CN107891821A - 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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- CN107891821A CN107891821A CN201711223580.0A CN201711223580A CN107891821A CN 107891821 A CN107891821 A CN 107891821A CN 201711223580 A CN201711223580 A CN 201711223580A CN 107891821 A CN107891821 A CN 107891821A
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- 238000010586 diagram Methods 0.000 description 4
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R9/00—Supplementary fittings on vehicle exterior for carrying loads, e.g. luggage, sports gear or the like
- B60R9/06—Supplementary fittings on vehicle exterior for carrying loads, e.g. luggage, sports gear or the like at vehicle front or rear
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
Abstract
The invention discloses the vehicle that can carry unmanned plane and carrying structure, control system, it is related to UAV flight and control technology field.A kind of vehicle for carrying unmanned plane, including vehicle body structure；The vehicle body structure afterbody is provided with UAV flight's structure, UAV flight's structure includes body and lid, the lid is installed on body by active connection so that the lid can deploy relative to body, the carrying platform of the lid of the expansion as unmanned plane.The present invention by vehicle tail set UAV flight's structure, the carrying structure it is a part of deployable, the part after expansion can be easy to UAV flight and manipulation as the carrying platform of unmanned plane.
Description
Technical field
The present invention relates to UAV flight 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 itself programme-control.There is maneuverability, rapid reaction, unmanned flight, operation to want for it
Ask the advantages of low.Unmanned plane is by carrying multiclass sensor, it is possible to achieve image real-time Transmission, high-risk areas detecting function, is
Satellite remote sensing and the strong supplement of traditional air remote sensing.At present, the use range 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 field applications such as production, drug law enforcement anti-smuggling, border patrol, public security anti-terrorism are very wide.Wherein, 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 lack the Special horizontal suitable for taking off, landing in current SUAV, still generally existing carrying process
The problem of platform and inconvenient manipulation.
The content of the invention
It is an object of the invention to：Overcome the deficiencies in the prior art, there is provided a kind of vehicle for carrying unmanned plane and take
Carry structure, control system.By setting UAV flight's structure in vehicle tail, a part for the carrying structure can open up the present invention
Open, the part after expansion can be easy to UAV flight and manipulation as the carrying platform of unmanned plane.
To realize above-mentioned target, the invention provides following technical scheme：
A kind of vehicle for carrying unmanned plane, including vehicle body structure；The vehicle body structure afterbody is provided with nothing
Man-machine carrying structure, UAV flight's structure include body and lid, and the lid is installed on this by active connection
On body so that the lid can deploy relative to body, the carrying platform of the lid of the expansion as unmanned plane.
Further, the lid of the expansion can be as the lifting support platform of unmanned plane.
Further, electromagnetically component is provided with the lid, magnetic firmware, nothing are provided with 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 stably lands.
Further, ejection structure is provided with the lid, when the unmanned plane needs to take off, passes through the ejection structure
Driving unmanned plane flies out or aids in unmanned plane to fly out by the ejection structure.
Further, the body be installed on vehicle body structure afterbody, have one fixed width supporting plate, the branch
Accommodating chamber of the space that fagging limits with the lid in folded state as unmanned plane.
Further, the body is body structure, and the accommodating chamber of the casing is indent in the space of vehicle body afterbody,
Or the accommodating chamber of the casing is to protrude from the space of vehicle body afterbody.
Preferably, the casing has opening and the installation cavity with open communication, and the lid can be opened and closed to be arranged on institute
State opening, when the lid is closed, the casing and lid form closing chamber, in the closing chamber to place it is foregoing nobody
Machine.
Further, the active connection is convertible rotational structure, and the lid can be overturn relative to casing to deploy
Or closure.
Or the active connection is flat-open type on-off structure, the lid can be relative to casing horizontal flat upwards
Move to deploy or close.
Or the active connection is rotary opening and closing structure, the lid can rotate up relative to casing in level
To deploy or close.
Further, charging structure, the input and vehicle mounted electric of the charging structure are provided with the body 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 connected with the wireless charging end of unmanned plane and/or data transmission terminal.
Further, wireless signal transceiver is provided with the lid, to position unmanned plane and be carried out with unmanned plane
Wireless telecommunications.
Further, UAV flight's structure is provided therebetween slow with vehicle body structure to be detachably connected
Rush structure.
Further, electric control lock is provided between the body and lid, the switch of the control circuit of the electric control lock is set
In in the display structure of car-mounted terminal.
Further, the lid after deployment, can carry out transverse shifting to extend laterally relative to body.
The invention also discloses a kind of UAV flight's structure, UAV flight's structure is installed on vehicle tail, bag
Include body and lid；The lid is installed on casing by active connection so that and the lid can deploy relative to body,
Carrying platform of the lid of the expansion as unmanned plane.
Further, the lid of the expansion can be as the lifting support platform of unmanned plane.
The invention also discloses a kind of control system of unmanned plane, the system includes unmanned plane, UAV flight's structure
And controller,
UAV flight's structure is installed on vehicle tail, including body and lid, and the lid passes through flexible connection
Part is installed on body so that the lid can deploy relative to body, and the lid of the expansion is put down as the carrying of unmanned plane
Platform；
The controller, it is connected with unmanned plane and UAV flight's structured communication, is controlled after foregoing lid expansion can be triggered
Unmanned plane processed flies out, and triggers the lid after control unmanned plane withdrawal and fold.
The present invention compared with prior art, as an example, has the following advantages that and accumulated due to using above technical scheme
Pole effect：By setting UAV flight's structure, a part of deployable, portion after expansion of the carrying structure in vehicle tail
Point can as the carrying platform of unmanned plane, specifically, the carrying platform can as the platform that rises and falls of unmanned plane, placement platform etc.,
It is easy to user to manipulate unmanned plane.When the carrying structure is packed up, unmanned plane can be played certain as the storage device of unmanned plane
Protective effect.
Brief description of the drawings
Fig. 1 is the vehicle structure schematic diagram provided in an embodiment of the present invention with open carrying structure.
Fig. 2 is the vehicle structure schematic diagram provided in an embodiment of the present invention with box-type carrying structure.
Fig. 3 is the vehicle structure schematic diagram provided in an embodiment of the present invention with indent box-type carrying structure.
Fig. 4 is the structural representation that unmanned plane provided in an embodiment of the present invention takes off from lid.
Fig. 5 is the structural representation of the lid provided in an embodiment of the present invention extended laterally.
Fig. 6 is the structural representation of UAV flight's structure provided in an embodiment of the present invention.
Fig. 7 is the frame construction drawing of control system provided in an embodiment of the present invention.
Description of reference numerals：
Vehicle 100, afterbody 110；
UAV flight's structure 200；Body 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.
Embodiment
Below in conjunction with the drawings and specific embodiments to the vehicle disclosed by the invention for carrying unmanned plane and carrying structure, control
System processed is described in further detail.It should be noted that technical characteristic or technical characteristic described in following embodiments
Combination is not construed as isolated, and they can be mutually combined so as to reach superior technique effect.In following implementations
In the accompanying drawing of example, the identical label that each accompanying drawing occurs represents identical feature or part, can be applied in different embodiments.
Therefore, once being defined in a certain Xiang Yi accompanying drawing, then it need not be further discussed in subsequent accompanying drawing.
It should be noted that structure depicted in this specification institute accompanying drawing, ratio, size etc., only coordinating explanation
Content disclosed in book, so that those skilled in the art understands and reads, it is not limited to invent enforceable restriction bar
Part, the modification of any structure, the change of proportionate relationship or the adjustment of size, do not influenceing the effect of invention can be generated and institute's energy
Under the purpose reached, it all should fall in the range of the disclosed technology contents of invention can be covered.The side of being preferable to carry out of the present invention
The scope of formula includes other realization, wherein described or discussion order can not be pressed, including is pressed according to involved function
Basic mode simultaneously or in the opposite order, carrys out perform function, this should be by the skill of embodiments of the invention art
Art personnel are understood.
It may be not discussed in detail for technology, method and apparatus known to person of ordinary skill in the relevant, but suitable
In the case of, the technology, method and apparatus should be considered as authorizing part for specification.Institute that is shown here and discussing
Have in example, any occurrence should be construed as merely exemplary, not as limitation.Therefore, exemplary embodiment
Other examples can have different values.
Embodiment
It is shown in Figure 1, a kind of vehicle 100 for carrying unmanned plane, including vehicle body structure.The vehicle body knot
Structure afterbody 110 is provided with UAV flight's structure 200, and UAV flight's structure 200 includes body 210 and lid 220, institute
State lid 220 to be installed on body 210 by active connection so that the lid 220 can deploy relative to body 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 for unmanned plane 300 as the lifting support platform of unmanned plane
Take off and/or land.
The unmanned plane 300, in the present embodiment, refers to unmanned vehicle, be it is a kind of with wireless remotecontrol or itself
Aircraft based on programme-control.
The lid 220 can be as the carrying platform of unmanned plane, and it can rigidly be put down made of metal or plastics
Platform.
The body 210, it is mainly used in 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 installed on vehicle body structure afterbody 110, have one fixed width supporting plate, support
One end of plate can be fixedly mounted and on vehicle tail 110, the other end of supporting 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.
With continued reference to shown in Fig. 1, the supporting plate is connected by jointed shaft with lid 220, and lid 220 can be relative to the hinge
Spindle is rotated to fold upwards, and lid 220 can be rotated downwards relative to the jointed shaft to deploy.Lid 220
During in folded state (lid 220 of dotted line in Fig. 1), the supporting plate limits with the lid 220 in folded state
Accommodating chamber of the space as unmanned plane 300, the accommodating chamber can place for unmanned plane 300.
Unmanned plane further protection is acted in view of body, the body 210 can also be body structure.Referring to figure
Shown in 2, the accommodating chamber of the casing can be to protrude from the space of vehicle body afterbody, or, shown in Figure 3, the case
The accommodating chamber of body is indent in the space of vehicle body afterbody.
Specifically, in the present embodiment, the casing has opening and the installation cavity with open communication, and the lid can be opened and closed
Ground is arranged on the opening, and when the lid is closed, the casing and lid form closing chamber, putting in the closing chamber
Put foregoing unmanned plane.Especially, the shape and size of the installation cavity are adapted with the unmanned plane so that the unmanned plane can
Stably as in the installation cavity, for example the installation cavity is according to the rotor quantity of unmanned plane, rotor and unmanned plane body junction
The annexation of structure and set 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 deploys or closed the mode of (fold) relative to body 210, can be by upset mode,
It is opened flat driven mode or rotation mode.
Specifically, the active connection can be convertible rotational structure, the lid can be overturn relative to casing with
Expansion or closure.Or the active connection is flat-open type on-off structure, the lid can be relative to casing horizontal upward
Translate to deploy or close.Or the active connection is rotary opening and closing structure, the lid can be relative to casing in level
Rotate up to deploy or close.
In the present embodiment, electromagnetically component can be provided with the lid 220, is set on the undercarriage of the unmanned plane
There is magnetic firmware, when unmanned plane needs landing, be powered to electromagnetically component, pass through the electromagnetically component and the magnetic suck of magnetic firmware
Effect, makes unmanned plane stably land.
The control circuit of the electromagnetically component set 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 produces magnetic, is easy to electromagnetically component and nobody
Magnetic firmware on machine undercarriage produces magnetic suck effect, unmanned plane is stably landed；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, be easy to unmanned plane to fly out.It is shown in Figure 4, illustrate what unmanned plane 300 flew out from lid 220
Exemplary plot.
Preferably, ejection structure is also provided with 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 aid in unmanned plane to fly out by the ejection structure.
Exemplified by a manner of being flown out using ejection structure as driving unmanned plane, in this example, ejection structure can 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 can include launching tube and launch power unit.The power of launching tube can use blasting type launch power, electricity
Magnetic-type launch power, vapour-pressure type launch power or elastic emission power, in the present embodiment, using blasting type launch power.Tool
Body can use following 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.Slide rail, cylinder are provided with 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,
Holes, low-pressure chamber, the front end top of low-pressure chamber are provided with transmitting push pedal；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 launching push pedal by gas pressure
Power is delivered on the unmanned plane of cylinder Inner Front End, and slide rail of the unmanned plane along cylinder inwall is launched.Preferably, to prevent unmanned plane from existing
Launching tube internal rotation, it can also set in the cylinder of launching tube spin-ended with being rotated when preventing that unmanned plane is launched in unmanned machine barrel
Block.Brake unit can be braked to ejection structure when needed, it is possible to increase the security of ejection structure.
The ejection structure as auxiliary fly out structure when, it can be set respectively on unmanned plane 300 and lid 220
Magnet, the magnet at least one is electromagnet；By control electromagnet poles the carry-on magnet of change and
There is like pole between magnet on flying platform, produce magnetic repulsion force and launch away unmanned plane from lid.
Certainly, the ejection structure can also be the simple elastic parts being arranged on lid, the elastic parts bag
Elastic construction and hitch structure are included, elastic construction can be drawn by hitch structure and unmanned aerial vehicle ejecting is gone out, the elasticity knot
Structure can use elastic sheet metal or spring etc..
It is shown in Figure 5, to reduce the influence taking off, land to vehicle of unmanned plane 300, the lid 220 after deployment,
Transverse shifting can be carried out to extend laterally relative to body 210 by transverse moving structure 230, so that lid 220 can enter one
Step is away from the vehicle tail 110.When withdrawing unmanned plane 300, by transverse moving structure 230 lid 220 can be controlled horizontal
To shift-in, close to the body 210, then can control lid 220 further to be folded relative to body 210.
One end of the transverse moving structure 230 can be with body 210 by being hinged axis connection, the other end of transverse moving structure 230
It is connected by horizontal sliding component with lid.The horizontal sliding component can using the expansion link that hydraulic cylinder or connecting rod drive come
Realize, belong to prior art, repeat no more.
In the present embodiment, charging structure, the input of the charging structure are also provided with the body and/or lid
End is connected with vehicle power, 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 connected 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 body 210 and lid 220, the control circuit of the electric control lock is opened
Pass is arranged in the display structure of car-mounted terminal, and after the electric control lock is opened, the lid can pass through active connection exhibition
Open.In this way, user directly can control lid to deploy relative to body by car-mounted terminal, and electric control lock can also improve nobody
The security that machine is placed in UAV flight's structure 200.
In the present embodiment, UAV flight's structure 200, to be detachably connected, is set therebetween with vehicle body structure
It is equipped with buffer structure.The buffer structure, preferably spring.
Another embodiment of the present invention, also disclose a kind of UAV flight's structure.
UAV flight's structure is installed on vehicle tail, including body and lid；The lid passes through flexible connection
Part is installed on casing so that the lid can deploy relative to body, and the lid of the expansion is put down as the carrying of unmanned plane
Platform.Preferably, the lid of the expansion can as the lifting support platform of unmanned plane, can be used for unmanned plane take off and/or
Landing.
The unmanned plane, in the present embodiment, refer to unmanned vehicle, be one kind with wireless remotecontrol or itself program
Aircraft based on control.
The lid can be as the carrying platform of unmanned plane, and it can be the rigid platfor made of metal or plastics.
The body, it is mainly used in being based on vehicle tail, limits out the reception space that can accommodate unmanned plane.Referring to Fig. 1
It is shown, main body can be installed on vehicle body structure afterbody, there is the supporting plate of one fixed width, one end of supporting plate can be with
In fixed installation and vehicle tail, the other end of supporting plate is flexibly connected lid.The width is carried out according to the size of unmanned plane
Set, for example in Fig. 1 set according to the height of unmanned plane.
The supporting plate can be connected by jointed shaft with lid, lid can be rotated upwards relative to the jointed shaft with
Fold, and lid can be rotated downwards relative to the jointed shaft to deploy.When lid is in folded state, the supporting plate
With accommodating chamber of the space that the lid in folded state limits as unmanned plane, the accommodating chamber can place for unmanned plane.
Unmanned plane further protection is acted in view of body, the body can also be body structure.The casing
Accommodating chamber can be to protrude from the space of vehicle body afterbody, or, the accommodating chamber of the casing is indent in vehicle body
The space of afterbody.Specifically, in the present embodiment, the casing has opening and the installation cavity with open communication, and the lid can
The opening is openedly and closedly arranged on, when the lid is closed, the casing and lid form closing chamber, are used in the closing chamber
To place foregoing 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 stably as in the installation cavity, for example the installation cavity is according to the rotor quantity of unmanned plane, rotor and unmanned owner
The annexation of body structure and set 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, it is unrestricted as an example, illustrate the three-dimensional structure diagram of UAV flight's structure.
The body 210 is body structure, including installation cavity 211, and the inside of installation cavity 211 has flexible wall 212, institute
State and lockhole 213 is provided with installation cavity 211, the lockhole 213 coordinates with the electric control lock on lid.
Preferably, firmware structure is provided with the installation cavity 211, unmanned plane is fixed in described accommodation section.
The firmware structure, simple fastener, such as buckle structure, locating pin structure, threaded fastener, magnetic absorption can be gathered
Fastener, or use Electronic control fastener.It is unrestricted as an example, for example the firmware structure is including being arranged on installation
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 connected with concave shaped cavity side, and it stretches out end can be with unmanned plane
Contacts side surfaces push against, so that unmanned plane be fixed, limitation unmanned plane is moved in concave shaped cavity.
In order to realize the stretching motion of telescoping mechanism, telescoping mechanism can be configured to the knot for including drive division and expansion link
Structure, expansion link and drive division drive connection.The drive division can select motor or hydraulic cylinder or cylinder.Certainly, above-mentioned driving
Structure is unrestricted as an example, as long as the power set of object reciprocal telescopic movement can be driven to can be applied to above-mentioned stretch
Mechanism.
The lid 220 deploys or closed the mode of (fold) relative to body 210, can be by upset mode,
It is opened flat driven mode or rotation mode.
Specifically, the active connection can be convertible rotational structure, the lid can be overturn relative to casing with
Expansion or closure.Or the active connection is flat-open type on-off structure, the lid can be relative to casing horizontal upward
Translate to deploy or close.Or the active connection is rotary opening and closing structure, the lid can be relative to casing in level
Rotate up to deploy or close.
In the present embodiment, electromagnetically component 221 can be provided with the lid 220, on the undercarriage of the unmanned plane
Magnetic firmware is provided with, when unmanned plane needs landing, is powered to electromagnetically component 221, is consolidated by the electromagnetically component 221 with magnetic
The magnetic suck effect of part, makes unmanned plane stably land.
The control circuit of the electromagnetically component 221 set 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 produces magnetic, is easy to electromagnetically component
221 produce magnetic suck effect with the magnetic firmware on unmanned plane undercarriage, unmanned plane is stably landed；Risen receiving unmanned plane
During 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, be easy to unmanned plane to fly out.
Preferably, ejection structure is also provided with 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 aid in unmanned plane to fly out by the ejection structure.
In the present embodiment, charging structure, the input of the charging structure are also provided with the body and/or lid
End is connected with vehicle power, 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 connected 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 body 210 are provided with the lid 220
Coordinate.The switch of the control circuit of the electric control lock 223 is arranged in the display structure of car-mounted terminal, when the electric control lock 223
After unlatching, the lid can be deployed by active connection.In this way, user directly can control lid phase by car-mounted terminal
Deploy for body, and electric control lock 223 can also improve the security that unmanned plane is placed in UAV flight's structure 200.
Wireless signal transceiver 222 is also provided with the lid 220, to position unmanned plane and and unmanned plane
Communicate wirelessly.
The record of embodiment before the ins and outs not being described in detail in the present embodiment refer to.
It is shown in Figure 7, it is another embodiment of the present invention, discloses a kind of control system of unmanned plane.
The system includes unmanned plane, UAV flight's structure and controller.
UAV flight's structure is installed on vehicle tail, including body and lid, and the lid passes through flexible connection
Part is installed on body so that the lid can deploy relative to body, and the lid of the expansion is put down as the carrying of unmanned plane
Platform.
The controller, it is connected with unmanned plane and UAV flight's structured communication, is controlled after foregoing lid expansion can be triggered
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, the structure of unmanned aerial vehicle (UAV) control can also be exclusively used in.The intelligent mobile terminal, such as mobile phone, tablet personal computer and various pendants
Wear formula smart machine.
UAV flight's structure can use the concrete structure in previous embodiment, will not be repeated here.
In superincumbent description, the disclosure is not intended as is limited to these aspects by its own.But at this
In the range of the protection of goal of disclosure, each component can optionally and operatively be merged with arbitrary number.In addition,
The term of picture " comprising ", " including " and " having " should be given tacit consent to being interpreted as including property or open rather than exclusive
Property or closure, unless it is explicitly defined as opposite implication.All technologies, science and technology or otherwise term all meet
Implication understood by one of ordinary skill in the art, unless it is defined as opposite implication.The public term found in dictionary should
Do not idealized very much or impractically explained very much when under the background in correlation technique document, unless present disclosure is clearly limited
Determine into such.Any change, the modification that the those of ordinary skill in field of the present invention does according to the disclosure above content, belong to right
The protection domain of claim.
Claims (18)
1. a kind of vehicle for carrying unmanned plane, including vehicle body structure, it is characterised in that：
The vehicle body structure afterbody is provided with UAV flight's structure, and UAV flight's structure includes body and lid
Body, the lid are installed on body by active connection so that the lid can deploy relative to body, the expansion
Carrying platform of the lid as unmanned plane.
2. vehicle according to claim 1, it is characterised in that：The lid of the expansion can be as the lifting support of unmanned plane
Platform.
3. vehicle according to claim 2, it is characterised in that：Be provided with electromagnetically component on the lid, it is described nobody
Magnetic firmware is provided with the undercarriage of machine, when unmanned plane needs landing, is powered to electromagnetically component, passes through the electromagnetically component
Acted on the magnetic suck of magnetic firmware, unmanned plane is stably landed.
4. vehicle according to claim 2, it is characterised in that：Ejection structure, the unmanned plane are provided with the lid
When needing to take off, drive unmanned plane to fly out by the ejection structure or aid in unmanned plane to fly out by the ejection structure.
5. vehicle according to claim 1, it is characterised in that：The body be installed on vehicle body structure afterbody,
Supporting plate with one fixed width, appearance of the space that the supporting plate limits with the lid in folded state as unmanned plane
Receive chamber.
6. vehicle according to claim 1, it is characterised in that：The body is body structure, the accommodating chamber of the casing
It is indent in the space of vehicle body afterbody, or the accommodating chamber of the casing is to protrude from the space of vehicle body afterbody.
7. vehicle according to claim 6, it is characterised in that：The casing has opening and the installation with open communication
Chamber, the lid can be opened and closed to be arranged on the opening, and when the lid is closed, the casing and lid form closing chamber,
Placing foregoing unmanned plane in the closing chamber.
8. vehicle according to claim 1, it is characterised in that：The active connection is convertible rotational structure, described
Lid can be overturn relative to casing to deploy or close.
9. 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 to deploy or close relative to casing in level.
10. vehicle according to claim 1, it is characterised in that：The active connection is rotary opening and closing structure, the lid
Body can be rotated up to deploy or close relative to casing in level.
11. vehicle according to claim 1, it is characterised in that：Charging structure is provided with the body and/or lid,
The input of the charging structure is connected with vehicle power, and the output end of the charging structure is provided with micro USB electrical interface or nothing
Micro USB electric contact, the wireless charging contact can be connected with the wireless charging end of unmanned plane and/or data transmission terminal.
12. vehicle according to claim 1, it is characterised in that：Wireless signal transceiver is provided with the lid, to
Position unmanned plane and communicated wirelessly with unmanned plane.
13. vehicle according to claim 1, its tagged word is：UAV flight's structure and vehicle body structure
To be detachably connected, buffer structure is provided therebetween.
14. vehicle according to claim 1, its tagged word is：Electric control lock is provided between the body and lid, institute
The switch for stating the control circuit of electric control lock is arranged in the display structure of car-mounted terminal.
15. vehicle according to claim 1, its tagged word is：The lid after deployment, can be carried out relative to body
Transverse shifting is to extend laterally.
A kind of 16. UAV flight's structure, it is characterised in that：UAV flight's structure is installed on vehicle tail, including this
Body and lid；
The lid is installed on body by active connection so that the lid can deploy relative to body, the expansion
Carrying platform of the lid as unmanned plane.
17. UAV flight's structure according to claim 16, it is characterised in that：The lid of the expansion can be used as nobody
The lifting support platform of machine.
A kind of 18. control system of unmanned plane, it is characterised in that：The system includes unmanned plane, UAV flight's structure and control
Device processed,
UAV flight's structure is installed on vehicle tail, including body and lid, and the lid is pacified by active connection
Loaded on body so that the lid can deploy relative to body, the carrying platform of the lid of the expansion as unmanned plane；
The controller, it is connected with unmanned plane and UAV flight's structured communication, nothing is controlled after foregoing lid expansion can be triggered
It is man-machine to fly out, and trigger the lid after control unmanned plane withdrawal and fold.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711223580.0A CN107891821A (en) | 2017-11-29 | 2017-11-29 | The vehicle and carrying structure, control system of unmanned plane can be carried |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711223580.0A CN107891821A (en) | 2017-11-29 | 2017-11-29 | The vehicle and carrying structure, control system of unmanned plane can be carried |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107891821A true CN107891821A (en) | 2018-04-10 |
Family
ID=61806629
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711223580.0A Pending CN107891821A (en) | 2017-11-29 | 2017-11-29 | The vehicle and carrying structure, control system of unmanned plane can be carried |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107891821A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622432A (en) * | 2018-04-27 | 2018-10-09 | 内蒙古工业大学 | A kind of pickup type vehicle-mounted unmanned aerial vehicle intelligence landing and autonomous continuation of the journey system |
| CN111319569A (en) * | 2018-12-14 | 2020-06-23 | 北京宝沃汽车有限公司 | Vehicle with a steering wheel |
| CN114834344A (en) * | 2022-04-19 | 2022-08-02 | 浙江吉利控股集团有限公司 | Spare tyre storage tank and vehicle |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106004626A (en) * | 2016-06-14 | 2016-10-12 | 郭永 | Vehicle-mounted multifunctional platform of unmanned aerial vehicle |
| CN205951840U (en) * | 2016-08-22 | 2017-02-15 | 纳恩博（北京）科技有限公司 | Install bin and haulage vehicle who is used for carrying on balance car |
| CN106828264A (en) * | 2017-01-17 | 2017-06-13 | 斑马信息科技有限公司 | Unmanned plane Vehicular system and its management method |
| CN107380038A (en) * | 2017-06-22 | 2017-11-24 | 天津航天中为数据系统科技有限公司 | A kind of SUAV Emergency Command Vehicle and command system and method |
| CN207657728U (en) * | 2017-11-29 | 2018-07-27 | 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 |
-
2017
- 2017-11-29 CN CN201711223580.0A patent/CN107891821A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106004626A (en) * | 2016-06-14 | 2016-10-12 | 郭永 | Vehicle-mounted multifunctional platform of unmanned aerial vehicle |
| CN205951840U (en) * | 2016-08-22 | 2017-02-15 | 纳恩博（北京）科技有限公司 | Install bin and haulage vehicle who is used for carrying on balance car |
| CN106828264A (en) * | 2017-01-17 | 2017-06-13 | 斑马信息科技有限公司 | Unmanned plane Vehicular system and its management method |
| CN107380038A (en) * | 2017-06-22 | 2017-11-24 | 天津航天中为数据系统科技有限公司 | A kind of SUAV Emergency Command Vehicle and command system and method |
| CN207657728U (en) * | 2017-11-29 | 2018-07-27 | 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 |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622432A (en) * | 2018-04-27 | 2018-10-09 | 内蒙古工业大学 | A kind of pickup type vehicle-mounted unmanned aerial vehicle intelligence landing and autonomous continuation of the journey system |
| CN108622432B (en) * | 2018-04-27 | 2021-09-14 | 内蒙古工业大学 | Intelligent take-off and landing and autonomous cruising system of pick up type vehicle-mounted unmanned aerial vehicle |
| CN111319569A (en) * | 2018-12-14 | 2020-06-23 | 北京宝沃汽车有限公司 | Vehicle with a steering wheel |
| CN111319569B (en) * | 2018-12-14 | 2021-09-07 | 北京宝沃汽车有限公司 | Vehicle with a steering wheel |
| CN114834344A (en) * | 2022-04-19 | 2022-08-02 | 浙江吉利控股集团有限公司 | Spare tyre storage tank and vehicle |
| CN114834344B (en) * | 2022-04-19 | 2023-08-18 | 浙江吉利控股集团有限公司 | Spare tire storage box and vehicle |
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