CN207725613U - A kind of unmanned plane with camera function - Google Patents
A kind of unmanned plane with camera function Download PDFInfo
- Publication number
- CN207725613U CN207725613U CN201820068529.0U CN201820068529U CN207725613U CN 207725613 U CN207725613 U CN 207725613U CN 201820068529 U CN201820068529 U CN 201820068529U CN 207725613 U CN207725613 U CN 207725613U
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- China
- Prior art keywords
- unmanned plane
- fuselage
- camera
- claw
- camera function
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Abstract
A kind of unmanned plane with camera function, including fuselage, at least four rotary wings and camera assembly that are fixedly connected with fuselage, the lower end of fuselage are provided with mounting platform, and camera assembly is rotatably provided in by the mechanism that rotates in a circumferential direction on mounting platform.The technical solution that can solve the rotation of existing unmanned plane camera is not perfect, and the flexibility used and practicability is limited and abdomen is equipped with camera unmanned plane are in landing, the technical issues of wiping can be brought the influences such as to touch to body and camera.
Description
Technical field
The utility model belongs to air vehicle technique field, especially a kind of unmanned plane with camera function.
Background technology
UAV, abbreviation unmanned plane (UAV) are a kind of new concept aircrafts being in rapidly developing, because of it
With maneuverability, reaction speed it is fast, without pilot steering, operation require it is low, a variety of mini-plants or object can be carried etc.
The features such as, and widely used.
Currently, the application range of unmanned plane has spread over the numerous areas such as civilian, scientific research even military affairs, national defence, especially
Be electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, anti-smuggling of enforcing the drug law, border patrol, public security anti-terrorism etc.
Aspect application is very wide, and image real-time Transmission, the function of high-risk areas real-time on-site detection, are to satellite remote sensing and traditional aviation
The strong supplement of remote sensing.
By unmanned plane progress filming image, real-time Transmission or when high-risk areas carries out real-time on-site detection, usually
Using on unmanned machine head visible light camera or other detection instruments complete.In the prior art, general peace
The holder of dress photography and vedio recording or other instruments is fixedly arranged at the bottom of unmanned plane, photography, camera shooting and others on holder
Detecting devices is fixed, and can only be shot and be detected according to the track and pitch angle of unmanned plane during flying, can not carried out
Comprehensive observation can only rely on the flight attitude for changing unmanned plane if being adjusted.
Invention content
The technical problem to be solved by the utility model is to provide a kind of unmanned planes with camera function, can solve existing
The technical solution of unmanned plane camera rotation is not perfect, and the flexibility used and practicability are limited and abdomen is equipped with camera shooting
The unmanned plane of head is in landing, the technical issues of wiping can be brought the influences such as to touch to body and camera.
In order to solve the above technical problems, technical solution used by the utility model is：
A kind of unmanned plane with camera function, including fuselage, at least four rotary wings that are fixedly connected with fuselage and
The lower end of camera assembly, fuselage is provided with mounting platform, and camera assembly is rotatably provided in installation by the mechanism that rotates in a circumferential direction and puts down
On platform；Mounting platform includes cross bar, left socle and right support, and cross bar is arranged by connecting shaft in fuselage lower end, and left socle is vertical
It is arranged in cross bar left end, right support is vertically arranged in the right end of cross bar, is formed between left socle, right support and cross bar for accommodating
The installation space of camera assembly, wherein each rotary wings are arranged by connecting rod on fuselage.
The above-mentioned mechanism that rotates in a circumferential direction includes first motor, the first claw, the second claw being engaged with the first claw and shaft,
First motor is fixed in left socle, and the first claw is fixed on first motor output shaft, and the second claw is set in
The left end of camera assembly, shaft are rotatably provided on right support, and the left end of shaft is fixed on the right end of camera assembly.
Above-mentioned shaft is arranged by bearing on right support.
The second motor is provided on above-mentioned fuselage, connecting shaft is fixed on the output shaft of the second motor.
The lower end of each connecting rod is provided with floor stand.
It is equipped with apparatus for descending in the bottom end of floor stand, apparatus for descending includes cylinder shell, cylinder shell sealed bottom, top
Tube plug be equipped with opening, connecting rod one end is fixedly connected with floor stand bottom end, the other end stretches into the opening of tube plug and with first
Sliding plug connects, and cavity is equipped between the first sliding plug and the second sliding plug, shock resistance mechanism is equipped in cavity, in the second sliding plug and cylinder
Elastic mechanism is equipped between enclosure base end wall.
Above-mentioned shock resistance mechanism is buffering cotton layer.
Above-mentioned elastic mechanism is adjustable spring.
The utility model has the following technical effect that：
1. the utility model provides complete set, the technical solution of feasible unmanned plane camera rotation；
2. camera assembly can adjust camera angle by the mechanism that rotates in a circumferential direction, the adjusting of pitch angle is carried out well；
3. when specific adjusting, the rotation of first the first claw of electric drive, since the first claw and the second claw connect, this
Sample can drive the second claw to rotate when the first claw rotates, to realize the rotation of camera assembly, the first claw well
Setting with the second claw keeps the two fixed, is not readily separated, structure is firm；
4. connecting shaft is fixed on the second motor, under the action of the second motor, entire camera assembly can carry out 360
Rotation, image pickup scope is wider.
Description of the drawings
The utility model is described in further detail with reference to the accompanying drawings and examples：
Fig. 1 is the overall structure diagram of the utility model；
Fig. 2 is the structural exploded view of mechanism of rotating in a circumferential direction in the utility model；
Fig. 3 is the schematic diagram for installing apparatus for descending in the utility model additional；
Fig. 4 is the utility model design sketch that camera assembly rotates when in use；
Fig. 5 is the structural schematic diagram of apparatus for descending in the utility model.
Specific implementation mode
As shown in Figure 1, a kind of unmanned plane with camera function, including fuselage 1, be fixedly connected with fuselage 1 at least four
The lower end of a rotary wings 2 and camera assembly, fuselage 1 is provided with mounting platform, and camera assembly can be turned by the mechanism that rotates in a circumferential direction
It is dynamic to be arranged on mounting platform；Mounting platform includes cross bar 4, left socle 5 and right support 6, and cross bar 4 is arranged by connecting shaft 7
Fuselage lower end, left socle 5 are vertically arranged in 4 left end of cross bar, and right support 6 is vertically arranged in the right end of cross bar 4, left socle 5, right branch
The installation space for accommodating camera assembly is formed between frame 6 and cross bar 4, wherein each rotary wings 2 are arranged by connecting rod 9
On the fuselage 1.
As shown in Fig. 2, the above-mentioned mechanism that rotates in a circumferential direction includes first motor 10, the first claw 11, is engaged with the first claw 11
The second claw 12 and shaft 14, first motor 10 be fixed in left socle 5, the first claw 11 be fixed at first electricity
On machine output shaft, the second claw is set in the left end of camera assembly 13, and shaft 14 is rotatably provided on right support 6, and shaft
14 left end is fixed on the right end of camera assembly.
Above-mentioned shaft 14 is arranged by bearing 15 on right support 6.
The second motor is provided on above-mentioned fuselage 1, connecting shaft 7 is fixed on the output shaft of the second motor.
As shown in figure 3, the lower end of each connecting rod 9 is provided with floor stand 8.
As shown in figure 4, using the above structure, when in use, first the first claw of electric drive rotation, due to the first claw
It is connected with the second claw, the second claw can be driven to rotate when the first claw rotates in this way, to realize camera shooting group well
The rotation of part, under the action of first motor and the second motor, entire camera assembly can carry out 360 rotation, image model
It encloses more extensively, can realize no dead angle camera shooting well in this way.
As shown in figure 5, being equipped with apparatus for descending in the bottom end of floor stand 8, apparatus for descending includes cylinder shell 16, cylinder shell
16 sealed bottoms, top tube plug 17 be equipped with opening, 18 one end of connecting rod is fixedly connected with 8 bottom end of floor stand, the other end stretches into
It is connect in the opening of tube plug 17 and with the first sliding plug 19, cavity 21, cavity 21 is equipped between the first sliding plug 19 and the second sliding plug 20
In be equipped with shock resistance mechanism, between 16 inner bottom end wall of the second sliding plug 20 and cylinder shell be equipped with elastic mechanism 3；
Using the structure, when unmanned plane lands, apparatus for descending by unmanned plane gravity and when falling, made by inertia force
With the first sliding plug 19 can oppress the shock resistance mechanism in cavity 21, under the cushioning effect of shock resistance mechanism, can prevent well
Element is damaged because of strenuous vibration in unmanned plane, meanwhile, the second sliding plug 14 is also oppressed so that and elastic mechanism 16 is compressed,
Under the cushioning effect of elastic mechanism 16, unmanned plane body can so smoothly fallen on the ground of hollow very much.
Optionally, shock resistance mechanism is buffering cotton layer.
Optionally, elastic mechanism 3 is adjustable spring.
Claims (8)
1. a kind of unmanned plane with camera function, including fuselage（1）With fuselage（1）At least four rotary wings being fixedly connected
（2）And camera assembly, it is characterised in that：The fuselage（1）Lower end be provided with mounting platform, camera assembly passes through circumferential rotation
Rotation mechanism is rotatably provided on mounting platform, and mounting platform includes cross bar（4）, left socle（5）And right support（6）, cross bar（4）
Pass through connecting shaft（7）It is arranged in fuselage lower end, left socle（5）It is vertically arranged in cross bar（4）Left end, right support（6）It is vertically arranged
In cross bar（4）Right end, left socle（5）, right support（6）And cross bar（4）Between the installation that is formed for accommodating camera assembly it is empty
Between, wherein each rotary wings（2）Pass through connecting rod（9）It is arranged in fuselage（1）On.
2. the unmanned plane according to claim 1 with camera function, it is characterised in that：The mechanism that rotates in a circumferential direction includes
First motor（10）, the first claw（11）And the first claw（11）Second claw of occlusion（12）And shaft（14）, first motor
（10）It is fixed at left socle（5）It is interior, the first claw（11）It is fixed on first motor output shaft, the second claw is arranged
In camera assembly（13）Left end, shaft（14）It is rotatably provided in right support（6）On, and shaft（14）Left end be fixed on and take the photograph
As the right end of component.
3. the unmanned plane according to claim 2 with camera function, it is characterised in that：The shaft（14）Pass through bearing
（15）It is arranged in right support（6）On.
4. the unmanned plane with camera function according to one of claims 1 to 3, it is characterised in that：The fuselage
（1）On be provided with the second motor, connecting shaft（7）It is fixed on the output shaft of the second motor.
5. the unmanned plane with camera function according to one of claims 1 to 3, it is characterised in that：Each connection
Bar（9）Lower end be provided with floor stand（8）.
6. the unmanned plane according to claim 5 with camera function, it is characterised in that：Floor stand（8）Bottom end be equipped with
Apparatus for descending, apparatus for descending include cylinder shell（16）, cylinder shell（16）Bottom is sealed set, cylinder shell（16）Top
Tube plug with opening is set（17）, connecting rod（18）One end and floor stand（8）Bottom end is fixedly connected, the other end stretches into tube plug（17）
Opening in and with the first sliding plug（19）Connection, the first sliding plug（19）With the second sliding plug（20）Between be equipped with cavity（21）, cavity
（21）In be equipped with shock resistance mechanism, in the second sliding plug（20）With cylinder shell（16）Elastic machine is equipped between the end wall of inner bottom
Structure（3）.
7. the unmanned plane according to claim 6 with camera function, it is characterised in that：The shock resistance mechanism is buffering
Cotton layer.
8. the unmanned plane with camera function described according to claim 6 or 7, it is characterised in that：The elastic mechanism（3）For
Adjustable spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820068529.0U CN207725613U (en) | 2018-01-16 | 2018-01-16 | A kind of unmanned plane with camera function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820068529.0U CN207725613U (en) | 2018-01-16 | 2018-01-16 | A kind of unmanned plane with camera function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207725613U true CN207725613U (en) | 2018-08-14 |
Family
ID=63082539
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820068529.0U Expired - Fee Related CN207725613U (en) | 2018-01-16 | 2018-01-16 | A kind of unmanned plane with camera function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207725613U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110243346A (en) * | 2019-06-19 | 2019-09-17 | 太原理工大学 | A kind of large-scale curved molded product plotting board and mapping method |
| WO2022040858A1 (en) * | 2020-08-24 | 2022-03-03 | 唐山哈船科技有限公司 | Anti-collision unmanned aerial vehicle for aerial photography and method therefor |
| CN117146141A (en) * | 2023-10-24 | 2023-12-01 | 杭州海康威视数字技术股份有限公司 | Tripod head camera |
-
2018
- 2018-01-16 CN CN201820068529.0U patent/CN207725613U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110243346A (en) * | 2019-06-19 | 2019-09-17 | 太原理工大学 | A kind of large-scale curved molded product plotting board and mapping method |
| CN110243346B (en) * | 2019-06-19 | 2021-05-25 | 太原理工大学 | Large curved surface modeling product surveying and mapping device and method |
| WO2022040858A1 (en) * | 2020-08-24 | 2022-03-03 | 唐山哈船科技有限公司 | Anti-collision unmanned aerial vehicle for aerial photography and method therefor |
| CN117146141A (en) * | 2023-10-24 | 2023-12-01 | 杭州海康威视数字技术股份有限公司 | Tripod head camera |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180814 Termination date: 20190116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |