CN207683777U - A kind of unmanned vehicle - Google Patents
A kind of unmanned vehicle Download PDFInfo
- Publication number
- CN207683777U CN207683777U CN201721798586.6U CN201721798586U CN207683777U CN 207683777 U CN207683777 U CN 207683777U CN 201721798586 U CN201721798586 U CN 201721798586U CN 207683777 U CN207683777 U CN 207683777U
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- CN
- China
- Prior art keywords
- fuselage
- unmanned vehicle
- imaging device
- control terminal
- mobile control
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- 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.)
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Abstract
The utility model discloses a kind of unmanned vehicles, imaging device including fuselage, below the fuselage, several horns on the fuselage, the mobile control terminal set on the propeller of each horn end and with the imaging device and propeller wireless connection, the fuselage is equipped with position laser illuminator system corresponding with the imaging device, and the laser illuminator system is wirelessly connected with the mobile control terminal.By the way that laser illuminator system corresponding with imaging device is arranged on fuselage, when the brightness of image of imaging device shooting is inadequate or in Night, laser illuminator system is opened by mobile control terminal and is illuminated, image frame is made to be more clear.The laser illuminator system is illuminated using lasing light emitter, not only compact, and weight is light, and power is small, and photoelectric conversion efficiency is high, and beam divergence angle is small, and illumination distances are remote, meets the practical application needs of unmanned vehicle conscientiously.
Description
Technical field
The utility model is related to aircraft fields, and in particular to a kind of unmanned vehicle with laser lighting.
Background technology
With the development of science and technology, unmanned plane become a kind of emerging technology, due to its flight stability, it is at low cost, can realize
The advantage that any angle flexibly moves, in recent years military attack, public security chase after paving, disaster search and rescue, agricultural investigation, publicity take photo by plane
Field is widely applied, and becomes important remote sensing platform.
Due to existing small drone small volume, in order to ensure the cruise duration of battery, and existing LED light, halogen
Not only volume is big for plain lamp or xenon lamp, photoelectric conversion efficiency is relatively low, and beam divergence angle is big, causes light intensity relatively low, limits photograph
Prescribed distance.Therefore existing small drone usually not installs lighting module, and unmanned plane is caused to be made in the insufficient region of illumination
Industry is limited, especially at night, there are the picture of shooting is unintelligible, detects the problems such as not in place.
Utility model content
The utility model provides a kind of unmanned vehicle, limited, shooting to solve work existing in the prior art
Picture is not clear enough, detects problem not in place.
In order to solve the above-mentioned technical problem, the technical solution of the utility model is：A kind of unmanned vehicle, including fuselage,
Imaging device below the fuselage, several horns on the fuselage, the spiral shell set on each horn end
The mobile control terminal revolved paddle and be wirelessly connected with the imaging device and propeller, the fuselage be equipped with position with it is described
The corresponding laser illuminator system of imaging device, the laser illuminator system are wirelessly connected with the mobile control terminal.
Further, the mobile control terminal is equipped with display and several controls switch.
Further, the laser illuminator system includes laser source unit and corresponding with the light-emitting window of the laser source unit
Beam-expanding collimation lens, the laser source unit includes lasing light emitter and wavelength conversion unit.
Further, first through hole and the second through-hole, the beam-expanding collimation lens are vertically respectively equipped on the fuselage
It is limited in second through-hole, the light beam that the laser source unit is sent out is by being projected to described expand after the first through hole
On collimation lens.
Further, it being equipped with distance measuring unit below the fuselage, the distance measuring unit is connect with the mobile control terminal,
And include at least one distance measuring sensor.
Further, the distance measuring sensor is laser range sensor.
Further, the driving mechanism that the body upper is equipped with a telescope support and is connect with the telescope support,
The driving mechanism is connect with the mobile control terminal, and the lasing light emitter and wavelength conversion unit are sequentially arranged in described along light path
On telescope support.
Further, the horn is linked with the fuselage.
Further, the main supplying cell and reserve battery being connected with each other, the main supplying cell are equipped in the fuselage
It is connect with the propeller and laser illuminator system.
The utility model provides a kind of unmanned vehicle, including fuselage, the imaging device below the fuselage, sets
In on the fuselage several horns, set on each horn end propeller and with the imaging device and propeller
The mobile control terminal being wirelessly connected, the fuselage are equipped with position laser illuminator system corresponding with the imaging device, institute
Laser illuminator system is stated to be wirelessly connected with the mobile control terminal.By the way that laser corresponding with imaging device is arranged on fuselage
Lighting device is opened by mobile control terminal and is swashed when the brightness of image of imaging device shooting is inadequate or in Night
Illuminating apparatus is illuminated, and image frame is made to be more clear.The laser illuminator system is illuminated using lasing light emitter, not only
Compact, weight is light, and power is small, and photoelectric conversion efficiency is high, and beam divergence angle is small, and illumination distances are remote, meets nothing conscientiously
The practical application of people's aircraft needs.
Description of the drawings
Fig. 1 is the main structure figure of the utility model unmanned vehicle；
Fig. 2 is the upward view of the utility model unmanned vehicle.
As shown in the figure：10, fuselage；110, support plate；20, distance measuring unit；30, imaging device；40, horn；50, spiral
Paddle；60, mobile control terminal；610, display；620, control switch；710, laser source unit；720, beam-expanding collimation lens；
80, telescope support；90, driving mechanism.
Specific implementation mode
The utility model is described in detail below in conjunction with the accompanying drawings：
As shown in Figs. 1-2, a kind of unmanned vehicle of the utility model, including fuselage 10, positioned at the lower section of the fuselage 10
Imaging device 30, several horns 40 on the fuselage 10, set on each 40 end of the horn propeller 50 and
The mobile control terminal 60 being wirelessly connected with the imaging device 30 and propeller 50, the fuselage 10 be equipped with position with it is described
30 corresponding laser illuminator system of imaging device.Specifically, in the present embodiment, horn 40 is equipped with 6, naturally it is also possible to be arranged 4
It is a or 8 etc., it not limits herein.The laser lighting that setting is wirelessly connected with mobile control terminal 60 below fuselage 10 fills
It sets, the position of laser illuminator system is corresponding with imaging device 30, and the light-emitting window and imaging for referring specifically to laser illuminator system herein fill
Set 30 camera shooting mouth correspondence.When the brightness of image that imaging device 30 takes is inadequate, when picture is not clear enough, pass through mobile control
Terminal 60 is opened laser illuminator system and is illuminated, and image is made to be more clear, when brightness of image is excessively high or in day mode,
Laser illuminator system is then closed, with using electricity wisely.In the present embodiment, camera or camera etc. may be used in imaging device 30, can
To shoot image or video.
Preferably, the mobile control terminal 60 is equipped with display 610 and several control switches 620, and display 610 is used
In image or video that display imaging device 30 is shot, consequently facilitating brightness and the clarity of image are observed, to preferably control
The switch of laser illuminator system processed；Several control switches 620 include the control of the control switch, laser illuminator system of propeller 50
The control switch etc. of switch, imaging device 30, the working condition for controlling unmanned vehicle.
Preferably, the horn 40 is linked with the fuselage 10, can be moved under the effect of external force around fuselage 10, to
When not working, horn 40 is retracted to 10 top of fuselage, to save occupied space.
Preferably, 10 lower section of the fuselage is equipped with distance measuring unit 20, and the distance measuring unit 20 is passed including at least one ranging
Sensor, the distance measuring sensor are preferably laser range sensor.In the present embodiment, there are one the distance measuring sensor is set, use
In measuring height of the unmanned vehicle apart from ground, focal length and the laser lighting of imaging device 30 can be highly adjusted according to this
The illumination distances of device, make image be more clear.
Preferably, the laser illuminator system includes laser source unit 710 and the light-emitting window with the laser source unit 710
Corresponding beam-expanding collimation lens 720, the laser source unit 710 include lasing light emitter and wavelength conversion unit, what lasing light emitter was sent out
Laser beam forms illuminating bundle after being converted by wavelength conversion unit, and by 720 beam-expanding collimation of beam-expanding collimation lens after
Projection is gone out, and lasing light emitter and wavelength conversion unit are packaged as a whole in the present embodiment.
Preferably, first through hole and the second through-hole (not marked in figure), institute are vertically equipped on the fuselage 10 successively
It states beam-expanding collimation lens 730 to be limited in second through-hole, the light beam that the laser source unit 710 is sent out passes through described first
It is projected to after through-hole on the beam-expanding collimation lens 730.Specifically, in the present embodiment, the inside of fuselage 10 is hollow-core construction, the
One through-hole and the second through-hole are respectively arranged in two pieces of support plates 110 up and down.
Preferably, the driving machine that 10 top of the fuselage is equipped with a telescope support 80 and is connect with the telescope support 80
Structure 90, the driving mechanism are connect with the mobile control terminal 60, the lasing light emitter and wavelength conversion unit along light path successively
On the telescope support 80, lasing light emitter and wavelength conversion unit can be packaged together, kept away of course for easy for installation
Exempt to be mutually shifted in flight course and the problems such as laser leaks.Specifically, telescope support 80 can drive lasing light emitter
It is moved relative to fuselage 10 with wavelength conversion unit, to change the distance between beam-expanding collimation lens 720, with according to picture
The illumination distances of the Level Change illuminating bundle of brightness and clarity and aircraft.
Preferably, the main supplying cell and reserve battery being connected with each other, the main supplying cell are equipped in the fuselage 10
It is connect with the propeller 50 and laser illuminator system.Specifically, main supplying cell also connects with distance measuring unit 20 and driving mechanism
It connects, for being powered to unmanned vehicle, when main supplying cell out of power, reserve battery can be opened and carry out auxiliary power supply.
In conclusion the utility model provides a kind of unmanned vehicle, including fuselage 10, it is located at 10 lower section of the fuselage
Imaging device 30, several horns 40 on the fuselage 10, set on each 40 end of the horn propeller 50 with
And the mobile control terminal 60 being wirelessly connected with the imaging device 30 and propeller 50, the fuselage 10 are equipped with position and institute
30 corresponding laser illuminator system of imaging device is stated, the laser illuminator system is wirelessly connected with the mobile control terminal 60.
By the way that corresponding with imaging device 30 laser illuminator system is arranged on fuselage 10, when the shooting of imaging device 30 brightness of image not
When enough or in Night, laser illuminator system is opened by mobile control terminal 60 and is illuminated, imaging device 30 is convenient for
Normal photographing.The laser illuminator system is illuminated using lasing light emitter, not only compact, and weight is light, and power is small, light
Photoelectric transformation efficiency is high, and beam divergence angle is small, and illumination distances are remote, meets the practical application needs of unmanned vehicle conscientiously.
Although the embodiment of the utility model is illustrated in specification, these embodiments are intended only as carrying
Show, should not limit the scope of protection of the utility model.Various omissions are carried out in the range of not departing from the utility model aims, are set
It changes and change should be included in the scope of protection of the utility model.
Claims (9)
1. a kind of unmanned vehicle, which is characterized in that imaging device including fuselage, below the fuselage, be set to it is described
Several horns on fuselage wirelessly connect set on the propeller of each horn end and with the imaging device and propeller
The mobile control terminal connect, the fuselage are equipped with position laser illuminator system corresponding with the imaging device, the laser
Lighting device is wirelessly connected with the mobile control terminal.
2. unmanned vehicle according to claim 1, which is characterized in that the mobile control terminal be equipped with display and
Several control switches.
3. unmanned vehicle according to claim 1, which is characterized in that the laser illuminator system includes laser source unit
Beam-expanding collimation lens corresponding with the light-emitting window of the laser source unit, the laser source unit include that lasing light emitter and wavelength turn
Change unit.
4. unmanned vehicle according to claim 3, which is characterized in that it is logical to be vertically respectively equipped with first on the fuselage
Hole and the second through-hole, the beam-expanding collimation lens are limited in second through-hole, and the light beam that the laser source unit is sent out is logical
It is projected on the beam-expanding collimation lens after crossing the first through hole.
5. unmanned vehicle according to claim 1, which is characterized in that distance measuring unit is equipped with below the fuselage, it is described
Distance measuring unit is connect with the mobile control terminal, and includes at least one distance measuring sensor.
6. unmanned vehicle according to claim 5, which is characterized in that the distance measuring sensor senses for laser ranging
Device.
7. unmanned vehicle according to claim 5, which is characterized in that the body upper be equipped with a telescope support and
The driving mechanism being connect with the telescope support, the driving mechanism are connect with the mobile control terminal, the lasing light emitter and
Wavelength conversion unit is sequentially arranged in along light path on the telescope support.
8. unmanned vehicle according to claim 1, which is characterized in that the horn is linked with the fuselage.
9. unmanned vehicle according to claim 1, which is characterized in that be equipped with the main power supply being connected with each other in the fuselage
Battery and reserve battery, the main supplying cell are connect with the propeller and laser illuminator system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721798586.6U CN207683777U (en) | 2017-12-21 | 2017-12-21 | A kind of unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721798586.6U CN207683777U (en) | 2017-12-21 | 2017-12-21 | A kind of unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207683777U true CN207683777U (en) | 2018-08-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721798586.6U Active CN207683777U (en) | 2017-12-21 | 2017-12-21 | A kind of unmanned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207683777U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082462A (en) * | 2017-12-21 | 2018-05-29 | 超视界激光科技（苏州）有限公司 | A kind of unmanned vehicle |
-
2017
- 2017-12-21 CN CN201721798586.6U patent/CN207683777U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082462A (en) * | 2017-12-21 | 2018-05-29 | 超视界激光科技（苏州）有限公司 | A kind of unmanned vehicle |
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