CN205589470U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205589470U CN205589470U CN201620367975.2U CN201620367975U CN205589470U CN 205589470 U CN205589470 U CN 205589470U CN 201620367975 U CN201620367975 U CN 201620367975U CN 205589470 U CN205589470 U CN 205589470U
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- fuselage
- unmanned plane
- fixed mount
- cushion rubber
- damping cushion
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Abstract
The utility model discloses an unmanned aerial vehicle, unmanned aerial vehicle includes fuselage, screw and screw mount, the screw install in the screw mount, the screw mount install in the fuselage, screw mount flexonics in the fuselage. The utility model provides an unmanned aerial vehicle, including fuselage, screw and screw mount, the screw is installed in the screw mount, and the screw mount is installed in the fuselage, screw mount flexonics in fuselage, because screw mount and fuselage flexonics, then the screw mount transmits in the vibrations of fuselage and diminishes, and unmanned aerial vehicle move stably, and the video camera taken pictures who is connected with the fuselage is clearly.
Description
Technical field
This utility model relates to vehicle technology field, particularly relates to a kind of unmanned plane.
Background technology
UAV is called for short " unmanned plane ", is to utilize radio robot and the programme-control dress provided for oneself
Put the not manned vehicle of manipulation.
Unmanned plane photography of taking photo by plane is using UAV as aerial platform, with airborne sensory equipment, such as height
Resolution CCD digital camera, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain
Win the confidence breath, with computer, image information is processed, and be fabricated to image according to certain required precision.
Use rigid connection between existing unmanned aerial vehicle body and propeller fixed mount, without damping link, cause electricity
The vibrations of machine are passed directly to fuselage, thus cause unmanned aerial vehicle body to shake, and fuselage vibrations can cause unmanned plane to fly
Row is not sufficiently stable and fuselage vibrations severe easily initiation firmware gets loose and causes aircraft malfunctioning, and air crash, fuselage shakes
May also result in the unsharp problem of camera shooting picture being connected with fuselage to occur.
Utility model content
Based on this, it is necessary to for rigid connection between unmanned aerial vehicle body and propeller fixed mount thus cause nothing
The problem of man-machine fuselage vibrations provides a kind of unmanned plane.
A kind of unmanned plane, described unmanned plane includes fuselage, propeller and propeller fixed mount, described propeller
Being installed on described propeller fixed mount, described propeller fixed mount is installed on described fuselage, and described propeller is solid
Determine frame to flexibly connect in described fuselage.
The unmanned plane that this utility model provides, including fuselage, propeller and propeller fixed mount, propeller is pacified
Being loaded on propeller fixed mount, propeller fixed mount is installed on fuselage, and propeller fixed mount flexibly connects in fuselage,
Owing to propeller fixed mount flexibly connects with fuselage, then propeller fixed mount is transmitted to the vibrations of fuselage and diminishes,
Unmanned plane is stable, and the camera shooting picture being connected with fuselage is clear.
Wherein in an embodiment, described unmanned plane also includes the first damping cushion rubber, described first damping rubber
Circle is located between described fuselage and described propeller fixed mount, one end of described first damping cushion rubber and described machine
Body abuts against, and the other end of described first damping cushion rubber abuts against with described propeller fixed mount.
Wherein in an embodiment, described unmanned plane also includes the column being located at described fuselage, described column
Arranging along a circumferencial direction, the line of multiple described columns forms a circle, and described first damping rubber snare sets
Outside in the circle that multiple described columns are formed.
Wherein in an embodiment, the described diameter of a circle that multiple described columns are formed subtracts with described first
The internal diameter of shake cushion rubber is equal.
Wherein in an embodiment, described unmanned plane also includes securing member, and described securing member passes described spiral shell
Rotation oar fixed mount is also arranged in described column to be fixed with described propeller fixed mount by described fuselage.
Wherein in an embodiment, described securing member is trip bolt.
Wherein in an embodiment, described unmanned plane also includes the second damping cushion rubber, described second damping rubber
Snare is located at described trip bolt, and when described trip bolt is tightened, described second damping cushion rubber is positioned at described
Between head and the described propeller fixed mount of trip bolt.
Wherein in an embodiment, the quantity of described column is four, and four described columns are along a circumference side
To being uniformly arranged on described fuselage.
Wherein in an embodiment, described fuselage is provided with the groove that can accommodate described first damping cushion rubber,
The degree of depth of described groove is less than the height of described first damping cushion rubber, and described first damping cushion rubber is placed in described recessed
In groove.
Accompanying drawing explanation
The explosive view of the unmanned plane that Fig. 1 provides for this utility model embodiment；
Fig. 2 is the installation diagram of Fig. 1.
Detailed description of the invention
For the ease of understanding this utility model, below with reference to relevant drawings, this utility model is carried out more comprehensively
Description.Accompanying drawing gives preferred embodiment of the present utility model.But, this utility model can be to be permitted
The most different forms realizes, however it is not limited to embodiment described herein.On the contrary, provide these to implement
The purpose of example is to make the understanding to disclosure of the present utility model more thorough comprehensively.
It should be noted that when element is referred to as " being fixed on " another element, and it can be directly at another
On individual element or element placed in the middle can also be there is.When an element is considered as " connection " another yuan
Part, it can be directly to another element or may be simultaneously present centering elements.Used herein
Term " vertical ", " level ", "left", "right" and similar statement simply to illustrate that mesh
's.
Unless otherwise defined, all of technology used herein and scientific terminology with belong to of the present utility model
The implication that those skilled in the art are generally understood that is identical.Institute in description of the present utility model herein
The term used is intended merely to describe the purpose of specific embodiment, it is not intended that in limiting this utility model.
Term as used herein " and/or " include the arbitrary and all of one or more relevant Listed Items
Combination.
Seeing Fig. 1 and Fig. 2, this utility model embodiment provides a kind of unmanned plane, and this unmanned plane includes fuselage
10, propeller 20 and propeller fixed mount 30, propeller 20 is installed on propeller fixed mount 30, propeller
Fixed mount 30 is installed on fuselage 10, and propeller fixed mount 30 flexibly connects in fuselage 10.
The unmanned plane that this utility model embodiment provides, including fuselage 10, propeller 20 and propeller fixed mount
30, propeller 20 is installed on propeller fixed mount 30, and propeller fixed mount 30 is installed on fuselage 10, spiral
Oar fixed mount 30 flexibly connects in fuselage 10, owing to propeller fixed mount 30 flexibly connects with fuselage 10, then
Propeller fixed mount 30 is transmitted to the vibrations of fuselage 10 and diminishes, and unmanned plane is stable, and with fuselage 10 even
The camera shooting picture connect is clear.
Seeing Fig. 1, in the present embodiment, this unmanned plane also includes the first damping cushion rubber 40, the first damping rubber
Circle 40 is located between fuselage 10 and propeller fixed mount 30, one end of the first damping cushion rubber 40 and fuselage 10
Abutting against, the other end of the first damping cushion rubber 40 abuts against with propeller fixed mount 30.
First damping cushion rubber 40, and the first damping cushion rubber are set between fuselage 10 and propeller fixed mount 30
One end of 40 abuts against with fuselage 10, and the other end of the first damping cushion rubber 40 offsets with propeller fixed mount 30
Connecing, when the electric machine rotation of unmanned plane, motor is transmitted to the vibrations of propeller fixed mount 30 by the first damping
Cushion rubber 40 is offset, and the vibrations being transmitted to fuselage 10 diminish, and unmanned plane is stable, and is connected with fuselage 10
Camera shooting picture clear.
Seeing Fig. 1, in the present embodiment, this unmanned plane also includes the column 12 being located at fuselage 10, column 12
Being uniformly arranged along a circumferencial direction, the line of multiple columns 12 forms a circle, and the first damping cushion rubber 40 overlaps
It is located at the outside of the circle that multiple column 12 is formed.The setting of column 12 can be so that the first damping cushion rubber 40
Fixing, the i.e. first damping cushion rubber 40 can be set in the outside of multiple column 12, at multiple columns 12
It is located under effect between fuselage 10 and propeller fixed mount 30, prevents the first damping cushion rubber 40 at fuselage 10
And the sideslip between propeller fixed mount 30.
Specifically, multiple columns 12 are formed diameter of a circle and the internal diameter of the first damping cushion rubber 40 are equal.
When diameter of a circle that multiple columns 12 are formed and the internal diameter of the first damping cushion rubber 40 are equal, the first damping rubber
Circle 40 is just sheathed on the outside of multiple column 12, preferably to fix the first damping cushion rubber 40.
The quantity of above-mentioned column 12 can be four, and four columns 12 are uniformly arranged on machine along a circumferencial direction
Body 10.The quantity of above-mentioned column 12 is also not necessarily limited to four, can be one, two, three or more than four
Individual.
Except fixing the mode of the first damping cushion rubber 40 above by column 12, in other embodiments, also
Can be provided with the groove that can accommodate the first damping cushion rubber 40 on fuselage 10, the degree of depth of groove is less than first
The height of damping cushion rubber 40, the first damping cushion rubber 40 is placed in groove.When the first damping cushion rubber 40 is put
After being placed in above-mentioned groove, the portion projects of the first damping cushion rubber 40 goes out above-mentioned groove, propeller fixed mount 30
It is installed on fuselage 10 to be held between fuselage 10 and propeller fixed mount 30 by the first damping cushion rubber 40,
Prevent the first damping cushion rubber 40 sideslip between fuselage 10 and propeller fixed mount 30.
Seeing Fig. 1 and Fig. 2, in the present embodiment, this unmanned plane also includes that securing member 50, securing member 50 are worn
Cross propeller fixed mount 30 and be arranged in column 12 to be fixed with propeller fixed mount 30 by fuselage 10.Tool
Body ground, above-mentioned securing member 50 is trip bolt.
Seeing Fig. 1 and Fig. 2, in the present embodiment, above-mentioned unmanned plane also includes the second damping cushion rubber 60, the
Two damping cushion rubbers 60 can be sheathed on trip bolt, and when trip bolt is tightened, the second damping cushion rubber 60 is positioned at
Between head and the propeller fixed mount 30 of trip bolt.The setting of the second damping cushion rubber 60 can be so that tight
Gu the damping between screw and propeller fixed mount 30.
Specifically, corresponding to the setting of aforementioned four column 12, the quantity of trip bolt can be also configured as
Four, and the quantity of the second damping cushion rubber 60 is also configured as four, is arranged with one on each trip bolt
Individual second damping cushion rubber 60.When after the second damping cushion rubber 60 sheathed on each trip bolt, spiral shell will be fastened
Nail is arranged in propeller fixed mount 30, and trip bolt can be arranged in machine through one end of propeller fixed mount 30
Above the column 12 of body 10, certainly, trip bolt can also be arranged in other positions of fuselage 10, and not
It is to be arranged in column 12.
Specifically, see Fig. 1 and Fig. 2, the fuselage 10 that this utility model embodiment provides be shaped as streamline
Type, and two spikes can be respectively arranged with in the left and right sides of the bottom of fuselage 10, when unmanned plane lands,
Unmanned plane can be easy under the effect of a spike and be supported in ground.
Embodiment described above only have expressed several embodiments of the present utility model, its describe more concrete and
In detail, but therefore can not be interpreted as the restriction to this utility model the scope of the claims.It should be pointed out that,
For the person of ordinary skill of the art, without departing from the concept of the premise utility, it is also possible to
Making some deformation and improvement, these broadly fall into protection domain of the present utility model.Therefore, this utility model
The protection domain of patent should be as the criterion with claims.
Claims (9)
1. a unmanned plane, described unmanned plane includes fuselage, propeller and propeller fixed mount, described spiral
Oar is installed on described propeller fixed mount, and described propeller fixed mount is installed on described fuselage, it is characterised in that
Described propeller fixed mount flexibly connects in described fuselage.
Unmanned plane the most according to claim 1, it is characterised in that described unmanned plane also includes that first subtracts
Shaking cushion rubber, described first damping cushion rubber is located between described fuselage and described propeller fixed mount, and described first
One end of damping cushion rubber abuts against with described fuselage, the other end of described first damping cushion rubber and described propeller
Fixed mount abuts against.
Unmanned plane the most according to claim 2, it is characterised in that described unmanned plane also includes being located at institute
Stating the column of fuselage, described column is arranged along a circumferencial direction, and the line of multiple described columns forms a circle,
Described first damping rubber snare is located at the outside of the circle that multiple described column is formed.
Unmanned plane the most according to claim 3, it is characterised in that the institute that multiple described columns are formed
State diameter of a circle equal with the internal diameter of described first damping cushion rubber.
Unmanned plane the most according to claim 3, it is characterised in that described unmanned plane also includes securing member,
Described securing member is through described propeller fixed mount and is arranged in described column with by described fuselage and described spiral
Oar fixed mount is fixed.
Unmanned plane the most according to claim 5, it is characterised in that described securing member is trip bolt.
Unmanned plane the most according to claim 6, it is characterised in that described unmanned plane also includes that second subtracts
Shake cushion rubber, described second damping rubber snare is located at described trip bolt, when described trip bolt is tightened, institute
State the second damping cushion rubber between the head and described propeller fixed mount of described trip bolt.
Unmanned plane the most according to claim 3, it is characterised in that the quantity of described column is four,
Four described columns are uniformly arranged on described fuselage along a circumferencial direction.
Unmanned plane the most according to claim 2, it is characterised in that be provided with on described fuselage and can accommodate
The groove of described first damping cushion rubber, the degree of depth of described groove is less than the height of described first damping cushion rubber, institute
State the first damping cushion rubber to be placed in described groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620367975.2U CN205589470U (en) | 2016-04-27 | 2016-04-27 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620367975.2U CN205589470U (en) | 2016-04-27 | 2016-04-27 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205589470U true CN205589470U (en) | 2016-09-21 |
Family
ID=56932373
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620367975.2U Active CN205589470U (en) | 2016-04-27 | 2016-04-27 | Unmanned aerial vehicle |
Country Status (1)
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| CN (1) | CN205589470U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828867A (en) * | 2016-12-30 | 2017-06-13 | 易瓦特科技股份公司 | Noise-proofing formula unmanned plane |
| WO2019204932A1 (en) * | 2018-04-25 | 2019-10-31 | Flir Unmanned Aerial Systems Ulc | Unmanned vehicle |
-
2016
- 2016-04-27 CN CN201620367975.2U patent/CN205589470U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828867A (en) * | 2016-12-30 | 2017-06-13 | 易瓦特科技股份公司 | Noise-proofing formula unmanned plane |
| WO2019204932A1 (en) * | 2018-04-25 | 2019-10-31 | Flir Unmanned Aerial Systems Ulc | Unmanned vehicle |
| US11767135B2 (en) | 2018-04-25 | 2023-09-26 | Flir Unmanned Aerial Systems Ulc | Unmanned vehicle |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |