CN207450283U - Picture shooting assembly and the unmanned vehicle with this picture shooting assembly - Google Patents
Picture shooting assembly and the unmanned vehicle with this picture shooting assembly Download PDFInfo
- Publication number
- CN207450283U CN207450283U CN201721246738.1U CN201721246738U CN207450283U CN 207450283 U CN207450283 U CN 207450283U CN 201721246738 U CN201721246738 U CN 201721246738U CN 207450283 U CN207450283 U CN 207450283U
- Authority
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- China
- Prior art keywords
- connector
- damping device
- fuselage
- mounting portion
- shooting assembly
- 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.)
- Withdrawn - After Issue
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Abstract
The utility model is related to aircraft fields, provide a kind of picture shooting assembly and the unmanned vehicle with this picture shooting assembly, and picture shooting assembly includes first and second connector, damping device, first and second holder and first and second photographic device.One damping device is connected between one end of the first connector and one end of the second connector, another damping device is connected between the other end of the first connector and the other end of the second connector.Damping device between one end of first connector and one end of the second connector installs the first holder, another damping device between the other end of the first connector and the other end of the second connector installs the second holder.First and second photographic device is respectively arranged in first and second holder.For unmanned vehicle in flight course, damping device is consistent to the damping effect of first and second photographic device, improves the uniformity of damping so that first and second photographic device can steadily be shot, so as to obtain high quality graphic.
Description
【Technical field】
The utility model is related to aircraft field more particularly to a kind of picture shooting assembly for unmanned vehicle and with this
The unmanned vehicle of picture shooting assembly.
【Background technology】
Unmanned vehicle in Investigating and rescue, aerial monitoring, polling transmission line, take photo by plane, aerial survey and military lead
Domain has a wide range of applications.
In current unmanned vehicle, the common picture shooting assembly needs for realizing pan-shot connect firmly two groups of holders up and down
And camera, and two groups of holders and camera and its connector are carried out at the same time with vibration damping processing.However, current picture shooting assembly damping effect
Fruit is bad, it is impossible to fully meet use demand.
【Utility model content】
In order to solve the above-mentioned technical problem, the utility model embodiment provides a kind of damping effect good picture shooting assembly and tool
There is the unmanned vehicle of this picture shooting assembly.
In order to solve the above-mentioned technical problem, the utility model embodiment provides following technical scheme：
A kind of picture shooting assembly, applied to unmanned vehicle, the unmanned vehicle includes fuselage.The picture shooting assembly bag
It includes：First and second connector, damping device, first and second holder and first and second photographic device.One damping device connection
Between one end of first connector and one end of second connector, another described damping device is connected to described
Between the other end of the other end of first connector and second connector, first and second connector and damping dress
It puts to enclose and sets to form one for accommodating the passage of the fuselage.Positioned at one end of first connector and second connector
The damping device between one end installs first holder, connects positioned at the other end of first connector and described second
Another described damping device between the other end of fitting installs second holder.First photographic device is installed on institute
The first holder is stated, second photographic device is installed on second holder.
In some embodiments, each damping device includes first surface, the first surface towards the fuselage,
One end of first connector is fixedly installed in the first surface of a damping device, first connector it is another
End is fixedly installed in the first surface of another damping device.
First connector includes the first mounting portion, first connecting portion and the second mounting portion, and the first connecting portion connects
It is connected between first mounting portion and the second mounting portion；First mounting portion is fixedly installed in damping device
First surface, second mounting portion are fixedly installed in the first surface of another damping device.
In some embodiments, first mounting portion and the second mounting portion are all perpendicular to the first connecting portion.
In some embodiments, each damping device includes the first installing plate, damper element and the second installing plate, institute
It states damper element to be sandwiched between first installing plate and the second installing plate, first installing plate is compared with the described second installation
Plate includes the first surface closer to the fuselage, first installing plate.
In some embodiments, the damper element is shock-absorbing ball.
In some embodiments, second installing plate includes second surface, and the second surface is towards the fuselage, institute
The one end for stating the second connector is fixedly installed in the second surface of a damping device, the other end of second connector
It is fixedly installed in the second surface of another damping device.
In some embodiments, second connector includes the 3rd mounting portion, second connecting portion and the 4th mounting portion, institute
Second connecting portion is stated to be connected between the 3rd mounting portion and the 4th mounting portion；3rd mounting portion is fixedly installed in one
The second surface of the damping device, the 4th mounting portion are fixedly installed in the second surface of another damping device.
In some embodiments, the 3rd mounting portion and the 4th mounting portion are all perpendicular to the second connecting portion.
In some embodiments, first holder is fixedly installed in the second installing plate of a damping device, institute
State the second installing plate that the second holder is fixedly installed in another damping device.
In some embodiments, first holder and/or the second holder are three-axis stability augmentation holder.
In some embodiments, first photographic device and/or the second photographic device include at least one camera lens.
The utility model embodiment also provides following technical scheme：
A kind of unmanned vehicle, including fuselage and above-described picture shooting assembly, the fuselage is accommodated in the passage,
One end of first connector is fixedly installed in the fuselage.
In some embodiments, the other end of first connector is arranged at intervals with the fuselage.
In some embodiments, the fuselage includes the first end and second end being oppositely arranged, first connector
One end is fixedly installed in the first end；In the unmanned vehicle flight, the first end is located at the downside of the fuselage,
The second end is located at the upside of the fuselage.
In some embodiments, the fuselage includes the first end and second end being oppositely arranged, first connector
One end is fixedly installed in the first end；In the unmanned vehicle flight, the first end is located at the left side of the fuselage,
The second end is located at the right side of the fuselage.
Compared with prior art, in the picture shooting assembly of the utility model embodiment, a damping device connection
Between one end of first connector and one end of second connector, another described damping device is connected to described
Between the other end of the other end of first connector and second connector so that unmanned vehicle is in flight course, institute
It is consistent to the damping effect of first photographic device, the second photographic device to state damping device, improves the uniformity of damping so that
First photographic device, the second photographic device can steadily be shot, so as to obtain high quality graphic.
【Description of the drawings】
One or more embodiments are illustrated by corresponding attached drawing, these exemplary illustrations not structure
The restriction of paired embodiment, the element for having same reference numbers label in attached drawing is expressed as similar element, unless there are special
It declares, composition does not limit the figure in attached drawing.
Fig. 1 is a kind of stereogram for unmanned vehicle that the utility model wherein embodiment provides；
Fig. 2 is the front view of unmanned vehicle shown in FIG. 1；
Fig. 3 is the front view of the picture shooting assembly of unmanned vehicle shown in FIG. 1；
Fig. 4 is the stereogram of picture shooting assembly shown in Fig. 3；
Fig. 5 is the stereogram of another angle of picture shooting assembly shown in Fig. 3.
【Specific embodiment】
For the ease of understanding the utility model, with reference to the accompanying drawings and detailed description, the utility model is carried out more
Detailed description.It should be noted that when element is expressed " being fixed on " another element, it can be directly in another element
Above or therebetween there may be one or more elements placed in the middle.When an element is expressed " connection " another element, it can
To be directly to another element or there may be one or more elements placed in the middle therebetween.This specification is used
Term " vertical ", " horizontal ", "left", "right", " interior ", " outer " and similar statement for illustrative purposes only.
Unless otherwise defined, the skill of technical and scientific term all used in this specification with belonging to the utility model
The normally understood meaning of technical staff in art field is identical.It is intended merely in the term used in the description of the utility model
The purpose of specific embodiment is described, is not intended to limitation the utility model.Term "and/or" bag used in this specification
Include the arbitrary and all combination of one or more relevant Listed Items.
In addition, as long as technical characteristic involved in the utility model difference embodiment disclosed below is each other not
Forming conflict can be combined with each other.
It please refers to Fig.1 and Fig. 2, the unmanned vehicle 100 that the utility model wherein embodiment provides includes 10 He of fuselage
Picture shooting assembly 20, the picture shooting assembly 20 are installed on fuselage 10.
Include the control circuit component being made of electronic components such as MCU, the control circuit component bag in the fuselage 10
Include multiple control modules, e.g., for control unmanned vehicle flight attitude flight control modules, for the unmanned vehicle that navigates
Big dipper module and for handling data processing module of the environmental information acquired in related airborne equipment etc..
The fuselage 10 includes the first end 102 being oppositely arranged and second end 104.It flies in the unmanned vehicle 100
When, the first end 102 and second end 104 are respectively positioned at the downside and upside of the fuselage 10.
Fig. 3 to Fig. 5 is referred to, the picture shooting assembly 20 includes the first connector 202, the second connector 204, damping dress
Put 206, the first holder 208, the second holder 210, the first photographic device 212 and the second photographic device 214.First connector
202 one end is fixedly installed in the fuselage 10, and a damping device 206 is fixedly installed in first connector 202
One end and the second connector 204 one end between, another described damping device 206 is fixedly installed in first connector
Between the other end of 202 other end and the second connector 204.First connector 202, the second connector 204 and damping
Device 206 encloses jointly to be set to form a passage 30, and the fuselage 10 is accommodated in the passage 30.First holder 208 and
Two holders 210 are respectively arranged in two damping devices 206, and first photographic device 212 is installed on first holder
208, second photographic device 214 is installed on second holder 210.
First connector 202 is strip, can be made by metal material or plastic material, such as magnesium alloy, to carry
For enough rigidity.First connector 202 includes the first mounting portion 2020,2022 and second mounting portion of first connecting portion
2024, the first connecting portion 2022 is connected between 2020 and second mounting portion 2024 of the first mounting portion.Described first
2020 and second mounting portion 2024 of mounting portion is mutually parallel, and all perpendicular to the first connecting portion 2022.First peace
Dress portion 2020 is fixedly installed in the first end 102 of the fuselage 10, and second mounting portion 2024 is spaced with the fuselage 10
It sets.
It is understood that in some other embodiments, first mounting portion 2020 can be fixedly installed in the machine
The first end 102 of body 10, and second mounting portion 2024 can be fixedly installed in the second end 104 of the fuselage 10.
Similarly, second connector 204 is strip, can be made by metal material or plastic material, such as magnalium closes
Gold, to provide enough rigidity.Second connector 204 includes the 3rd mounting portion 2040, second connecting portion 2042 and the 4th
Mounting portion 2044, the second connecting portion 2042 are connected between the 3rd mounting portion 2040 and the 4th mounting portion 2044.Institute
It states the 3rd mounting portion 2040 and the 4th mounting portion 2044 is mutually parallel, and all perpendicular to the second connecting portion 2042, and
First mounting portion 2020, the second mounting portion 2024, the 3rd mounting portion 2040 and the 4th mounting portion 2044 are all mutually parallel.
It is understood that in some other embodiments, the first connector 202 and 204 length of the second connector are adjustable
It is whole, for example, using stretching structure, to be adapted to various sizes of aircraft.
The number of the damping device 206 is two, one of them described damping device 206 is fixedly installed in described first
Between 2020 and the 3rd mounting portion 2040 of mounting portion, another described damping device 206 is installed on second mounting portion 2024
Between the 4th mounting portion 2044.
Each damping device 206 includes the first installing plate 2060,2062 and second installing plate 2064 of damper element, institute
It states damper element 2062 to be sandwiched between 2060 and second installing plate 2064 of the first installing plate, 2060 phase of the first installing plate
For the second installing plate 2064 closer to the fuselage 10.First installing plate 2060 includes first surface 2061, and described the
One surface 2061 is towards the fuselage 10.Second installing plate 2064 includes second surface 2065, the second surface 2065
Also towards the fuselage 10.
First mounting portion 2020 is fixedly mounted in the first surface 2061 of one of them damping device 206,
The 3rd mounting portion 2044 is fixedly mounted in the first surface 2061 of another damping device 206；Subtract described in one of them
The 3rd mounting portion 2040 is fixedly mounted in the second surface 2065 of shake device 206, another damping device 206
The 4th mounting portion 2044 is fixedly mounted in the second surface 2065.
First installing plate, 2060 and second installing plate 2064 is all the tablet of square, each damping device
206 are respectively arranged at 2060 He of the first installing plate including 4 described 2062,4 damper elements 2062 of damper element
4 angles of the second installing plate 2064.
It is understood that in some other embodiments, first mounting portion 2020, the second mounting portion 2024, the
Three mounting portions 2040 and the 4th mounting portion 2044 can be omitted, and the both ends of first connecting portion 2022 are directly fixedly connected respectively
First installing plate 2060 of two damping devices 206, the both ends of second connecting portion 2022 are directly fixedly connected with two respectively
Second installing plate 2064 of the damping device 206.
The damper element 2062 is shock-absorbing ball, is made by elastic material, such as rubber material.
It is understood that in some other embodiments, the damper element 2062 can be elasticity shock structure or its
His damper element, as long as the damping between 2060 and second installing plate 2064 of the first installing plate can be reached.It is described to subtract
The number and distribution mode of element 2062 are shaken, can be changed according to actual needs.First installing plate, 2060 and second installing plate
2064 are not limited to the tablet of square, can change according to actual needs, for example, rectangle or circular tablet.
First holder 208 is fixedly installed in the second installing plate 2064 of one of them damping device 206, the
One holder 208 is located at the opposite sides of the damping device 206 with fuselage 10 respectively.Similarly, second holder 210 is fixed
The second installing plate 2064 of another damping device 206 is installed on, the second holder 210 is located at described respectively with fuselage 10
The opposite sides of damping device 206.First holder, 208 and second holder 210 is arranged at the opposite sides of the fuselage 10.
First holder, 208 and second holder 210 is all three-axis stability augmentation holder, each three-axis stability augmentation holder 208,210
The first photographic device 208 in-flight or the second photographic device 210 increase on three axis steady：Course axis (Yaw), pitching
Axis (Pitch) and roll axis (Roll).The pitch axis is perpendicular to roll axis, and course axis is perpendicular to pitch axis and roll axis.
Each holder 208,210 includes：First motor, the second motor and the 3rd motor.In the rotor of first motor
Mandrel is coaxial with roll axis.The central shaft of the rotor of second motor and pitch axis are coaxial, and the central shaft of the rotor of the 3rd motor
It is coaxial with course axis.The stator of 3rd motor is installed on the second installing plate 2064 of the damping device 206 by mounting base, the
The rotor of three motors connects the stator of the second motor, and the rotor of the second motor connects the stator of the first motor.
It is understood that in some other embodiments, the 3rd motor can be omitted, and the stator of the second motor leads to
Cross the second installing plate 2064 that mounting base is installed on the damping device 206.
First photographic device 208 is fixedly installed in the rotor of the first motor of the first holder 208, and the second camera shooting fills
Put the rotor of 210 the first motors for being fixedly installed in the second holder 210.210 court of first photographic device 208 and the second photographic device
It sets round about, and the light shaft coaxle of the optical axis of the first photographic device 208 and the second photographic device 210.
It is understood that in some other embodiments, 208 and second holder 210 of the first holder can be single shaft
Holder.First photographic device, 212 and second photographic device 214 can include more than one camera lens.
In 100 flight of unmanned vehicle of the utility model embodiment, since a damping device 206 is connected to
Between one end of first connector 202 and one end of second connector 20, another described damping device 206 connects
Between the other end of first connector 202 and the other end of second connector 204, the damping device 206 is right
First photographic device 208, the damping effect of the second photographic device 210 are consistent, improve the uniformity of damping so that first takes the photograph
As device 208, the second photographic device 210 can steadily be shot, so as to obtain high quality graphic.
In addition, the motor on three axis of the first holder 208 and the second holder 210 understands the same rotation of the output phase to keep first
208 and second photographic device 210 of photographic device is increased steady simultaneously.In this case, the first photographic device 208 and the second camera shooting
Device 210 further can steadily obtain high quality graphic, for being spliced into panoramic picture.
Moreover, the picture shooting assembly 20 can flexibly increase damping device according to actual demand, for example, increasing described in two
Every one end 102,104 of damping device 206 namely the fuselage 10 all has there are two the damping device 206.In the fuselage
10 every one end 102,104, two damping devices 206 are stacked, one end connection of first connector 202
One damping device 206, one end of second connector 204 connect another damping device 206.
It is understood that in some other embodiments, the unmanned vehicle 100 is in flight, the first end
102 and second end 104 can respectively be located at the fuselage 10 208 and second holder 210 of the left and right sides namely first holder
It is located at the left and right sides of the fuselage 10 respectively.
Finally it should be noted that：Above example is only to illustrate the technical solution of the utility model, rather than its limitations；
Under the thinking of the utility model, it can also be combined between the technical characteristic in above example or different embodiments,
Step can be realized with random order, and many other variations of the different aspect there are the utility model as described above, be
Simplicity, they do not provide in details；Although the utility model is described in detail with reference to the foregoing embodiments, this
The those of ordinary skill in field should be understood：It can still modify to the technical solution recorded in foregoing embodiments,
Or equivalent substitution is carried out to which part technical characteristic；And these are changed or are replaced, and do not make the sheet of appropriate technical solution
Matter departs from the scope of various embodiments of the utility model technical solution.
Claims (16)
1. a kind of picture shooting assembly (20), applied to unmanned vehicle (100), the unmanned vehicle (100) includes fuselage (10),
It is characterized in that, the picture shooting assembly (20) includes：
First connector (202), the second connector (204)；
Damping device (206), a damping device (206) are connected to one end of first connector (202) and described
Between one end of second connector (204), another described damping device (206) is connected to first connector (202)
Between the other end of the other end and second connector (204), first connector (202), second connector
(204) enclose with the damping device (206) and set to form one for accommodating the passage (30) of the fuselage (10)；
First holder (208), the second holder (210), positioned at one end of first connector (202) and second connector
(204) damping device (206) between one end installs first holder (208), positioned at first connector
(202) another described damping device (206) installation institute between the other end and the other end of second connector (204)
State the second holder (210)；
First photographic device (212), the second photographic device (214), first photographic device (212) are installed on first cloud
Platform (208), second photographic device (214) are installed on second holder (210).
2. picture shooting assembly (20) according to claim 1, which is characterized in that each damping device (206) includes the
One surface (2061), the first surface (2061) are fixed towards the fuselage (10), one end of first connector (202)
The first surface (2061) of a damping device (206) is installed on, the other end of first connector (202) fixes peace
First surface (2061) loaded on damping device another described (206).
3. picture shooting assembly (20) according to claim 2, which is characterized in that first connector (202) includes first
Mounting portion (2020), first connecting portion (2022) and the second mounting portion (2024), the first connecting portion (2022) are connected to institute
It states between the first mounting portion (2020) and the second mounting portion (2024)；
First mounting portion (2020) is fixedly installed in the first surface (2061) of a damping device (206), described
Second mounting portion (2024) is fixedly installed in the first surface (2061) of another damping device (206).
4. picture shooting assembly (20) according to claim 3, which is characterized in that first mounting portion (2020) and the second peace
Dress portion (2024) is all perpendicular to the first connecting portion (2022).
5. according to claim 2 to 4 any one of them picture shooting assembly (20), which is characterized in that each damping device
(206) the first installing plate (2060), damper element (2062) and the second installing plate (2064), the damper element (2062) are included
It is sandwiched between first installing plate (2060) and the second installing plate (2064), first installing plate (2060) is compared with described
Second installing plate (2064) includes the first surface closer to the fuselage (10), first installing plate (2060)
(2061)。
6. picture shooting assembly (20) according to claim 5, which is characterized in that the damper element (2062) is shock-absorbing ball.
7. picture shooting assembly (20) according to claim 5, which is characterized in that second installing plate (2064) includes second
Surface (2065), the second surface (2065) fix peace towards the fuselage (10), one end of second connector (204)
Second surface (2065) loaded on a damping device (206), the other end of second connector (204) are fixedly mounted
In the second surface (2065) of another damping device (206).
8. picture shooting assembly (20) according to claim 7, which is characterized in that second connector (204) includes the 3rd
Mounting portion (2040), second connecting portion (2042) and the 4th mounting portion (2044), the second connecting portion (2042) are connected to institute
It states between the 3rd mounting portion (2040) and the 4th mounting portion (2044)；
3rd mounting portion (2040) is fixedly installed in the second surface (2065) of a damping device (206), described
4th mounting portion (2044) is fixedly installed in the second surface (2065) of another damping device (206).
9. picture shooting assembly (20) according to claim 8, which is characterized in that the 3rd mounting portion (2040) and the 4th peace
Dress portion (2044) is all perpendicular to the second connecting portion (2042).
10. picture shooting assembly (20) according to claim 5, which is characterized in that first holder (208) is fixedly installed in
The second installing plate (2064) of one damping device (206), second holder (210) are fixedly installed in described in another
The second installing plate (2064) of damping device (206).
11. picture shooting assembly (20) according to claim 1, which is characterized in that first holder (208) and/or second
Holder (210) is three-axis stability augmentation holder.
12. picture shooting assembly (20) according to claim 1, which is characterized in that first photographic device (212) and/or
Second photographic device (214) includes at least one camera lens.
13. a kind of unmanned vehicle (100), which is characterized in that including fuselage (10) and as described in any one of claim 1 to 12
Picture shooting assembly (20), the fuselage (10) is accommodated in the passage (30), and one end of first connector (202) is fixed
It is installed on the fuselage (10).
14. unmanned vehicle (100) according to claim 13, which is characterized in that first connector (202) it is another
One end is arranged at intervals with the fuselage (10).
15. the unmanned vehicle (100) according to claim 13 or 14, which is characterized in that the fuselage (10) includes phase
To the first end (102) of setting and second end (104), one end of first connector (202) is fixedly installed in described first
It holds (102)；In the unmanned vehicle (100) flight, the first end (102) is located at the downside of the fuselage (10), institute
State the upside that second end (104) is located at the fuselage (10).
16. the unmanned vehicle (100) according to claim 13 or 14, which is characterized in that the fuselage (10) includes phase
To the first end (102) of setting and second end (104), one end of first connector (202) is fixedly installed in described first
It holds (102)；In the unmanned vehicle (100) flight, the first end (102) is located at the left side of the fuselage (10), institute
State the right side that second end (104) is located at the fuselage (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721246738.1U CN207450283U (en) | 2017-09-26 | 2017-09-26 | Picture shooting assembly and the unmanned vehicle with this picture shooting assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721246738.1U CN207450283U (en) | 2017-09-26 | 2017-09-26 | Picture shooting assembly and the unmanned vehicle with this picture shooting assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207450283U true CN207450283U (en) | 2018-06-05 |
Family
ID=62284324
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721246738.1U Withdrawn - After Issue CN207450283U (en) | 2017-09-26 | 2017-09-26 | Picture shooting assembly and the unmanned vehicle with this picture shooting assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207450283U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107618672A (en) * | 2017-09-26 | 2018-01-23 | 深圳市道通智能航空技术有限公司 | Picture shooting assembly and the unmanned vehicle with this picture shooting assembly |
-
2017
- 2017-09-26 CN CN201721246738.1U patent/CN207450283U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107618672A (en) * | 2017-09-26 | 2018-01-23 | 深圳市道通智能航空技术有限公司 | Picture shooting assembly and the unmanned vehicle with this picture shooting assembly |
| WO2019062126A1 (en) * | 2017-09-26 | 2019-04-04 | 深圳市道通智能航空技术有限公司 | Photographing assembly and unmanned aerial vehicle having same |
| CN107618672B (en) * | 2017-09-26 | 2020-03-20 | 深圳市道通智能航空技术有限公司 | Shooting assembly and unmanned aerial vehicle with same |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20180605 Effective date of abandoning: 20200320 |
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| AV01 | Patent right actively abandoned |