CN206766329U - One kind is taken photo by plane unmanned plane - Google Patents
One kind is taken photo by plane unmanned plane Download PDFInfo
- Publication number
- CN206766329U CN206766329U CN201720662749.1U CN201720662749U CN206766329U CN 206766329 U CN206766329 U CN 206766329U CN 201720662749 U CN201720662749 U CN 201720662749U CN 206766329 U CN206766329 U CN 206766329U
- Authority
- CN
- China
- Prior art keywords
- horn
- plane
- support bar
- unmanned plane
- taken photo
- 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.)
- Active
Links
Abstract
Taken photo by plane unmanned plane the utility model discloses one kind, one kind is taken photo by plane unmanned plane, including body, the surrounding sidewall symmetry of the body opens up fluted, the groove is internally provided with support bar, one end of the support bar is provided with projection, the other end of the support bar is fixedly connected with horn, the inside of the horn is provided with motor, the upper end of the motor is connected with propeller by propeller axis of rotation, four expansion links are symmetrically installed between the horn and body centered on support bar, the outer end of the expansion link is provided with spring, the horn is fixedly connected with guardrail close to the side of outer end；Using the structure of expansion link and spring between the utility model horn and body, while using the mobility support between support bar and body, impulsive force can be reduced when wing collides; effectively protection body; the toughness of device is improved, overall structure is scientific and reasonable, and durability is strong.
Description
Technical field
It the utility model is related to unmanned air vehicle technique field, specially one kind is taken photo by plane unmanned plane.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application, it is unmanned plane
Really just need；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring
The application in infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, is greatly expanded
The purposes of unmanned plane in itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.
But unmanned plane of the prior art, machine propeller protrude outside, lack certain protection device, unmanned plane
Propeller is easily collided in flight course, causes the damage of unmanned plane, meanwhile, the flank of unmanned plane is adopted in the prior art
With the mode being fixedly connected, collision causes well damage due to a lack of mobile buffer gear, and the serious forgiveness of machine is relatively low, nobody
Machine lacks certain cushioning effect in landing, and the protectiveness equipment of unmanned plane has much room for improvement.
Utility model content
The purpose of this utility model is to provide one kind and taken photo by plane unmanned plane, to solve the machine proposed in above-mentioned background technology
Propeller protrudes outside, lacks certain protection device, unmanned plane propeller in flight course is easily collided, and causes nothing
Man-machine damage, meanwhile, the flank of unmanned plane by the way of being fixedly connected, due to a lack of mobile delay by collision in the prior art
The problem of punch mechanism causes well damage, and the serious forgiveness of machine is relatively low, and unmanned plane lacks certain cushioning effect in landing.
To achieve the above object, the utility model provides following technical scheme：One kind is taken photo by plane unmanned plane, including body, institute
The surrounding sidewall symmetry for stating body opens up fluted, and the groove is internally provided with support bar, and one end of the support bar is set
Be equipped with projection, and support bar by projection with being flexibly connected between groove, the other end of the support bar is fixedly connected with horn,
The inside of the horn is provided with motor, and the upper end of the motor is connected with spiral by propeller axis of rotation
Oar, is symmetrically installed with four expansion links centered on support bar between the horn and body, the outer end of the expansion link is all provided with
Spring is equipped with, the horn is fixedly connected with guardrail close to the side of outer end, and the lower end of horn is fixedly connected by expansion link
There is support feet, the expansion link outer end between the support feet and horn is provided with spring, and the upper end of the body is provided with light
Volt, and the lower end for being internally located at photovoltaic of body is provided with battery, the lower end for the being internally located at battery installation of the body
There is the first servomotor, the lower end of first servomotor is provided with camera bracket, and the lower end of the camera bracket leads to
Cross photographic head spin axis and be rotatably connected to camera, and the inside of camera bracket is provided with the second servomotor, described second watches
Motor is taken by being rotatablely connected between transmission mechanism and photographic head spin axis, the motor, the first servomotor, camera and
Second servomotor is electrically connected between battery.
Further, the upper surface of the body is in arc surfaced.
Further, connected between the camera bracket and the first servomotor by axis of rotation.
Further, the support feet is symmetrically arranged with four, and four support feets pass through elasticity between spring and horn
Connection.
Further, the guardrail is symmetrically arranged with four, and four guardrails are in semicircle shape.
Further, the lateral ends of the guardrail raise up in arcuation, and the peak of guardrail is higher than propeller.
Compared with prior art, the beneficial effects of the utility model are：Expansion link and spring are used between horn and body
Structure, while using the mobility support between support bar and body, impulsive force can be reduced when wing collide, effectively guarantor
Body is protected, improves the toughness of device, the guardrail on the outside of propeller effectively protects propeller, while has certain safety guarantee,
The lower end of horn is provided with support feet by expansion link and spring, reduces impact during body landing, effective protection device sheet
Body structure, the photovoltaic that body upper end is set can make full use of solar power generation, ensure the power supply capacity of device, overall structure section
It is reasonable to learn, and durability is strong.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model；
Fig. 2 is top view of the present utility model；
Fig. 3 is outside drawing of the present utility model.
In reference：1- propellers；2- propeller rotating shafts；3- springs；4- expansion links；5- bodies；6- photovoltaics；7- electric power storages
Pond；8- horns；9- motors；10- support bars；11- is raised；12- grooves；13- camera brackets；The servomotors of 14- first；
15- cameras；16- photographic head spin axis；17- transmission mechanisms；The servomotors of 18- second；19- support feets；20- guardrails.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme：One kind is taken photo by plane unmanned plane, including body 5, body 5
Surrounding sidewall symmetry open up fluted 12, groove 12 is internally provided with support bar 10, and one end of support bar 10 is provided with convex
11 are played, and support bar 10, by being flexibly connected between projection 11 and groove 12, the other end of support bar 10 is fixedly connected with horn
8, the inside of horn 8 is provided with motor 9, and the upper end of motor 9 is rotatably connected to propeller 1 by propeller rotating shaft 2,
Four expansion links 4 are symmetrically installed between horn 8 and body 5 centered on support bar 10, the outer end of expansion link 4 is provided with bullet
Spring 3, horn 8 is fixedly connected with guardrail 20 close to the side of outer end, and the lower end of horn 8 is fixedly connected with branch by expansion link 4
Spike 19, the outer end of expansion link 4 between support feet 19 and horn 8 are provided with spring 3, and the upper end of body 5 is provided with photovoltaic 6,
And the lower end for being internally located at photovoltaic 6 of body 5 is provided with battery 7, the lower end for being internally located at battery 7 of body 5 is provided with
First servomotor 14, the lower end of the first servomotor 14 are provided with camera bracket 13, and the lower end of camera bracket 13 passes through
Photographic head spin axis 16 is rotatably connected to camera 15, and the inside of camera bracket 13 is provided with the second servomotor 18, and second
Servomotor 18 by being rotatablely connected between transmission mechanism 17 and photographic head spin axis 16, motor 9, the first servomotor 14,
The servomotor 18 of camera 15 and second is electrically connected between battery 7.
Further, the upper surface of body 5 is in arc surfaced, increases the light-receiving area and intensity of photovoltaic 6.
Further, connected between the servomotor 14 of camera bracket 13 and first by axis of rotation, ensure camera
15 comprehensive shooting angle.
Further, support feet 19 is symmetrically arranged with four, and four support feets 19 pass through bullet between spring 3 and horn 8
Property connection, slow down impulsive force during landing, protection body is in itself.
Further, guardrail 20 is symmetrically arranged with four, and four guardrails 20 are in semicircle shape.
Further, the lateral ends of guardrail 20 raise up in arcuation, and the peak of guardrail 20 is higher than propeller 1,
Propeller 1 is protected, improves safety guarantee.
Operation principle：Altogether using the structure of 16 expansion links 4 and spring 3 between four horns 8 and body 5, and simultaneously
Using the mobility support between support bar 10 and body 5, impulsive force can be reduced when wing collides, effectively protect body 5,
The toughness of device is improved, the guardrail 20 in the outside of propeller 1 effectively protects propeller 1, while has certain safety guarantee, horn
8 lower end is provided with support feet 19 by expansion link 4 and spring 3, reduces impact when body 5 lands, effective protection device
This body structure, the photovoltaic 6 that the upper end of body 5 is set can make full use of solar power generation, ensure the power supply capacity of device, first watches
Take motor 14 and ensure rotation of the camera 15 in horizontal plane, the second servomotor 18 ensures that camera 15 turns in perpendicular
It is dynamic, it ensure that the comprehensive shooting angle of camera 15；While there has been shown and described that embodiment of the present utility model, for
For one of ordinary skill in the art, it is possible to understand that can be right in the case where not departing from principle of the present utility model and spirit
These embodiments carry out a variety of change, modification, replacement and modification, and the scope of the utility model is by appended claims and its is equal
Thing limits.
Claims (6)
- The unmanned plane 1. one kind is taken photo by plane, including body（5）, it is characterised in that：The body（5）Surrounding sidewall symmetry offer it is recessed Groove（12）, the groove（12）Be internally provided with support bar（10）, the support bar（10）One end be provided with projection（11）, And support bar（10）Pass through projection（11）With groove（12）Between be flexibly connected, the support bar（10）The other end be fixedly connected There is horn（8）, the horn（8）Inside motor is installed（9）, the motor（9）Upper end pass through propeller Rotating shaft（2）It is rotatably connected to propeller（1）, the horn（8）With body（5）Between with support bar（10）Centered on be symmetrically installed There are four expansion links（4）, the expansion link（4）Outer end be provided with spring（3）, the horn（8）Close to the side of outer end It is fixedly connected with guardrail（20）, and horn（8）Lower end pass through expansion link（4）It is fixedly connected with support feet（19）, the support Pin（19）With horn（8）Between expansion link（4）Outer end is provided with spring（3）, the body（5）Upper end photovoltaic is installed （6）, and body（5）Be internally located at photovoltaic（6）Lower end battery is installed（7）, the body（5）Be internally located at electric power storage Pond（7）Lower end the first servomotor is installed（14）, first servomotor（14）Lower end be provided with camera bracket （13）, the camera bracket（13）Lower end pass through photographic head spin axis（16）It is rotatably connected to camera（15）, and camera Support（13）Inside the second servomotor is installed（18）, second servomotor（18）Pass through transmission mechanism（17）With taking the photograph As head rotating shaft（16）Between be rotatablely connected, the motor（9）, the first servomotor（14）, camera（15）Watched with second Take motor（18）And battery（7）Between be electrically connected with.
- The unmanned plane 2. one kind according to claim 1 is taken photo by plane, it is characterised in that：The body（5）Upper surface be in cambered surface Shape.
- The unmanned plane 3. one kind according to claim 1 is taken photo by plane, it is characterised in that：The camera bracket（13）Watched with first Take motor（14）Between connected by axis of rotation.
- The unmanned plane 4. one kind according to claim 1 is taken photo by plane, it is characterised in that：The support feet（19）It is symmetrically arranged with four It is individual, and four support feets（19）Pass through spring（3）With horn（8）Between elastic connection.
- The unmanned plane 5. one kind according to claim 1 is taken photo by plane, it is characterised in that：The guardrail（20）It is symmetrically arranged with four It is individual, and four guardrails（20）It is in semicircle shape.
- The unmanned plane 6. one kind according to claim 1 is taken photo by plane, it is characterised in that：The guardrail（20）Lateral ends be in arc Shape raises up, and guardrail（20）Peak be higher than propeller（1）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720662749.1U CN206766329U (en) | 2017-06-08 | 2017-06-08 | One kind is taken photo by plane unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720662749.1U CN206766329U (en) | 2017-06-08 | 2017-06-08 | One kind is taken photo by plane unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206766329U true CN206766329U (en) | 2017-12-19 |
Family
ID=60637017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720662749.1U Active CN206766329U (en) | 2017-06-08 | 2017-06-08 | One kind is taken photo by plane unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206766329U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341059A (en) * | 2018-03-21 | 2018-07-31 | 安徽云翼航空技术有限公司 | A kind of battlefield is scouted and defence unmanned plane |
| CN108791917A (en) * | 2018-04-10 | 2018-11-13 | 清远市巨劲科技有限公司 | A kind of unmanned plane of taking photo by plane of multi-faceted shooting |
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| CN109367803A (en) * | 2018-09-29 | 2019-02-22 | 国网浙江省电力有限公司 | Suitable for boisterous multi-functional unmanned plane |
| CN110844057A (en) * | 2019-11-28 | 2020-02-28 | 湖南库里斯智能科技有限公司 | Multi-functional environmental protection unmanned aerial vehicle that patrols and examines |
| CN111137466A (en) * | 2020-01-13 | 2020-05-12 | 深圳市星图智控科技有限公司 | Unmanned aerial vehicle capable of being monitored and monitoring shooting method of unmanned aerial vehicle |
| CN116767500A (en) * | 2022-02-23 | 2023-09-19 | 张庆玲 | Multi-range multi-azimuth laser mapping system |
-
2017
- 2017-06-08 CN CN201720662749.1U patent/CN206766329U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341059A (en) * | 2018-03-21 | 2018-07-31 | 安徽云翼航空技术有限公司 | A kind of battlefield is scouted and defence unmanned plane |
| CN108791917A (en) * | 2018-04-10 | 2018-11-13 | 清远市巨劲科技有限公司 | A kind of unmanned plane of taking photo by plane of multi-faceted shooting |
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| CN109367803A (en) * | 2018-09-29 | 2019-02-22 | 国网浙江省电力有限公司 | Suitable for boisterous multi-functional unmanned plane |
| CN110844057A (en) * | 2019-11-28 | 2020-02-28 | 湖南库里斯智能科技有限公司 | Multi-functional environmental protection unmanned aerial vehicle that patrols and examines |
| CN111137466A (en) * | 2020-01-13 | 2020-05-12 | 深圳市星图智控科技有限公司 | Unmanned aerial vehicle capable of being monitored and monitoring shooting method of unmanned aerial vehicle |
| CN116767500A (en) * | 2022-02-23 | 2023-09-19 | 张庆玲 | Multi-range multi-azimuth laser mapping system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206766329U (en) | One kind is taken photo by plane unmanned plane | |
| CN202071985U (en) | Novel plane symmetrical layout type multi-rotor unmanned air vehicle | |
| CN106218873B (en) | A kind of anti-crash protection structure of unmanned plane | |
| CN204776028U (en) | Unmanned vehicles | |
| CN207257974U (en) | A kind of unmanned plane landing buffer frame | |
| CN105438458A (en) | Double-layer and eight-rotor-wing aircraft | |
| CN106275423A (en) | A kind of novel unmanned plane rotor aerodynamics structure | |
| CN206087353U (en) | For military use unmanned aerial vehicle with monitor function | |
| CN105059541A (en) | Novel multi-axis unmanned aerial vehicle | |
| CN107878736A (en) | One kind is used for plant protection unmanned plane frame damping device | |
| CN208412145U (en) | A kind of plant protection drone for herbal sprinkling | |
| CN209097009U (en) | A kind of damping device of unmanned plane during flying device | |
| CN106927042A (en) | A kind of unmanned plane of changeable form | |
| CN206194832U (en) | Retinue unmanned aerial vehicle battery compartment structure | |
| CN206664920U (en) | A kind of telescopic energy-saving unmanned plane of support | |
| CN205931255U (en) | Spherical unmanned aerial vehicle based on ARM | |
| CN216332732U (en) | Scalable comprehensive protection device of unmanned aerial vehicle | |
| CN210761306U (en) | Old city reforms transform and uses unmanned aerial vehicle shock-absorbing structure | |
| CN206939075U (en) | A kind of strong unmanned plane of endurance | |
| CN207773460U (en) | A kind of plant protection drone of anticollision | |
| CN207972789U (en) | A kind of unmanned plane wing of curved surface optimization | |
| CN205971875U (en) | Unmanned aerial vehicle landing protection architecture | |
| CN207670682U (en) | A kind of unmanned plane support construction of stability when can improve ejection | |
| CN207860443U (en) | A kind of unmanned plane protective device with shock-absorbing protecting function | |
| CN206704544U (en) | One kind is used for fire rescue unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190227 Address after: 065000 No. 8, No. 3 Road, Langfang Economic and Technological Development Zone, Hebei Province Patentee after: Langfang Intelligent Environmental Ecology Industry Research Institute Co., Ltd. Address before: 518000 C street, South Oil garden, Ping long road, Pinghu street, Longgang District, Shenzhen, Guangdong, 701 Patentee before: Shenzhen casdream Technology Co., Ltd. |