CN207670659U - A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation - Google Patents
A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation Download PDFInfo
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- CN207670659U CN207670659U CN201721754322.0U CN201721754322U CN207670659U CN 207670659 U CN207670659 U CN 207670659U CN 201721754322 U CN201721754322 U CN 201721754322U CN 207670659 U CN207670659 U CN 207670659U
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Abstract
The utility model discloses six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation, including fuselage, there is body cover on the fuselage, antenna is housed after the body cover, there is GPS navigation module on the fuselage, cantilever is housed among the fuselage, include motor mount on the cantilever, upper brushless motor, lower brushless motor, there is battery case in the fuselage back lower place, the belly is equipped with cushion socket, it is provided with shock-absorbing ball among the cushion socket, there is Z axis electric rotating machine below the cushion socket, Y-axis electric rotating machine, X-axis electric rotating machine, camera installing plate is housed on the X-axis electric rotating machine, camera is housed in the camera installing plate, the fuselage side-lower is equipped with undercarriage.Advantageous effect is：The utility model is simple in structure, light-weight, and powerful, accurate positioning, cruise duration is long, and landing is steady, and by three-axis stability augmentation holder, shooting angle and direction switch speed are fast, and shooting acquires high-definition camera and picture without dead angle.
Description
Technical field
The utility model belongs to unmanned plane apparatus field, and in particular to a kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation.
Background technology
After unmanned plane is generalized to people's daily life, the unmanned machine equipment of mapping is often used, typically with one
The electronic corresponding camera of UAV flight of kind completes special shooting work by the control to camera and unmanned plane, because
During electronic unmanned plane during flying, it is the quantity of increase rotor substantially to lean on propeller lift, traditional increasing power way, though
Motivation level so is increased, increases load-carrying ability, but this way increases the weight of unmanned plane itself, shortens instead
Cruise duration, and the equipment such as camera carried, due to there is no damping and a three axis holder amendments, very fuzzy, figure when shooting
Image distortion, effect are poor.
So, a kind of electronic unmanned plane is needed, own wt is light, simple in structure, and powerful, cruise duration is long,
With shock-damping structure and three axis holders, the unmanned plane of energy multi-angled shooting.
Invention content
The purpose of this utility model be that solve the above-mentioned problems and provide a kind of three-axis stability augmentation up and down six rotors without
It is man-machine.
The utility model is achieved through the following technical solutions above-mentioned purpose：
A kind of three-axis stability augmentation six rotor wing unmanned aerial vehicles, including fuselage up and down, there is body cover on the fuselage, after the body cover
Equipped with antenna, GPS mounting bases are housed on the fuselage, is equipped in the GPS mounting bases and lengthens carbon pipe, filled on the lengthening carbon pipe
There is GPS navigation module, cantilever is housed among the fuselage, described cantilever one end is equipped with motor mount, the motor mount
It is upper that upper brushless motor is housed, upper blade is housed on the upper brushless motor, lower brushless motor, institute are housed under the motor mount
It states and lower blade is housed on lower brushless motor, the fuselage back lower place is equipped with battery case, and the belly is equipped with cushion socket, described
It is provided with shock-absorbing ball among cushion socket, Z axis electric rotating machine is housed below the cushion socket, rotation is housed under the Z axis electric rotating machine
Pivoted arm, described rotating arm one end are equipped with Y-axis electric rotating machine, roll arm, roll arm one end are housed on the Y-axis electric rotating machine
Equipped with X-axis electric rotating machine, camera installing plate is housed on the X-axis electric rotating machine, camera is housed in the camera installing plate, it is described
Fuselage side-lower is equipped with undercarriage, and the undercarriage lower end is equipped with hinged threeway, floor stand is housed in the hinged threeway, described
Floor stand both ends are cased with shock-absorbing sleeve.
In order to further increase performance, the GPS navigation module is arranged with the lengthening carbon pipe, passes through the lengthening carbon
The stretching of pipe, the GPS navigation module avoid the signal interference between unmanned plane electronic component, and positioning is more accurate.
In order to further increase performance, three cantilevers are housed, material is Carbon fibe pipe, is strengthened among the fuselage
Unmanned plane overall construction intensity alleviates the own wt of unmanned plane.
In order to further increase performance, the motor mount is fitted with the upper brushless motor, is equipped with below
The lower brushless motor increases the motivation level of unmanned plane by the structure of motor setting up and down.
In order to further increase performance, the belly is equipped with the cushion socket, eight is provided among the cushion socket
A shock-absorbing ball, material are high-tension silica gel, by the cushioning effect of the shock-absorbing ball, filter the vibrations in flight course,
Ensure the image-capturing resolution of the camera.
In order to further increase performance, the Z axis electric rotating machine, the Z axis electric rotating machine are housed below the cushion socket
The rotating arm is housed down, described rotating arm one end is equipped with the Y-axis electric rotating machine, is equipped on the Y-axis electric rotating machine described
Roll arm, roll arm one end are equipped with the X-axis electric rotating machine, the camera installing plate are housed on the X-axis electric rotating machine,
The camera is housed in the camera installing plate, by being rotated to the control of three motors, 360 ° of the camera is driven to regard entirely
Angle rotation shooting.
In order to further increase performance, the fuselage side-lower is equipped with two undercarriages, and material is Carbon fibe pipe, and two
The angle at 45 ° of undercarriage described in root, the undercarriage bottom end are fallen equipped with the hinged threeway, described be hinged in threeway equipped with described
Ground frame, the floor stand both ends are cased with the shock-absorbing sleeve, and material is foam, ensure that unmanned plane rises and falls steady by take-off and landing device
Property.
Advantageous effect is：The utility model is simple in structure, light-weight, and powerful, accurate positioning, cruise duration is long,
Landing is steady, and by three-axis stability augmentation holder, shooting angle and direction switch speed are fast, shooting without dead angle, acquire high-definition camera and
Picture.
Description of the drawings
Fig. 1 is the three-dimensional view of six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation described in the utility model, and Fig. 2 is this practicality
A kind of novel left view stereogram of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation, Fig. 3 is a kind of three axis described in the utility model
Increase the vertical view of steady six rotor wing unmanned aerial vehicles up and down；
1, fuselage；2, body cover；3, antenna；4, GPS navigation module；5, carbon pipe is lengthened；6, GPS mounting bases；7, cantilever；8、
Motor mount；9, upper brushless motor；10, upper blade；11, lower brushless motor；12, lower blade；13, battery case；14, damping
Seat；15, shock-absorbing ball；16, Z axis electric rotating machine；17, rotating arm；18, Y-axis electric rotating machine；19, roll arm；20, X-axis electric rotating
Machine；21, camera installing plate；22, camera；23, undercarriage；24, hinged threeway；25, floor stand；26, shock-absorbing sleeve.
Specific implementation mode
The utility model is described in further detail below in conjunction with the accompanying drawings：
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of three-axis stability augmentation six rotor wing unmanned aerial vehicles up and down, including fuselage 1 are arranged on fuselage 1
There is body cover 2, antenna 3 is housed after body cover 2, by antenna 3 for radio station communicates, the ends PC software communicates with the external world, keeps number
According to transmission, GPS mounting bases 6 are housed on fuselage 1, is equipped in GPS mounting bases 6 and lengthens carbon pipe 5, lengthened and GPS navigation is housed on carbon pipe 5
Module 4, GPS navigation module 4 avoid the signal interference between unmanned plane electronic component by the extension of lengthening carbon pipe 5, position
More precisely, three cantilevers 7 are housed, material is Carbon fibe pipe, strengthens unmanned plane overall construction intensity, is mitigated among fuselage 1
The own wt of unmanned plane, cantilever 7 one end are equipped with motor mount 8, and motor mount 8 is fitted with brushless motor 9, on
Upper blade 10 is housed, motor mount 8 is equipped with lower brushless motor 11, is equipped with down on lower brushless motor 11 below on brushless motor 9
Blade 12 increases the motivation level of unmanned plane by the structure of power setting up and down, and 1 back lower place of fuselage is equipped with battery case 13, machine
1 abdomen of body is equipped with cushion socket 14, and eight shock-absorbing balls 15 are provided among cushion socket 14, and material is high-tension silica gel, passes through damping
The cushioning effect of ball 15 filters the vibrations in flight course, ensures that the image-capturing resolution of camera 22,14 lower section of cushion socket are equipped with Z
Axis electric rotating machine 16,16 shaft end of Z axis electric rotating machine are ined succession rotating arm 17, and 17 lower end of rotating arm passes through with Y-axis electric rotating machine 18
Screw is fixed, and roll arm 19 is housed on 18 shaft end of Y-axis electric rotating machine, and 19 one end of roll arm passes through spiral shell with X-axis electric rotating machine 20
Silk is fixed, and camera installing plate 21 is housed on 20 shaft end of X-axis electric rotating machine, camera 22 is housed in camera installing plate 21, by Z
The control rotation of axis electric rotating machine 16,20 3 Y-axis electric rotating machine 18, X-axis electric rotating machine motors, drives 360 ° of camera 22 complete
Visual angle rotation shooting, machine, 1 side-lower be equipped with two undercarriages 23, material be Carbon fibe pipe, two 23 angles at 45 ° of undercarriage,
23 bottom end of undercarriage is equipped with hinged threeway 24, and floor stand 25 is housed in hinged threeway 24, and 25 both ends of floor stand are cased with shock-absorbing sleeve 26,
Material is foam, ensures the stationarity that unmanned plane rises and falls by take-off and landing device.
The basic principles and main features and advantage of the utility model have been shown and described above.The technical staff of the industry
It should be appreciated that the present utility model is not limited to the above embodiments, the above embodiments and description only describe this
The principle of utility model, on the premise of not departing from the spirit and scope of the utility model, the utility model also has various change
And improvement, these various changes and improvements fall within the scope of the claimed invention.The utility model requires protection scope
It is defined by appending claims and equivalents.
Claims (9)
1. a kind of three-axis stability augmentation six rotor wing unmanned aerial vehicles up and down, including fuselage has body cover on the fuselage, is filled after the body cover
There is antenna, GPS mounting bases are housed on the fuselage, is equipped in the GPS mounting bases and lengthens carbon pipe, be equipped on the lengthening carbon pipe
GPS navigation module, is equipped with cantilever among the fuselage, and described cantilever one end is equipped with motor mount, on the motor mount
Equipped with upper brushless motor, upper blade is housed on the upper brushless motor, lower brushless motor is housed under the motor mount, it is described
Lower blade is housed, the fuselage back lower place is equipped with battery case, and the belly is equipped with cushion socket, described to subtract on lower brushless motor
It is provided with shock-absorbing ball among shake seat, Z axis electric rotating machine is housed below the cushion socket, rotation is housed under the Z axis electric rotating machine
Arm, described rotating arm one end are equipped with Y-axis electric rotating machine, and roll arm, roll arm one end dress are housed on the Y-axis electric rotating machine
There is X-axis electric rotating machine, camera installing plate is housed on the X-axis electric rotating machine, camera, the machine are housed in the camera installing plate
Body side-lower is equipped with undercarriage, and the undercarriage lower end is equipped with hinged threeway, floor stand is housed in the hinged threeway, described to fall
Ground frame both ends are cased with shock-absorbing sleeve.
2. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：The GPS navigation
Module is arranged with the lengthening carbon pipe.
3. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：Among the fuselage
Equipped with three cantilevers, material is Carbon fibe pipe.
4. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：The motor installation
Seat is fitted with the upper brushless motor, and the lower brushless motor is housed below.
5. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：The belly
Equipped with the cushion socket, eight shock-absorbing balls are provided among the cushion socket, material is high-tension silica gel.
6. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：Under the cushion socket
Side is equipped with the Z axis electric rotating machine, and the rotating arm is housed under the Z axis electric rotating machine, and described rotating arm one end is equipped with the Y
Axis electric rotating machine, the roll arm is equipped on the Y-axis electric rotating machine, and roll arm one end is equipped with the X-axis electric rotating machine.
7. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：The camera installation
The camera is housed on plate.
8. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：Under the fuselage side
Side is equipped with two undercarriages, and material is Carbon fibe pipe, two undercarriage angles at 45 °.
9. six rotor wing unmanned aerial vehicles above and below a kind of three-axis stability augmentation according to claim 1, it is characterised in that：The hinged threeway
Upper that the floor stand is housed, the floor stand both ends are cased with the shock-absorbing sleeve, and material is foam.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721754322.0U CN207670659U (en) | 2017-12-15 | 2017-12-15 | A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721754322.0U CN207670659U (en) | 2017-12-15 | 2017-12-15 | A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207670659U true CN207670659U (en) | 2018-07-31 |
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| CN201721754322.0U Active CN207670659U (en) | 2017-12-15 | 2017-12-15 | A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109632096A (en) * | 2018-12-19 | 2019-04-16 | 长春理工大学 | The multispectral investigation camera of unmanned plane |
| CN111846208A (en) * | 2020-07-28 | 2020-10-30 | 东南大学 | Long-endurance three-dimensional modeling unmanned aerial vehicle system for lower tunnel |
-
2017
- 2017-12-15 CN CN201721754322.0U patent/CN207670659U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109632096A (en) * | 2018-12-19 | 2019-04-16 | 长春理工大学 | The multispectral investigation camera of unmanned plane |
| CN111846208A (en) * | 2020-07-28 | 2020-10-30 | 东南大学 | Long-endurance three-dimensional modeling unmanned aerial vehicle system for lower tunnel |
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