with it is described
Each cell in battery pack is electrically connected with；The equalization control module uses passive resistance energy consumption balance control model, with
Cell terminal voltage in lithium battery group is balanced foundation, and the equalization control module is according to battery pack information acquisition module reality
When the data that collect equilibrium treatment is done to certain section or a few section cells.
6. the rotary wind type depopulated helicopter for patrolling and examining communication base station according to claim 1, it is characterised in that：The rotor
Formula depopulated helicopter also includes global positioning module, course sensing module, highly sensing module, air speed sensing module, flight appearance
State sensing module；The UAV Flight Control device is electrically connected with global positioning module, course sensing module, highly sensing
Module, air speed sensing module, flight attitude sensing module.
7. the rotary wind type depopulated helicopter for patrolling and examining communication base station according to claim 6, it is characterised in that：It is described complete
Ball locating module is gps satellite locating module or big-dipper satellite locating module；The air speed sensing module is pitot；The boat
It is three axle magnetic course transmitters to sensing module；The highly sensing module is semiconductor silicon pressure resistance type pressure-altitude sensor；
The flight attitude sensing module includes the vertical gyroscope of detection depopulated helicopter pitching/tilt attitude angle and detects that nobody is straight
The angular rate gyroscope of the machine of liter pitching/tilt attitude angular rate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621360911.6U CN206258112U (en) | 2016-12-13 | 2016-12-13 | Rotary wind type depopulated helicopter for patrolling and examining communication base station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621360911.6U CN206258112U (en) | 2016-12-13 | 2016-12-13 | Rotary wind type depopulated helicopter for patrolling and examining communication base station |
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| Publication Number | Publication Date |
|---|---|
| CN206258112U true CN206258112U (en) | 2017-06-16 |
Family
ID=59028935
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| Application Number | Title | Priority Date | Filing Date |
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| CN201621360911.6U Active CN206258112U (en) | 2016-12-13 | 2016-12-13 | Rotary wind type depopulated helicopter for patrolling and examining communication base station |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
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