CN206590121U - A kind of multi-functional unmanned plane with dispenser - Google Patents
A kind of multi-functional unmanned plane with dispenser Download PDFInfo
- Publication number
- CN206590121U CN206590121U CN201720337149.8U CN201720337149U CN206590121U CN 206590121 U CN206590121 U CN 206590121U CN 201720337149 U CN201720337149 U CN 201720337149U CN 206590121 U CN206590121 U CN 206590121U
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- China
- Prior art keywords
- unmanned plane
- dispenser
- functional
- control board
- steering wheel
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000000463 material Substances 0.000 claims abstract description 11
- 239000003381 stabilizer Substances 0.000 claims abstract description 7
- 230000005236 sound signal Effects 0.000 claims description 8
- 230000007704 transition Effects 0.000 claims description 3
- 229920000049 Carbon (fiber) Polymers 0.000 claims 1
- 239000004917 carbon fiber Substances 0.000 claims 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical group C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims 1
- 238000012544 monitoring process Methods 0.000 abstract description 5
- 238000007689 inspection Methods 0.000 abstract description 3
- 238000011835 investigation Methods 0.000 abstract description 3
- 230000009467 reduction Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical group [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
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- 230000004048 modification Effects 0.000 description 1
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- 238000006467 substitution reaction Methods 0.000 description 1
Abstract
The utility model discloses a kind of multi-functional unmanned plane with dispenser, including unmanned plane body and remote control, propeller, wireless transceiver, GPS location stabilizer, control board and functional part are installed on the unmanned plane body, remote control is controlled by wireless transceiver and control board to the landing of unmanned plane body, flight and each functional part, and the functional part includes dispenser, high-definition camera, major light and the loudspeaker being electrically connected with the control board；The dispenser includes dispenser steering wheel and movable lock pin, and dispenser steering wheel can open lock pin in the presence of remote control and realize article and deliver.The utility model has the functions such as the investigation of landform ground, goods and materials dispensing, high-altitude voice, floodlighting, night flying, practical, is suitable for carrying out rescue and relief work, fire-fighting and rescue, public security monitoring and road administration, coast defence, forest, electric power inspection etc..
Description
Technical field
The utility model is related to a kind of unmanned vehicle, specially a kind of multi-functional unmanned plane with dispenser.
Background technology
Telecontrolled aircraft is a kind of self-powered, small aircraft flown by remote control control, and a remote control is planted using crossing
Unmanned plane can obtain the important information on ground, such as image, including static picture and video, and multi-rotor unmanned aerial vehicle is because of the letter of its structure
The features such as list, low cost, good manipulation ability, can a variety of loads such as integrated GPS, moving camera complete complex task, it is existing
Stage most of remotely-piloted vehicles are only the functions of having possessed remote control and flight, and its structure, function are single, and are not had necessarily
Practicality.And, it is necessary to which one kind can carry out dispensing goods and materials, carry out the disaster relief functions such as high-altitude voice, floodlighting in rescue and relief work
Unmanned plane.
Utility model content
For defect of the prior art, the utility model provides a kind of multi-functional unmanned plane with dispenser, and it has
There are the functions such as the investigation of landform ground, goods and materials dispensing, high-altitude voice, floodlighting, night flying, it is practical, it is suitable for carrying out
Rescue and relief work, fire-fighting and rescue, public security monitoring and road administration, coast defence, forest, electric power inspection etc..
The utility model discloses a kind of multi-functional unmanned plane with dispenser, including unmanned plane body and remote control,
Propeller, wireless transceiver, GPS location stabilizer, control board and functional part are installed on the unmanned plane body, it is distant
Control device is controlled by wireless transceiver and control board to the landing of unmanned plane body, flight and each functional part,
The functional part includes dispenser, high-definition camera, major light and the loudspeaker being electrically connected with the control board；
The dispenser is located at middle side part under unmanned plane body, and the high-definition camera is located in the middle part of the front side of unmanned plane body, described
Major light and loudspeaker are located at the both sides of high-definition camera respectively, and the loudspeaker is connected with intercom audio signal；Institute
Stating dispenser includes dispenser steering wheel and movable lock pin, and dispenser steering wheel can open lock pin in the presence of remote control and realize
Article is delivered.
The utility model sets dispenser, high-definition camera, major light and loudspeaker, high pitch loudspeaker on unmanned plane body
Be connected with intercom audio signal so that being simply possible to use in the unmanned plane taken photo by plane has more utility functions；Taken the photograph by high definition
Camera is by ground or to be scouted the image photographic of object and beams back ground monitoring end, and ground monitoring end is according to ground or scouts object
Situation come the flight, landing and feature operation of remotely pilotless machine；Dispenser is opened by remote control device dispenser steering wheel
Lock pin, is delivered so as to obtain the disaster relief supplies hooked in pin or fire extinguisher bomb and other items and realize；Major light can be illuminated to ground,
It is easy to scout, reconnoitre or rescue, while also contributing to unmanned plane night flying；Loudspeaker is used cooperatively with intercom, ground
The sound of intercom, to loudspeaker, realizes that high-altitude voice is propagandaed directed to communicate by the audio signal transmission of intercom on unmanned plane.
Further, in order to obtain apparent view data, and multi-angled shooting is realized, the high-definition camera is
Zoom camera, high-definition camera is arranged on unmanned plane body by head, and high-definition camera can realize left and right by head
With the rotation of above-below direction.Zoom camera autozoom or can pass through remote control manual zoom.
Further, to protect each electrical part and functional part, the unmanned plane body includes frame and nose shell, frame
Upper to install the wireless transceiver, GPS location stabilizer, control board, functional part and propeller, the head is covered
Cover in frame.
Further, it is reduction windage, realizes preferably balance, the nose shell is disc structure, at discoidal bottom
An arc-shaped protrusions are provided with the middle part of disk, arc-shaped protrusions are connected with chassis cambered surface transition.
Further, undercarriage is also symmetrically set with the unmanned plane body, undercarriage includes being sequentially connected connecing
Undercarriage steering wheel, linkage and support body, undercarriage steering wheel and the control board be electrically connected with, and undercarriage steering wheel passes through
Linkage carries out folding and unfolding to support body.Undercarriage can be stablely supported at level point when being easy to unmanned plane body to land, and not
Each functional part for damaging and being set to below unmanned plane body can be supported, and undercarriage is packed up during flight, makes missile will not be in the air
Undercarriage is hooked or touched, in order to avoid winding, which can not be delivered, article or even influences unmanned plane during flying, and undercarriage is packed up and also has
Beneficial to reduction windage to keep the balance of unmanned plane during flying
Further, for landing balance and damping is better achieved, the support body is inverted T-shaped, and the bottom of support body is laterally
The thin end of the scroll, and shock-absorbing sleeve be cased with the thin end of the scroll；When unmanned plane body flight, undercarriage described in two respectively beat to the left and right by two outsides
Open and pack up.
Further, the propeller is the multiple of even number amount, and propeller includes horn and blade, and horn can turn with frame
Connect dynamicly, the free end of horn is provided with motor, and the output shaft and blade of motor are detachably connected.
Further, the propeller is 6 or 8, and the output shaft of the blade and motor is connected through a screw thread, screw thread
To screw direction identical with the direction of rotation of motor.Being connected through a screw thread can easily fast assembling-disassembling blade, the side of screwing of screw thread
To identical with the direction of rotation of motor, blade is set not released because of the rotation of motor.
Further, the frame is carbon fibre material, and the nose shell is PLA materials.
Further, be the direction of illumination of flexible modulation major light, the major light by rotating shaft rotationally with frame
Connection.
The beneficial effects of the utility model are：Compared with prior art, the utility model is multiple functional, simple to operate, can
, can with multiple functions such as remote zoom camera, the investigation of landform ground, high-altitude dialogue, floodlighting and remote dispensing goods and materials
Remote control distance is 2000 meters or so, and its flying height is up to 500 meters, and flying speed reaches 15 meters per second, and wind loading rating is up to 6 grades of left sides
The right side, 40 minutes or so cruising time, and the flight at night can also be met by the irradiation of major light, utility function is strong,
Can be readily applied to fire-fighting and rescue, road administration inspection, coast defence patrol, public security monitoring, power-line patrolling, forest fire protection, land surveying and
The fields such as agricultural plant protection.
Brief description of the drawings
, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
The accompanying drawing used required in embodiment or description of the prior art is briefly described.In all of the figs, it is similar
Element or part are general by similar reference mark.In accompanying drawing, each element or part might not be according to actual ratios
Draw.
Fig. 1 is one of structural representation of the present utility model；
Fig. 2 (the horn folding of propeller, pulls down blade, drop for the two of structural representation of the present utility model
State)；
Fig. 3 is the structural representation of the utility model dispenser；
Fig. 4 is the structural representation of the utility model undercarriage.
Embodiment
The embodiment of technical solutions of the utility model is described in detail below in conjunction with accompanying drawing.Following examples are only
For clearly illustrating the technical solution of the utility model, therefore example is only used as, and this practicality can not be limited with this
New protection domain.
As shown in Figure 1 to Figure 3, the utility model discloses a kind of multi-functional unmanned plane with dispenser 5, including nobody
Being connected with machine body 10, remote control 20 and intercom 30, the remote control 20 of the present embodiment on display screen 22, display screen 22 to show
Show and power supply, propeller 3, wireless transceiver, GPS are installed on the image that the transmission of high-definition camera 6 comes, the unmanned plane body 10
Orientation stabilizer, control board and functional part, remote control 20 is by wireless transceiver and control board to unmanned plane
Landing, flight and each functional part of body 10 are controlled, and this is prior art, and therefore not to repeat here.The function part
Part includes dispenser 5, high-definition camera 6, major light 7 and the loudspeaker 8 being electrically connected with the control board；It is described to throw
Device 5 is put positioned at 10 times middle side parts of unmanned plane body, the dispenser 5 includes dispenser steering wheel 51 and mobilizable lock pin 52, throws
Device steering wheel 51 is put to open lock pin 52 by steering wheel connecting rod 54 in the presence of remote control 20 and realize article and deliver.Dispenser steering wheel
51 rotation direction is different and is moved with pendulum lock pin 52 along its axis, when lock pin 52 closes the breach 53 of dispenser 5, can hook
Missile, lock pin 52 move and make a breach 53 when, the missile hooked drops from breach 53, realize deliver.
The high-definition camera 6 is located in the middle part of the front side of unmanned plane body 10, in order to obtain apparent view data, and
And multi-angled shooting is realized, the high-definition camera 6 is Zoom camera, and high-definition camera 6 is arranged on unmanned plane by head
On body 10, high-definition camera 6 can realize the rotation of left and right and above-below direction by head.Zoom camera can pass through remote control
Zoom is realized in 20 operation.
The both sides of high-definition camera 6 are respectively equipped with the major light 7 and loudspeaker 8, are the photograph of flexible modulation major light 7
Direction is penetrated, the major light 7 is rotationally connected by motor-driven rotating shaft with frame 1, motor and the control board
It is electrically connected with, certain major light 7 can also be articulated and connected with frame 1, manually adjust its direction.The loudspeaker 8 and intercom
30 audio signals are connected, and the audio signal of the intercom acceptance division on unmanned plane draws the audio input end for being connected to loudspeaker 8, by
Intercom 30 on ground sends voice, and speech play is realized by the intercom acceptance division on unmanned plane, loudspeaker 8.
As shown in Figure 1, Figure 2 and Figure 4, to protect each electrical part and functional part, the unmanned plane body 10 includes frame 1
With nose shell 2, frame 1 is carbon fibre material, and strong light-weight, the nose shell 2 is that PLA is the biodegradable material of PLA
Matter, material environment friendly and degradable.The wireless transceiver, GPS location stabilizer, control board, function are installed in frame 1
Part and propeller 3, the nose shell 2 are covered in frame 1.For reduction windage, preferably balance, the nose shell are realized
2 be disc structure, and an arc-shaped protrusions 21 are provided with the middle part of discoidal chassis, and arc-shaped protrusions 21 are connected with chassis cambered surface transition.
Undercarriage 4 is also left and right symmetrically arranged in the frame 1 of unmanned plane body 10, undercarriage 4 includes being sequentially connected the undercarriage connect
Steering wheel 41, linkage 42 and support body 43, support body 43 is inverted T-shaped, and the bottom of support body 43 is horizontal the thin end of the scroll 44, the thin end of the scroll 44
On be cased with shock-absorbing sleeve 45, undercarriage steering wheel 41 is electrically connected with the control board, and undercarriage steering wheel 41 passes through linkage
42 pairs of support bodys 41 carry out folding and unfolding, when unmanned plane 10 flight of body, and receipts are opened in two outsides to undercarriage 4 described in two to the left and right respectively
Rise.Undercarriage 4 can be stablely supported at level point when being easy to unmanned plane body 10 to land, and will not support damage to unmanned plane body
Each functional part that 10 lower sections are set, and undercarriage 4 is packed up during flight, missile is not hooked or is touched in the air and rise and fall
Frame 4, in order to avoid winding can not deliver article or even influence unmanned plane during flying, and pack up undercarriage 4 be also beneficial to reduction windage with
Keep the balance of unmanned plane during flying.
Propeller 3 is multiple for even number amount, and propeller 3 is 8 in the present embodiment, and propeller 3 includes horn 31 and blade
32, horn 31 is rotatably coupled with frame 1, with convenient retracted unmanned plane.When horn 31 deploys upwards, the lock on the top of horn 31
The lateral pin of locking mechanism under the action of the spring locks horn 31 and frame 1, it is necessary to when putting down horn 31, lateral pin is stirred with hand,
Lateral pin is set to be separated with horn, so that it may to put down horn 31.The free end of horn 31 is provided with motor 33, the output shaft and oar of motor 33
Leaf 32 is detachably connected.The middle part of blade 32 is provided with screwed hole, the output shaft of motor 33 is provided with screw thread by adapter
Axle 34 (as shown in Figure 2), both are connected through a screw thread, screw thread to screw direction identical with the direction of rotation of motor 33.Pass through spiral shell
Line connection can easily fast assembling-disassembling blade 32, screw thread to screw direction identical with the direction of rotation of motor 33, make blade 32 not
It can be released because of the rotation of motor 33.
The utility model sets dispenser 5, high-definition camera 6, major light 7 and loudspeaker 8 on unmanned plane body 10,
Loudspeaker 8 is connected with the audio signal of intercom 30 so that being simply possible to use in the unmanned plane taken photo by plane has more utility functions；It is logical
High-definition camera 6 is crossed by ground or to be scouted the image photographic of object and beams back remote control 20, remote control 20 is according to ground or detects
The situation for examining object carrys out the flight, landing and feature operation of remotely pilotless machine；Dispenser 5 is by remote control 20 come remote control dispenser
Steering wheel 51 and open lock pin 52 so that disaster relief supplies for hooking in lock pin 52 or fire extinguisher bomb and other items are realized and delivered；Major light 7
Ground can be illuminated, be easy to scout, reconnoitre or rescue, while also contributing to unmanned plane night flying；Loudspeaker 8 with it is right
Say that machine 30 is used cooperatively, the sound of ground intercom 30 is by the audio signal transmission of intercom on unmanned plane 30 to loudspeaker
8, realize that high-altitude voice is propagandaed directed to communicate.
Finally it should be noted that：Various embodiments above is only limited to illustrate the technical solution of the utility model, rather than to it
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, or to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type, it all should cover among claim of the present utility model and the scope of specification.
Claims (10)
1. pacify on a kind of multi-functional unmanned plane with dispenser, including unmanned plane body and remote control, the unmanned plane body
Equipped with propeller, wireless transceiver, GPS location stabilizer, control board and functional part, remote control passes through wireless transceiver
The landing of unmanned plane body, flight and each functional part are controlled with control board, it is characterised in that：The function
Part includes dispenser, high-definition camera, major light and the loudspeaker being electrically connected with the control board；It is described to deliver
Device be located at unmanned plane body under middle side part, the high-definition camera be located at unmanned plane body front side in the middle part of, the major light and
Loudspeaker is located at the both sides of high-definition camera respectively, and the loudspeaker is connected with intercom audio signal；The dispenser
Including dispenser steering wheel and movable lock pin, dispenser steering wheel can open lock pin in the presence of remote control and realize article and throw
Put.
2. the multi-functional unmanned plane according to claim 1 with dispenser, it is characterised in that：The high-definition camera is
Zoom camera, high-definition camera is arranged on unmanned plane body by head, and high-definition camera can realize left and right by head
With the rotation of above-below direction.
3. the multi-functional unmanned plane according to claim 1 with dispenser, it is characterised in that：The unmanned plane body bag
Installed in including rack and nose shell, frame the wireless transceiver, GPS location stabilizer, control board, functional part and
Propeller, the nose shell is covered in frame.
4. the multi-functional unmanned plane according to claim 3 with dispenser, it is characterised in that：The nose shell is disk
Structure, is provided with an arc-shaped protrusions in the middle part of discoidal chassis, and arc-shaped protrusions are connected with chassis cambered surface transition.
5. the multi-functional unmanned plane according to claim 1 with dispenser, it is characterised in that：On the unmanned plane body
Undercarriage is also symmetrically set with, undercarriage includes being sequentially connected undercarriage steering wheel, linkage and the support body connect, undercarriage
Steering wheel is electrically connected with the control board, and undercarriage steering wheel carries out folding and unfolding by linkage to support body.
6. the multi-functional unmanned plane according to claim 5 with dispenser, it is characterised in that：The support body is inverted T-shaped,
The bottom of support body is horizontal the thin end of the scroll, and shock-absorbing sleeve is cased with the thin end of the scroll；When unmanned plane body flight, undercarriage described in two point
Two outside openings are not packed up to the left and right.
7. the multi-functional unmanned plane according to claim 1 with dispenser, it is characterised in that：The propeller is even number
That measures is multiple, and propeller includes horn and blade, and horn is rotatably coupled with frame, and the free end of horn is provided with motor,
The output shaft of motor and blade are detachably connected.
8. the multi-functional unmanned plane according to claim 7 with dispenser, it is characterised in that：The propeller is 6
Or 8, the output shaft of the blade and motor is connected through a screw thread, screw thread to screw direction identical with the direction of rotation of motor.
9. the multi-functional unmanned plane according to claim 3 with dispenser, it is characterised in that:The frame is carbon fiber
Material, the nose shell is PLA materials.
10. the multi-functional unmanned plane according to claim 1 with dispenser, it is characterised in that:The major light passes through
Rotating shaft is rotationally connected with frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720337149.8U CN206590121U (en) | 2017-03-31 | 2017-03-31 | A kind of multi-functional unmanned plane with dispenser |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720337149.8U CN206590121U (en) | 2017-03-31 | 2017-03-31 | A kind of multi-functional unmanned plane with dispenser |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206590121U true CN206590121U (en) | 2017-10-27 |
Family
ID=60123157
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|---|---|---|---|
| CN201720337149.8U Expired - Fee Related CN206590121U (en) | 2017-03-31 | 2017-03-31 | A kind of multi-functional unmanned plane with dispenser |
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| CN (1) | CN206590121U (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108248848A (en) * | 2018-02-10 | 2018-07-06 | 黄山市金罡石无人机科技有限责任公司 | A kind of multi-functional multi-rotor unmanned aerial vehicle |
| CN108275275A (en) * | 2018-03-23 | 2018-07-13 | 京杭遥感技术（杭州）有限公司 | Unmanned plane throwing mechanism, unmanned plane and the delivering method based on unmanned plane |
| CN108371767A (en) * | 2018-01-30 | 2018-08-07 | 陈迈 | A kind of police multi-functional flight rescue system of fire-fighting |
| CN108553771A (en) * | 2018-04-16 | 2018-09-21 | 钱文娟 | A kind of fire-fighting and rescue method |
| CN108657453A (en) * | 2018-05-17 | 2018-10-16 | 邓江红 | A kind of unmanned aerial vehicle onboard lighting device |
| CN108909982A (en) * | 2018-05-08 | 2018-11-30 | 张博文 | A kind of unmanned plane lifebuoy jettison system |
| CN110360986A (en) * | 2019-07-03 | 2019-10-22 | 航天东方红卫星有限公司 | A kind of portable star catalogue part landform mapping system |
| CN112776984A (en) * | 2021-03-15 | 2021-05-11 | 国网新疆电力有限公司巴州供电公司 | Unmanned aerial vehicle fixed point throwing device |
| CN114637032A (en) * | 2022-05-19 | 2022-06-17 | 长安大学 | Landslide hazard monitoring equipment deployed by unmanned aerial vehicle and self-adaptive fixing method thereof |
| CN117002732A (en) * | 2023-10-07 | 2023-11-07 | 成都天域航通科技有限公司 | Unmanned aerial vehicle-based throwing device and control system |
-
2017
- 2017-03-31 CN CN201720337149.8U patent/CN206590121U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108371767A (en) * | 2018-01-30 | 2018-08-07 | 陈迈 | A kind of police multi-functional flight rescue system of fire-fighting |
| CN108248848A (en) * | 2018-02-10 | 2018-07-06 | 黄山市金罡石无人机科技有限责任公司 | A kind of multi-functional multi-rotor unmanned aerial vehicle |
| CN108275275A (en) * | 2018-03-23 | 2018-07-13 | 京杭遥感技术（杭州）有限公司 | Unmanned plane throwing mechanism, unmanned plane and the delivering method based on unmanned plane |
| CN108553771A (en) * | 2018-04-16 | 2018-09-21 | 钱文娟 | A kind of fire-fighting and rescue method |
| CN108553771B (en) * | 2018-04-16 | 2020-12-15 | 绍兴柯桥日臻化纤有限公司 | Fire rescue method |
| CN108909982A (en) * | 2018-05-08 | 2018-11-30 | 张博文 | A kind of unmanned plane lifebuoy jettison system |
| CN108657453A (en) * | 2018-05-17 | 2018-10-16 | 邓江红 | A kind of unmanned aerial vehicle onboard lighting device |
| CN110360986A (en) * | 2019-07-03 | 2019-10-22 | 航天东方红卫星有限公司 | A kind of portable star catalogue part landform mapping system |
| CN112776984A (en) * | 2021-03-15 | 2021-05-11 | 国网新疆电力有限公司巴州供电公司 | Unmanned aerial vehicle fixed point throwing device |
| CN114637032A (en) * | 2022-05-19 | 2022-06-17 | 长安大学 | Landslide hazard monitoring equipment deployed by unmanned aerial vehicle and self-adaptive fixing method thereof |
| CN117002732A (en) * | 2023-10-07 | 2023-11-07 | 成都天域航通科技有限公司 | Unmanned aerial vehicle-based throwing device and control system |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171027 |