CN107719653A - A kind of monitoring unmanned plane - Google Patents
A kind of monitoring unmanned plane Download PDFInfo
- Publication number
- CN107719653A CN107719653A CN201710877278.0A CN201710877278A CN107719653A CN 107719653 A CN107719653 A CN 107719653A CN 201710877278 A CN201710877278 A CN 201710877278A CN 107719653 A CN107719653 A CN 107719653A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- rotor
- motor
- camera
- main body
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
A kind of monitoring unmanned plane, the application unmanned plane main body is box-like, the front and rear sides of unmanned plane main body are respectively provided with a rotor support, rotor motor is installed in the outboard end of rotor support, each corresponding 24 rotor blades of rotor motor, rotor blade is arranged on the rotating shaft outer wall of rotor motor, rotor blade angularly around corresponding rotor motor rotating shaft center line one week, a pair of motor fixing frames are arranged at the bottom of unmanned plane main body, motor fixing frame is installed with camera motor, the rotating shaft of camera motor is arranged on movable camera both sides, a side inductor is respectively installed on front side of the support of the both sides of the camera of movable camera, unmanned plane main body both sides are respectively provided with a lateral connector bar, the end of lateral connector bar is connected with inverted T shaped frame top.The application uav bottom can be with Full-automatic camera shooting head, and landing gear designs in both sides, do not influence so to land, and landing gear bottom end has beam, can be very good to reduce the impact that landing is brought.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of monitoring unmanned plane.
Background technology
Constantly carried out with social, science and technology continues to develop, and the continuous progress of unmanned air vehicle technique, increasing field starts
Using unmanned plane, wherein detection field belongs to the extremely rapid unmanned plane of development and mainly led to one of field, monitoring unmanned plane
The camera for crossing uav bottom is fixed what route operation was realized, and the prison at no dead angle can be realized under certain route planning
Control, because its bottom is provided with large-scale camera, generally requires voluntarily to land again therefore landing stability is bigger ask
Topic.
The content of the invention
In order to solve above-mentioned problem, the present invention provides a kind of monitoring unmanned plane, and the uav bottom can be complete
Automatic camera head, landing gear designs in both sides, does not influence so to land, and landing gear bottom end has beam, can be very
The impact that good reduction landing is brought, for up to this purpose, the present invention provides a kind of monitoring unmanned plane, including unmanned plane main body,
Rotor support, rotor motor, rotor blade, movable camera, camera motor, motor fixing frame, side inductor, lateral connector bar
With inverted T shaped frame, the unmanned plane main body is box-like, and the front and rear sides of the unmanned plane main body are respectively provided with a rotor support,
Rotor motor is installed, each rotor motor corresponds to 2-4 rotor blade, the rotor in the outboard end of the rotor support
Blade is arranged on the rotating shaft outer wall of rotor motor, and the rotor blade is angularly around the center line one for the rotating shaft for corresponding to rotor motor
A pair of motor fixing frames are arranged at week, the bottom of the unmanned plane main body, and the motor fixing frame is installed with camera motor, institute
The rotating shaft for stating camera motor is arranged on movable camera both sides, the support front side of the both sides of the camera of the movable camera
One side inductor is respectively installed, the unmanned plane main body both sides are respectively provided with a lateral connector bar, the end of the lateral connector bar
Portion is connected with inverted T shaped frame top.
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.
There are a pair of damping suckers further improvement of the present invention, the end of the base of the inverted T shaped frame, set damping sucker
It can reduce and be impacted caused by landing.
The present invention provides a kind of monitoring unmanned plane, improves and obtains on the basis of traditional unmanned plane, drop can be greatly reduced
Fall caused vibrations, mitigate vibrations and the longevity is used on influence caused by camera, indirect raising unmanned plane and its camera
Life, used particularly suitable for monitoring 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 inductor；10th, lateral connector bar；11st, inverted T shaped frame；12nd, damping sucker.
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 monitoring unmanned plane, and the uav bottom can be with Full-automatic camera shooting head, and landing gear is designed in both sides,
Do not influence so to land, and landing gear bottom end has beam, can be very good to reduce the impact that landing is brought.
The application provides a kind of embodiment.A kind of monitoring unmanned plane as shown in Figure 1, including unmanned plane main body 1, rotor
Support 2, rotor motor 3, rotor blade 4, movable camera 6, camera motor 7, motor fixing frame 8, side inductor 9, side connect
Extension bar 10 and inverted T shaped frame 11, the unmanned plane main body 1 are box-like, and the front and rear sides of the unmanned plane main body 1 are respectively provided with one
Rotor support 2, rotor motor 3, each rotor motor 3 corresponding 2-4 rotor are installed in the outboard end of the rotor support 2
Blade 4, the rotor blade 4 are arranged on the rotating shaft outer wall of rotor motor 3, and the rotor blade 4 is angularly around corresponding rotor electricity
A pair of motor fixing frames 8, the motor fixing frame 8 are arranged at the center line of the rotating shaft of machine 3 one week, the bottom of the unmanned plane main body 1
Camera motor 7 is installed with, the rotating shaft of the camera motor 7 is arranged on the both sides of movable camera 6, the activity shooting
A side inductor 9 is respectively installed on front side of the support of the both sides of first 6 camera, the both sides of unmanned plane main body 1 are respectively provided with
One lateral connector bar 10, the end of the lateral connector bar 10 are connected with the inverted T shaped top of frame 11.
The application provides a kind of specific embodiment, a kind of monitoring unmanned plane, including unmanned plane main body 1, rotor support 2,
Rotor motor 3, rotor blade 4, movable camera 6, camera motor 7, motor fixing frame 8, side inductor 9, lateral connector bar 10
With inverted T shaped frame 11, the unmanned plane main body 1 is box-like, and the front and rear side of the unmanned plane main body is installed with infrared inductor,
Inductor is set to be monitored with surrounding environment, the front and rear sides of the unmanned plane main body 1 are respectively provided with a rotor support
2, rotor motor 3, the corresponding 2-4 rotor blade 4 of each rotor motor 3, institute are installed in the outboard end of the rotor support 2
The rotating shaft outer wall that rotor blade 4 is arranged on rotor motor 3 is stated, the rotor blade 4 is angularly around the rotating shaft of corresponding rotor motor 3
Center line one week, a pair of motor fixing frames 8 are arranged at the bottom of the unmanned plane main body 1, and the motor fixing frame 8 is installed with
Camera motor 7, the rotating shaft of the camera motor 7 are arranged on the both sides of movable camera 6, the shooting of the movable camera 6
One side inductor 9 is respectively installed, the both sides of unmanned plane main body 1 are respectively provided with a side connection on front side of the support of the both sides of head
Bar 10, the end of the lateral connector bar 10 are connected with the inverted T shaped top of frame 11, and the end of the base of the inverted T shaped frame, which has a pair, to be subtracted
Sucker is shaken, sets damping sucker to reduce caused by landing and impacts.
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 monitoring unmanned plane, including unmanned plane main body（1）, rotor support（2）, rotor motor（3）, rotor blade（4）、
Movable camera（6）, camera motor（7）, motor fixing frame（8）, side inductor（9）, lateral connector bar（10）With inverted T shaped frame
（11）, it is characterised in that：The unmanned plane main body（1）To be box-like, the unmanned plane main body（1）Front and rear sides be respectively provided with one
Individual rotor support（2）, the rotor support（2）Outboard end on rotor motor is installed（3）, each rotor motor（3）It is right
Answer 2-4 rotor blade（4）, the rotor blade（4）Installed 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）Bottom there are a pair of motors to consolidate
Determine frame（8）, the motor fixing frame（8）It is installed with camera motor（7）, the camera motor（7）Rotating shaft installation
In movable camera（6）Both sides, the movable camera（6）Camera both sides support on front side of the sense of side is respectively installed
Answer device（9）, the unmanned plane main body（1）Both sides are respectively provided with a lateral connector bar（10）, the lateral connector bar（10）End
With inverted T shaped frame（11）Top is connected.
2. one kind monitoring unmanned plane according to claim 1, it is characterised in that：The unmanned plane main body（1）It is front and rear
Side is installed with infrared inductor（5）.
3. one kind monitoring unmanned plane according to claim 1, it is characterised in that：The inverted T shaped frame（11）Base
There are a pair of damping suckers end（12）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710877278.0A CN107719653A (en) | 2017-09-25 | 2017-09-25 | A kind of monitoring unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710877278.0A CN107719653A (en) | 2017-09-25 | 2017-09-25 | A kind of monitoring unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107719653A true CN107719653A (en) | 2018-02-23 |
Family
ID=61207917
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710877278.0A Pending CN107719653A (en) | 2017-09-25 | 2017-09-25 | A kind of monitoring unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107719653A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
| CN204250368U (en) * | 2014-11-14 | 2015-04-08 | 北华航天工业学院 | A kind of mini quadrotor of Intelligent aerial photography |
| CN105015767A (en) * | 2015-07-09 | 2015-11-04 | 湖北省机电研究设计院股份公司 | Multi-rotor type unmanned aircraft system with fire detecting function |
| CN204822090U (en) * | 2015-06-23 | 2015-12-02 | 深圳飞豹航天航空科技有限公司 | Unmanned aerial vehicle |
| CN204937509U (en) * | 2015-09-17 | 2016-01-06 | 彭家成 | A kind of invigilator's unmanned plane |
| CN106114814A (en) * | 2016-07-22 | 2016-11-16 | 四川克瑞斯航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN205837224U (en) * | 2016-07-15 | 2016-12-28 | 张宇川 | A kind of scalable is taken photo by plane unmanned plane |
| CN106379121A (en) * | 2016-11-28 | 2017-02-08 | 江苏洛尧智慧通信科技有限公司 | Air-ground synchronous monitoring robot |
-
2017
- 2017-09-25 CN CN201710877278.0A patent/CN107719653A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204250368U (en) * | 2014-11-14 | 2015-04-08 | 北华航天工业学院 | A kind of mini quadrotor of Intelligent aerial photography |
| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
| CN204822090U (en) * | 2015-06-23 | 2015-12-02 | 深圳飞豹航天航空科技有限公司 | Unmanned aerial vehicle |
| CN105015767A (en) * | 2015-07-09 | 2015-11-04 | 湖北省机电研究设计院股份公司 | Multi-rotor type unmanned aircraft system with fire detecting function |
| CN204937509U (en) * | 2015-09-17 | 2016-01-06 | 彭家成 | A kind of invigilator's unmanned plane |
| CN205837224U (en) * | 2016-07-15 | 2016-12-28 | 张宇川 | A kind of scalable is taken photo by plane unmanned plane |
| CN106114814A (en) * | 2016-07-22 | 2016-11-16 | 四川克瑞斯航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN106379121A (en) * | 2016-11-28 | 2017-02-08 | 江苏洛尧智慧通信科技有限公司 | Air-ground synchronous monitoring robot |
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| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180223 |
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