CN207657728U - The vehicle and carrying structure, control system of unmanned plane can be carried - Google Patents
The vehicle and carrying structure, control system of unmanned plane can be carried Download PDFInfo
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- CN207657728U CN207657728U CN201721624767.7U CN201721624767U CN207657728U CN 207657728 U CN207657728 U CN 207657728U CN 201721624767 U CN201721624767 U CN 201721624767U CN 207657728 U CN207657728 U CN 207657728U
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Abstract
The utility model discloses the vehicle that can carry unmanned plane and carrying structure, control systems, are related to UAV flight and control technology field.A kind of vehicle carrying unmanned plane, including vehicle body structure；The vehicle body structure tail portion is provided with UAV flight's structure, UAV flight's structure includes ontology and lid, the lid is installed on by active connection on ontology so that the lid can be unfolded relative to ontology, the carrying platform of the lid of the expansion as unmanned plane.The utility model by vehicle tail be arranged UAV flight's structure, the carrying structure it is a part of deployable, the part after expansion can be used as the carrying platform of unmanned plane, be convenient for UAV flight and manipulation.
Description
Technical field
The utility model is related to UAV flights and control technology field.
Background technology
Unmanned vehicle, abbreviation unmanned plane (UAV, Unmanned Aerial Vehicle) is one kind with radio
Not manned vehicle based on remote control or the control of itself program.It is wanted with maneuverability, rapid reaction, unmanned flight, operation
Seek low advantage.Unmanned plane may be implemented image real-time Transmission, high-risk areas detecting function, be by carrying multiclass sensor
The strong supplement of satellite remote sensing and traditional air remote sensing.Currently, the use scope of unmanned vehicle widened it is military,
Scientific research, civilian three big field, specifically electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, crops are estimated
The fields applications such as production, drug law enforcement anti-smuggling, border patrol, public security anti-terrorism are very wide.Wherein, it is used because small unmanned vehicles have
Simply, the features such as relatively more convenient is carried, it is especially prominent in the application of civilian aspect.
But current small drone, the Special horizontal suitable for taking off, landing still is lacked in generally existing carrying process
Platform and the problem of manipulation inconvenience.
Invention content
The purpose of this utility model is that：A kind of vehicle carrying unmanned plane is overcome the deficiencies of the prior art and provide
And carrying structure, control system.The utility model by vehicle tail be arranged UAV flight's structure, the one of the carrying structure
Part is deployable, and the part after expansion can be used as the carrying platform of unmanned plane, is convenient for UAV flight and manipulation.
To realize that above-mentioned target, the utility model provide following technical solution：
A kind of vehicle carrying unmanned plane, including vehicle body structure；The vehicle body structure tail portion is provided with nothing
Man-machine carrying structure, UAV flight's structure include ontology and lid, and the lid is installed on this by active connection
On body so that the lid can be unfolded relative to ontology, the carrying platform of the lid of the expansion as unmanned plane.
Further, the lid of the expansion can be used as the lifting support platform of unmanned plane.
Further, it is provided with electromagnetically component on the lid, magnetic firmware, nothing are provided on the undercarriage of the unmanned plane
It is man-machine when needing landing, it is powered to electromagnetically component, is acted on by the magnetic suck of the electromagnetically component and magnetic firmware, make nobody
Machine steadily lands.
Further, it is provided with ejection structure on the lid, when the unmanned plane needs to take off, passes through the ejection structure
Driving unmanned plane flies out or assists unmanned plane to fly out by the ejection structure.
Further, the ontology is to be installed on vehicle body structure tail portion, support plate with one fixed width, the branch
Accommodating chamber of the space that fagging is limited with the lid in folded state as unmanned plane.
Further, the ontology is body structure, and the accommodating chamber of the babinet is indent in the space of vehicle body tail portion,
Or the accommodating chamber of the babinet is to protrude from the space of vehicle body tail portion.
Preferably, there is the babinet opening and the installation cavity with open communication, the lid can be opened and closed to be arranged in institute
State opening, when the lid is closed, the babinet and lid form closing chamber, in the closing chamber to place it is aforementioned nobody
Machine.
Further, the active connection is convertible rotational structure, and the lid can be overturn relative to babinet to be unfolded
Or it is closed.
Alternatively, the active connection is flat-open type on-off structure, the lid can be put down relative to babinet in horizontal direction
It moves to be unfolded or be closed.
Alternatively, the active connection is rotary opening and closing structure, the lid can be rotated up relative to babinet in level
To be unfolded or be closed.
Further, charging structure, the input terminal and vehicle mounted electric of the charging structure are provided on the ontology and/or lid
Source connects, and the output end of the charging structure is provided with micro USB electrical interface or wireless charging contact, the wireless charging contact
It can be connect with the wireless charging end of unmanned plane and/or data transmission terminal.
Further, it is provided with wireless signal transceiver on the lid, to position unmanned plane and be carried out with unmanned plane
Wireless telecommunications.
Further, UAV flight's structure is to be detachably connected with vehicle body structure, is provided therebetween slow
Rush structure.
Further, electric control lock, the switch setting of the control circuit of the electric control lock are provided between the ontology and lid
In in the display structure of car-mounted terminal.
Further, the lid after deployment, can carry out transverse shifting to be laterally extended relative to ontology.
The invention also discloses a kind of UAV flight's structure, UAV flight's structure is installed on vehicle tail
Portion, including ontology and lid；The lid is installed on by active connection on babinet so that the lid can be relative to ontology
Expansion, the carrying platform of the lid of the expansion as unmanned plane.
Further, the lid of the expansion can be used as the lifting support platform of unmanned plane.
The invention also discloses a kind of control systems of unmanned plane, and the system comprises unmanned plane, UAV flights
Structure and controller,
UAV flight's structure is installed on vehicle tail, including ontology and lid, and the lid passes through flexible connection
Part is installed on ontology so that the lid can be unfolded relative to ontology, and the lid of the expansion is flat as the carrying of unmanned plane
Platform；
The controller is communicated to connect with unmanned plane and UAV flight's structure, is controlled after capable of triggering aforementioned lid expansion
Unmanned plane processed flies out, and triggers the lid after control unmanned plane withdrawal and fold.
The utility model due to using the technology described above, compared with prior art, as an example, has the following advantages that
And good effect：By vehicle tail be arranged UAV flight's structure, the carrying structure it is a part of deployable, after expansion
The part can be used as the carrying platform of unmanned plane, specifically, the carrying platform can be used as the platform that rises and falls, the placement platform of unmanned plane
Deng convenient for user's manipulation unmanned plane.When the carrying structure is packed up, the storage device of unmanned plane is can be used as, one is played to unmanned plane
Fixed protective effect.
Description of the drawings
Fig. 1 is the vehicle structure schematic diagram with open carrying structure that the utility model embodiment provides.
Fig. 2 is the vehicle structure schematic diagram with box-type carrying structure that the utility model embodiment provides.
Fig. 3 is the vehicle structure schematic diagram with indent box-type carrying structure that the utility model embodiment provides.
Fig. 4 is the structural schematic diagram that the unmanned plane that the utility model embodiment provides takes off from lid.
Fig. 5 is the structural schematic diagram for the lid being laterally extended that the utility model embodiment provides.
Fig. 6 is the structural schematic diagram for UAV flight's structure that the utility model embodiment provides.
Fig. 7 is the frame construction drawing for the control system that the utility model embodiment provides.
Reference sign：
Vehicle 100, tail portion 110；
UAV flight's structure 200；Ontology 210, installation cavity 211, flexible wall 212, lockhole 213；Lid 220, electromagnetically
Component 221, wireless signal transceiver 222, electric control lock 223；Transverse moving structure 230；
Unmanned plane 300.
Specific implementation mode
To the vehicle disclosed by the utility model for carrying unmanned plane and knot is carried below in conjunction with the drawings and specific embodiments
Structure, control system are described in further detail.It should be noted that the technical characteristic or technology described in following embodiments are special
The combination of sign is not construed as isolated, they can be combined with each other to reach superior technique effect.Following
In the attached drawing of embodiment, the identical label that each attached drawing occurs represents identical feature or component, can be applied to different implementations
In example.Therefore, once being defined in a certain Xiang Yi attached drawing, then it need not further be begged in subsequent attached drawing
By.
It should be noted that structure, ratio, size etc. depicted in this specification institute attached drawing, only coordinating explanation
The revealed content of book is not limited to the enforceable limit of utility model so that those skilled in the art understands and reads
Fixed condition, the modification of any structure, the change of proportionate relationship or the adjustment of size, in the work(that does not influence utility model and can be generated
Under effect and the purpose that can reach, it should all fall in the range of the revealed technology contents of utility model can be covered.This practicality
The range of novel preferred embodiment includes other realization, wherein described or discussion the sequence, including root can not be pressed
According to involved function by it is basic simultaneously in the way of or in the opposite order, to execute function, this should be by the reality of the utility model
A person of ordinary skill in the field is applied to be understood.
Technology, method and apparatus known to person of ordinary skill in the relevant may be not discussed in detail, but suitable
In the case of, the technology, method and apparatus should be considered as authorizing part of specification.Institute that is shown here and discussing
Have in example, any occurrence should be construed as merely illustrative, not as limitation.Therefore, exemplary embodiment
Other examples can have different values.
Embodiment
It is shown in Figure 1, a kind of vehicle 100 carrying unmanned plane, including vehicle body structure.The vehicle body knot
Structure tail portion 110 is provided with UAV flight's structure 200, and UAV flight's structure 200 includes ontology 210 and lid 220, institute
It states lid 220 to be installed on ontology 210 by active connection so that the lid 220 can be unfolded relative to ontology 210, institute
State carrying platform of the lid 220 of expansion as unmanned plane 300.
Preferably, the lid 220 of the expansion can be used as the lifting support platform of unmanned plane, can be used for unmanned plane 300
Take off and/or land.
The unmanned plane 300 refers to unmanned vehicle in the present embodiment, be it is a kind of with wireless remotecontrol or itself
Aircraft based on program control.
The lid 220 can rigidly be put down made of metal or plastics as the carrying platform of unmanned plane
Platform.
The ontology 210 is mainly used for being based on vehicle tail, limits out the reception space that can accommodate unmanned plane 300.Ginseng
As shown in Figure 1, main body 210 can be to be installed on vehicle body structure tail portion 110, support plate with one fixed width, support
One end of plate can be fixedly mounted on vehicle tail 110, and the other end of support plate is flexibly connected lid 220.The width root
It is configured according to the size of unmanned plane, for example in Fig. 1 is set according to the height of unmanned plane 200.
Shown in Fig. 1, the support plate is connect by articulated shaft with lid 220, and lid 220 can be relative to the hinge
Spindle is rotated upwards can downwards be rotated to be unfolded with folding and lid 220 relative to the articulated shaft.Lid 220
When in folded state (lid 220 of dotted line in Fig. 1), the support plate is limited with the lid 220 in folded state
Accommodating chamber of the space as unmanned plane 300, the accommodating chamber can be placed for unmanned plane 300.
In view of ontology acts on unmanned plane further protection, the ontology 210 can also be body structure.Referring to figure
Shown in 2, the accommodating chamber of the babinet can be to protrude from the space of vehicle body tail portion, alternatively, shown in Figure 3, the case
The accommodating chamber of body is indent in the space of vehicle body tail portion.
Specifically, in the present embodiment, there is the babinet opening and the installation cavity with open communication, the lid can be opened and closed
Ground setting is in the opening, and when the lid is closed, the babinet and lid form closing chamber, putting in the closing chamber
Set aforementioned unmanned plane.Especially, the shape and size of the installation cavity are adapted with the unmanned plane so that the unmanned plane can
Steadily as in the installation cavity, for example the installation cavity is according to the rotor quantity of unmanned plane, rotor and unmanned plane main body knot
The connection relation of structure and be arranged so that rotor can be put into the special chamber of rotor, agent structure can be put into the special chamber of main body.
The lid 220 is unfolded relative to ontology 210 or is closed the mode of (fold), can be by overturning mode,
It is opened flat driven mode or rotation mode.
Specifically, the active connection can be convertible rotational structure, the lid can relative to babinet overturn with
Expansion is closed.Alternatively, the active connection is flat-open type on-off structure, the lid can be relative to babinet in horizontal direction
Translation is to be unfolded or be closed.Alternatively, the active connection is rotary opening and closing structure, the lid can be relative to babinet in level
It rotates up to be unfolded or be closed.
In the present embodiment, it can be provided with electromagnetically component on the lid 220, be arranged on the undercarriage of the unmanned plane
There is magnetic firmware, when unmanned plane needs landing, is powered to electromagnetically component, passes through the magnetic suck of the electromagnetically component and magnetic firmware
Effect, makes unmanned plane steadily land.
The control circuit for the electromagnetically component being arranged on the lid 220 and the controller of unmanned plane connect, and can connect
When receiving unmanned plane landing instruction, interlock circuit is connected so that electromagnetically component generates magnetic, convenient for electromagnetically component and nobody
Magnetic firmware on machine undercarriage generates magnetic suck effect, and unmanned plane is made steadily to land；In the instruction for receiving unmanned plane and taking off
When, cut off interlock circuit so that electromagnetically component loses magnetism, electromagnetically between the magnetic firmware on component and unmanned plane undercarriage
Magnetic suck event resolves, fly out convenient for unmanned plane.It is shown in Figure 4, illustrate what unmanned plane 300 flew out from lid 220
Exemplary plot.
Preferably, it is also provided with ejection structure on the lid 220, when the unmanned plane needs to take off, passes through institute
Ejection structure driving unmanned plane is stated to fly out or assist unmanned plane to fly out by the ejection structure.
For in such a way that ejection structure flies out as driving unmanned plane, in this example, ejection structure may include transmitting
Unit, brake unit, control unit, described control unit control the transmitter unit and brake unit.As an example rather than limit
System, transmitter unit may include launching tube and launch power unit.Blasting type launch power, electricity may be used in the power of launching tube
Magnetic-type launch power, vapour-pressure type launch power or elastic emission power, in the present embodiment, using blasting type launch power.Tool
Body may be used such as lower structure.The both ends of the cylinder of launching tube are respectively arranged with upper end cover and bearing base, and cylinder is preferably adopted
With the glass-reinforced plastic material of high intensity, cylinder back-end is by being threadably mounted on bearing base.Sliding rail, cylinder are provided on cylinder inboard wall
Internal rear end isolation is provided with low-pressure chamber, holes and hyperbaric chamber, since cylinder back-end portion, forward end set gradually hyperbaric chamber,
The front end top of holes, low-pressure chamber, low-pressure chamber is provided with transmitting push plate；Low-pressure chamber and hyperbaric chamber pass through holes unicom, hyperbaric chamber
Bottom is placed with the fire in a stove before fuel is added and transmitting explosion medicine, and the fire in a stove before fuel is added is connected with electric signal transmitting terminal.After igniting, by emitting push plate by gas pressure
Power is transmitted on the unmanned plane of cylinder Inner Front End, and unmanned plane is launched along the sliding rail of cylinder inner wall.Preferably, to prevent unmanned plane from existing
It rotates, can also be arranged in the cylinder of launching tube spin-ended with preventing from rotating when unmanned plane emits in unmanned machine barrel in launching tube
Block.Brake unit can when needed brake ejection structure, can improve the safety of ejection structure.
The ejection structure as auxiliary fly out structure when, can be arranged on unmanned plane 300 and lid 220 respectively
Magnet, the magnet at least one be electromagnet；By control electromagnet poles variation make carry-on magnet and
There is like pole between magnet on flying platform, generate magnetic repulsion force and launch away unmanned plane from lid.
Certainly, the ejection structure can also be the simple elastic parts being set on lid, the elastic parts packet
Elastic construction and hitch structure are included, elastic construction can be drawn by hitch structure, unmanned aerial vehicle ejecting is gone out, the elasticity knot
Elastic sheet metal or spring etc. may be used in structure.
It is shown in Figure 5, to reduce the influence taking off, land to vehicle of unmanned plane 300, the lid 220 after deployment,
By transverse moving structure 230 transverse shifting can be carried out relative to ontology 210 to be laterally extended, so that lid 220 can be into one
Step is far from the vehicle tail 110.When withdrawing unmanned plane 300, it is horizontal that the lid 220 can be controlled by transverse moving structure 230
To shift-in, close to the ontology 210, then lid 220 can control further to be folded relative to ontology 210.
One end of the transverse moving structure 230 can pass through hinged axis connection, the other end of transverse moving structure 230 with ontology 210
It is connect with lid by horizontal sliding component.Hydraulic cylinder may be used in the horizontal sliding component or the telescopic rod of connecting rod driving comes
It realizes, belongs to the prior art, repeat no more.
In the present embodiment, charging structure, the input of the charging structure are also provided on the ontology and/or lid
End is connected with a vehicle-mounted power supply, and the output end of the charging structure is provided with micro USB electrical interface or wireless charging contact, the nothing
Micro USB electric contact can be connect with the wireless charging end of unmanned plane and/or data transmission terminal.And it is provided with nothing on the lid
Line signal transceiver, to position unmanned plane and be communicated wirelessly with unmanned plane.
Preferably, electric control lock is provided between the ontology 210 and lid 220, the control circuit of the electric control lock is opened
Pass is set in the display structure of car-mounted terminal, and after the electric control lock is opened, the lid can pass through active connection exhibition
It opens.It is unfolded relative to ontology in this way, user directly can control lid by car-mounted terminal, and electric control lock can also improve nobody
Machine is placed in the safety in UAV flight's structure 200.
In the present embodiment, UAV flight's structure 200 is to be detachably connected with vehicle body structure, is set therebetween
It is equipped with buffer structure.The buffer structure, preferably spring.
Another embodiment of the utility model also discloses a kind of UAV flight's structure.
UAV flight's structure is installed on vehicle tail, including ontology and lid；The lid passes through flexible connection
Part is installed on babinet so that the lid can be unfolded relative to ontology, and the lid of the expansion is flat as the carrying of unmanned plane
Platform.Preferably, the lid of the expansion can be used as the lifting support platform of unmanned plane, can be used for unmanned plane take off and/or
Landing.
The unmanned plane refers to unmanned vehicle in the present embodiment, be one kind with wireless remotecontrol or itself program
Aircraft based on control.
The lid can be able to be the rigid platfor made of metal or plastics as the carrying platform of unmanned plane.
The ontology is mainly used for being based on vehicle tail, limits out the reception space that can accommodate unmanned plane.Referring to Fig. 1
Shown, main body can be to be installed on vehicle body structure tail portion, support plate with one fixed width, and one end of support plate can be with
It is fixedly mounted on vehicle tail, the other end of support plate is flexibly connected lid.The width is carried out according to the size of unmanned plane
Setting, for example in Fig. 1 set according to the height of unmanned plane.
The support plate can be connect by articulated shaft with lid, lid can upwards be rotated relative to the articulated shaft with
It folds and lid can be downwards rotated relative to the articulated shaft to be unfolded.When lid is in folded state, the support plate
Accommodating chamber of the space limited with the lid in folded state as unmanned plane, the accommodating chamber can be placed for unmanned plane.
In view of ontology acts on unmanned plane further protection, the ontology can also be body structure.The babinet
Accommodating chamber can be protrude from the space of vehicle body tail portion, alternatively, the accommodating chamber of the babinet be indent in vehicle body
The space of tail portion.Specifically, in the present embodiment, the babinet has opening and the installation cavity with open communication, and the lid can
Openedly and closedly it is arranged in the opening, when the lid is closed, the babinet and lid form closing chamber, are used in the closing chamber
To place aforementioned unmanned plane.Especially, the shape and size of the installation cavity are adapted with the unmanned plane so that it is described nobody
Machine can be steadily as in the installation cavity, for example the installation cavity is according to the rotor quantity of unmanned plane, rotor and unmanned owner
The connection relation of body structure and be arranged so that rotor can be put into the special chamber of rotor, agent structure can be put into the special chamber of main body.
It is shown in Figure 6, by way of example and not limitation, illustrate the three-dimensional structure diagram of UAV flight's structure.
The ontology 210 is body structure, including installation cavity 211, and 211 inside of the installation cavity has flexible wall 212, institute
It states and is provided with lockhole 213 on installation cavity 211, the lockhole 213 coordinates with the electric control lock on lid.
Preferably, it is provided with firmware structure on the installation cavity 211, unmanned plane to be fixed in described accommodation section.
The firmware structure can acquire simple fastener, such as buckle structure, locating pin structure, threaded fastener, magnetic absorption
Fastener, or use Electronic control fastener.By way of example and not limitation, for example the firmware structure includes that setting is being installed
Telescoping mechanism inside chamber 211, telescoping mechanism have the stretching state and retracted state stretched out from side installation cavity side wall.It is described
When telescoping mechanism is located at stretching state, one end of telescoping mechanism is connect with concave shaped cavity side, and stretching out end can be with unmanned plane
Side contact push against, so that unmanned plane be fixed, limitation unmanned plane moves in concave shaped cavity.
In order to realize the stretching motion of telescoping mechanism, telescoping mechanism can be configured to include driving portion and telescopic rod knot
Structure, telescopic rod are drivingly connected with driving portion.The driving portion can select motor or hydraulic cylinder or cylinder.Certainly, above-mentioned driving
Structure by way of example and not limitation, as long as it is above-mentioned flexible that the power plant of object reciprocal telescopic movement can be driven to can be applied to
Mechanism.
The lid 220 is unfolded relative to ontology 210 or is closed the mode of (fold), can be by overturning mode,
It is opened flat driven mode or rotation mode.
Specifically, the active connection can be convertible rotational structure, the lid can relative to babinet overturn with
Expansion is closed.Alternatively, the active connection is flat-open type on-off structure, the lid can be relative to babinet in horizontal direction
Translation is to be unfolded or be closed.Alternatively, the active connection is rotary opening and closing structure, the lid can be relative to babinet in level
It rotates up to be unfolded or be closed.
In the present embodiment, it can be provided with electromagnetically component 221 on the lid 220, on the undercarriage of the unmanned plane
It is provided with magnetic firmware, when unmanned plane needs landing, is powered to electromagnetically component 221, it is solid by the electromagnetically component 221 and magnetic
The magnetic suck of part acts on, and unmanned plane is made steadily to land.
The control circuit for the electromagnetically component 221 being arranged on the lid 220 and the controller of unmanned plane connect, Neng Gou
When receiving unmanned plane landing instruction, interlock circuit is connected so that electromagnetically component 221 generates magnetism, convenient for electromagnetically component
221 generate magnetic suck effect with the magnetic firmware on unmanned plane undercarriage, and unmanned plane is made steadily to land；It is risen receiving unmanned plane
When winged instruction, interlock circuit is cut off so that electromagnetically component 221 loses magnetism, electromagnetically component 221 and unmanned plane undercarriage
On magnetic firmware between magnetic suck event resolves, fly out convenient for unmanned plane.
Preferably, it is also provided with ejection structure on the lid 220, when the unmanned plane needs to take off, passes through institute
Ejection structure driving unmanned plane is stated to fly out or assist unmanned plane to fly out by the ejection structure.
In the present embodiment, charging structure, the input of the charging structure are also provided on the ontology and/or lid
End is connected with a vehicle-mounted power supply, and the output end of the charging structure is provided with micro USB electrical interface or wireless charging contact, the nothing
Micro USB electric contact can be connect with the wireless charging end of unmanned plane and/or data transmission terminal.And it is provided with nothing on the lid
Line signal transceiver, to position unmanned plane and be communicated wirelessly with unmanned plane.
Preferably, electric control lock 223, the electric control lock 223 and the lockhole 213 on ontology 210 are provided on the lid 220
Cooperation.The switch of the control circuit of the electric control lock 223 is set in the display structure of car-mounted terminal, when the electric control lock 223
After unlatching, the lid can be unfolded by active connection.In this way, user directly can control lid phase by car-mounted terminal
Ontology is unfolded, and electric control lock 223 can also improve the safety that unmanned plane is placed in UAV flight's structure 200.
Wireless signal transceiver 222 is also provided on the lid 220, to position unmanned plane and and unmanned plane
It communicates wirelessly.
The technical detail not being described in detail in the present embodiment can refer to the record of preceding embodiment.
It is shown in Figure 7, it is another embodiment of the utility model, discloses a kind of control system of unmanned plane.
The system comprises unmanned plane, UAV flight's structure and controllers.
UAV flight's structure is installed on vehicle tail, including ontology and lid, and the lid passes through flexible connection
Part is installed on ontology so that the lid can be unfolded relative to ontology, and the lid of the expansion is flat as the carrying of unmanned plane
Platform.
The controller is communicated to connect with unmanned plane and UAV flight's structure, is controlled after capable of triggering aforementioned lid expansion
Unmanned plane processed flies out, and triggers the lid after control unmanned plane withdrawal and fold.
The controller can be the structure member on car-mounted terminal, or the function part on intelligent mobile terminal
Part can also be exclusively used in the structure of unmanned aerial vehicle (UAV) control.The intelligent mobile terminal, such as mobile phone, tablet computer and various pendants
Wear formula smart machine.
The concrete structure in previous embodiment may be used in UAV flight's structure, and details are not described herein.
In the above description, the disclosure of the utility model is not intended to its own being limited to these aspects.But
Within the scope of the protection of goal of present disclosure, each component can selectively and operatively be merged with arbitrary number.
In addition, as the term of " comprising ", " including " and " having " should give tacit consent to it is being interpreted as including property or open, rather than
Exclusive or closure, unless it is explicitly defined as opposite meaning.All technologies, science and technology or otherwise term are all
Meet meaning understood by one of ordinary skill in the art, unless it is defined as opposite meaning.The public art found in dictionary
Language should not be idealized very much under the background of the relevant technologies document or impractically be explained very much, unless present disclosure clearly will
It is defined as like that.Any change, the modification that the those of ordinary skill in the utility model field does according to the disclosure above content,
Belong to the protection domain of claims.
Claims (10)
1. a kind of vehicle carrying unmanned plane, including vehicle body structure, it is characterised in that：
The vehicle body structure tail portion is provided with UAV flight's structure, and UAV flight's structure includes ontology and lid
Body, the lid are installed on by active connection on ontology so that the lid can be unfolded relative to ontology, the expansion
Carrying platform of the lid as unmanned plane.
2. vehicle according to claim 1, it is characterised in that：Be provided with electromagnetically component on the lid, it is described nobody
It is provided with magnetic firmware on the undercarriage of machine, when unmanned plane needs landing, is powered to electromagnetically component, passes through the electromagnetically component
It is acted on the magnetic suck of magnetic firmware, unmanned plane is made steadily to land.
3. vehicle according to claim 1, it is characterised in that：The ontology be installed on vehicle body structure tail portion,
Support plate with one fixed width, appearance of the space that the support plate is limited with the lid in folded state as unmanned plane
Receive chamber.
4. vehicle according to claim 1, it is characterised in that：The ontology is body structure, the accommodating chamber of the babinet
For indent in the space of vehicle body tail portion or the accommodating chamber of the babinet be to protrude from the space of vehicle body tail portion.
5. vehicle according to claim 4, it is characterised in that：The babinet has opening and the installation with open communication
Chamber, the lid can be opened and closed setting in the opening, and when the lid is closed, the babinet and lid form closing chamber,
Placing aforementioned unmanned plane in the closing chamber.
6. vehicle according to claim 1, it is characterised in that：The active connection is flat-open type on-off structure, described
Lid can be translated up in level to be unfolded or be closed relative to babinet.
7. vehicle according to claim 1, it is characterised in that：Charging structure, institute are provided on the ontology and/or lid
The input terminal for stating charging structure is connected with a vehicle-mounted power supply, and the output end of the charging structure is provided with micro USB electrical interface or wireless
Charging contact, the wireless charging contact can be connect with the wireless charging end of unmanned plane and/or data transmission terminal.
8. vehicle according to claim 1, tagged word are：UAV flight's structure is with vehicle body structure
It is detachably connected, buffer structure is provided therebetween.
9. a kind of UAV flight's structure, it is characterised in that：UAV flight's structure is installed on vehicle tail, including ontology
And lid；
The lid is installed on by active connection on ontology so that the lid can be unfolded relative to ontology, the expansion
Carrying platform of the lid as unmanned plane.
10. a kind of control system of unmanned plane, it is characterised in that：The system comprises unmanned plane, UAV flight's structure and controls
Device processed,
UAV flight's structure is installed on vehicle tail, including ontology and lid, and the lid is pacified by active connection
Loaded on ontology so that the lid can be unfolded relative to ontology, the carrying platform of the lid of the expansion as unmanned plane；
The controller is communicated to connect with unmanned plane and UAV flight's structure, and nothing is controlled after capable of triggering aforementioned lid expansion
It is man-machine to fly out, and trigger the lid after control unmanned plane withdrawal and fold.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721624767.7U CN207657728U (en) | 2017-11-29 | 2017-11-29 | The vehicle and carrying structure, control system of unmanned plane can be carried |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721624767.7U CN207657728U (en) | 2017-11-29 | 2017-11-29 | The vehicle and carrying structure, control system of unmanned plane can be carried |
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| CN207657728U true CN207657728U (en) | 2018-07-27 |
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| CN201721624767.7U Active CN207657728U (en) | 2017-11-29 | 2017-11-29 | The vehicle and carrying structure, control system of unmanned plane can be carried |
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| CN (1) | CN207657728U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107891821A (en) * | 2017-11-29 | 2018-04-10 | 上海量明科技发展有限公司 | The vehicle and carrying structure, control system of unmanned plane can be carried |
| CN112049498A (en) * | 2020-07-29 | 2020-12-08 | 成都震风航空技术有限公司 | Automatic hangar of unmanned aerial vehicle |
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2017
- 2017-11-29 CN CN201721624767.7U patent/CN207657728U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107891821A (en) * | 2017-11-29 | 2018-04-10 | 上海量明科技发展有限公司 | The vehicle and carrying structure, control system of unmanned plane can be carried |
| CN107891821B (en) * | 2017-11-29 | 2024-07-12 | 上海量明科技发展有限公司 | Vehicle capable of carrying unmanned aerial vehicle, carrying structure and control system |
| CN112049498A (en) * | 2020-07-29 | 2020-12-08 | 成都震风航空技术有限公司 | Automatic hangar of unmanned aerial vehicle |
| CN112049498B (en) * | 2020-07-29 | 2021-08-03 | 成都震风航空技术有限公司 | Automatic hangar of unmanned aerial vehicle |
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