CN208110040U - A kind of aerial device with airborne laser radar - Google Patents
A kind of aerial device with airborne laser radar Download PDFInfo
- Publication number
- CN208110040U CN208110040U CN201820468843.8U CN201820468843U CN208110040U CN 208110040 U CN208110040 U CN 208110040U CN 201820468843 U CN201820468843 U CN 201820468843U CN 208110040 U CN208110040 U CN 208110040U
- Authority
- CN
- China
- Prior art keywords
- laser radar
- adjustable plate
- airborne laser
- aerial device
- secured adjusted
- 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
Landscapes
- Optical Radar Systems And Details Thereof (AREA)
Abstract
The utility model discloses a kind of aerial devices with airborne laser radar for equipment technical field of taking photo by plane, including unmanned base, secured adjusted frame is installed below the bottom plate of the unmanned base, the secured adjusted frame includes eight risers for surrounding square, it is fixedly welded respectively on the riser by cross bar, adjustable plate is provided in the secured adjusted frame, it is fixed between the adjustable plate and unmanned base by fastener, the fastener includes thread barrel and stud, the utility model is convenient for the setting by large circle and small circle ring in adjustable plate, make airborne laser radar that can keep stable during aircraft flight, it is convenient for continuously measuring, airborne laser radar can carry out upper-lower height adjusting, it is also convenient for being dismantled, when being flown and being landed, decoupling rod jolts convenient for buffering, protect laser radar.
Description
Technical field
The utility model relates to equipment technical field of taking photo by plane, specially a kind of aerial device with airborne laser radar.
Background technique
With the development of unmanned air vehicle technique, application surface is more and more wider, embodies not in civil field and military domain
Can or scarce importance, especially aeroplane photography using more and more extensive, had become using unmanned plane as aeroplane photography platform
The mainstream developed at present.The camera of unmanned plane is mainly using holder as carrying platform at present, however the unmanned plane in working
It is influenced by external environment and oneself factor influences, fuselage and holder can inevitably shake, and will result in phase in this way
Machine is unstable, influences camera imaging or photograph coincidence factor and then influences the panorama manufacturing in image later period.On the other hand, traditional nothing
Man-machine cradle head structure is complicated, and weight bearing is big, and cost of manufacture is high.So needing a kind of knot with the development of unmanned plane technology
Structure is simple, stablizes, practical, at low cost aerial device.
A kind of such as anti-interference aerial device of unmanned plane gravity of number of patent application CN201420093707.7 comprising connection
Device, imaging device, fixed frame, steering engine and damper group, described attachment device one end pass through gimbal suspension bearing A and unmanned plane
Body connection, the other end are connect by gimbal suspension bearing B with fixed frame, and the imaging device is fixed on the fixed frame.
The damper group includes damper group A and damper group B.The fixed frame passes through damper group A and the unmanned plane body
Connection, is connect by damper group B with the unmanned plane undercarriage.Such device is not easy to carrying out aerial device into stable put
It sets, is easy to be influenced by fuselage flight angle when being taken photo by plane, measurement shooting is impacted, is based on this, the utility model
A kind of aerial device with airborne laser radar is devised, to solve the above problems.
Utility model content
The purpose of this utility model is to provide a kind of aerial devices with airborne laser radar, to solve above-mentioned background
The unmanned plane in work proposed in technology is influenced by external environment and oneself factor influences, and fuselage and holder can be inevitable
Shake, it is unstable to will result in camera in this way；It is not easy to carry out aerial device to stablize placement, the appearance when being taken photo by plane
Vulnerable to the influence of fuselage flight angle, the problem of being impacted to measurement shooting.
To achieve the above object, the utility model provides the following technical solutions：A kind of taking photo by plane with airborne laser radar
Device, including unmanned base, the bottom plate lower section of the unmanned base are equipped with secured adjusted frame, and the secured adjusted frame includes enclosing
At eight risers of square, it is fixedly welded on the riser by cross bar, is provided in the secured adjusted frame respectively
Adjustable plate is fixed between the adjustable plate and unmanned base by fastener, and the fastener includes thread barrel and stud, described
Stud is screwed onto thread barrel, and the stud runs through adjustable plate, and the lower end of the stud is bolted with wing nut, the adjusting
The bottom of plate is provided with decoupling rod, and the bottom of the decoupling rod is equipped with mounting seat, and the bottom of the mounting seat is provided with
Laser radar.
Preferably, round through slot is offered in the adjustable plate, is in that a straight line is provided with two groups first turn in the round through slot
Axis, is movably set with large circle in the first rotating shaft, and a straight line is provided with two group of second shaft in the large circle, described
It is movably set with small circle ring in second shaft, cross-bar is provided on the small circle ring, is provided with decoupling rod in the cross-bar
Fixed lid.
Preferably, first rotating shaft described in two groups and two group of second shaft are perpendicular arranged in a crossed manner.
Preferably, the outer edge of the adjustable plate offers sliding slot, and the riser is plugged in sliding slot.
Preferably, the decoupling rod includes damping sleeve, and flexible inserted link is plugged in the damping sleeve, described flexible slotting
The lower end of bar is fixedly installed spring, and the other end of the spring is fixedly connected with the intracavity bottom of damping sleeve.
Compared with prior art, the utility model has the beneficial effects that：The utility model is convenient for through great circle in adjustable plate
The setting of ring and small circle ring makes airborne laser radar that can keep stable during aircraft flight, is convenient for continuously surveying
Amount, airborne laser radar can carry out upper-lower height adjusting, be also convenient for being dismantled, and when being flown and being landed, decoupling rod is just
It jolts in buffering, protects laser radar.
Detailed description of the invention
In order to illustrate more clearly of the technical solution of the utility model embodiment, make required for being described below to embodiment
Attached drawing is briefly described, it should be apparent that, the drawings in the following description are merely some embodiments of the present invention,
For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings
Other attached drawings.
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model adjustable plate structural schematic diagram；
Fig. 3 is the utility model decoupling rod structural schematic diagram.
In attached drawing, parts list represented by the reference numerals are as follows：
The unmanned base of 1-, 2- secured adjusted frame, 3- riser, 4- cross bar, 5- adjustable plate, 6- thread barrel, 7- stud, 8- butterfly
Nut, 9- decoupling rod, 10- mounting seat, 11- laser radar, 12- circle through slot, 13- first rotating shaft, 14- large circle, 15- second
Shaft, 16- small circle ring, 17- cross-bar, the fixed lid of 18- decoupling rod, 19- sliding slot, 20- damping sleeve, 21- spring, 22- are flexible
Inserted link.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without creative efforts
All other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution：A kind of dress of taking photo by plane with airborne laser radar
It sets, including unmanned base 1, secured adjusted frame 2 is installed below the bottom plate of unmanned base 1, secured adjusted frame 2 includes surrounding pros
Eight risers 3 of body are fixedly welded on riser 3 respectively by cross bar 4, adjustable plate 5 are provided in secured adjusted frame 2, are adjusted
It is fixed between section plate 5 and unmanned base 1 by fastener, fastener includes thread barrel 6 and stud 7, and stud 7 is screwed onto thread barrel
In 6, stud 7 runs through adjustable plate 5, and the lower end of stud 7 is bolted with wing nut 8, and the bottom of adjustable plate 5 is provided with decoupling rod 9,
The bottom of decoupling rod 9 is equipped with mounting seat 10, and the bottom of mounting seat 10 is provided with laser radar 11.
Wherein, round through slot 12 is offered in adjustable plate 5, is in that a straight line is provided with two groups of first rotating shafts 13 in circle through slot 12,
It is movably set with large circle 14 in first rotating shaft 13, a straight line is provided with two group of second shaft 15 in large circle 14, second turn
It is movably set with small circle ring 16 on axis 15, cross-bar 17 is provided on small circle ring 16, decoupling rod is provided in cross-bar 17 and fixes
Lid 18.
Wherein, two groups of first rotating shafts 13 and two group of second shaft 15 are perpendicular arranged in a crossed manner.
Wherein, the outer edge of adjustable plate 5 offers sliding slot 19, and riser 3 is plugged in sliding slot 19.
Wherein, decoupling rod 9 includes damping sleeve 20, is plugged with flexible inserted link 22 in damping sleeve 20, and stretch inserted link 22
Lower end is fixedly installed spring 21, and the other end of spring 21 is fixedly connected with the intracavity bottom of damping sleeve 19.
One of the present embodiment has particular application as：Laser radar 11 is mounted in mounting seat 10, adjustable plate 5 is flying
Device carries out in flight course, and first rotating shaft 13 and the second shaft 15 make large circle 14 and small circle ring 16 carry out center of gravity adjusting, makes to swash
Optical radar 11 stablizes state directed downwardly in one always, is convenient for measuring, passes through thread barrel 6, stud 7 and wing nut 8
It is adjusted convenient for the height to adjustable plate 5, riser 3 is connected in sliding slot 19, convenient for the stabilization of adjustable plate 5, in decoupling rod 9
Spring 21 is convenient for impact of the buffering to laser radar 11 when flight is jolted and landed, and protects to laser radar 11.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
Particular features, structures, materials, or characteristics described in conjunction with this embodiment or example are contained at least one of the utility model
In embodiment or example.In the present specification, schematic expression of the above terms be not necessarily referring to identical embodiment or
Example.Moreover, particular features, structures, materials, or characteristics described can be in any one or more embodiment or examples
In can be combined in any suitable manner.
The preferred embodiment in the utility model disclosed above is only intended to help to illustrate the utility model.Preferred embodiment is simultaneously
There is no the details that detailed descriptionthe is all, also not limiting the utility model is only the specific embodiment.Obviously, according to this theory
The content of bright book can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably
The principles of the present invention and practical application are explained, so that skilled artisan be enable to better understand and utilize this
Utility model.The utility model is limited only by the claims and their full scope and equivalents.
Claims (5)
1. a kind of aerial device with airborne laser radar, including unmanned base (1), it is characterised in that：The unmanned base
(1) it is equipped with secured adjusted frame (2) below bottom plate, the secured adjusted frame (2) includes eight risers for surrounding square
(3), it is fixedly welded respectively on the riser (3) by cross bar (4), is provided with adjustable plate in the secured adjusted frame (2)
(5), it is fixed between the adjustable plate (5) and unmanned base (1) by fastener, the fastener includes thread barrel (6) and spiral shell
Column (7), the stud (7) are screwed onto thread barrel (6), and the stud (7) runs through adjustable plate (5), the lower end of the stud (7)
Portion is bolted with wing nut (8), and the bottom of the adjustable plate (5) is provided with decoupling rod (9), the bottom peace of the decoupling rod (9)
Equipped with mounting seat (10), the bottom of the mounting seat (10) is provided with laser radar (11).
2. a kind of aerial device with airborne laser radar according to claim 1, it is characterised in that：The adjustable plate
(5) it is offered in round through slot (12), a straight line is provided with two groups of first rotating shafts (13) in the round through slot (12), described first
It is movably set in shaft (13) large circle (14), a straight line is provided with two group of second shaft in the large circle (14)
(15), it is movably set with small circle ring (16) on second shaft (15), is provided with cross-bar (17) on the small circle ring (16),
The fixed lid (18) of decoupling rod is provided in the cross-bar (17).
3. a kind of aerial device with airborne laser radar according to claim 2, it is characterised in that：Described in two groups
One shaft (13) and two group of second shaft (15) are perpendicular arranged in a crossed manner.
4. a kind of aerial device with airborne laser radar according to claim 2, it is characterised in that：The adjustable plate
(5) outer edge offers sliding slot (19), and the riser (3) is plugged in sliding slot (19).
5. a kind of aerial device with airborne laser radar according to claim 1, it is characterised in that：The decoupling rod
(9) include damping sleeve (20), be plugged with flexible inserted link (22) in the damping sleeve (20), under the flexible inserted link (22)
End is fixedly installed spring (21), and the other end of the spring (21) is fixedly connected with the intracavity bottom of damping sleeve (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820468843.8U CN208110040U (en) | 2018-03-30 | 2018-03-30 | A kind of aerial device with airborne laser radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820468843.8U CN208110040U (en) | 2018-03-30 | 2018-03-30 | A kind of aerial device with airborne laser radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208110040U true CN208110040U (en) | 2018-11-16 |
Family
ID=64120448
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820468843.8U Expired - Fee Related CN208110040U (en) | 2018-03-30 | 2018-03-30 | A kind of aerial device with airborne laser radar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208110040U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110683063A (en) * | 2019-09-27 | 2020-01-14 | 中国科学院沈阳自动化研究所 | Laser radar passive vibration damping device for large-load unmanned aerial vehicle |
| CN111880562A (en) * | 2020-07-16 | 2020-11-03 | 河南理工大学 | Unmanned aerial vehicle ground-imitating flying device based on laser radar |
-
2018
- 2018-03-30 CN CN201820468843.8U patent/CN208110040U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110683063A (en) * | 2019-09-27 | 2020-01-14 | 中国科学院沈阳自动化研究所 | Laser radar passive vibration damping device for large-load unmanned aerial vehicle |
| CN111880562A (en) * | 2020-07-16 | 2020-11-03 | 河南理工大学 | Unmanned aerial vehicle ground-imitating flying device based on laser radar |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203996917U (en) | A kind of unmanned vehicle | |
| CN201626554U (en) | Three-freedom-degree inertia stabilization aerial photography cradle head | |
| CN208110040U (en) | A kind of aerial device with airborne laser radar | |
| CN109690166B (en) | Cloud platform damping device and shooting device | |
| CN204124373U (en) | Unmanned plane twin shaft video cradle head structure | |
| CN205721377U (en) | A kind of multi-rotor aerocraft | |
| CN205554623U (en) | Optical zoom nacelle | |
| CN106956768A (en) | Aircraft | |
| CN106428595A (en) | Built-in image stabilization cradle head for miniature unmanned aerial vehicle | |
| CN106904286B (en) | A kind of UAV electro-optical pod's damping device | |
| JP7244084B2 (en) | Electronic parts and aircraft equipped with such electronic parts | |
| CN108891611A (en) | A kind of aircraft | |
| CN107380473A (en) | A kind of vertical stable clouds terrace system and unmanned plane | |
| CN202748029U (en) | Image motion compensation device for aerial survey of unmanned aerial vehicle | |
| CN203681878U (en) | Damping device of multi-lens aerial photography stabilized platform | |
| CN206871377U (en) | A kind of three axle gondolas with Fast-Balance regulatory function | |
| CN108725817A (en) | A kind of four axis unmanned planes with stabilization function | |
| CN218537086U (en) | Surveying and mapping aerial photography aircraft | |
| CN207141420U (en) | A kind of vertical stable clouds terrace system and unmanned plane | |
| CN203780804U (en) | Shock-absorption shooting cradle head of aircraft | |
| CN211618110U (en) | Diaxon VTOL unmanned aerial vehicle | |
| CN204776018U (en) | Many rotors aircraft of taking photo by plane | |
| CN211468795U (en) | Unmanned aerial vehicle with couple | |
| CN207258004U (en) | A kind of picture shooting assembly and the unmanned plane with this picture shooting assembly | |
| CN207826583U (en) | A kind of multifunction camera cover and its aerial survey gondola |
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: 20181116 Termination date: 20190330 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |