CN209159990U - Damping device is used in a kind of landing of unmanned plane - Google Patents
Damping device is used in a kind of landing of unmanned plane Download PDFInfo
- Publication number
- CN209159990U CN209159990U CN201821965445.3U CN201821965445U CN209159990U CN 209159990 U CN209159990 U CN 209159990U CN 201821965445 U CN201821965445 U CN 201821965445U CN 209159990 U CN209159990 U CN 209159990U
- Authority
- CN
- China
- Prior art keywords
- fixed
- unmanned plane
- damping device
- rotating shaft
- support frame
- 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
Landscapes
- Vibration Prevention Devices (AREA)
Abstract
The utility model relates to air vehicle technique fields, and disclose a kind of unmanned plane landing damping device, including drone body, the drone body bottom is fixedly installed with fixed station, the equal movable sleeve in the quadrangle of the fixed station is connected to bolt, the quadrangle of the fixed station is connected to positioning table by bolt movable sleeve, the elastic set of the equal pivot bush unit in the outer surface of the bolt, the bottom of the positioning table is fixedly installed with video recorder main body, the bottom of the drone body is fixedly installed with fixed rotating shaft, the quantity of the fixed rotating shaft is two, the outer surface movable sleeve of the fixed rotating shaft is connected to support frame, the quantity of support frame as described above is two.Unmanned plane landing damping device, and elastic sleeve acts between fixed station and positioning table, so that the bounce that video recorder main body is subject to is buffered by elastic sleeve, the bounce for avoiding video recorder main body from being subject to is transmitted in drone body, to have the function that buffering.
Description
Technical field
The utility model relates to air vehicle technique field, damping device is used in specially a kind of unmanned plane landing.
Background technique
Unmanned plane is one kind by aircraft unmanned, reusable on power drive, machine, civilian unmanned owner
It is divided into consumer level and technical grade, following to have wide application in multiple industries, as aircraft, unmanned plane has fixation
Three kinds of wing, helicopter, more rotors types, three have his own strong points, and more rotors occupy advantage, global model in current miniaturization type
In enclosing, the management policy of unmanned plane follows navigation substantially, and more strictly, unmanned plane of essentially taking photo by plane currently on the market passes through sky
Middle photography or aeroplane photography obtain top view from aerial photographing earth landforms, and the video camera taken photo by plane can be controlled by photographer,
It can also automatically snap or remotely control.
Unmanned plane is in landing since the vibration that gravity can rebound on the ground, and rebound can damage the inside of unmanned plane
Part, adverse effect is caused to housing construction or airborne equipment for this, and existing unmanned plane landing gear is essentially all
Rigid material can aggravate the transmitting of vibration, to influence unmanned plane.
Utility model content
In view of the deficiencies of the prior art, the utility model provides a kind of unmanned plane landing damping device, has
The advantages of buffering, solves unmanned plane in landing since gravity can rebound on the ground, and the vibration to rebound can damage nothing
The part of man-machine inside causes adverse effect to housing construction or airborne equipment for this, and existing unmanned plane landing gear
It is essentially all rigid material, the transmitting of vibration can be aggravated, thus the problem of influencing unmanned plane.
The utility model provides the following technical solutions: a kind of unmanned plane landing damping device, including unmanned plane sheet
Body, the drone body bottom are fixedly installed with fixed station, and the equal movable sleeve in the quadrangle of the fixed station is connected to bolt, described solid
The quadrangle for determining platform is connected to positioning table by bolt movable sleeve, and the elastic set of the equal pivot bush unit in the outer surface of the bolt is described fixed
The bottom of position platform is fixedly installed with video recorder main body, and the bottom of the drone body is fixedly installed with fixed rotating shaft, described solid
The quantity for determining shaft is two, and the outer surface movable sleeve of the fixed rotating shaft is connected to support frame, and the quantity of support frame as described above is two
A, the bottom of support frame as described above is fixedly installed with idler wheel, and the quantity of the idler wheel is four, and four idler wheels are uniformly divided into two
Group, and two groups of idler wheels are evenly distributed on the bottom of two support frames, the both ends of two support frames as described above are fixedly installed with positioning
Shaft, the equal movable sleeve in the outer surface of four positioning rotating shafts are connected to fixed link, the equal movable sleeve in the inside of four fixed links
It is connected to sliding block, connecting rod is fixedly connected between two sliding blocks, the outer surface movable sleeve of the connecting rod is connected to transmission bullet
Spring, the internal activity of the fixed link are socketed with the adjustment spring for being located at connection rod outer surface.
Preferably, the bottom of the fixed station and the top of positioning table are contacted with elastic sleeve.
Preferably, the both ends of support frame as described above with the outer surface pivot bush unit of fixed rotating shaft.
Preferably, the both ends of the connecting rod run through fixed link and extend to the inside of fixed link and the side with sliding block
It is fixedly connected.
Preferably, the both ends of the driving spring with one end pivot bush unit of fixed link, the one of two fixed links
End is sequentially connected by driving spring.
Preferably, the end thereof contacts of the other side of the sliding block and adjustment spring, the other side of the sliding block pass through adjusting
Spring and the inner wall of fixed link are sequentially connected.
Be compared with the prior art, the utility model have it is following the utility model has the advantages that
Unmanned plane landing damping device makes two support frames convenient for rotation by fixed rotating shaft, and cooperation connects
Extension bar is contacted with two fixed links, so that two support frames are connected with each other, and adjustment spring acts on sliding block so that connecting rod with
The position of fixed link keeps stablizing, so that carrying out damping to drone body after rotating between two support frames, prevents from shaking
It is dynamic to be transmitted in drone body by support frame, and elastic sleeve acts between fixed station and positioning table, so that video recording owner
The bounce that body is subject to is buffered by elastic sleeve, and the bounce for avoiding video recorder main body from being subject to is transmitted to drone body
On, to have the function that buffering.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the side view of Fig. 1；
Fig. 3 is the enlarged drawing of A in Fig. 1.
In figure: 1, drone body；2, fixed station；3, bolt；4, positioning table；5, elastic sleeve；6, video recorder main body；7, solid
Determine shaft；8, support frame；9, idler wheel；10, positioning rotating shaft；11, fixed link；12, sliding block；13, connecting rod；14, driving spring；
15, adjustment spring.
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 making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1-3, a kind of unmanned plane landing damping device, including drone body 1, drone body 1
Bottom is fixedly installed with fixed station 2, and the equal movable sleeve in the quadrangle of fixed station 2 is connected to bolt 3, and the quadrangle of fixed station 2 is living by bolt 3
It is dynamic to be socketed with positioning table 4, the elastic set 5 of the equal pivot bush unit in the outer surface of bolt 3, the bottom of fixed station 2 and the top of positioning table 4
It is contacted with elastic sleeve 5, the bottom of positioning table 4 is fixedly installed with video recorder main body 6, and the bottom of drone body 1 is fixedly mounted
There is fixed rotating shaft 7, the quantity of fixed rotating shaft 7 is two, and the outer surface movable sleeve of fixed rotating shaft 7 is connected to support frame 8, support frame 8
Both ends with the outer surface pivot bush unit of fixed rotating shaft 7, the quantity of support frame 8 is two, and the bottom of support frame 8 is fixedly mounted
There is idler wheel 9, the quantity of idler wheel 9 is four, and four rolling 9 is uniformly divided into two groups, and two groups of idler wheels 9 are evenly distributed on two supports
The bottom of frame 8, the both ends of two support frames 8 are fixedly installed with positioning rotating shaft 10, and the outer surface of four positioning rotating shafts 10 is living
Dynamic to be socketed with fixed link 11, the equal movable sleeve in the inside of four fixed links 11 is connected to sliding block 12, is fixedly connected between two sliding blocks 12
There is connecting rod 13, the both ends of connecting rod 13 run through fixed link 11 and extend to the inside of fixed link 11 and the side with sliding block 12
It is fixedly connected, the outer surface movable sleeve of connecting rod 13 is connected to driving spring 14, and the internal activity of fixed link 11, which is socketed with to be located at, to be connected
The adjustment spring 15 of 13 outer surface of extension bar, the both ends of driving spring 14 with one end pivot bush unit of fixed link 11, two fixations
One end of bar 11 is sequentially connected by driving spring 14, the other side of sliding block 12 and the end thereof contacts of adjustment spring 15, sliding block 12
The other side be sequentially connected by the inner wall of adjustment spring 15 and fixed link 11, two support frames 8 are made just by fixed rotating shaft 7
In rotation, mating connection bar 13 is contacted with two fixed links 11, so that two support frames 8 are connected with each other, and adjustment spring 15 is made
For sliding block 12, so that the position of connecting rod 13 and fixed link 11 keeps stablizing, so that after rotating between two support frames 8
Damping is carried out to drone body 1, vibration is prevented to be transmitted in drone body 1 by support frame 8, and elastic sleeve 5 acts on
Between fixed station 2 and positioning table 4, so that the bounce that video recorder main body 6 is subject to is buffered by elastic sleeve 5, avoid recording a video
The bounce that owner's body 6 is subject to is transmitted in drone body 1, to have the function that buffering.
Working principle: after drone body 1 is landed, idler wheel 9 and ground face contact, and revolve two support frames 8 to both sides
Turn, so that two connecting rods 13 are elongated, and compress adjustment spring 15 thereon, so that drone body 1 be made slowly to drop
It is extremely minimum, it is last steady.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane landing damping device, including drone body (1), it is characterised in that: the unmanned plane sheet
Body (1) bottom is fixedly installed with fixed station (2), and the equal movable sleeve in quadrangle of the fixed station (2) is connected to bolt (3), the fixation
The quadrangle of platform (2) is connected to positioning table (4) by bolt (3) movable sleeve, and the equal pivot bush unit in outer surface of the bolt (3) is elastic
It covers (5), the bottom of the positioning table (4) is fixedly installed with video recorder main body (6), and the bottom of the drone body (1) is fixed
It is equipped with fixed rotating shaft (7), the quantity of the fixed rotating shaft (7) is two, the outer surface pivot bush unit of the fixed rotating shaft (7)
Have support frame (8), the quantity of support frame as described above (8) is two, and the bottom of support frame as described above (8) is fixedly installed with idler wheel (9), institute
The quantity for stating idler wheel (9) is four, and four idler wheels (9) are uniformly divided into two groups, and two groups of idler wheels (9) are evenly distributed on two
The bottom of support frame (8), the both ends of two support frames as described above (8) are fixedly installed with positioning rotating shaft (10), four positioning
The equal movable sleeve in outer surface of shaft (10) is connected to fixed link (11), and the equal movable sleeve in inside of four fixed links (11) is connected to cunning
Block (12) is fixedly connected with connecting rod (13) between two sliding blocks (12), the outer surface movable sleeve of the connecting rod (13)
It is connected to driving spring (14), the internal activity of the fixed link (11) is socketed with the adjustment spring positioned at connecting rod (13) outer surface
(15)。
2. a kind of unmanned plane landing damping device according to claim 1, it is characterised in that: the fixed station
(2) top of bottom and positioning table (4) is contacted with elastic sleeve (5).
3. a kind of unmanned plane landing damping device according to claim 1, it is characterised in that: support frame as described above
(8) outer surface pivot bush unit of the both ends with fixed rotating shaft (7).
4. a kind of unmanned plane landing damping device according to claim 1, it is characterised in that: the connecting rod
(13) both ends run through fixed link (11) and extend to the inside of fixed link (11) and be fixedly connected with the side of sliding block (12).
5. a kind of unmanned plane landing damping device according to claim 1, it is characterised in that: the driving spring
(14) one end of one end pivot bush unit of the both ends with fixed link (11), two fixed links (11) passes through driving spring
(14) it is sequentially connected.
6. a kind of unmanned plane landing damping device according to claim 1, it is characterised in that: the sliding block (12)
The other side and adjustment spring (15) end thereof contacts, the other side of the sliding block (12) passes through adjustment spring (15) and fixed link
(11) inner wall transmission connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821965445.3U CN209159990U (en) | 2018-11-27 | 2018-11-27 | Damping device is used in a kind of landing of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821965445.3U CN209159990U (en) | 2018-11-27 | 2018-11-27 | Damping device is used in a kind of landing of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209159990U true CN209159990U (en) | 2019-07-26 |
Family
ID=67340500
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821965445.3U Active CN209159990U (en) | 2018-11-27 | 2018-11-27 | Damping device is used in a kind of landing of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209159990U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455704A (en) * | 2020-12-07 | 2021-03-09 | 国网河北省电力有限公司雄安新区供电公司 | Single screw unmanned aerial vehicle prevent weighing down device |
-
2018
- 2018-11-27 CN CN201821965445.3U patent/CN209159990U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455704A (en) * | 2020-12-07 | 2021-03-09 | 国网河北省电力有限公司雄安新区供电公司 | Single screw unmanned aerial vehicle prevent weighing down device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106892097B (en) | A kind of vehicle-mounted unmanned aerial vehicle for road condition monitoring | |
| CN101298283B (en) | Airborne tripod head apparatus for collecting aerial information and use thereof | |
| CN103029834B (en) | Small electric unmanned helicopter aerial photography system based on front-end triaxial-type pan-tilt | |
| CN209159990U (en) | Damping device is used in a kind of landing of unmanned plane | |
| WO2019007130A1 (en) | Landing gear and unmanned aerial vehicle having same | |
| CN210852973U (en) | Unmanned aerial vehicle undercarriage takes photo by plane | |
| CN111703589A (en) | Ground simulation platform with image motion compensation for aerial camera detection | |
| CN209535498U (en) | A kind of night routing inspection unmanned plane | |
| CN211718766U (en) | Unmanned aerial vehicle aerial photography survey and drawing balancing unit | |
| CN212797299U (en) | Light weight unmanned aerial vehicle frame that falls | |
| CN211167458U (en) | Remote control unmanned aerial vehicle high altitude anti-wind anti-shake device | |
| CN218929782U (en) | Aerospace high stability unmanned aerial vehicle | |
| CN112389652B (en) | Land use changes shoots and uses unmanned aerial vehicle with picture transmission function | |
| CN107972853A (en) | Aerial photography aircraft undercarriage two level shock-damping structure | |
| CN211618110U (en) | Diaxon VTOL unmanned aerial vehicle | |
| CN115246489A (en) | Aerial photography is with balanced unmanned aerial vehicle that stabilizes | |
| CN211996125U (en) | Unmanned aerial vehicle with shock-absorbing function | |
| CN211943756U (en) | Unmanned aerial vehicle intelligent control wireless transmission structure | |
| CN114061546A (en) | Unmanned aerial vehicle aerial survey data and aerial survey method thereof | |
| CN213057492U (en) | Unmanned aerial vehicle is with frame shock-absorbing structure that plays | |
| CN215436911U (en) | Anti-seismic and anti-falling civil unmanned aerial vehicle | |
| CN216581019U (en) | Unmanned aerial vehicle with camera rotation feature | |
| CN210852972U (en) | Unmanned aerial vehicle aerial photography survey and drawing balancing unit | |
| CN216546755U (en) | Horizontal shock absorption connecting device for unmanned aerial vehicle surveying and mapping | |
| CN219468051U (en) | Remote sensing image acquisition device based on unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |