CN106586010A - Inspection device based on quadrotor unmanned aerial vehicle - Google Patents
Inspection device based on quadrotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106586010A CN106586010A CN201611012863.6A CN201611012863A CN106586010A CN 106586010 A CN106586010 A CN 106586010A CN 201611012863 A CN201611012863 A CN 201611012863A CN 106586010 A CN106586010 A CN 106586010A
- Authority
- CN
- China
- Prior art keywords
- screen
- tooth bar
- inspection device
- groove
- 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.)
- Pending
Links
- 238000007689 inspection Methods 0.000 title claims abstract description 16
- 230000004297 night vision Effects 0.000 claims description 4
- 239000004744 fabric Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract description 5
- 238000005265 energy consumption Methods 0.000 abstract description 2
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 208000027418 Wounds and injury Diseases 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 230000006378 damage Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 241001124569 Lycaenidae Species 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C1/00—Registering, indicating or recording the time of events or elapsed time, e.g. time-recorders for work people
- G07C1/20—Checking timed patrols, e.g. of watchman
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses an inspection device based on a quadrotor unmanned aerial vehicle, which comprises a body in a hollow structure, wherein a screen acquisition device is arranged in a groove, a hollow cavity is arranged above the screen acquisition device, a first drive motor is fixedly connected on an inner wall of the hollow cavity, an output end of the first drive motor is connected with a gear matched with a rack, an installation board is arranged at the bottom of the rack, two installation grooves for the screen acquisition device are arranged at the bottom of the installation board, a protection housing is arranged blow the screen acquisition device, a placement slot is formed in a side wall of the body, a supporting bar is arranged in the placement slot, a moving block is fixedly connected with the supporting bar, a second drive motor is arranged on one side of the moving block, and a second gear is fixedly installed on a side wall of the moving block. With the inspection device, energy consumption of the flying unmanned aerial vehicle is reduced, the flight time of the unmanned aerial vehicle is prolonged, the inspection efficiency is high, and the application scope is wide.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of inspection device for being based on four rotor unmanned aircrafts.
Background technology
China is vast in territory, populous, is the country that natural disaster, accident take place frequently.Particularly electric power in recent years
Emergency management and rescue task is aggravated, and the patrol task of power emergency rescue department is extremely heavy.
With the progress of science, the application of unmanned plane is more and more extensive.Unmanned plane is not limited by takeoff and anding place, can be hung down
Straight landing, hovering, can flight flexible to any one direction the features such as.
But, existing unmanned plane perform search mission when there is many deficiencies, such as unmanned plane in flight, due to
Strut is exposed to aircraft outside, increased resistance during aircraft flight, increased the power consumption of unmanned plane, reduces unmanned plane
Flying distance, simultaneously as unmanned plane camera lens is exposed below body, easily receive damage, single camera patrols and examines efficiency
Low, this makes unmanned plane that a definite limitation is subject in application.
The content of the invention
The invention aims to solve shortcoming present in prior art, and the one kind for proposing based on four rotors nobody
The inspection device of aircraft.
To achieve these goals, present invention employs following technical scheme：
A kind of inspection device for being based on four rotor unmanned aircrafts, including body, the body is hollow structure, the body
Bottom is provided with groove, and screen harvester is provided with the groove, and middle cavity is provided with above the screen harvester, described
The inwall of middle cavity is provided with tooth bar mounting groove, and tooth bar, the inwall of the middle cavity are slidably connected in the tooth bar mounting groove
On be fixedly connected with the first motor, the outfan of first motor is connected with gear, the wheel and rack phase
Matching, the bottom of the tooth bar extends to middle cavity outside, and the bottom of the tooth bar is provided with installing plate, and the installing plate top is outer
Wall vertical direction is provided with bulge-structure, and the bulge-structure horizontal direction is provided with installing hole, and the installing plate is by installing
Hole is fixedly connected with tooth bar, and the bottom of the installing plate is provided with two screen harvester mounting grooves, the screen harvester
Be fixedly installed in screen harvester mounting groove, be provided with protection shell below the screen harvester, protection shell with
The outer wall of body is flexibly connected, and the organism sidewall is provided with article putting groove, support bar, the article putting groove are provided with the article putting groove
Side wall near screen harvester is provided with spherical mounting groove, and in the spherical mounting groove spherical activity is rotatably connected to
Block, the movable block is fixedly connected with support bar, and the side of the movable block is provided with the second motor, and described second drives electricity
The outfan of machine is connected with second gear, and the second gear is fixedly installed on the side wall of movable block.
Preferably, the bottom outer wall of the body is provided with external screw thread, and the inwall of the protection shell is provided with female thread,
The body is connected with protection outer casing screw.
Preferably, the quantity of the support bar is two to four, and the support bar is symmetricly set in organism bottom, described
The bottom of strut is fixedly connected with cushion pad.
Preferably, the screen harvester is high-definition camera instrument, thermal infrared imager or night vision device.
Preferably, the side wall of the body is provided with cushion, and the cushion is bubble cloth or buffer rubber gasket.
In the present invention, two screen harvester mounting grooves can carry two such as high-definition camera instrument, thermal infrared imager or night
Depending on the screen harvester of instrument etc., make to patrol and examine in hgher efficiency more accurate, protect shell to protect screen harvester from accidental wound
Evil, unmanned plane take off it is steady after, the second motor makes support bar be retracted in article putting groove, when reducing unmanned plane during flying
Energy consumption, makes that the unmanned plane during flying time is longer, and the scope of application is wider.
Description of the drawings
Fig. 1 is a kind of structural representation of inspection device for being based on four rotor unmanned aircrafts proposed by the present invention.
In figure：1 body, 2 screen harvesters, 3 first motors, 4 gears, 5 tooth bars, 6 protection shells, 7 second are driven
Galvanic electricity machine, 8 movable blocks, 9 support bars.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than the embodiment of whole.
With reference to Fig. 1, a kind of inspection device for being based on four rotor unmanned aircrafts, including body 1, body 1 is hollow structure,
The bottom of body 1 is provided with groove, and screen harvester 2 is provided with groove, and the top of screen harvester 2 is provided with middle cavity, in
The inwall of cavity is provided with tooth bar mounting groove, and tooth bar 5 is slidably connected in tooth bar mounting groove, is fixedly connected on the inwall of middle cavity
The outfan for having the first motor 3, the first motor 3 is connected with gear 4, and gear 4 matches with tooth bar 5, the bottom of tooth bar 5
Portion extends to middle cavity outside, and the bottom of tooth bar 5 is provided with installing plate, and installing plate top exterior walls vertical direction is provided with raised knot
Structure, bulge-structure horizontal direction is provided with installing hole, and installing plate is fixedly connected by installing hole with tooth bar 5, the bottom of installing plate
Two screen harvester mounting grooves are provided with, screen harvester 2 is fixedly installed in screen harvester mounting groove, and screen is adopted
The lower section of acquisition means 2 is provided with protection shell 6, and protection shell 6 is flexibly connected with the outer wall of body 1, and the side wall of body 1 is provided with glove
Groove, is provided with support bar 9 in article putting groove, article putting groove is provided with spherical mounting groove, spherical installation near the side wall of screen harvester 2
Spherical movable block 8 is rotatably connected in groove, movable block 8 is fixedly connected with support bar 9, the side of movable block 8 is provided with the second drive
Galvanic electricity machine 7, the outfan of the second motor 7 is connected with gear, and gear is fixedly installed on the side wall of movable block 8, body 1
Bottom outer wall is provided with external screw thread, and the inwall for protecting shell 6 is provided with female thread, and body 1 is threadedly coupled with protection shell 6,
The quantity of strut 9 is two to four, and support bar 9 is symmetricly set in the bottom of body 1, and the bottom of support bar 9 is fixedly connected with buffering
Pad, screen harvester 2 is high-definition camera instrument, thermal infrared imager or night vision device, and the side wall of body 1 is provided with cushion, is buffered
Layer is bubble cloth or buffer rubber gasket, and two screen harvester mounting grooves can carry two such as high-definition camera instrument, infrared thermal imagery
The screen harvester 2 of instrument or night vision device etc., by installing hole by the Fast Installation of screen harvester 2 on installing plate, make to patrol
More accurately, after unmanned plane takes off steadily, the second motor 7 drives second gear to rotate, and makes support bar 9 be retracted to glove for inspection
In groove, when unmanned plane performs task, make the unmanned plane scope of application wider, protect shell 6 to protect screen harvester 2 from meaning
Outer injury.
Operation principle：First the screen harvester 2 of two difference in functionalitys is separately mounted to into two screen harvester peaces
In tankage, quickly it is being connected with tooth bar 5 by the projection on installing plate, after unmanned plane takes off steadily, the band of the second motor 7
Dynamic second gear is rotated, and support bar 9 is retracted in article putting groove, protects shell 6 to protect screen harvester 2 from accidental wound
Evil.
The above, the only present invention preferably specific embodiment, but protection scope of the present invention is not limited thereto,
Any those familiar with the art the invention discloses technical scope in, technology according to the present invention scheme and its
Inventive concept equivalent or change in addition, all should be included within the scope of the present invention.
Claims (5)
1. a kind of inspection device for being based on four rotor unmanned aircrafts, including body（1）, the body（1）For hollow structure, its
It is characterised by, the body（1）Bottom be provided with groove, screen harvester is provided with the groove（2）, the screen collection
Device（2）Top be provided with middle cavity, the inwall of the middle cavity is provided with tooth bar mounting groove, the tooth bar mounting groove and slides
It is connected with tooth bar（5）, on the inwall of the middle cavity the first motor is fixedly connected with（3）, first motor（3）
Outfan be connected with gear（4）, the gear（4）With tooth bar（5）Match, the tooth bar（5）Bottom extend to it is hollow
Chamber outside, the tooth bar（5）Bottom be provided with installing plate, the installing plate top exterior walls vertical direction is provided with bulge-structure,
The bulge-structure horizontal direction is provided with installing hole, and the installing plate is by installing hole and tooth bar（5）It is fixedly connected, the peace
The bottom of dress plate is provided with two screen harvester mounting grooves, the screen harvester（2）It is fixedly installed in screen collection dress
Put in mounting groove, the screen harvester（2）Lower section be provided with protection shell（6）, protect shell（6）With body（1）It is outer
Wall is flexibly connected, the body（1）Side wall is provided with article putting groove, and in the article putting groove support bar is provided with（9）, the article putting groove leans on
Nearly screen harvester（2）Side wall be provided with spherical mounting groove, be rotatably connected to spherical activity in the spherical mounting groove
Block（8）, the movable block（8）With support bar（9）It is fixedly connected, the movable block（8）Side be provided with the second motor
（7）, second motor（7）Outfan be connected with second gear, the second gear is fixedly installed in movable block（8）
Side wall on.
2. a kind of inspection device for being based on four rotor unmanned aircrafts according to claim 1, it is characterised in that the machine
Body（1）Bottom outer wall be provided with external screw thread, the protection shell（6）Inwall be provided with female thread, the body（1）With guarantor
Shield shell（6）Threaded connection.
3. a kind of inspection device for being based on four rotor unmanned aircrafts according to claim 1, it is characterised in that described
Strut（9）Quantity be two to four, the support bar（9）It is symmetricly set in body（1）Bottom, the support bar（9）Bottom
Portion is fixedly connected with cushion pad.
4. a kind of inspection device for being based on four rotor unmanned aircrafts according to claim 1, it is characterised in that described to regard
Screen harvester（2）For high-definition camera instrument, thermal infrared imager or night vision device.
5. a kind of inspection device for being based on four rotor unmanned aircrafts according to claim 1, it is characterised in that the machine
Body（1）Side wall be provided with cushion, the cushion is bubble cloth or buffer rubber gasket.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2016108086103 | 2016-09-08 | ||
| CN201610808610 | 2016-09-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106586010A true CN106586010A (en) | 2017-04-26 |
Family
ID=58591468
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611012863.6A Pending CN106586010A (en) | 2016-09-08 | 2016-11-17 | Inspection device based on quadrotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106586010A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107458616A (en) * | 2017-07-25 | 2017-12-12 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane with high-definition camera defencive function |
| CN108809473A (en) * | 2018-07-18 | 2018-11-13 | 四川厚德航通科技有限公司 | A kind of three mould of miniaturization machine-carried type navigation countermeasure set |
| CN110243346A (en) * | 2019-06-19 | 2019-09-17 | 太原理工大学 | A kind of large-scale curved molded product plotting board and mapping method |
| CN113477669A (en) * | 2021-07-07 | 2021-10-08 | 南京大学 | Mobile hydrothermal recycling high-salt high-COD (chemical oxygen demand) dangerous waste treatment device |
-
2016
- 2016-11-17 CN CN201611012863.6A patent/CN106586010A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107458616A (en) * | 2017-07-25 | 2017-12-12 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane with high-definition camera defencive function |
| CN108809473A (en) * | 2018-07-18 | 2018-11-13 | 四川厚德航通科技有限公司 | A kind of three mould of miniaturization machine-carried type navigation countermeasure set |
| CN110243346A (en) * | 2019-06-19 | 2019-09-17 | 太原理工大学 | A kind of large-scale curved molded product plotting board and mapping method |
| CN110243346B (en) * | 2019-06-19 | 2021-05-25 | 太原理工大学 | Large curved surface modeling product surveying and mapping device and method |
| CN113477669A (en) * | 2021-07-07 | 2021-10-08 | 南京大学 | Mobile hydrothermal recycling high-salt high-COD (chemical oxygen demand) dangerous waste treatment device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106586010A (en) | Inspection device based on quadrotor unmanned aerial vehicle | |
| CN102774492B (en) | A kind of small-sized depopulated helicopter fuselage | |
| CN105691613A (en) | Unmanned aerial vehicle ascending and descending smoothly and control method | |
| CN106809402A (en) | The automatic auxiliary landing system and its control method of rotor wing unmanned aerial vehicle | |
| CN106218873A (en) | The anti-protection structure of crashing of a kind of unmanned plane | |
| CN107972861B (en) | Unmanned aerial vehicle | |
| CN105083521A (en) | Airship | |
| CN205060006U (en) | Four -rotor unmanned aerial vehicle | |
| CN106927042A (en) | A kind of unmanned plane of changeable form | |
| CN207670659U (en) | A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation | |
| CN107985573A (en) | A kind of auxiliary liter of device of buoyancy for unmanned plane | |
| CN206288234U (en) | A kind of inspection device for being based on four rotor unmanned aircrafts | |
| CN207670657U (en) | A kind of plain type quadrotor drone | |
| CN107985574A (en) | A kind of auxiliary liter of unmanned plane of buoyancy | |
| CN206125411U (en) | Can be at unmanned aerial vehicle of arbitrary topography descending | |
| CN207985227U (en) | A kind of easy-to-dismount unmanned plane of taking photo by plane of camera | |
| CN205931255U (en) | Spherical unmanned aerial vehicle based on ARM | |
| CN205060007U (en) | Four portable rotor unmanned aerial vehicle | |
| CN207106869U (en) | 360 ° of monitor-type rotor wing unmanned aerial vehicles | |
| CN213768958U (en) | Vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN204623832U (en) | Communication interference protection type quadrotor | |
| CN207550500U (en) | A kind of Portable unmanned machine | |
| CN202961882U (en) | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device | |
| CN206367592U (en) | A kind of plant protection unmanned plane | |
| CN107757886B (en) | A many rotor unmanned aerial vehicle for teenagers' science popularization education |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170426 |
|
| WD01 | Invention patent application deemed withdrawn after publication |