CN108263628A - A kind of six axis unmanned planes - Google Patents
A kind of six axis unmanned planes Download PDFInfo
- Publication number
- CN108263628A CN108263628A CN201711425562.0A CN201711425562A CN108263628A CN 108263628 A CN108263628 A CN 108263628A CN 201711425562 A CN201711425562 A CN 201711425562A CN 108263628 A CN108263628 A CN 108263628A
- Authority
- CN
- China
- Prior art keywords
- camera
- roll
- axle bed
- axis
- installing plate
- 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
- 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
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- 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
- B64D43/00—Arrangements or adaptations of instruments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Abstract
The present invention relates to the six axis unmanned planes of one kind in aviation UAV field, including fuselage, CCD camera assembly and the circuit control system on fuselage, the CCD camera assembly includes infrared thermal imaging camera and holder camera, the edge of machine body base extends to form the horn more than six roots of sensation outward, the end of horn is provided with the motor sub-assembly of rotor, the antishock device for installing camera holder is equipped in the lower section of machine body base, the antishock device includes mounting bracket and installing plate, shock-absorbing ball is equipped between installing plate and mounting bracket, rotary shaft has been extended downwardly in installing plate, the middle-end of rotary shaft and end are connected separately with the first roll axis and the second roll axis, holder camera and infrared thermal imaging camera are separately mounted on the first roll axle bed and the second roll axle bed.The configuration of the present invention is simple, flight stability, shockproof effect are good, can carry out shooting in the weather of night or gray haze and nor affect on its shooting effect.
Description
Technical field
The present invention relates to aviation UAV field, more particularly to a kind of six axis unmanned planes.
Background technology
Unmanned plane is the unmanned aircraft manipulated using radio robot and the program provided for oneself control, and unmanned plane can
To complete camera shooting in severe, even dangerous environment, detection, scout, search and rescue etc. a series of activity, it can be carried more
Advanced technical equipment, such as high definition camera device, the radar for penetrating leaf, the miniature spectrometer device that chemical capacity is provided,
So as to complete multiple special and significant tasks.
Traditional unmanned plane because itself light structure, need not be manned, can be completed in severe, even dangerous environment
The activities such as camera shooting, detection, and it is widely used in the field of taking photo by plane.In general, the video camera taken photo by plane is controlled by the photographer on ground, to
Satisfactory image is obtained, still, is had at least the following problems during taking photo by plane：1st, when shooting airflow influence or nobody
Situations such as machine fuselage rolls, vibration can all influence the effect of capture apparatus；It 2nd, also can be direct in the shooting of the weather of night or gray haze
It influences the effect of capture apparatus or even normal photographing can not be carried out.
Invention content
Present invention aim to address disadvantages described above, provide a kind of six axis unmanned planes, simple in structure, shooting is stablized, and is fitted
It is used in night.
The purpose of the present invention is what is be accomplished by the following way：
A kind of six axis unmanned planes, including fuselage, CCD camera assembly and the circuit control system on fuselage, the camera shooting
Head assembly includes infrared thermal imaging camera and holder camera, and the fuselage includes hood and machine body base, the edge of machine body base
The horn more than six roots of sensation is extended to form outward, and the end of horn is provided with the motor sub-assembly of rotor, the circuit control system
Including master control borad, flight controller, CCD camera assembly, supplying cell and GPS, flight controller, CCD camera assembly, power supply electricity
Pond, GPS and motor sub-assembly are connect with master control borad, which is also associated with data link and electron speed regulator, each horse
It is all connected with up to component there are one the electron speed regulator for being used to adjust rotating speed, is equipped with that camera is installed in the lower section of machine body base
The antishock device of holder, the antishock device include mounting bracket and installing plate, installing plate be detachably mounted to mounting bracket it
On, it is equipped with shock-absorbing ball between installing plate and mounting bracket, the edge of mounting bracket is set there are four the connecting portion extended outward,
Movable bearing support is connected on each connecting portion, movable bearing support is structure of right angle tyoe, one end right-angle side and mounting bracket activity
Connection, the other end connect fixation with horn, have extended downwardly rotary shaft in installing plate, the middle-end of rotary shaft and end connect respectively
There are the first roll axis and the second roll axis, and the first roll axle bed and second are arranged on the first roll axis and the second roll axis
Roll axle bed, the first roll axle bed and the second roll axle bed take the shape of the letter U structure, and holder camera and infrared thermal imaging camera are installed respectively
On the first roll axle bed and the second roll axle bed.
Preferably：The bottom of the machine body base be equipped with support device, the support device include support base and with branch
The support foot rest of seat connection is supportted, the bottom of support base extends down equipped with symmetrical two support foot rests, which is in three
Angular structure is equipped between support foot rest and support base and serves motor, motor is served to be connect by lead with master control borad.
Preferably：The horn is equipped with the GPS antenna up extended, and lower part and the movable bearing support of GPS antenna pass through
Screw is fixed, and GPS antenna is connect by conducting wire with master control borad.
Preferably：The edge of the hood, which extends outwardly, to be set there are four connecting portion, in the inside of four connecting portions
Equipped with magnetite one, the four corners of the pedestal are equipped with the magnetite two mutually adsorbed with magnetite one, make the two attracting solid by magnetic force
It is fixed.
Preferably：The hood is made by full carbon fiber.
It is had the beneficial effect that caused by the present invention：
1) the configuration of the present invention is simple, flight stability, be easily manipulated, have additional antishock device, utilize the damping side of shock-absorbing ball
Formula can eliminate the most low-frequency vibration of unmanned plane generation, enhance shooting effect；
2) compared with prior art, increasing on the antishock device of the present invention has infrared thermal imaging camera, can be at night
Or the weather of gray haze carries out shooting and nor affects on its shooting effect.
Description of the drawings
Fig. 1 is the overall structure diagram of the embodiment of the present invention；
In figure, 1 is infrared thermal imaging camera, and 2 be holder camera, and 3 be horn, and 4 be rotor, and 5 be motor sub-assembly, and 6 be peace
Stent is filled, 7 be installing plate, and 8 be shock-absorbing ball, and 9 be movable bearing support, and 10 be rotary shaft, and 11 be the first roll axle bed, and 12 is horizontal for second
Roller shaft seat, 13 be support foot rest, and 14 be GPS antenna, and 15 be hood.
Specific embodiment
The present invention is described in further detail with specific embodiment below in conjunction with the accompanying drawings.
The present embodiment, with reference to Fig. 1, embodiment structure includes fuselage, CCD camera assembly and the circuit control on fuselage
System processed, the CCD camera assembly include infrared thermal imaging camera 1 and holder camera 2, and the fuselage includes hood 15 and fuselage
Pedestal, the hood of the present embodiment are integrally made of full carbon fiber, and the edge of machine body base extends to form more than the six roots of sensation outward
Horn 3, the end of horn 3 are provided with the motor sub-assembly 5 of rotor 4.
The circuit control system of the present embodiment includes master control borad, flight controller, CCD camera assembly, supplying cell and GPS,
Flight controller, CCD camera assembly, supplying cell, GPS and motor sub-assembly 5 are connect with master control borad, which is also associated with
Data link and electron speed regulator, each motor sub-assembly 5 are all connected with that there are one for adjusting the electron speed regulator of rotating speed.
The antishock device for installing camera holder is equipped in the lower section of machine body base, which includes installation branch
Frame 6 and installing plate 7, installing plate 7 are detachably mounted on mounting bracket 6, are equipped between installing plate 7 and mounting bracket 6
Shock-absorbing ball 8, the edge of mounting bracket 6 are set there are four the connecting portion extended outward, and movable branch is connected on each connecting portion
Seat 9, movable bearing support 9 are structure of right angle tyoe, and one end right-angle side is flexibly connected with mounting bracket 6, and the other end connect solid with horn 3
It is fixed, rotary shaft 10 is extended downwardly in installing plate 7, the middle-end of rotary shaft 10 and end are connected separately with the first roll axis and second
Roll axis, and the first roll axle bed 11 and the second roll axle bed 12 are arranged on the first roll axis and the second roll axis, first
11 and second roll axle bed 12 of roll axle bed takes the shape of the letter U structure, and holder camera 2 and infrared thermal imaging camera 1 are separately mounted to first
On 11 and second roll axle bed 12 of roll axle bed.
In addition, the bottom of the machine body base is equipped with support device, which includes support base and connects with support base
The support foot rest 13 connect, the bottom of support base extend down equipped with symmetrical two support foot rests 13, which is in three
Angular structure is equipped between support foot rest 13 and support base and serves motor, motor is served to be connect by lead with master control borad.The machine
Arm 3 is equipped with the GPS antenna 14 up extended, and lower part and the movable bearing support 9 of GPS antenna 14 are screwed, GPS antenna 14
It is connect by conducting wire with master control borad.
In order to be more convenient dismounting, extend outwardly at the edge of hood 15 and set there are four connecting portion, in four connecting portions
Inside be equipped with magnetite one, the four corners of the pedestal are equipped with the magnetite two mutually adsorbed with magnetite one, both make to pass through magnetic force
Attracting fixation.The configuration of the present invention is simple, is easily manipulated flight stability, has additional antishock device, utilizes the damping side of shock-absorbing ball 8
Formula can eliminate the most low-frequency vibration of unmanned plane generation, enhance shooting effect；Compared with prior art, the present invention's
Increasing on antishock device has infrared thermal imaging camera 1, can carry out shooting in the weather of night or gray haze and nor affect on its shooting
Effect.
The above content is combine specific preferred embodiment further description made for the present invention, it is impossible to assert this
The specific implementation of invention is confined to these explanations.For those of ordinary skill in the art to which the present invention belongs, not
Under the premise of being detached from present inventive concept, several simple deduction or replace can also be made, are regarded as protection scope of the present invention.
Claims (5)
1. a kind of six axis unmanned planes, including fuselage, CCD camera assembly and the circuit control system on fuselage, the camera
Component includes infrared thermal imaging camera and holder camera, and the fuselage includes hood and machine body base, and the edge of machine body base is past
The outer horn extended to form more than the six roots of sensation, the end of horn is provided with the motor sub-assembly of rotor, the circuit control system packet
Include master control borad, flight controller, CCD camera assembly, supplying cell and GPS, flight controller, CCD camera assembly, supplying cell,
GPS and motor sub-assembly are connect with master control borad, which is also associated with data link and electron speed regulator, each groups of motors
Part is all connected with that there are one for adjusting the electron speed regulator of rotating speed, it is characterised in that：It is equipped with to pacify in the lower section of machine body base
The antishock device of camera holder is filled, which includes mounting bracket and installing plate, and installing plate is detachably mounted to pacify
It fills on stent, is equipped with shock-absorbing ball between installing plate and mounting bracket, the edge of mounting bracket sets that there are four extend outward
Connecting portion, is connected with movable bearing support on each connecting portion, and movable bearing support is structure of right angle tyoe, one end right-angle side and installation
Stent is flexibly connected, and the other end connect fixation with horn, rotary shaft, the middle-end of rotary shaft and end have been extended downwardly in installing plate
The first roll axis and the second roll axis are connected separately with, and the first roll axis is arranged on the first roll axis and the second roll axis
Seat and the second roll axle bed, the first roll axle bed and the second roll axle bed take the shape of the letter U structure, holder camera and infrared thermal imaging camera
It is separately mounted on the first roll axle bed and the second roll axle bed.
2. a kind of six axis unmanned plane according to claim 1, it is characterised in that：The bottom of the machine body base is equipped with support
Device, the support device include support base and the support foot rest that connect with support base, and the bottom of support base extends down to be equipped with pair
Two support foot rests claimed, support foot rest structure triangular in shape are equipped between support foot rest and support base and serve motor, serve
Motor is connect by lead with master control borad.
3. according to a kind of six axis unmanned plane described in claims 1 or 2, it is characterised in that：The horn, which is equipped with, up to be extended
GPS antenna, lower part and the movable bearing support of GPS antenna be screwed, and GPS antenna is connect by conducting wire with master control borad.
4. a kind of six axis unmanned plane according to claim 3, it is characterised in that：The edge of the hood, which extends outwardly, to be equipped with
Four connecting portions are equipped with magnetite one in the inside of four connecting portions, and the four corners of the pedestal are equipped with mutually inhales with magnetite one
Attached magnetite two makes the two by the attracting fixation of magnetic force.
5. a kind of six axis unmanned plane according to claim 4, it is characterised in that：The hood is made by full carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711425562.0A CN108263628A (en) | 2017-12-25 | 2017-12-25 | A kind of six axis unmanned planes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711425562.0A CN108263628A (en) | 2017-12-25 | 2017-12-25 | A kind of six axis unmanned planes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108263628A true CN108263628A (en) | 2018-07-10 |
Family
ID=62772445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711425562.0A Pending CN108263628A (en) | 2017-12-25 | 2017-12-25 | A kind of six axis unmanned planes |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108263628A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109178311A (en) * | 2018-09-27 | 2019-01-11 | 广州市华科尔科技股份有限公司 | A kind of double holder unmanned planes that shooting visual angle is wide |
| WO2020019350A1 (en) * | 2018-07-27 | 2020-01-30 | 深圳市大疆创新科技有限公司 | Control method and apparatus for unmanned aerial vehicle and unmanned aerial vehicle |
-
2017
- 2017-12-25 CN CN201711425562.0A patent/CN108263628A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020019350A1 (en) * | 2018-07-27 | 2020-01-30 | 深圳市大疆创新科技有限公司 | Control method and apparatus for unmanned aerial vehicle and unmanned aerial vehicle |
| CN109178311A (en) * | 2018-09-27 | 2019-01-11 | 广州市华科尔科技股份有限公司 | A kind of double holder unmanned planes that shooting visual angle is wide |
| CN109178311B (en) * | 2018-09-27 | 2024-02-20 | 广州市华科尔科技股份有限公司 | Shooting visual angle is wide two cloud platform unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180710 |