CN107757882A - A kind of unmanned plane with rubber-tyred landing pad - Google Patents
A kind of unmanned plane with rubber-tyred landing pad Download PDFInfo
- Publication number
- CN107757882A CN107757882A CN201710876802.2A CN201710876802A CN107757882A CN 107757882 A CN107757882 A CN 107757882A CN 201710876802 A CN201710876802 A CN 201710876802A CN 107757882 A CN107757882 A CN 107757882A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- rotor
- main body
- rotating shaft
- fixed mount
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/04—Arrangement or disposition on aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/66—Convertible alighting gear; Combinations of different kinds of ground or like engaging elements
Abstract
A kind of unmanned plane with rubber-tyred landing pad, the application unmanned plane main body is box-like, the front and rear sides of the unmanned plane main body are respectively provided with a rotor support, rotor motor is installed in the outboard end of the rotor support, each corresponding 24 rotor blades of rotor motor, the rotor blade is arranged on the rotating shaft outer wall of rotor motor, the rotor blade angularly around corresponding rotor motor rotating shaft center line one week, the unmanned plane main body both sides are respectively provided with a side fixed mount, the side fixed mount is connected with rotating shaft, the outboard end of the rotating shaft of the side fixed mount is provided with buffering wheel, respectively there is a reverse V-shaped frame unmanned plane main body both sides, the connection end of the reverse V-shaped frame is sleeved on the middle part of the rotating shaft of side fixed mount.The present invention provides a kind of unmanned plane with rubber-tyred landing pad, innovative that wheeled landing and support landing be combined with each other, and such combination, which can be greatly reduced caused by unmanned plane landing, to be impacted, and then improves the service life of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of unmanned plane for landing with rubber-tyred and padding.
Background technology
Modern science and technology is constantly improving, and unmanned air vehicle technique development is extremely rapid, and landing is in the unmanned plane course of work
Very big technical barrier, because can produce certain impact in its descent, this impact can be to the body of unmanned plane
Certain damage is caused, and then reduces the life-span of unmanned plane, traditional rotary wind type unmanned plane is using building in its descent
Pad or damping sucker are landed, but certain damage are still resulted in actual mechanical process, and wheeled landing then without
Problem above.
The content of the invention
In order to solve above-mentioned problem, the present invention provides a kind of unmanned plane with rubber-tyred landing pad, innovative
Wheeled landing and support landing are be combined with each other, such combination, which can be greatly reduced caused by unmanned plane landing, to be impacted, and then
The service life of unmanned plane is improved, for up to this purpose, the present invention provides a kind of unmanned plane with rubber-tyred landing pad, including nobody
Owner's body, rotor support, rotor motor, rotor blade, side fixed mount, buffering wheel and reverse V-shaped frame, the unmanned plane main body are box
Shape, the front and rear sides of the unmanned plane main body are respectively provided with a rotor support, installed in the outboard end of the rotor support
There is rotor motor, each rotor motor corresponds to 2-4 rotor blade, and the rotor blade is arranged on outside the rotating shaft of rotor motor
Wall, the rotor blade angularly around corresponding rotor motor rotating shaft center line one week, the unmanned plane main body both sides are respectively pacified
Equipped with a side fixed mount, the side fixed mount is connected with rotating shaft, and the outboard end of the rotating shaft of the side fixed mount is provided with buffering wheel,
Respectively there is a reverse V-shaped frame unmanned plane main body both sides, and the connection end of the reverse V-shaped frame is sleeved in the rotating shaft of side fixed mount
Portion.
Further improvement of the present invention, the front and rear side of the unmanned plane main body are installed with infrared inductor, set sense
Device is answered to be monitored with surrounding environment.
A pair of motor fixing frames are arranged at further improvement of the present invention, the bottom of the unmanned plane main body, and the motor is fixed
Frame is installed with camera motor, and the rotating shaft of the camera motor is arranged on movable camera both sides, and bottom sets monitoring
Camera can expand monitoring range.
The present invention provides a kind of unmanned plane with rubber-tyred landing pad, and the unmanned plane is mainly used in rotor wing unmanned aerial vehicle, and it drops
Fall mechanism to design by the way of support is combined using wheeled, design buffering wheel in former V-type landing gear, in such descent
Buffering wheel first can contact with each other with ground, and so as to discharge substantial amounts of impact, landing gear contacts with each other with ground afterwards, sets above
The application original creation is calculated as, significantly reduces after and is impacted caused by unmanned plane landing, improve the service life of unmanned plane.
Brief description of the drawings
Fig. 1 is schematic diagram of the present invention；
Component in figure is：
1st, unmanned plane main body；2nd, rotor support；3rd, rotor motor；4th, rotor blade；5th, infrared inductor；6th, movable camera；
7th, camera motor；8th, motor fixing frame；9th, side fixed mount；10th, buffering wheel；11st, reverse V-shaped frame.
Embodiment
The present invention is described in further detail with embodiment below in conjunction with the accompanying drawings：
The present invention provides a kind of unmanned plane with rubber-tyred landing pad, innovative by wheeled landing and support landing mutually knot
Close, such combination, which can be greatly reduced caused by unmanned plane landing, to be impacted, and then improves the service life of unmanned plane.
The application provides a kind of embodiment.A kind of unmanned plane with rubber-tyred landing pad as shown in Figure 1, including unmanned plane
Main body 1, rotor support 2, rotor motor 3, rotor blade 4, side fixed mount 9, buffering wheel 10 and reverse V-shaped frame 11, the unmanned plane
For main body 1 to be box-like, the front and rear sides of the unmanned plane main body 1 are respectively provided with a rotor support 2, the rotor support 2 it is outer
Rotor motor 3, each rotor motor 3 corresponding 2-4 rotor blade 4 are installed, the rotor blade 4 is arranged on rotation on side end
The rotating shaft outer wall of wing motor 3, the rotor blade 4 angularly around corresponding rotor motor 3 rotating shaft center line one week, the nothing
The man-machine both sides of main body 1 are respectively provided with a side fixed mount 9, and the side fixed mount 9 is connected with rotating shaft, the rotating shaft of the side fixed mount 9
Outboard end buffering wheel 10 is installed, respectively there are a reverse V-shaped frame 11, the company of the reverse V-shaped frame 11 in the both sides of unmanned plane main body 1
Connect the middle part that end is sleeved on the rotating shaft of side fixed mount 9.
A kind of specific embodiment of the application offer, a kind of unmanned plane with rubber-tyred landing pad, including unmanned plane main body 1,
Rotor support 2, rotor motor 3, rotor blade 4, side fixed mount 9, buffering wheel 10 and reverse V-shaped frame 11, the unmanned plane main body 1 are
Box-like, the front and rear side of the unmanned plane main body is installed with infrared inductor, sets inductor to be supervised with surrounding environment
Control, the front and rear sides of the unmanned plane main body 1 are respectively provided with a rotor support 2, pacified in the outboard end of the rotor support 2
Equipped with rotor motor 3, the corresponding 2-4 rotor blade 4 of each rotor motor 3, the rotor blade 4 is arranged on rotor motor 3
Rotating shaft outer wall, the rotor blade 4 angularly around corresponding rotor motor 3 rotating shaft center line one week, the unmanned plane main body 1
Both sides are respectively provided with a side fixed mount 9, and the side fixed mount 9 is connected with rotating shaft, the outboard end peace of the rotating shaft of the side fixed mount 9
Equipped with buffering wheel 10, respectively there is a reverse V-shaped frame 11 both sides of unmanned plane main body 1, and the connection end of the reverse V-shaped frame 11 is sleeved on
A pair of motor fixing frames are arranged at the middle part of the rotating shaft of side fixed mount 9, the bottom of the unmanned plane main body, and the motor fixing frame is fixed
Camera motor is installed, the rotating shaft of the camera motor is arranged on movable camera both sides, and bottom sets monitoring camera
Monitoring range can be expanded.
The above described is only a preferred embodiment of the present invention, it is not the limit for making any other form to the present invention
System, and any modification made according to technical spirit of the invention or equivalent variations, still fall within present invention model claimed
Enclose.
Claims (3)
1. a kind of unmanned plane with rubber-tyred landing pad, including unmanned plane main body（1）, rotor support（2）, rotor motor（3）, rotation
Wing blade（4）, side fixed mount（9）, buffering wheel（10）With reverse V-shaped frame（11）, it is characterised in that：The unmanned plane main body（1）For
It is box-like, the unmanned plane main body（1）Front and rear sides one rotor support is respectively installed（2）, the rotor support（2）Outside
Rotor motor is installed on end（3）, each rotor motor（3）Corresponding 2-4 rotor blade（4）, the rotor blade（4）Peace
Mounted in rotor motor（3）Rotating shaft outer wall, the rotor blade（4）Angularly around corresponding rotor motor（3）Rotating shaft center
Line one week, the unmanned plane main body（1）Both sides are respectively provided with a side fixed mount（9）, the side fixed mount（9）It is connected with rotating shaft,
The side fixed mount（9）The outboard end of rotating shaft buffering wheel is installed（10）, the unmanned plane main body（1）Both sides respectively have one to fall
V-type frame（11）, the reverse V-shaped frame（11）Connection end be sleeved on side fixed mount（9）Rotating shaft middle part.
A kind of 2. unmanned plane with rubber-tyred landing pad according to claim 1, it is characterised in that：The unmanned plane main body
（1）Front and rear side be installed with infrared inductor（5）.
A kind of 3. unmanned plane with rubber-tyred landing pad according to claim 1, it is characterised in that：The unmanned plane main body
（1）Bottom have a pair of motor fixing frames（8）, the motor fixing frame（8）It is installed with camera motor（7）, it is described to take the photograph
As head motor（7）Rotating shaft be arranged on movable camera（6）Both sides.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710876802.2A CN107757882A (en) | 2017-09-25 | 2017-09-25 | A kind of unmanned plane with rubber-tyred landing pad |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710876802.2A CN107757882A (en) | 2017-09-25 | 2017-09-25 | A kind of unmanned plane with rubber-tyred landing pad |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107757882A true CN107757882A (en) | 2018-03-06 |
Family
ID=61267556
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710876802.2A Pending CN107757882A (en) | 2017-09-25 | 2017-09-25 | A kind of unmanned plane with rubber-tyred landing pad |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107757882A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205022905U (en) * | 2015-08-14 | 2016-02-10 | 湖北易瓦特科技股份有限公司 | Undercarriage is telescopic flight equipment |
| CN106542084A (en) * | 2016-10-17 | 2017-03-29 | 合肥齐飞信息技术有限公司 | A kind of anti-crash formula of Autonomous Control falling speed is taken photo by plane unmanned plane |
| CN106828889A (en) * | 2017-01-19 | 2017-06-13 | 福州大学 | Unmanned plane protection device and its method of work |
-
2017
- 2017-09-25 CN CN201710876802.2A patent/CN107757882A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205022905U (en) * | 2015-08-14 | 2016-02-10 | 湖北易瓦特科技股份有限公司 | Undercarriage is telescopic flight equipment |
| CN106542084A (en) * | 2016-10-17 | 2017-03-29 | 合肥齐飞信息技术有限公司 | A kind of anti-crash formula of Autonomous Control falling speed is taken photo by plane unmanned plane |
| CN106828889A (en) * | 2017-01-19 | 2017-06-13 | 福州大学 | Unmanned plane protection device and its method of work |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180306 |