CN209126967U - A kind of police catching formula rotor wing unmanned aerial vehicle - Google Patents
A kind of police catching formula rotor wing unmanned aerial vehicle Download PDFInfo
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- CN209126967U CN209126967U CN201821911590.3U CN201821911590U CN209126967U CN 209126967 U CN209126967 U CN 209126967U CN 201821911590 U CN201821911590 U CN 201821911590U CN 209126967 U CN209126967 U CN 209126967U
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Abstract
The utility model discloses a kind of police catching formula rotor wing unmanned aerial vehicles, including unmanned plane main body, rotor and arresting agency, unmanned plane main body includes shell, top cover, flies control mainboard and lithium battery, fly the inside that control mainboard is fixedly connected on shell, lithium battery is located at the top for flying control mainboard and is slidably connected with shell, the junction of lithium battery and shell is equipped with sliding slot, and the surface of shell is equipped with the top cover being fastened and connected, and the bottom of shell is fixedly connected with support frame；Rotor is fixedly connected on the edge of shell in a ring, and one end of rotor is fixedly connected with the casing and the other end is fixedly connected with brushless motor, and the output end of brushless motor is fixedly connected with propeller；Arresting agency is fixedly connected on the bottom of shell.The utility model avoids damaging aircraft, convenient for users to looking for and getting, convenient for punishing and educating to user, while aircraft out of control being avoided to fall, reduce the security risk for arresting aircraft by being equipped with arresting agency in the bottom of unmanned plane.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of police catching formula rotor wing unmanned aerial vehicle.
Background technique
With the development of science and technology, in life production process, the use scope of rotor wing unmanned aerial vehicle is more and more extensive, by
Have many advantages, such as maneuverability in rotor wing unmanned aerial vehicle, have a smooth flight, therefore rotor wing unmanned aerial vehicle is also applied to retail stores management transport
System is used for carry, transport and delivery items.As the cost for unmanned plane of taking photo by plane reduces, many players can buy and take photo by plane
Unmanned plane is taken photo by plane, and certain airspaces forbid unmanned vehicle to fly, and people's police can shoot down the unmanned plane in the airspace.
Currently, lacking the break catching apparatus to unmanned plane of taking photo by plane in market, the unmanned plane after directly shooting down is being unable to control
In the case where can directly damage, user cannot be searched out, the purpose of warning and education can not be played to user, and fallen
Unmanned plane be easy on ground people or object damage, there are biggish security risks.For this reason, it may be necessary to design a kind of new skill
Art scheme, which is given, to be solved.
Utility model content
The purpose of this utility model is to provide a kind of police catching formula rotor wing unmanned aerial vehicle, the utility model passes through at nobody
The bottom of machine be equipped with arresting agency, avoid damaging aircraft, convenient for users to looking for and getting, convenient for user into
Row punishment and education, while aircraft out of control being avoided to fall, reduce the security risk for arresting aircraft.
To achieve the above object, the utility model provides the following technical solutions: a kind of police catching formula rotor wing unmanned aerial vehicle, packet
Unmanned plane main body, rotor and arresting agency are included, the unmanned plane main body includes shell, top cover, flies control mainboard and lithium battery, described
Fly the inside that control mainboard is fixedly connected on shell, the lithium battery is located at the top for flying control mainboard and is slidably connected with shell, institute
The junction for stating lithium battery and shell is equipped with sliding slot, and the surface of the shell is equipped with the top cover being fastened and connected, the bottom of the shell
Portion is fixedly connected with support frame；The rotor is fixedly connected on the edge of shell, one end of the rotor and shell in a ring
It is fixedly connected and the other end is fixedly connected with brushless motor, the output end of the brushless motor is fixedly connected with propeller；It is described
Arresting agency is fixedly connected on the bottom of shell, and the arresting agency includes fixed frame, rotating bar, stepper motor and folding stand,
The rotating bar is located at the inside of fixed frame and is rotatablely connected with fixed frame, and the stepper motor is fixedly connected on the top of fixed frame
Portion, the folding stand are made of the first brace and the second brace interconnection, the infall of first brace and the second brace
Equipped with rotation axis, the bottom of the folding stand is fixedly connected with claw.
As an improvement of the above technical solution, the bottom of the shell be equipped with camera, the camera by holder with
Unmanned plane main body is fixedly connected, and the camera is connected with control mainboard is flown.
As an improvement of the above technical solution, the inside of the fixed frame is equipped with accommodation groove, and the bottom of the fixed frame is solid
Surely it is connected with pulsed coil, the pulsed coil is located at the left side of folding stand, and the pulsed coil is connected with control mainboard is flown.
As an improvement of the above technical solution, the bottom of the fixed frame is vertically connected with guide plate, in the guide plate
Guide groove is offered, the end of the rotation axis is embedded in guide groove and is slidably connected with guide groove.
As an improvement of the above technical solution, the inside of the fixed frame is equipped with accommodation groove, and the rotating bar is located at accommodating
In slot and right end stretches out in outside fixed frame, and the inside of the accommodation groove is equipped with the first sliding block and the second sliding block that are slidably connected, institute
The bottom for stating accommodation groove offers open slot, and institute's open slot is slidably connected with folding stand.
As an improvement of the above technical solution, rotating bar left-half surface is equipped with screw thread, a left side for the rotating bar
Half part is connect with the first sliding block by threads turn, and the right half part of the rotating bar is slidably connected with the second sliding block, described
The right side of rotating bar is fixedly connected with driven gear.
As an improvement of the above technical solution, the output end of the stepper motor is fixedly connected with driving gear, the master
Moving gear engages connection with driven gear, and the stepper motor is connected with control mainboard is flown.
As an improvement of the above technical solution, first brace and the first sliding block are rotatablely connected, second brace with
The rotation connection of second sliding block.
Compared with prior art, the beneficial effects of the utility model are as follows:
1, the utility model is by being equipped with arresting agency in the bottom of unmanned plane, convenient for the aircraft to fly to aerial violation
Captured, avoid damaging aircraft, convenient for users to looking for and getting, while convenient for user carry out punishment and
Education, arrests aircraft by using arresting agency, aircraft out of control is avoided to fall, and the peace for arresting aircraft is reduced
Full blast danger.
2, the utility model is used cooperatively by using folding stand and pulsed coil, is connect convenient for the signal to aircraft
Capable interference is taken in, keeps aircraft out of hand, so that convenient arrest aircraft, by using the rotating bar for driving screw thread
Folding stand is driven, convenient to be grabbed while folding stand stretches out, structure is simple, and high reliablity is hardly damaged, drop
The cost that low-dimensional is repaired.
Detailed description of the invention
Fig. 1 is police catching formula rotor wing unmanned aerial vehicle positive structure diagram described in the utility model；
Fig. 2 is police catching formula rotor wing unmanned aerial vehicle side structure schematic view described in the utility model；
Fig. 3 is fixed frame schematic diagram of internal structure described in the utility model.
In figure: unmanned plane main body -1, rotor -2, arresting agency -3, shell -4, top cover -5 fly control mainboard -6, lithium battery -
7, sliding slot -8, support frame -9, brushless motor -10, propeller -11, fixed frame -12, rotating bar -13, stepper motor -14, folding
Frame -15, the first brace -16, the second brace -17, rotation axis -18, claw -19, camera -20, pulsed coil -21, guide plate -
22, guide groove -23, accommodation groove -24, the first sliding block -25, the second sliding block -26, open slot -27, screw thread -28, driven gear -29,
Driving gear -30.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe.
It please refers to Fig. 1-3 the utility model and a kind of technical solution is provided: a kind of police catching formula rotor wing unmanned aerial vehicle, including nothing
Man-machine main body 1, rotor 2 and arresting agency 3, the unmanned plane main body 1 include shell 4, top cover 5, fly control mainboard 6 and lithium battery 7,
The winged control mainboard 6 is fixedly connected on the inside of shell 4, and the lithium battery 7 is located at the top for flying control mainboard 6 and slides with shell 4
The junction of dynamic connection, the lithium battery 7 and shell 4 is equipped with sliding slot 8, and the surface of the shell 4 is equipped with the top cover being fastened and connected
5, the bottom of the shell 4 is fixedly connected with support frame 9；The rotor 2 is fixedly connected on the edge of shell 4, institute in a ring
The one end for stating rotor 2 is fixedly connected with shell 4 and the other end is fixedly connected with brushless motor 10, the output of the brushless motor 10
End is fixedly connected with propeller 11；The arresting agency 3 is fixedly connected on the bottom of shell 4, and the arresting agency 3 includes fixing
Frame 12, rotating bar 13, stepper motor 14 and folding stand 15, the rotating bar 13 be located at the inside of fixed frame 12 and with fixed frame 12
Rotation connection, the stepper motor 14 are fixedly connected on the top of fixed frame 12, and the folding stand 15 is by the first brace 16 and the
Two braces, 17 interconnection is constituted, and the infall of first brace 16 and the second brace 17 is equipped with rotation axis 18, the folding
The bottom of frame 15 is fixedly connected with claw 19, by being fixedly connected with claw 19 in the bottom of folding stand 15, is convenient for folding stand 15
It is grabbed while stretching, improves the convenience of break catching apparatus.
It is further improved ground, as shown in Figs. 1-2: the bottom of the shell 4 is equipped with camera 20, and the camera 20 passes through
Holder is fixedly connected with unmanned plane main body 1, and the camera 20 is connected with control mainboard 6 is flown, by being equipped in the bottom of shell 4
Camera 20 facilitates operator's remote control to arrest unmanned plane and arrests to other aircraft, convenient for other aircraft
It is tracked.
It is further improved ground, as shown in Figs. 1-2: the bottom of the fixed frame 12 is fixedly connected with pulsed coil 21, described
Pulsed coil 21 is located at the left side of folding stand 15, and the pulsed coil 21 is connected with control mainboard 6 is flown, by fixed frame 12
Bottom is equipped with pulsed coil 21, carries out electromagnetic interference convenient for arresting unmanned plane to other aircraft, other aircraft is made to lose control
System, is arrested convenient for arresting unmanned plane to it.
It is further improved ground, as shown in Figure 3: the bottom of the fixed frame 12 is vertically connected with guide plate 22, the guiding
Guide groove 23 is offered in plate 22, the end of the rotation axis 18 is embedded in guide groove 23 and is slidably connected with guide groove 23,
By being vertically connected with the guide plate 22 with guide groove 23 in the bottom of fixed frame 12, structure is unstable when folding stand 15 being avoided to move
It is fixed and shift, improve arrest unmanned plane arrest accuracy.
It is further improved ground, as shown in Figure 3: the inside of the fixed frame 12 is equipped with accommodation groove 24, the rotating bar 13
In in accommodation groove 24 and right end stretches out in outside fixed frame 12, the inside of the accommodation groove 24 is equipped with the first sliding block 25 being slidably connected
With the second sliding block 26, the bottom of the accommodation groove 24 offers open slot 27, and institute's open slot 27 is slidably connected with folding stand 15, leads to
It crosses the inside in fixed frame 12 and is equipped with accommodation groove 24, facilitate the driving sliding of rotating bar 13 to be moved, thus Foldable frame 15
Stretching motion is carried out, by being equipped with open slot 27 in the bottom of accommodation groove 24, frame 15 convenient for folding is moved.
It is further improved ground, as shown in Figure 3: the 13 left-half surface of rotating bar is equipped with screw thread 28, the rotating bar
13 left-half is rotatablely connected with the first sliding block 25 by screw thread 28, the right half part of the rotating bar 13 and the second sliding block 26
It is slidably connected, the right side of the rotating bar 13 is fixedly connected with driven gear 29, by 13 left-half surface of rotating bar
Equipped with screw thread 28, convenient for driving the first sliding block 25 to horizontally slip in accommodation groove 24, second is driven to slide by the characteristic that bar connects
Block 26 moves synchronously in accommodation groove 24.
Specifically with improvement, as shown in Figure 3: the output end of the stepper motor 14 is fixedly connected with driving gear 30, described
Driving gear 30 engages connection with driven gear 29, and the stepper motor 14 is connected with control mainboard 6 is flown, by stepper motor
14 output end is fixedly connected with driving gear 30, convenient for passing through 13 rotational motion of gear connecting band turn lever.
More specifically with improvement, as shown in Figure 3: first brace 16 and the first sliding block 25 are rotatablely connected, and described second tiltedly
Bar 17 and the second sliding block 26 are rotatablely connected, and convenient for making the transverse shifting of the first sliding block 25 and the second sliding block 26, drive folding stand 15
Longitudinal movement is conveniently arrested unmanned plane stretching claw 19 and is clamped.
The unmanned plane main body -1 of the utility model, rotor -2, arresting agency -3, shell -4, top cover -5, fly control mainboard -6,
Lithium battery -7, sliding slot -8, support frame -9, brushless motor -10, propeller -11, fixed frame -12, rotating bar -13, stepper motor -
14, folding stand -15, the first brace -16, the second brace -17, rotation axis -18, claw -19, camera -20, pulsed coil -21,
It is guide plate -22, guide groove -23, accommodation groove -24, the first sliding block -25, the second sliding block -26, open slot -27, screw thread -28, driven
Gear -29, driving gear -30, component are universal standard part or component, its structure and principle as known to those skilled in the art
All it can be learnt by technical manual or be known by routine experiment method for this technology personnel, which is specially
FC1212-S flies control mainboard, and the utility model is by being equipped with arresting agency 3 in the bottom of unmanned plane, convenient for flying to aerial violation
Aircraft captured, avoid damaging aircraft, convenient for users to looking for and getting, while convenient for user into
Row punishment and education, arrest aircraft by using arresting agency 3, avoid aircraft out of control from falling, reduction is arrested
The security risk of aircraft.
The utility model when arresting to violation aircraft, arrest unmanned plane and fly to flying for violation by operator's control
Row device, the scene that operator is passed back by camera 20 are adjusted to unmanned plane is arrested, and make to arrest unmanned plane and fly in violation of rules and regulations
The top of aircraft, then starting impulse coil 21, carries out signal interference to violation aircraft, keeps its out of hand, then control
Stepper motor 14 processed rotates, and drives the first sliding block 25 to be moved through to middle part by rotating bar 13, the first brace 16 drives rotation axis
18 move down along guide groove 23, so that control the second brace 17 movement, makes the second sliding block 26 along the surface synchronization of rotating bar 13
It is mobile to middle part, folding stand 15 is extended downwardly, while 19 pairs of violation aircraft of claw being driven to arrest, avoids directly shooting down
Aircraft bring security risk.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (8)
1. a kind of police catching formula rotor wing unmanned aerial vehicle, including unmanned plane main body (1), rotor (2) and arresting agency (3), feature
Be: the unmanned plane main body (1) includes shell (4), top cover (5), flies control mainboard (6) and lithium battery (7), the winged control mainboard
(6) it is fixedly connected on the inside of shell (4), the lithium battery (7) is located at the top for flying control mainboard (6) and slides with shell (4)
Connection, the lithium battery (7) and the junction of shell (4) are equipped with sliding slot (8), and the surface of the shell (4), which is equipped with, to be fastened and connected
Top cover (5), the bottom of the shell (4) is fixedly connected with support frame (9)；The rotor (2) is fixedly connected on shell in a ring
One end of the edge of body (4), the rotor (2) is fixedly connected with shell (4) and the other end is fixedly connected with brushless motor
(10), the output end of the brushless motor (10) is fixedly connected with propeller (11)；The arresting agency (3) is fixedly connected on shell
The bottom of body (4), the arresting agency (3) include fixed frame (12), rotating bar (13), stepper motor (14) and folding stand
(15), the rotating bar (13) is located at the inside of fixed frame (12) and is rotatablely connected with fixed frame (12), the stepper motor
(14) it is fixedly connected on the top of fixed frame (12), the folding stand (15) is intersected by the first brace (16) and the second brace (17)
It connects and composes, the infall of first brace (16) and the second brace (17) is equipped with rotation axis (18), the folding stand (15)
Bottom be fixedly connected with claw (19).
2. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: the bottom of the shell (4)
Portion is equipped with camera (20), and the camera (20) is fixedly connected by holder with unmanned plane main body (1), the camera (20)
It is connected with winged control mainboard (6).
3. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: the fixed frame (12)
Bottom is fixedly connected with pulsed coil (21), and the pulsed coil (21) is located at the left side of folding stand (15), the pulsed coil
(21) it is connected with winged control mainboard (6).
4. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: the fixed frame (12)
Bottom is vertically connected with guide plate (22), is offered guide groove (23) in the guide plate (22), the end of the rotation axis (18)
Portion is embedded in guide groove (23) and is slidably connected with guide groove (23).
5. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: the fixed frame (12)
Inside is equipped with accommodation groove (24), and the rotating bar (13) is located in accommodation groove (24) and right end stretches out in fixed frame (12) outside, institute
The inside for stating accommodation groove (24) is equipped with the first sliding block (25) and the second sliding block (26) being slidably connected, the bottom of the accommodation groove (24)
Portion offers open slot (27), and institute's open slot (27) is slidably connected with folding stand (15).
6. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: the rotating bar (13) is left
Half part surface is equipped with screw thread (28), and the left-half of the rotating bar (13) and the first sliding block (25) are rotated by screw thread (28)
Connection, right half part and the second sliding block (26) of the rotating bar (13) are slidably connected, and the right side of the rotating bar (13) is solid
Surely driven gear (29) are connected with.
7. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: the stepper motor (14)
Output end be fixedly connected with driving gear (30), the driving gear (30) engages connection, the step with driven gear (29)
It is connected into motor (14) with control mainboard (6) is flown.
8. a kind of police catching formula rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: first brace (16)
It is rotatablely connected with the first sliding block (25), second brace (17) and the second sliding block (26) are rotatablely connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821911590.3U CN209126967U (en) | 2018-11-20 | 2018-11-20 | A kind of police catching formula rotor wing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821911590.3U CN209126967U (en) | 2018-11-20 | 2018-11-20 | A kind of police catching formula rotor wing unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN209126967U true CN209126967U (en) | 2019-07-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821911590.3U Active CN209126967U (en) | 2018-11-20 | 2018-11-20 | A kind of police catching formula rotor wing unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367778A (en) * | 2018-11-20 | 2019-02-22 | 南京森林警察学院 | A kind of police catching formula rotor wing unmanned aerial vehicle |
| CN112193416A (en) * | 2020-09-29 | 2021-01-08 | 北京二郎神科技有限公司 | Unmanned aerial vehicle and logistics distribution system |
-
2018
- 2018-11-20 CN CN201821911590.3U patent/CN209126967U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367778A (en) * | 2018-11-20 | 2019-02-22 | 南京森林警察学院 | A kind of police catching formula rotor wing unmanned aerial vehicle |
| CN112193416A (en) * | 2020-09-29 | 2021-01-08 | 北京二郎神科技有限公司 | Unmanned aerial vehicle and logistics distribution system |
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