CN109383798A - A kind of vehicle-mounted police UAV system - Google Patents
A kind of vehicle-mounted police UAV system Download PDFInfo
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- CN109383798A CN109383798A CN201710658442.9A CN201710658442A CN109383798A CN 109383798 A CN109383798 A CN 109383798A CN 201710658442 A CN201710658442 A CN 201710658442A CN 109383798 A CN109383798 A CN 109383798A
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- 230000006698 induction Effects 0.000 claims abstract description 24
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 24
- 238000009434 installation Methods 0.000 claims abstract description 14
- 230000000903 blocking effect Effects 0.000 claims abstract description 4
- 230000005484 gravity Effects 0.000 claims description 9
- 230000006641 stabilisation Effects 0.000 claims description 6
- 238000011105 stabilization Methods 0.000 claims description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 3
- 230000037396 body weight Effects 0.000 abstract description 4
- 230000005611 electricity Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention discloses a kind of vehicle-mounted police UAV system, belong to air vehicle technique field, vehicle-mounted unmanned aerial vehicle takes off and lands and force aid system and blocks system, it takes off and the force aid system that lands includes two taking off and the power assisting device that lands, taking off and land driving device and radio induction charging device, two take off and the both ends for the power assisting device that lands are respectively equipped with the stabilizing member that takes off and land；Vehicle-mounted unmanned aerial vehicle includes fuselage, four side axles and landing balance system, and fuselage is equipped with ultrasonic distance measuring module installing port, and the top of fuselage is equipped with telecontrol antenna, and side axle is equipped with image capture module installing port and driving motor, and driving motor is equipped with multiple rotors；The system of blocking includes transversal stretching radical occlusion device and just flexible radical occlusion device.Cylinder block strength of the present invention is high, body weight is small, fuselage balance, at low cost and easy for installation, takeoff operational simple and stable, guarantees unmanned plane balance, realizes radio induction charging, guarantees unmanned plane electricity consumption.
Description
Technical field
The present invention relates to a kind of UAV system to belong to unmanned plane more particularly to a kind of vehicle-mounted police UAV system
Technical field.
Background technique
In recent years, the attack of terrorism frequently occurs with incident of violence, and at the same time, traffic congestion is on the rise so that police
Vehicle cannot first time arrival event scene, or obstruction and intersection of the sight by front vehicles during chasing
Influence, cause track target loss.
At the same time, some areas people's police are by being equipped with 360 degree rotation camera head monitor police vehicle in police vehicle roof
Ambient state information, but it can only monitor police vehicle ambient state information, in addition, when congestion occurs in road, it can only
It observes front short distance traffic condition, is unable to get farther away road information.
Multi-rotor unmanned aerial vehicle is since the advantages that its is easily operated, easy to maintain, is in cable inspection, fire monitoring, ecological protection
Etc. multiple fields be widely used.Traditional unmanned plane is in practical applications, most of to be flown using remote control control, right
Operator is more demanding.It is most of to be navigated using GPS positioning or loaded using unmanned plane further for the unmanned plane of self-navigation
Camera carries out vision guided navigation, can not work normally using the unmanned plane of GPS navigation in the poor region of GPS signal, and utilizes
The unmanned plane of camera vision guided navigation is affected by factors such as light, and positioning accuracy is relatively low, in addition, certainly for major part
The multi-rotor unmanned aerial vehicle of leading boat, environment sensing unit are mounted on multi-rotor unmanned aerial vehicle body, need through the micro- of body
The information that processor acquires environment sensing unit analyzes and determines that processing speed is slow, judges that precision is low, and for existing
For vehicle-mounted police unmanned plane, the mode of artificial help-fly is mostly used to take off greatly, this mode is cumbersome, and unmanned plane takes off
It is unstable, it is easy to cause unmanned plane lateral deviation or failure of taking off, is unfavorable for the progress of takeoff operational.
Summary of the invention
The main object of the present invention is to provide for a kind of vehicle-mounted police UAV system, to solve body in the prior art
Intensity is low, body weight is big, fuselage is difficult to balance, at high cost and installation is inconvenient, takeoff operational is cumbersome, it is unstable to take off, easily leads
Cause unmanned plane lateral deviation or take off failure the problem of.
The purpose of the present invention can reach by using following technical solution:
A kind of vehicle-mounted police UAV system, including vehicle-mounted unmanned aerial vehicle, take off and land and force aid system and block system, institute
State the force aid system that takes off and land include two be parallel to each other take off and the power assisting device that lands, take off described in two and land power-assisted dress
It is equipped with two between setting to take off and land driving device and a radio induction charging device, takes off described in two and the power assisting device that lands
Both ends are respectively equipped with the stabilizing member that takes off and land；The vehicle-mounted unmanned aerial vehicle includes fuselage, four side axles, detachable carry axis and landing
Balance system, four side axles are symmetrically arranged on the fuselage, and the landing balance system is symmetrically arranged in described in two
The two sides of side axle, the front of the fuselage are equipped with ultrasonic distance measuring module installing port, and the top of the fuselage is equipped with remote control day
Line, installation part is equipped in four side axles, and the installation part is equipped with image capture module installing port, sets on the installation part
There is connector, driving motor and multiple fixing pieces are equipped on the installation part and the connector, is set on the driving motor
There are multiple rotors, the rotor is equipped with rotor stabilizing member；The system of blocking includes transversal stretching radical occlusion device and just stretches
Radical occlusion device, the transversal stretching radical occlusion device and the just flexible radical occlusion device constitute enclosure space, the vehicle-mounted unmanned aerial vehicle
Setting is taken off in the enclosure space, described in two and the two sides for the power assisting device that lands, and the just flexible radical occlusion device setting exists
It takes off described in two and the front for the power assisting device that lands.
Further, the landing balance system includes landing stable equilibrium's axis and arc balance element, the arc balance
Slide slot is equipped in part, landing stable equilibrium's axis is arranged in the slide slot, and gravity sensing is equipped in the fuselage and is filled
It sets and balance control device, the gravity sensing device is described flat for incuding the landing stable equilibrium shaft balancing state
Weighing apparatus control device is in a vertical state for controlling landing stable equilibrium's axis, and the fuselage is made to keep equilibrium state.
Further, inner loop control unit and outer loop-control unit are equipped in the balance control device；The inner ring control
Unit processed is used to control the posture of landing stable equilibrium's axis and the arc balance element；The outer loop-control unit is for controlling
Make the angle of position and the arc balance element of the landing stable equilibrium's axis in the arc balance element.
Further, landing stable equilibrium's axis is metal shaft, and the end of landing stable equilibrium's axis is equipped with power-assist
Sliding structure, the power-assist sliding structure smoothly slide in the slide slot for the landing stable equilibrium axis.
Further, the end of landing stable equilibrium's axis and the junction of the slide slot are equipped with and slide locked knot
Structure, the locking structure that slides prevent described for being locked after fuselage balance to landing stable equilibrium's axis
Landing stable equilibrium's axis breaks away.
Further, the outside of the arc balance element is equipped with yielding rubber layer, and the yielding rubber layer is used at nobody
When machine lands, vibration is reduced, the outside both ends of the arc balance element are equipped with wireless induction localizing emission device, described wireless
Induction localizing emission device is connect with the gravity sensing device and the balance control device respectively.
Further, take off described in two and the power assisting device that lands in be equipped with sliding slot, it is described take off and land stabilizing member with
It is described to take off and driving device connection of landing, it is described take off and driving device of land control described in take off and the stabilizing member that lands is in institute
State sliding in sliding slot.
Further, it is described take off and the inside for the stabilizing member that lands be equipped with arc balance element card slot, the arc balance element
Card slot by the sliding slot slide clamping described in arc balance element, it is described take off and the stabilizing member that lands on be additionally provided with vehicle-mounted letter
Number reception device and wireless induction position receiver device, the cab signal reception device is for receiving vehicle-mounted instruction, and by vehicle
It carries instruction input to take off and driving device of land to described, the wireless induction position receiver device and wireless induction positioning
Emitter cooperation, for incuding described take off and land the distance between stabilizing member and the arc balance element.
Further, it is described take off and land arc balance element telescopic shaft and arc balance element axis are equipped in stabilizing member,
The arc balance element telescopic shaft is set on the arc balance element axis, and the arc balance element axis is flat in the arc
Weigh and stretch in part telescopic shaft, when arc balance element described in the arc balance element card slot clamping, the arc balance element axis and
The arc balance element telescopic shaft is put in the slide slot, described to take off and stabilization of landing when the vehicle-mounted unmanned aerial vehicle takes off
Part unclamps the arc balance element.
Further, the end of transversal stretching radical occlusion device is equipped with linking arm, and the linking arm is equipped with connection cooperation knot
Structure, the connection fit structure are made of mutually matched connecting groove and connection boss, are set on the just flexible radical occlusion device
There is water proof rubber pad.
Advantageous effects of the invention: vehicle-mounted police UAV system according to the invention, it is provided by the invention vehicle-mounted
Police UAV system, solves in the prior art that cylinder block strength is low, body weight is big, fuselage is difficult to balance, at high cost and peace
Dress is inconvenient, takeoff operational is cumbersome, it is unstable to take off, easily lead to unmanned plane lateral deviation or take off failure the problem of, pass through landing
Stable equilibrium's axis and arc balance element can be good at guaranteeing the balance of unmanned plane, can have by the power assisting device that takes off and land
Effect keeps take off balance and the landing stabilization of unmanned plane, guarantees unmanned plane safety, can be effective by radio induction charging device
Guarantee the radio induction charging of unmanned plane in the non-use state, i.e., unmanned plane, which is once drop to, takes off and land on power assisting device
Wireless charging can be realized, can effectively ensure that the normal electricity consumption of unmanned plane.
Detailed description of the invention
Fig. 1 is the stereoscopic schematic diagram of a preferred embodiment of vehicle-mounted police UAV system according to the invention.
In figure: 1- takes off and lands power assisting device, 2- sliding slot, and 3- takes off and land stabilizing member, and 4- takes off and land driving
Device, 5- cab signal reception device, 6- arc balance element card slot, 7- arc balance element telescopic shaft, 8- arc balance element axis,
9- radio induction charging device, 10- wireless induction localizing emission device, 11- ultrasonic distance measuring module installing port, 12- image are adopted
Collecting module installing port, 13- laterally blocks support device, 14- transversal stretching radical occlusion device, 15- linking arm, 16- connecting groove,
The just flexible radical occlusion device of 17-, 18- water proof rubber pad, 19- telecontrol antenna, 20- fuselage, 21- side axle, the positioning of 22- wireless induction connect
Receiving apparatus, 23- installation part, 24- connector, 25- driving motor, 26- rotor stabilizing member, 27- rotor, 28- fixing piece, 29- can
Carry axis is dismantled, 30-360 ° without dead angle video camera, 31- landing stable equilibrium's axis, 32- arc balance element, 33- slide slot.
Specific embodiment
To make the more clear and clear technical solution of the present invention of those skilled in the art, below with reference to examples and drawings
The present invention is described in further detail, and embodiments of the present invention are not limited thereto.
As shown in Figure 1, the vehicle-mounted police UAV system of one kind provided in this embodiment, including vehicle-mounted unmanned aerial vehicle, take off and
Landing force aid system and block system, it is described take off and the force aid system that land include two be parallel to each other take off and power-assisted of landing fills
Set 1, take off described in two and the power assisting device 1 that lands between be equipped with two and take off and land driving device 4 and a radio induction charging fill
9 are set, takes off described in two and the both ends for the power assisting device 1 that lands is respectively equipped with the stabilizing member 3 that takes off and land；The vehicle-mounted unmanned aerial vehicle packet
Fuselage 20, four side axles 21, detachable carry axis 29 and landing balance system are included, four side axles 21 are symmetrically arranged in the machine
On body 20, the two sides of two side axles 21 are symmetrically arranged in the landing balance system, and the front of the fuselage 20 is equipped with
Ultrasonic distance measuring module installing port 11, the top of the fuselage 20 are equipped with telecontrol antenna 19, are equipped with peace in four side axles 21
Piece installing 23, the installation part 23 are equipped with image capture module installing port 12, and the installation part 23 is equipped with connector 24, described
Driving motor 25 and multiple fixing pieces 28 are equipped on installation part 23 and the connector 24, the driving motor 25 is equipped with more
A rotor 27, the rotor 27 are equipped with rotor stabilizing member 26；The system of blocking includes transversal stretching radical occlusion device 14 and just
Flexible radical occlusion device 17, the transversal stretching radical occlusion device 14 and the just flexible radical occlusion device 17 constitute enclosure space, described
Vehicle-mounted unmanned aerial vehicle setting is taken off in the enclosure space, described in two and the two sides for the power assisting device 1 that lands, and described just stretch is blocked
Device 17 takes off and the front for the power assisting device 1 that lands described in being arranged in two.
Further, in the present embodiment, as shown in Figure 1, the landing balance system includes landing stable equilibrium's axis 31
With arc balance element 32, the arc balance element 32 is interior to be equipped with slide slot 33, and the landing stable equilibrium axis 31 is arranged described
In slide slot 33, gravity sensing device and balance control device are equipped in the fuselage 20, the gravity sensing device is for feeling
The equilibrium state of landing stable equilibrium's axis 31 is answered, the balance control device is for controlling the landing stable equilibrium axis 31
It is in a vertical state, so that the fuselage 20 is kept equilibrium state, the balance control device is interior equipped with inner loop control unit and outer
Ring control unit；The inner loop control unit is used to control the appearance of landing stable equilibrium's axis 31 and the arc balance element 32
State；The outer loop-control unit is used to control position of the landing stable equilibrium's axis 31 in the arc balance element 32, and
The angle of the arc balance element 32.
Further, in the present embodiment, as shown in Figure 1, the landing stable equilibrium axis 31 is metal shaft, the landing
The end of stable equilibrium's axis 31 is equipped with power-assist sliding structure, and the power-assist sliding structure exists for the landing stable equilibrium axis 31
It is smoothly slided in the slide slot 33, the end of landing stable equilibrium's axis 31 and the junction of the slide slot 33 are equipped with and slide
Row locking structure, the locking structure that slides is for carrying out the landing stable equilibrium axis 31 after the fuselage 20 balance
It is locked, prevent the landing stable equilibrium axis 31 from breakking away.
Further, in the present embodiment, as shown in Figure 1, the outside of the arc balance element 32 is equipped with yielding rubber layer,
The yielding rubber layer is used in unmanned plane landing, reduces vibration, and the outside both ends of the arc balance element 32 are equipped with nothing
Line incudes localizing emission device 10, the wireless induction localizing emission device 10 respectively with the gravity sensing device and described flat
Weigh control device connection, take off described in two and the power assisting device 1 that land in be equipped with sliding slot 2, it is described take off and land stabilizing member 3 and
It is described to take off and the connection of driving device 4 of landing, it is described take off and driving device 4 of land control described in take off and the stabilizing member 3 that lands
It is slided in the sliding slot 2.
Further, in the present embodiment, as shown in Figure 1, described take off and the inside for the stabilizing member 3 that lands is flat equipped with arc
Weigh part card slot 6, the arc balance element card slot 6 by the sliding slot 2 slide clamping described in arc balance element 32, described
Cab signal reception device 5 and wireless induction position receiver device 22, the cab signal are additionally provided on winged and landing stabilizing member 3
Reception device 5 is taken off and driving device 4 of land for receiving vehicle-mounted instruction, and by vehicle-mounted instruction input to described, it is described wirelessly
Incude position receiver device 22 and the wireless induction localizing emission device 10 to cooperate, for incuding described take off and stabilization of landing
The distance between part 3 and the arc balance element 32, it is described take off and land arc balance element telescopic shaft 7 is equipped in stabilizing member 3
With arc balance element axis 8, the arc balance element telescopic shaft 7 is set on the arc balance element axis 8, and the arc is flat
The part axis 8 that weighs stretches in the arc balance element telescopic shaft 7, arc balance element described in 6 clamping of arc balance element card slot
When 32, the arc balance element axis 8 and the arc balance element telescopic shaft 7 are put in the slide slot 33, the vehicle-mounted nothing
It is man-machine when taking off, it is described to take off and the stabilizing member 3 that lands unclamps the arc balance element 32.
Further, in the present embodiment, as shown in Figure 1, the end of the transversal stretching radical occlusion device 14 is equipped with connection
Arm 15, the linking arm 15 are equipped with connection fit structure, and the connection fit structure is by mutually matched 16 He of connecting groove
Boss composition is connected, the just flexible radical occlusion device 17 is equipped with water proof rubber pad 18.
In conclusion in the present embodiment, it is provided in this embodiment according to the vehicle-mounted police UAV system of the present embodiment
Vehicle-mounted police UAV system, solves in the prior art that cylinder block strength is low, body weight is big, fuselage is difficult to balance, at high cost
And installation is inconvenient, takeoff operational is cumbersome, it is unstable to take off, easily lead to unmanned plane lateral deviation or take off failure the problem of, pass through
Landing stable equilibrium's axis and arc balance element can be good at guaranteeing the balance of unmanned plane, pass through the power assisting device energy that takes off and land
Enough take off balance and landing stabilizations for effectively keeping unmanned plane, guarantee unmanned plane safety, can by radio induction charging device
The radio induction charging of unmanned plane in the non-use state is effectively ensured, i.e. unmanned plane once drop to the power-assisted dress that takes off and land
It sets and wireless charging can be realized, can effectively ensure that the normal electricity consumption of unmanned plane.
The above, further embodiment only of the present invention, but scope of protection of the present invention is not limited thereto, and it is any
Within the scope of the present disclosure, according to the technique and scheme of the present invention and its design adds those familiar with the art
With equivalent substitution or change, protection scope of the present invention is belonged to.
Claims (10)
1. a kind of vehicle-mounted police UAV system, including vehicle-mounted unmanned aerial vehicle, takes off and land and force aid system and block system, it is special
Sign is: it is described take off and the force aid system that lands include two be parallel to each other take off and the power assisting device that lands (1), take off described in two
And be equipped with two between landing power assisting device (1) and take off and driving device of landing (4) and a radio induction charging device (9), two institutes
The both ends for stating the power assisting device (1) that takes off and land are respectively equipped with take off and land stabilizing member (3)；The vehicle-mounted unmanned aerial vehicle includes machine
Body (20), four side axles (21), detachable carry axis (29) and landing balance system, four side axles (21) are symmetrically arranged in institute
It states on fuselage (20), the two sides of two side axles (21) are symmetrically arranged in the landing balance system, the fuselage (20)
Front is equipped with ultrasonic distance measuring module installing port (11), and the top of the fuselage (20) is equipped with telecontrol antenna (19), described in four
It is equipped in side axle (21) installation part (23), the installation part (23) is equipped with image capture module installing port (12), the peace
Piece installing (23) is equipped with connector (24), be equipped on the installation part (23) and the connector (24) driving motor (25) and
Multiple fixing pieces (28), the driving motor (25) are equipped with multiple rotors (27), and the rotor (27) is stablized equipped with rotor
Part (26)；The system of blocking includes transversal stretching radical occlusion device (14) and just flexible radical occlusion device (17), the transversal stretching
Radical occlusion device (14) and described just flexible radical occlusion device (17) constitute enclosure space, and the vehicle-mounted unmanned aerial vehicle is arranged in the closing
It takes off in space, described in two and the two sides of the power assisting device that lands (1), just flexible radical occlusion device (17) setting rises described in two
Winged and landing power assisting device (1) front.
2. the vehicle-mounted police UAV system of one kind according to claim 1, it is characterised in that: the landing balance system packet
Landing stable equilibrium's axis (31) and arc balance element (32) are included, is equipped with slide slot (33) in the arc balance element (32), it is described
Stable equilibrium's axis (31) setting land in the slide slot (33), gravity sensing device and balance are equipped in the fuselage (20)
Control device, the gravity sensing device are used to incude the equilibrium state of landing stable equilibrium's axis (31), the balance control
Device processed is in a vertical state for controlling the landing stable equilibrium axis (31), and the fuselage (20) is made to keep equilibrium state.
3. the vehicle-mounted police UAV system of one kind according to claim 2, it is characterised in that: in the balance control device
Equipped with inner loop control unit and outer loop-control unit；The inner loop control unit is for controlling the landing stable equilibrium axis (31)
With the posture of the arc balance element (32)；The outer loop-control unit is for controlling the landing stable equilibrium axis (31) in institute
State the position in arc balance element (32) and the angle of the arc balance element (32).
4. the vehicle-mounted police UAV system of one kind according to claim 2, it is characterised in that: landing stable equilibrium's axis
It (31) is metal shaft, the end of landing stable equilibrium's axis (31) is equipped with power-assist sliding structure, and the power-assist sliding structure is used
It is smoothly slided in the slide slot (33) in the landing stable equilibrium axis (31).
5. the vehicle-mounted police UAV system of one kind according to claim 4, it is characterised in that: landing stable equilibrium's axis
(31) junction of end and the slide slot (33), which is equipped with, slides locking structure, and the locking structure that slides is for described
After fuselage (20) balance, the landing stable equilibrium axis (31) is locked, prevents the landing stable equilibrium axis (31) from sending out
It is raw to break away.
6. the vehicle-mounted police UAV system of one kind according to claim 2, it is characterised in that: the arc balance element (32)
Outside be equipped with yielding rubber layer, the yielding rubber layer be used for unmanned plane landing when, reduce vibration, the arc balance element
(32) outside both ends are equipped with wireless induction localizing emission device (10), and the wireless induction localizing emission device (10) is respectively
It is connect with the gravity sensing device and the balance control device.
7. the vehicle-mounted police UAV system of one kind according to claim 6, it is characterised in that: take off and land described in two and help
It is equipped with sliding slot (2) in power device (1), it is described to take off and the stabilizing member that land (3) and described take off and driving device of landing (4) company
Connect, it is described take off and driving device of landing (4) control described in take off and the stabilizing member that land (3) slides in the sliding slot (2).
8. the vehicle-mounted police UAV system of one kind according to claim 7, it is characterised in that: described to take off and stabilization of landing
The inside of part (3) is equipped with arc balance element card slot (6), and the arc balance element card slot (6) passes through the sliding in the sliding slot (2)
Arc balance element (32) described in clamping, it is described take off and the stabilizing member that lands (3) on be additionally provided with cab signal reception device (5) and nothing
Line incudes position receiver device (22), and the cab signal reception device (5) is used to receive vehicle-mounted instruction, and vehicle-mounted instruction is defeated
Enter to described and take off and driving device of landing (4), the wireless induction position receiver device (22) and the wireless induction position
Emitter (10) cooperation, for incude it is described take off and the stabilizing member that lands (3) and the arc balance element (32) between away from
From.
9. the vehicle-mounted police UAV system of one kind according to claim 8, it is characterised in that: described to take off and stabilization of landing
Arc balance element telescopic shaft (7) and arc balance element axis (8) are equipped in part (3), the arc balance element telescopic shaft (7) is arranged
On the arc balance element axis (8), the arc balance element axis (8) is stretched in the arc balance element telescopic shaft (7)
Contracting, when arc balance element (32) described in arc balance element card slot (6) clamping, the arc balance element axis (8) and described
Arc balance element telescopic shaft (7) is put in the slide slot (33), described to take off and land steady when the vehicle-mounted unmanned aerial vehicle takes off
Determine part (3) and unclamps the arc balance element (32).
10. the vehicle-mounted police UAV system of one kind according to claim 1, it is characterised in that: the transversal stretching blocks
The end of device (14) is equipped with linking arm (15), and the linking arm (15) is equipped with connection fit structure, the connection cooperation knot
Structure is made of mutually matched connecting groove (16) and connection boss, and described just flexible radical occlusion device (17) are equipped with water proof rubber
It pads (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710658442.9A CN109383798A (en) | 2017-08-04 | 2017-08-04 | A kind of vehicle-mounted police UAV system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710658442.9A CN109383798A (en) | 2017-08-04 | 2017-08-04 | A kind of vehicle-mounted police UAV system |
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| CN109383798A true CN109383798A (en) | 2019-02-26 |
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| CN201710658442.9A Pending CN109383798A (en) | 2017-08-04 | 2017-08-04 | A kind of vehicle-mounted police UAV system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111694369A (en) * | 2020-07-09 | 2020-09-22 | 中国人民警察大学 | Night patrol control system for police unmanned aerial vehicle |
| CN114162029A (en) * | 2021-10-27 | 2022-03-11 | 江苏日盈电子股份有限公司 | Vehicle with multi-rotor unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2007141795A1 (en) * | 2006-06-08 | 2007-12-13 | Israel Aerospace Industries Ltd. | Unmanned air vehicle system |
| CN105739523A (en) * | 2015-12-07 | 2016-07-06 | 北京航空航天大学 | Police vehicle-mounted unmanned aerial vehicle monitoring system and control method |
| KR101644151B1 (en) * | 2016-05-12 | 2016-08-11 | (주)원지리정보 | 3D space information monitoring system using intelligent drone |
| CN205942437U (en) * | 2016-07-25 | 2017-02-08 | 南充驭云创新科技有限公司 | A unmanned aerial vehicle for fish finding and flight remote control system thereof |
| KR101720028B1 (en) * | 2015-12-02 | 2017-03-28 | 유콘시스템 주식회사 | Wireless power charging apparatus for unmanned aerial vehicle |
| CN207089656U (en) * | 2017-08-04 | 2018-03-13 | 上海裕芮信息技术有限公司 | A kind of vehicle-mounted police UAS |
-
2017
- 2017-08-04 CN CN201710658442.9A patent/CN109383798A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2007141795A1 (en) * | 2006-06-08 | 2007-12-13 | Israel Aerospace Industries Ltd. | Unmanned air vehicle system |
| KR101720028B1 (en) * | 2015-12-02 | 2017-03-28 | 유콘시스템 주식회사 | Wireless power charging apparatus for unmanned aerial vehicle |
| CN105739523A (en) * | 2015-12-07 | 2016-07-06 | 北京航空航天大学 | Police vehicle-mounted unmanned aerial vehicle monitoring system and control method |
| KR101644151B1 (en) * | 2016-05-12 | 2016-08-11 | (주)원지리정보 | 3D space information monitoring system using intelligent drone |
| CN205942437U (en) * | 2016-07-25 | 2017-02-08 | 南充驭云创新科技有限公司 | A unmanned aerial vehicle for fish finding and flight remote control system thereof |
| CN207089656U (en) * | 2017-08-04 | 2018-03-13 | 上海裕芮信息技术有限公司 | A kind of vehicle-mounted police UAS |
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| CN111694369A (en) * | 2020-07-09 | 2020-09-22 | 中国人民警察大学 | Night patrol control system for police unmanned aerial vehicle |
| CN114162029A (en) * | 2021-10-27 | 2022-03-11 | 江苏日盈电子股份有限公司 | Vehicle with multi-rotor unmanned aerial vehicle |
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