CN209634722U - A kind of agricultural prospecting anticollision unmanned plane - Google Patents
A kind of agricultural prospecting anticollision unmanned plane Download PDFInfo
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- CN209634722U CN209634722U CN201920062617.4U CN201920062617U CN209634722U CN 209634722 U CN209634722 U CN 209634722U CN 201920062617 U CN201920062617 U CN 201920062617U CN 209634722 U CN209634722 U CN 209634722U
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- fixedly connected
- unmanned plane
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- prospecting
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Abstract
The utility model discloses a kind of agricultural prospecting anticollision unmanned planes, including undercarriage, cabin is fixedly connected at center at the top of the undercarriage, rotor fagging is fixedly connected at the top of the cabin, the top movable of the rotor fagging is connected with rotary fan, and the bottom of the cabin is fixedly connected with prospecting camera.The utility model passes through undercarriage, cabin, rotor fagging, rotary fan, reconnoitre camera, support plate, fixed frame, Anti-bumping protection pad, first buffer spring, portable pillar, Crashworthy plate, movable plate, the setting of fixed link and the second buffer spring, during unmanned plane lands or flies effective protection can be carried out to unmanned plane, prevent to collide and damage, it solves simultaneously and reconnoitres unmanned plane now, since exploration range is big, ground control uncontrollable factor is too many, unmanned plane does not have collision prevention function simultaneously, once colliding, serious person even directly damages the problem of body.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of agricultural prospecting anticollision unmanned plane.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned vehicle of presetting apparatus manipulation, unmanned plane is actually the general designation of unmanned vehicle, from technical standpoint
Definition can be divided into: this is several for unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol
Major class, compared with manned aircraft, it has small in size, low cost, easy to use, low to operational environment requirement, battlefield existence energy
The advantages that power is stronger, since UAV has great significance to Future Air Combat, each main military country, the world all exists
The development work for stepping up to carry out UAV also gradually enters into its in life with the disclosure of unmanned air vehicle technique knowledge
His every aspect, for example take photo by plane with agriculture field etc., wherein agricultural prospecting unmanned plane is that a wide range of plantation is contracted necessary to family,
It can bring great convenience to user, while save a large amount of cost of labor, but reconnoitre unmanned plane now, due to exploration
Range is big, and ground control uncontrollable factor is too many, while unmanned plane does not have collision prevention function, once it collides, serious person
Body is even directly damaged, brings economic loss to user.
Utility model content
The purpose of this utility model is to provide a kind of agricultural prospecting anticollision unmanned planes, have the advantages of anticollision, solve
Unmanned plane is reconnoitred now, and since exploration range is big, ground control uncontrollable factor is too many, while unmanned plane does not have anticollision function
Can, once collide, serious person even directly damage body the problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of agricultural prospecting anticollision unmanned plane, including
Undercarriage is fixedly connected with cabin at the center at the top of the undercarriage, rotor fagging is fixedly connected at the top of the cabin,
The top movable of the rotor fagging is connected with rotary fan, and the bottom of the cabin is fixedly connected with prospecting camera, described
The inside of cabin is respectively arranged with battery and controller, and battery and controller are electrically connected, and the inside of the undercarriage is fixed
It is connected with support plate, the bottom of the support plate is fixedly connected with fixed frame, and the surface of the undercarriage is fixedly connected with anticollision
Neonychium, the two sides of the fixed frame inner cavity top are fixedly connected to the first buffer spring, the bottom of first buffer spring
Portion is fixedly connected with portable pillar, and the outside that the bottom of the portable pillar is through to fixed frame is fixedly connected with Crashworthy plate, the work
Dynamic column, which is located inside fixed frame, is fixedly connected with movable plate on the outside of one end, the two sides of the fixed frame intracavity bottom are fixed to be connected
It is connected to fixed link, movable plate and the inner wall sliding contact with movable plate, the fixed link top are run through in one end of the fixed link
The surface of one end is socketed with the second buffer spring, the fixed company in the top of second buffer spring and the top of fixed frame inner cavity
It connects.
Preferably, movable chamber is offered at the center of the fixed frame bottom, at the center of the movable chamber inner cavity top
It is fixedly connected with third buffer spring, the top of the movable chamber inner cavity and two sides for being located at third buffer spring are fixedly connected with
Flexible buffer board is fixedly connected at the top of the bottom of the elastic buffer plate and Crashworthy plate.
Preferably, the bottom of fixed frame inner cavity two sides is fixedly connected to link block, and the side of the link block is opened
Equipped with sliding slot, the inner wall of the movable plate one end and sliding slot far from portable pillar is slidably connected.
Preferably, the front of the cabin has been connected through hinge activity hatch door, and the positive right side of hatch door is fixed to be connected
It is connected to knob.
Preferably, the bottom of the undercarriage is fixedly connected with idler wheel, and the bottom of the Crashworthy plate is fixedly connected with friction
Pad.
Compared with prior art, the beneficial effects of the utility model are as follows:
1, the utility model passes through undercarriage, cabin, rotor fagging, rotary fan, prospecting camera, support plate, fixation
The setting of frame, Anti-bumping protection pad, the first buffer spring, portable pillar, Crashworthy plate, movable plate, fixed link and the second buffer spring, In
Effective protection can be carried out to unmanned plane during unmanned plane landing or flight, prevent to collide and damage, solve simultaneously
It has determined and has reconnoitred unmanned plane now, since exploration range is big, ground control uncontrollable factor is too many, while unmanned plane is without anti-
Hit function, once collide, serious person even directly damage body the problem of.
2, the utility model passes through the setting of movable chamber, third buffer spring and elastic buffer plate, can enhance Crashworthy plate pair
The Anti-bumping protection performance of unmanned plane, improves the robustness of unmanned plane, through the setting of link block and sliding slot, above and below movable plate
It can guarantee the stability moved inside sliding slot when mobile, to improve the crashworthiness of unmanned plane, pass through hatch door and idler wheel
Setting, the convenient battery to engine room inside carries out installation and replacement, and idler wheel facilitates unmanned plane landing to slide, and avoids straight with ground
Contact, enhances the service life of unmanned plane, by the setting of friction pad, in unmanned plane landing, friction pad first with ground
Contact, friction pad wearing coefficient is very high, avoids by anti-skidding processing, and friction pad can protect Crashworthy plate, improve nothing
Man-machine crashworthiness.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model fixed frame internal structure cross-sectional view；
Fig. 3 is the partial enlarged view in the utility model Fig. 2 at A.
In figure: 1 undercarriage, 2 cabins, 3 rotor faggings, 4 rotary fans, 5 prospecting cameras, 6 support plates, 7 fixed frames, 8
Anti-bumping protection pad, 9 first buffer springs, 10 portable pillars, 11 Crashworthy plates, 12 movable plates, 13 fixed links, 14 second buffer springs,
15 movable chambers, 16 third buffer springs, 17 elastic buffer plates, 18 link blocks, 19 sliding slots, 20 hatch doors, 21 idler wheels, 22 friction pads.
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 is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3, a kind of agricultural prospecting anticollision unmanned plane, including undercarriage 1, the bottom of undercarriage 1 is please referred to be fixedly connected
There is idler wheel 21, the bottom of Crashworthy plate 11 is fixedly connected with friction pad 22, by the setting of friction pad 22, in unmanned plane landing,
For friction pad 22 first with ground face contact, 22 wearing coefficient of friction pad is very high, avoids by anti-skidding processing, friction pad 22 can be to anti-
It hits plate 11 to be protected, improves the crashworthiness of unmanned plane, be fixedly connected with cabin 2, cabin at the center at 1 top of undercarriage
2 front has been connected through hinge activity hatch door 20, and the positive right side of hatch door 20 is fixedly connected with knob, passes through hatch door 20 and rolling
The setting of wheel 21, the convenient battery to inside cabin 2 carries out installation and replacement, and idler wheel 21 facilitates unmanned plane landing to slide, and keeps away
Exempt from directly to contact with ground, enhance the service life of unmanned plane, the top of cabin 2 is fixedly connected with rotor fagging 3, rotor fagging
3 top movable is connected with rotary fan 4, and the bottom of cabin 2 is fixedly connected with prospecting camera 5, and the inside of cabin 2 is set respectively
It is equipped with battery and controller, and battery and controller are electrically connected, the inside of undercarriage 1 is fixedly connected with support plate 6, support plate
6 bottom is fixedly connected with fixed frame 7, and movable chamber 15 is offered at the center of 7 bottom of fixed frame, 15 inner cavity top of movable chamber
It is fixedly connected with third buffer spring 16 at center, the top of 15 inner cavity of the movable chamber and two sides for being located at third buffer spring 16 are equal
It is fixedly connected with elastic buffer plate 17, the bottom of elastic buffer plate 17 is fixedly connected with the top of Crashworthy plate 11, passes through movable chamber
15, the setting of third buffer spring 16 and elastic buffer plate 17 can enhance Crashworthy plate 11 to the Anti-bumping protection performance of unmanned plane, mention
The high robustness of unmanned plane, the surface of undercarriage 1 are fixedly connected with Anti-bumping protection pad 8, and the two sides of 7 inner cavity top of fixed frame are equal
It is fixedly connected with the first buffer spring 9, the bottom of the first buffer spring 9 is fixedly connected with portable pillar 10,7 inner cavity two sides of fixed frame
Bottom be fixedly connected to link block 18, the side of link block 18 offers sliding slot 19, and movable plate 12 is far from portable pillar 10
One end and the inner wall of sliding slot 19 are slidably connected, can when movable plate 12 moves up and down by the setting of link block 18 and sliding slot 19
Guarantee the stability moved inside sliding slot 19, to improve the crashworthiness of unmanned plane, the bottom of portable pillar 10 is through to solid
The outside for determining frame 7 is fixedly connected with Crashworthy plate 11, and portable pillar 10, which is located on the outside of 7 inside one end of fixed frame, is fixedly connected with movement
Plate 12, the two sides of 7 intracavity bottom of fixed frame are fixedly connected to fixed link 13, one end of fixed link 13 through movable plate 12 and with
The surface of the inner wall sliding contact of movable plate 12,13 top one end of fixed link is socketed with the second buffer spring 14, the second buffering elastic
Be fixedly connected at the top of the top of spring 14 and 7 inner cavity of fixed frame, by undercarriage 1, cabin 2, rotor fagging 3, rotary fan 4,
Reconnoitre camera 5, support plate 6, fixed frame 7, Anti-bumping protection pad 8, the first buffer spring 9, portable pillar 10, Crashworthy plate 11, movement
The setting of plate 12, fixed link 13 and the second buffer spring 14 can carry out unmanned plane during unmanned plane lands or flies
Effective protection prevents to collide and damage, while solving and reconnoitring unmanned plane now, since exploration range is big, ground
The uncontrollable factor of control is too many, while unmanned plane does not have collision prevention function, once colliding, serious person is even directly damaged
The problem of body.
The standardized element used in this specification arrived can commercially, the components such as idler wheel and elastic buffer plate
Can be carried out according to the record of the description and the appended drawings it is customized, the specific connection type of each part be all made of in the prior art at
The conventional means such as ripe bolt, rivet, welding, in addition connection type of the circuit connection using routine in the prior art, herein not
Remake out specific narration.
In use, can be put into after user has debugged built-in controller and ground control unit according to correct way
Exploration uses, and prospecting camera 5 can survey agriculture situation in flight course, when unmanned plane needs to land, rubs first
Scrubbing pad 22 and ground touch, and secondly idler wheel 21 just can be with ground face contact, and the Crashworthy plate 11 at 22 top of friction pad passes through ground
Reaction force third buffer spring 16 and elastic buffer plate 17 can be squeezed, while it is also slow to first by portable pillar 10
It rushes spring 9 to be squeezed, while portable pillar 10 can drive movable plate 12 to slide up and down on 13 surface of fixed link when moving, simultaneously
Second buffer spring 14 can play cushioning buffer effect to movable plate 12, and the Anti-bumping protection pad 8 of 1 surface of undercarriage setting can be to rising
The surface for falling frame 1 carries out effective protection, improves the anti-collision effect of the unmanned plane, is suitble to promote the use of.
In summary: the agricultural reconnoitre anticollision unmanned plane, by undercarriage 1, cabin 2, fixed frame 7, Anti-bumping protection pad 8,
First buffer spring 9, portable pillar 10, Crashworthy plate 11, movable plate 12, fixed link 13, the second buffer spring 14, movable chamber 15,
The cooperation of three buffer springs 16 and elastic buffer plate 17, solves and reconnoitres unmanned plane now, since exploration range is big, ground control
Uncontrollable factor it is too many, while unmanned plane do not have collision prevention function, once collide, serious person even directly damage body
The problem of.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of agricultural prospecting anticollision unmanned plane, including undercarriage (1), it is characterised in that: the center at the top of the undercarriage (1)
Place is fixedly connected with cabin (2), is fixedly connected with rotor fagging (3) at the top of the cabin (2), the rotor fagging (3)
Top movable is connected with rotary fan (4), and the bottom of the cabin (2) is fixedly connected with prospecting camera (5), the cabin
(2) inside is respectively arranged with battery and controller, and battery and controller are electrically connected, and the inside of the undercarriage (1) is solid
Surely it is connected with support plate (6), the bottom of the support plate (6) is fixedly connected with fixed frame (7), the surface of the undercarriage (1)
It is fixedly connected with Anti-bumping protection pad (8), the two sides of fixed frame (7) inner cavity top are fixedly connected to the first buffer spring
(9), the bottom of first buffer spring (9) is fixedly connected with portable pillar (10), and the bottom of the portable pillar (10) is through to
The outside of fixed frame (7) is fixedly connected with Crashworthy plate (11), and the portable pillar (10) is located at the outside of the internal one end of fixed frame (7)
It is fixedly connected with movable plate (12), the two sides of fixed frame (7) intracavity bottom are fixedly connected to fixed link (13), described solid
Movable plate (12) and the inner wall sliding contact with movable plate (12), fixed link (13) top one are run through in one end of fixed pole (13)
The surface at end is socketed with the second buffer spring (14), the top of second buffer spring (14) and the top of fixed frame (7) inner cavity
Portion is fixedly connected.
2. a kind of agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that: fixed frame (7) bottom
Center at offer movable chamber (15), be fixedly connected with third buffer spring at the center of movable chamber (15) inner cavity top
(16), the top of movable chamber (15) inner cavity and be located at third buffer spring (16) two sides be fixedly connected to elastic buffer
Plate (17) is fixedly connected at the top of the bottom and Crashworthy plate (11) of the elastic buffer plate (17).
3. a kind of agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that: fixed frame (7) inner cavity
The bottom of two sides is fixedly connected to link block (18), and the side of the link block (18) offers sliding slot (19), the movement
The inner wall of plate (12) one end and sliding slot (19) far from portable pillar (10) is slidably connected.
4. a kind of agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that: the front of the cabin (2)
It has been connected through hinge activity hatch door (20), the positive right side of the hatch door (20) is fixedly connected with knob.
5. a kind of agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that: the bottom of the undercarriage (1)
Portion is fixedly connected with idler wheel (21), and the bottom of the Crashworthy plate (11) is fixedly connected with friction pad (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920062617.4U CN209634722U (en) | 2019-01-15 | 2019-01-15 | A kind of agricultural prospecting anticollision unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920062617.4U CN209634722U (en) | 2019-01-15 | 2019-01-15 | A kind of agricultural prospecting anticollision unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209634722U true CN209634722U (en) | 2019-11-15 |
Family
ID=68477784
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920062617.4U Expired - Fee Related CN209634722U (en) | 2019-01-15 | 2019-01-15 | A kind of agricultural prospecting anticollision unmanned plane |
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| CN (1) | CN209634722U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111017204A (en) * | 2020-01-13 | 2020-04-17 | 深圳市星图智控科技有限公司 | Rapid take-off and landing unmanned aerial vehicle and take-off and landing control method of unmanned aerial vehicle |
| CN112224409A (en) * | 2020-10-13 | 2021-01-15 | 西北工业大学 | Unmanned aerial vehicle that utility tunnel detected |
| CN112373678A (en) * | 2020-11-23 | 2021-02-19 | 中国人民解放军军事科学院国防科技创新研究院 | Many rotor unmanned aerial vehicle aid landing gear |
| CN113772083A (en) * | 2021-10-22 | 2021-12-10 | 湖南文理学院 | Unmanned aerial vehicle for personnel tracking |
| CN114056588A (en) * | 2021-11-01 | 2022-02-18 | 中国水利水电第九工程局有限公司 | Unmanned aerial vehicle for hydraulic engineering construction detection |
| WO2022040904A1 (en) * | 2020-08-25 | 2022-03-03 | 唐山哈船科技有限公司 | Unmanned aerial vehicle cruise device for port safety monitoring |
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- 2019-01-15 CN CN201920062617.4U patent/CN209634722U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017204A (en) * | 2020-01-13 | 2020-04-17 | 深圳市星图智控科技有限公司 | Rapid take-off and landing unmanned aerial vehicle and take-off and landing control method of unmanned aerial vehicle |
| WO2022040904A1 (en) * | 2020-08-25 | 2022-03-03 | 唐山哈船科技有限公司 | Unmanned aerial vehicle cruise device for port safety monitoring |
| CN112224409A (en) * | 2020-10-13 | 2021-01-15 | 西北工业大学 | Unmanned aerial vehicle that utility tunnel detected |
| CN112224409B (en) * | 2020-10-13 | 2022-09-20 | 西北工业大学 | Unmanned aerial vehicle that utility tunnel detected |
| CN112373678A (en) * | 2020-11-23 | 2021-02-19 | 中国人民解放军军事科学院国防科技创新研究院 | Many rotor unmanned aerial vehicle aid landing gear |
| CN113772083A (en) * | 2021-10-22 | 2021-12-10 | 湖南文理学院 | Unmanned aerial vehicle for personnel tracking |
| CN113772083B (en) * | 2021-10-22 | 2023-08-25 | 湖南文理学院 | Unmanned aerial vehicle for personnel tracking |
| CN114056588A (en) * | 2021-11-01 | 2022-02-18 | 中国水利水电第九工程局有限公司 | Unmanned aerial vehicle for hydraulic engineering construction detection |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191115 Termination date: 20220115 |
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| CF01 | Termination of patent right due to non-payment of annual fee |