CN205311898U - Anticollision unmanned aerial vehicle - Google Patents
Anticollision unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205311898U CN205311898U CN201620057174.6U CN201620057174U CN205311898U CN 205311898 U CN205311898 U CN 205311898U CN 201620057174 U CN201620057174 U CN 201620057174U CN 205311898 U CN205311898 U CN 205311898U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- anticollision ring
- fuselage
- ring
- horn
- Prior art date
- 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.)
- Expired - Fee Related
Links
- 229920000742 Cotton Polymers 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000005553 drilling Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000011176 pooling Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000011664 signaling Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Landscapes
- Support Of Aerials (AREA)
Abstract
The utility model provides an anticollision unmanned aerial vehicle, the reciprocating impact tunnel drilling machine comprises a machine body, fuselage swing joint all around has 4 horns, the horn end is equipped with the rotor, the rotor outside is equipped with branch anticollision ring, the fuselage lower part is equipped with two parallel arrangement's support frame, be equipped with camera device between the support frame, the fuselage upper surface is equipped with solar cell, four the rotor outside is equipped with main anticollision ring, and this anticollision unmanned aerial vehicle has following beneficial effect: this unmanned aerial vehicle sets up the crashproof ring sum owner of branch anticollision ring in the rotor outside, collides the wall body when effectively preventing unmanned aerial vehicle flight and damages the rotor, has buffer function's support frame in the underpart setting, make when falling to the ground more steady, the collapsible shrink of wing, portable.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, particularly relates to a kind of crashproof unmanned plane.
Background technology
UAV, is called for short unmanned plane (UAV), is a kind of new concept weapon being in developing rapidly equipment, its have maneuverability, reaction quickly, unmanned flight, operation require low advantage. Unmanned plane is by carrying multiclass sensor, it is possible to achieve image real-time Transmission, high-risk areas detecting function, is that satellite remote sensing supplements with the strong of tradition air remote sensing. At present, the use scope of unmanned plane has widened military affairs, scientific research, civilian three big fields, specifically electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism very wide.
Need to fly in difference comparatively rugged environment just because of it, the probability of its damage is very big, and especially rotor part is a bit damaged if having, will result in imbalance, and damage, and, unmanned plane launches due to horn, volume is bigger, not portable, particularly arrive field and take photo by plane, carry extremely inconvenience.
Utility model content
For solving above-mentioned technical problem, the utility model proposes a kind of crashproof unmanned plane, including fuselage, described fuselage surrounding is connected with 4 horns, and described horn end is provided with rotor, is provided with a point anticollision ring outside described rotor; Described underbelly is provided with two bracing frames be arrangeding in parallel, is provided with camera head between support frame as described above; Described fuselage upper surface is provided with solaode; It is provided with main anticollision ring outside four described rotors.
Preferably, described horn and described fuselage junction are provided with setting up and down two engaging lug, described engaging lug center is provided with through hole, described horn stretches between two described engaging lugs, through there being latch in described through hole, described latch is through described horn, and described horn rotates in two described engaging lugs.
Preferably, it is provided with limited block between two described engaging lugs.
Preferably, support frame as described above includes stand, described stand lower end is connected to bumper bracket, described stand is provided with projection, described bumper bracket end is provided with arc snap ring, described arc card is located on described projection, and described projection bottom is provided with fixed block, is provided with spring between described arc snap ring end and described fixed block.
Preferably, described main anticollision ring is tangent with described point of anticollision ring periphery, and described main anticollision ring is provided with internal thread hole, is provided with screw in described internal thread hole, and described screw is pressed on described point anticollision ring.
Preferably, described main anticollision ring is that foam is cotton.
The crashproof unmanned plane that the utility model proposes has following beneficial effect: 1, this unmanned plane arranges point anticollision ring and a main anticollision ring outside rotor, effectively prevent from colliding body of wall during unmanned plane during flying and damaging rotor, 2, the bracing frame with pooling feature is set at underpart, when making to land more steady, 3, wing collapsible, it is simple to carry.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, below the accompanying drawing used required during embodiment is described is briefly described.
Fig. 1 is top view of the present utility model;
Fig. 2 is side view of the present utility model;
Fig. 3 is the schematic diagram of receiving state of the present utility model;
Fig. 4 is horn of the present utility model and fuselage scheme of installation;
Fig. 5 is the side schematic view of bracing frame of the present utility model;
Wherein, 1-fuselage, 2-horn, 3-rotor, 4-divides anticollision ring, 5-camera head, 6-solaode, the main anticollision ring of 7-, 8-engaging lug, 9-limited block, 10-stand, 11-bumper bracket, 12-projection, 13-arc snap ring, 14-fixed block, 15-spring, 16-screw.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described.
As shown in Figure 1, Figure 2, the utility model proposes a kind of crashproof unmanned plane, including fuselage 1, described fuselage 1 surrounding is connected with 4 horns 2, and described horn 2 end is provided with rotor 3, it is provided with point anticollision ring 4 outside described rotor 3, being rotated by rotor 3, the power under producing, for preventing rotor 3 collision obstacle, setting up a circle anticollision ring outside rotor 3, a point anticollision ring 4 is connected with horn 2; Described fuselage 1 bottom is provided with two bracing frames be arrangeding in parallel, is provided with camera head 5 between support frame as described above, and camera head 5 can be revolving photographic head, it is provided that bigger angle of taking photo by plane; Described fuselage 1 upper surface is provided with solaode 6, and solaode 6 is connected with the control circuit within fuselage 1, as stand-by power supply, after unmanned plane drops, is provided that stand-by power supply is to send position signalling; It is provided with main anticollision ring 7 outside four described rotors 3, main anticollision ring 7 is fastened on outside four points of anticollision rings 4, namely for crashproof further, horn 2 can be reinforced again, wherein, described main anticollision ring 7 is tangent with described point of anticollision ring 4 periphery, described main anticollision ring 7 is provided with internal thread hole, screw 16 it is provided with in described internal thread hole, described screw 16 is pressed on described point anticollision ring 4, main anticollision ring 7 can be more stable be arranged on complete machine outer ring, described main anticollision ring 7 is that foam is cotton, has good anti-collision effect.
Wherein, such as Fig. 3, shown in Fig. 4, unmanned plane is carried for the ease of receiver, it is provided with setting up and down two engaging lug 8 with described fuselage 1 junction at described horn 2, described engaging lug 8 center is provided with through hole, described horn 2 stretches between two described engaging lugs 8, through there being latch in described through hole, the described latch described horn 2 of traverse, described horn 2 rotates in described engaging lug 8, simultaneously, it is provided with limited block 9 between two described engaging lugs 8, when horn 2 turns to engaging lug in the same horizontal line, it is butted on limited block 9, prevent horn 2 from offseting, when needs are received, horn 2 is rotated away from limited block 9 direction, it is made to press close near fuselage 1, whole equipment volume is made to reduce, it is easy to carry.
In order to ensure the stability that unmanned plane lands, as shown in Figure 5, bracing frame is have pooling feature, support frame as described above includes stand 10, described stand 10 lower end is connected to bumper bracket 11, described stand 10 is provided with projection 12, described bumper bracket 11 end is provided with arc snap ring 13, described arc snap ring 13 is placed on described projection 12, described projection 12 bottom is provided with fixed block 14, it is provided with spring 15 between described arc snap ring 13 end and described fixed block 14, its working method is, during unmanned plane landing, bracing frame first lands, bumper bracket 11 one end of bottom is under pressure, level is turned to along projection 12, spring 15 is compressed, play buffering effect, when taking off, bumper bracket 11 slowly leaves ground due to the effect of spring 15.
The multiple amendment of embodiment be will be apparent from for those skilled in the art, and generic principles defined herein when without departing from spirit or scope of the present utility model, can realize in other embodiments. Therefore, this utility model is not intended to be limited to the embodiments shown herein, and is to fit to the widest scope consistent with principles disclosed herein and features of novelty.
Claims (6)
1. a crashproof unmanned plane, it is characterised in that include fuselage, described fuselage surrounding is connected with 4 horns, and described horn end is provided with rotor, is provided with a point anticollision ring outside described rotor; Described underbelly is provided with two bracing frames be arrangeding in parallel, is provided with camera head between support frame as described above; Described fuselage upper surface is provided with solaode; It is provided with main anticollision ring outside four described rotors.
2. crashproof unmanned plane according to claim 1, it is characterized in that, described horn and described fuselage junction are provided with setting up and down two engaging lug, described engaging lug center is provided with through hole, described horn stretches between two described engaging lugs, through there being latch in described through hole, described latch is through described horn, and described horn rotates in two described engaging lugs.
3. crashproof unmanned plane according to claim 2, it is characterised in that be provided with limited block between two described engaging lugs.
4. crashproof unmanned plane according to claim 1, it is characterized in that, support frame as described above includes stand, described stand lower end is connected to bumper bracket, described stand is provided with projection, and described bumper bracket end is provided with arc snap ring, and described arc card is located on described projection, described projection bottom is provided with fixed block, is provided with spring between described arc snap ring end and described fixed block.
5. crashproof unmanned plane according to claim 1, it is characterised in that described main anticollision ring is tangent with described point of anticollision ring periphery, and described main anticollision ring is provided with internal thread hole, is provided with screw in described internal thread hole, described screw is pressed on described point anticollision ring.
6. crashproof unmanned plane according to claim 1 or 5, it is characterised in that described main anticollision ring is that foam is cotton.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620057174.6U CN205311898U (en) | 2016-01-21 | 2016-01-21 | Anticollision unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620057174.6U CN205311898U (en) | 2016-01-21 | 2016-01-21 | Anticollision unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205311898U true CN205311898U (en) | 2016-06-15 |
Family
ID=56205128
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620057174.6U Expired - Fee Related CN205311898U (en) | 2016-01-21 | 2016-01-21 | Anticollision unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205311898U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005384A (en) * | 2016-06-20 | 2016-10-12 | 深圳市勤新科技有限公司 | Unmanned aerial vehicle with high protection performance |
| CN106081079A (en) * | 2016-08-15 | 2016-11-09 | 张琬彬 | A kind of crashproof leg of unmanned plane rotor |
| CN107128482A (en) * | 2017-05-03 | 2017-09-05 | 李秀荣 | A kind of anticollision unmanned plane |
| TWI620689B (en) * | 2017-01-24 | 2018-04-11 | 林清富 | Solar cell module for unmanned aerial vehicle |
| CN108343899A (en) * | 2018-03-28 | 2018-07-31 | 德清县新城照明器材有限公司 | A kind of outdoor illumination with anti-theft feature |
| CN108622426A (en) * | 2018-04-26 | 2018-10-09 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN108945445A (en) * | 2018-09-13 | 2018-12-07 | 浙江省国土勘测规划有限公司 | A kind of four wing mapping unmanned planes based on oblique photograph |
| CN109050949A (en) * | 2018-06-29 | 2018-12-21 | 河南聚合科技有限公司 | A kind of 100 meters of floatability aerial unattended frontier defenses warning cloud platforms |
| CN115339629A (en) * | 2022-09-01 | 2022-11-15 | 扬州宇安电子科技有限公司 | Antenna scanning period measuring device capable of automatically adjusting posture according to change of surrounding environment |
-
2016
- 2016-01-21 CN CN201620057174.6U patent/CN205311898U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005384A (en) * | 2016-06-20 | 2016-10-12 | 深圳市勤新科技有限公司 | Unmanned aerial vehicle with high protection performance |
| CN106081079A (en) * | 2016-08-15 | 2016-11-09 | 张琬彬 | A kind of crashproof leg of unmanned plane rotor |
| TWI620689B (en) * | 2017-01-24 | 2018-04-11 | 林清富 | Solar cell module for unmanned aerial vehicle |
| CN107128482A (en) * | 2017-05-03 | 2017-09-05 | 李秀荣 | A kind of anticollision unmanned plane |
| CN108974339A (en) * | 2017-05-03 | 2018-12-11 | 李秀荣 | A kind of anticollision unmanned plane |
| CN108974339B (en) * | 2017-05-03 | 2020-11-24 | 汕头市瀛寰智能科技有限公司 | Anticollision unmanned aerial vehicle |
| CN108343899A (en) * | 2018-03-28 | 2018-07-31 | 德清县新城照明器材有限公司 | A kind of outdoor illumination with anti-theft feature |
| CN108622426A (en) * | 2018-04-26 | 2018-10-09 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN108622426B (en) * | 2018-04-26 | 2019-11-08 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN109050949A (en) * | 2018-06-29 | 2018-12-21 | 河南聚合科技有限公司 | A kind of 100 meters of floatability aerial unattended frontier defenses warning cloud platforms |
| CN108945445A (en) * | 2018-09-13 | 2018-12-07 | 浙江省国土勘测规划有限公司 | A kind of four wing mapping unmanned planes based on oblique photograph |
| CN115339629A (en) * | 2022-09-01 | 2022-11-15 | 扬州宇安电子科技有限公司 | Antenna scanning period measuring device capable of automatically adjusting posture according to change of surrounding environment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205311898U (en) | Anticollision unmanned aerial vehicle | |
| CN107544541B (en) | Unmanned aerial vehicle control method and system | |
| CN108583920A (en) | A kind of control method of unmanned plane marine landing platform and UAV Landing | |
| CN106809402B (en) | Automatic auxiliary landing system of rotor unmanned aerial vehicle and control method thereof | |
| CN203294310U (en) | Retractable undercarriage of unmanned aerial vehicle | |
| CN204895868U (en) | Novel foldable unmanned aerial vehicle | |
| CN203528816U (en) | Aerial photo unmanned plane | |
| CN206704529U (en) | A kind of camera oblique photograph unmanned plane of four rotor five | |
| CN107444608A (en) | A kind of new unmanned plane | |
| CN206615406U (en) | The automatic auxiliary landing system of rotor wing unmanned aerial vehicle | |
| CN105292477A (en) | Wrist type portable accompanying flight autonomous supervision unmanned aerial vehicle | |
| CN206782069U (en) | A kind of buffer of unmanned plane | |
| CN206544595U (en) | A kind of crash structure of fire-fighting unmanned plane | |
| CN106240807B (en) | A kind of integrated unmanned plane of collection photodetection | |
| CN203593169U (en) | Aerial photography unmanned plane | |
| CN204368424U (en) | A kind of can at the rotary wind type unmanned plane of drop in water surface | |
| CN207141366U (en) | One kind is taken photo by plane unmanned plane | |
| CN108082478B (en) | Early warning type unmanned aerial vehicle monitoring and investigation system | |
| CN104149971A (en) | Unmanned plane | |
| CN205589460U (en) | Be used for air -borne early warning unmanned aerial vehicle | |
| CN206437206U (en) | A kind of unmanned plane of contact charging | |
| CN202102301U (en) | Super long-range unmanned aerial vehicle control system based on civil mobile phone network | |
| CN109108935A (en) | A kind of empty comprehensive Detecting Robot in land and investigation control system | |
| CN204548507U (en) | A kind of Portable unmanned machine observation system | |
| CN206797696U (en) | A kind of new unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160615 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |