CN206243457U - A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle - Google Patents
A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN206243457U CN206243457U CN201621317078.7U CN201621317078U CN206243457U CN 206243457 U CN206243457 U CN 206243457U CN 201621317078 U CN201621317078 U CN 201621317078U CN 206243457 U CN206243457 U CN 206243457U
- Authority
- CN
- China
- Prior art keywords
- lower section
- body cradle
- aerial vehicle
- unmanned aerial
- landing gear
- 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
- 239000006260 foam Substances 0.000 claims abstract description 8
- 230000005611 electricity Effects 0.000 claims description 2
- 230000000630 rising effect Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 abstract description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle, including undercarriage fixed plate, fixed mount is installed in the undercarriage fixed plate, the fixed mount lower section is provided with body cradle, motor control assembly is installed on the body cradle, bolt is provided with the body cradle, the body cradle lower section is provided with the hack lever that rises and falls, the hack lever lower end of rising and falling is provided with floor stand, the floor stand two ends are set with foam sleeve cushion socket, the fixed mount lower section is provided with connected unit, and the connected unit lower section is provided with head link.Beneficial effect is：The installation that the utility model passes through fixed mount, runing rest and carry frame, it is multiple functional, by the setting of undercarriage, meet various complicated landform parks condition, by the setting of motor control assembly, so that the frame body that rises and falls realizes automatic deploying and retracting so that unmanned plane realizes that 360 ° shoot without dead angle when taking photo by plane.
Description
Technical field
The utility model belongs to multi-rotor unmanned aerial vehicle equipment, and in particular to a kind of automatic deploying and retracting for multi-rotor unmanned aerial vehicle
Landing gear structure.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.Can be divided into from technical standpoint definition：Depopulated helicopter, unmanned fixed-wing aircraft,
Unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc., unmanned plane press application field, can be divided into it is military with it is civilian.It is military
Aspect, unmanned plane is divided into reconnaissance plane and target drone, and unmanned plane+sector application is the real firm need of unmanned plane.At present taking photo by plane, agriculture
The application in the fields such as industry plant protection, mapping, has greatly expanded unmanned plane purposes in itself.In addition, many model telecontrolled aircrafts
It is referred to as unmanned plane.
With continuing to develop and ripe for unmanned air vehicle technique, unmanned plane has been widely used for taking photo by plane being searched and rescued with field and leads
Domain, is equipped with high speed camera and video camera on unmanned plane, because field flight environment of vehicle is changeable, the undercarriage of unmanned plane is critically important,
Present most unmanned plane is all unmanned plane of taking photo by plane, but undercarriage can disturb camera to shoot when taking photo by plane so that camera
There is dead angle in 360 ° of shootings.The design solves these problems well so that unmanned plane more facilitates in work high above the ground.
Utility model content
The purpose of this utility model be that provide to solve the above problems it is a kind of for multi-rotor unmanned aerial vehicle from
Dynamic operation of landing gear structure.
The utility model is achieved through the following technical solutions above-mentioned purpose：
A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle, including undercarriage fixed plate, the undercarriage
Fixed mount is installed, the fixed mount lower section is provided with body cradle, motor control dress is provided with the body cradle in fixed plate
Put, bolt is provided with the body cradle, the body cradle lower section is provided with the hack lever that rises and falls, and the hack lever lower end of rising and falling is provided with
Floor stand, the floor stand two ends are set with foam sleeve cushion socket, and the fixed mount lower section is provided with connected unit, the connection
Platform lower section is provided with head link, and the head link lower section is provided with head rotating driving device, the head rotation
Drive device lower section is provided with runing rest, and the runing rest lower section is provided with carry device, is set inside the carry device
It is equipped with rotating driving device.
In said structure, by the setting to the motor control assembly parameter, when unmanned plane is parked, rise and fall frame body
Open, in flight course, the frame body that rises and falls is packed up, it is ensured that unmanned plane does not have blocking for undercarriage when taking photo by plane, and realizes 360 °
Shot without dead angle, and when unmanned plane lands, by the cooperation of the motor control assembly and the foam sleeve cushion socket
Realize buffering, it is ensured that the safe landing of unmanned plane.
In order to further improve performance, the motor driver is bolted to the body cradle lower section by described.
In order to further improve performance, the motor driver is rectangle.
In order to further improve performance, the body cradle is provided with two, is separately positioned on the connected unit both sides.
In order to further improve performance, the carry device is hollow structure.
In order to further improve performance, the undercarriage fixed plate is hinged with the following face of the fixed mount, described to be hinged
Frame is hinged with the hack lever that rises and falls, and the hack lever that rises and falls is hinged with the floor stand, the head rotating driving device with it is described
Head link is hinged.
Beneficial effect is：The installation that the utility model passes through fixed mount, runing rest and carry frame, it is multiple functional, lead to
The setting of undercarriage is crossed, meet various complicated landform parks condition, by the setting of motor control assembly so that undercarriage master
Body realizes automatic deploying and retracting so that unmanned plane realizes that 360 ° shoot without dead angle when taking photo by plane.
Brief description of the drawings
Fig. 1 is a kind of stereopsis of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle described in the utility model
Figure；
Fig. 2 is a kind of knot of automatic deploying and retracting landing gear structure floor stand for multi-rotor unmanned aerial vehicle described in the utility model
Structure schematic diagram.
1st, undercarriage fixed plate；2nd, bolt；3rd, body cradle；4th, rise and fall hack lever；5th, foam sleeve cushion socket；6th, motor control
Device；7th, runing rest；8th, carry device；9th, head rotating driving device；10th, head link；11st, connected unit；12nd, land
Frame；13rd, fixed mount；14th, rotating driving device.
Specific embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings：
As Figure 1-Figure 2, a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle, including undercarriage is fixed
Plate 1, is provided with fixed mount 13 in undercarriage fixed plate 1, the lower section of fixed mount 13 is provided with body cradle 3, electricity is provided with body cradle 3
Machine control device 6, motor control assembly 6 is used to control the folding and unfolding of hack lever 4 of rising and falling, and bolt 2, body cradle 3 are provided with body cradle 3
Lower section is provided with the hack lever 4 that rises and falls, and the lower end of hack lever 4 of rising and falling is provided with floor stand 12, and floor stand 12 is used to increase the landing of unmanned plane
Area, makes UAV Landing more steady, and the two ends of floor stand 12 are set with foam sleeve cushion socket 5, and foam sleeve cushion socket 5 is used
In vibrations when unmanned plane lands are reduced, the lower section of fixed mount 13 is provided with connected unit 11, and the lower section of connected unit 11 is provided with head company
Frame 10 is connect, the lower section of head link 10 is provided with head rotating driving device 9, and the lower section of head rotating driving device 9 is provided with rotation
Turn support 7, the lower section of runing rest 7 is provided with carry device 8, and carry device 8 is internally provided with rotating driving device 14.
In said structure, by the setting to the parameter of motor control assembly 6, when unmanned plane is parked, the frame body that rises and falls is beaten
Open, in flight course, the frame body that rises and falls is packed up, it is ensured that unmanned plane does not have blocking for undercarriage when taking photo by plane, realize 360 ° of nothings
Dead angle shoots, and when unmanned plane lands, buffering is realized by the cooperation of motor control assembly 6 and foam sleeve cushion socket 5,
Ensure the safe landing of unmanned plane.
In order to further improve performance, motor driver is fixed on the lower section of body cradle 3 by bolt 2, and motor drives dress
Rectangle is set to, body cradle 3 is provided with two, is separately positioned on the both sides of connected unit 11, carry device 8 is hollow structure, is risen and fallen
Frame fixed plate 1 is hinged with the following face of fixed mount 13, and body cradle 3 is hinged with the hack lever 4 that rises and falls, and the hack lever 4 that rises and falls cuts with scissors with floor stand 12
Connect, head rotating driving device 9 is hinged with head link 10.
General principle of the present utility model, principal character and advantage has been shown and described above.The technical staff of the industry
It should be appreciated that the utility model is not restricted to the described embodiments, the simply explanation described in above-described embodiment and specification is originally
The principle of utility model, on the premise of the utility model spirit and scope are not departed from, the utility model also has various change
And improvement, these changes and improvements are both fallen within the range of claimed the utility model.The utility model claims scope
Defined by appending claims and its effect thing.
Claims (6)
1. a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle, including undercarriage fixed plate, it is characterised in that：Institute
State and fixed mount is installed in undercarriage fixed plate, the fixed mount lower section is provided with body cradle, and electricity is provided with the body cradle
Machine control device, is provided with bolt on the body cradle, the body cradle lower section is provided with the hack lever that rises and falls, described to rise and fall under hack lever
End is provided with floor stand, and the floor stand two ends are set with foam sleeve cushion socket, and the fixed mount lower section is provided with connected unit,
The connected unit lower section is provided with head link, and the head link lower section is provided with head rotating driving device, described
Head rotating driving device lower section is provided with runing rest, and the runing rest lower section is provided with carry device, the carry dress
Put and be internally provided with rotating driving device.
2. a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：
The motor driver is bolted to the body cradle lower section by described.
3. a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle according to claim 2, it is characterised in that：
The motor driver is rectangle.
4. a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：
The body cradle is provided with two, is separately positioned on the connected unit both sides.
5. a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：
The carry device is hollow structure.
6. a kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：
The undercarriage fixed plate is hinged with the following face of the fixed mount, and the body cradle is hinged with the hack lever that rises and falls, described
The hack lever that falls is hinged with the floor stand, and the head rotating driving device is hinged with the head link.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621317078.7U CN206243457U (en) | 2016-12-02 | 2016-12-02 | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621317078.7U CN206243457U (en) | 2016-12-02 | 2016-12-02 | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206243457U true CN206243457U (en) | 2017-06-13 |
Family
ID=59003407
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621317078.7U Active CN206243457U (en) | 2016-12-02 | 2016-12-02 | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206243457U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444666A (en) * | 2017-07-25 | 2017-12-08 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of taking photo by plane with camera damping device |
| CN108609163A (en) * | 2018-04-10 | 2018-10-02 | 清远市巨劲科技有限公司 | A kind of mapping unmanned plane lifting shock bracket |
| CN108725767A (en) * | 2018-05-29 | 2018-11-02 | 钦州学院 | A kind of unmanned plane for express transportation |
| CN110979679A (en) * | 2019-12-27 | 2020-04-10 | 深圳市无限天空科技有限公司 | a drone for photography |
| CN111232190A (en) * | 2020-03-24 | 2020-06-05 | 广州扬坪机电科技有限公司 | Aerial photography unmanned aerial vehicle flight take-off and landing support equipment |
| CN111532420A (en) * | 2020-06-08 | 2020-08-14 | 珠海市双捷科技有限公司 | UAV landing gear and UAV |
| CN112977810A (en) * | 2021-04-26 | 2021-06-18 | 国网天津市电力公司 | All-weather inspection unmanned aerial vehicle and operation method |
-
2016
- 2016-12-02 CN CN201621317078.7U patent/CN206243457U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444666A (en) * | 2017-07-25 | 2017-12-08 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of taking photo by plane with camera damping device |
| CN108609163A (en) * | 2018-04-10 | 2018-10-02 | 清远市巨劲科技有限公司 | A kind of mapping unmanned plane lifting shock bracket |
| CN108725767A (en) * | 2018-05-29 | 2018-11-02 | 钦州学院 | A kind of unmanned plane for express transportation |
| CN110979679A (en) * | 2019-12-27 | 2020-04-10 | 深圳市无限天空科技有限公司 | a drone for photography |
| CN111232190A (en) * | 2020-03-24 | 2020-06-05 | 广州扬坪机电科技有限公司 | Aerial photography unmanned aerial vehicle flight take-off and landing support equipment |
| CN111532420A (en) * | 2020-06-08 | 2020-08-14 | 珠海市双捷科技有限公司 | UAV landing gear and UAV |
| CN112977810A (en) * | 2021-04-26 | 2021-06-18 | 国网天津市电力公司 | All-weather inspection unmanned aerial vehicle and operation method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206243457U (en) | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle | |
| CN205293068U (en) | Undercarriage device that can receive and release automatically | |
| CN206012932U (en) | The combination aircraft that a kind of dirigible and unmanned plane are combined | |
| CN106143889B (en) | A kind of quadrotor of undercarriage as handgrip | |
| CN103552686B (en) | A kind of compound type duct aerial reconnaissance machine people | |
| CN105691606B (en) | A kind of the unmanned plane device and control method in high cruise duration | |
| CN104260873B (en) | A kind of delta-wing aircraft | |
| CN205293106U (en) | Novel unmanned aerial vehicle nacelle mounting structure | |
| CN102556336A (en) | Wing fast unfolding device for folding-wing unmanned plane | |
| CN205239913U (en) | Top load unmanned aerial vehicle convenient to take off and land fast | |
| CN108791859B (en) | Rotor unmanned aerial vehicle who supports closely fast | |
| CN204587305U (en) | The electronic unmanned plane of multifunctional foldable eight rotor | |
| CN204173155U (en) | A kind of delta-wing aircraft | |
| CN111559499B (en) | Spherical unmanned aerial vehicle and working method | |
| CN107097949A (en) | A kind of VTOL fixed-wing unmanned plane | |
| CN205554578U (en) | High time of endurance's unmanned aerial vehicle device | |
| CN103803071B (en) | Engineering-type rotary wind type unmanned vehicle | |
| CN203428026U (en) | Small duct-type aircraft | |
| CN213168519U (en) | Air-ground dual-purpose unmanned aerial vehicle | |
| CN206307266U (en) | A kind of multi-rotor unmanned aerial vehicle double damping undercarriage | |
| CN206367581U (en) | New many rotor multi-purpose unmanned aerial vehicles | |
| CN205131661U (en) | Novel adherence unmanned aerial vehicle device | |
| CN204916172U (en) | Unmanned train's aircraft of integrated circuit debugging control system | |
| CN212313298U (en) | Small-sized solar unmanned aerial vehicle | |
| CN205293069U (en) | Full topography undercarriage device of unmanned vehicles |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |