CN206939046U - The frame and unmanned plane of unmanned plane - Google Patents
The frame and unmanned plane of unmanned plane Download PDFInfo
- Publication number
- CN206939046U CN206939046U CN201720799484.XU CN201720799484U CN206939046U CN 206939046 U CN206939046 U CN 206939046U CN 201720799484 U CN201720799484 U CN 201720799484U CN 206939046 U CN206939046 U CN 206939046U
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- China
- Prior art keywords
- horn
- mounting surface
- frame
- fuselage
- unmanned plane
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Abstract
The frame and unmanned plane of a kind of unmanned plane, including：Fuselage, fuselage have relative horn mounting surface, horn mounting surface and horizontal plane；Horn, horn have first end and the second end, first end and the horn mounting surface pivotable connection of horn；At least two horns are installed, the first end of adjacent horn has spacing in vertical direction on horn mounting surface.Horn can abut on horn mounting surface at various height, realize that the layering of horn folds.Folded by the layering of horn so that no matter the Design of length of horn how long, can not also be clashed after folding, ensure that the length of horn.
Description
Technical field
It the utility model is related to the technical field of unmanned plane, and in particular to a kind of horn folding unmanned plane frame and bag
Include the unmanned plane of this frame.
Background technology
With the rise for camera work of taking photo by plane, it is outgoing very universal to carry unmanned plane of taking photo by plane.But traditional unmanned plane
Horn is all fixed, therefore the space that unmanned plane takes is very big.Horn is made folding, unmanned plane can be caused to receive
Volume is smaller when receiving, also more portable.
At present, the foldable mode of horn be by fuselage from four horns to frame among doubling, so can be very effective
Ground utilization space.But the problem of existing is must make it that horn is shorter if horn is to doubling among fuselage, and install
Blade on horn can not be too big, causes that the efficiency of unmanned plane is low, and cruising time is also restrained.
Based on above mentioned problem, it is desirable to provide a kind of unmanned plane frame using new horn folding mode so that ensureing
In the case that horn length is not short, the foldable of unmanned plane horn is realized.
Utility model content
The technical problem that the utility model solves is how in the case where ensureing that horn length is not short, realizes unmanned plane machine
Arm it is foldable.
In order to solve the above technical problems, the utility model provides a kind of frame of unmanned plane, including：Fuselage, the fuselage
With relative horn mounting surface, the horn mounting surface and horizontal plane；Horn, the horn have first end and second
End, the first end of the horn and the horn mounting surface pivotable connection；At least two are provided with the horn mounting surface
Spacing in vertical direction be present in the horn, the first end of the adjacent horn.
Optionally, there is spacing in the first end of the adjacent horn in the horizontal direction.
Optionally, the spacing of the first end of the adjacent horn in vertical direction is equal, the adjacent horn
The spacing of first end in the horizontal direction is equal.
Optionally, it is provided with undercarriage on the second end of the horn in lowest part in vertical direction.
Optionally, the undercarriage is raised vertically down.
Optionally, the fuselage is arranged to cuboid, and the fuselage has two relative horn mounting surfaces.
Optionally, two horns are installed on the horn mounting surface.
Optionally, it is provided with motor on the second end of the horn；The motor is higher than the fuselage in vertical direction.
Optionally, the groove for accommodating the motor, the opening court of the groove are provided with the horn mounting surface
To the outside of the fuselage.
Optionally, the first end of the horn is connected by spring rotary shaft with the horn mounting surface.
Optionally, battery installation section is provided with the fuselage, for installing battery.
The utility model also provides a kind of unmanned plane, and it includes above-mentioned frame.
Compared with prior art, the technical solution of the utility model has the advantages that：A kind of unmanned plane machine is provided
Frame, it includes fuselage and horn.Wherein, there is relative horn mounting surface, horn mounting surface and horizontal plane, horn on fuselage
Multiple horns, one end and the horn mounting surface pivotable connection of each horn are installed, horn can pass through rotation on mounting surface
Leave out or recline horn mounting surface.Because one end of adjacent horn has spacing in vertical direction, horn can be not
Same height is abutted on horn mounting surface, realizes that the layering of horn folds.Folded by the layering of horn so that no matter horn
Design of length how long, fold after can not also clash, ensure that the length of horn.
Brief description of the drawings
Fig. 1 is the schematic perspective view of unmanned plane frame of the present utility model, shows that horn leaves horn mounting surface in figure
State during expansion；
Fig. 2 is the schematic perspective view of unmanned plane frame of the present utility model, shows that horn reclines horn mounting surface in figure
State during storage；
Fig. 3 is the front view of Fig. 2 unmanned plane frame.
Embodiment
The problem of existing for the folding mode of current unmanned plane horn, new machine is used the utility model proposes a kind of
The unmanned plane frame of arm folding mode so that in the case where ensureing that horn length is not short, realize the foldable of unmanned plane horn.
It is understandable to enable above-mentioned purpose, feature and beneficial effect of the present utility model to become apparent, below in conjunction with the accompanying drawings
Specific embodiment of the utility model is described in detail.
With reference to figure 1 and Fig. 2, a kind of frame 1 of unmanned plane, it includes fuselage 10 and horn 20.Wherein, fuselage 10 has phase
To horn mounting surface 11, horn mounting surface 11 is the surface with horizontal plane on fuselage 10.Each horn mounting surface 11
On be fitted with two horns 20.Horn 20 is in shaft-like, and it has the end 22 of first end 21 and second, and the first end 21 of horn 20 is led to
Cross spring rotary shaft 14 and the pivotable connection of horn mounting surface 11.First end 21 rotates around spring rotary shaft 14 so that horn 20 can
With the horn mounting surface 11 that leaves or recline.The top at the second end 22 is provided with motor 23, and the top of motor 23 is provided with spiral
Oar (not shown).Fuselage 10 has battery installation section 12, battery is arranged in battery installation section 12, battery is motor 23
Electric energy is provided, motor 23 drives propeller rotational, and unmanned plane starts working flight.
When needing to use unmanned plane, user is by rotating the first end 21 of horn 20 so that horn 20 leaves horn
Mounting surface 11 outwards deploys, as shown in Figure 1.When unmanned plane need not be used, user's direction whirler opposite before
The first end 21 of arm 20 so that horn 20 is abutted on horn mounting surface 11, as shown in Figure 2.By the folding of horn 20, in nothing
During man-machine storage, the space of unmanned plane frame 1 is reduced so that unmanned plane is more portable.
In the present embodiment, fuselage 10 has two relative horn mounting surfaces 11.But fuselage is not limited to only two machines
Arm mounting surface, in other embodiments, it is possible to have more logarithm purpose horn mounting surface, but horn mounting surface is total necessary
It is even number, such as four either six or more horn mounting surfaces, wherein horn mounting surface is relative two-by-two.
With reference to figure 3, in the present embodiment, two horns 20, two horns are only installed on each horn mounting surface 11
The center of 20 first end 21, which is in vertical direction (Fig. 3 X-direction), has space D 1.Due to the first end of two horns 20
21 have space D 1 in vertical direction, and horn 20 can abut on horn mounting surface 11 at various height, realize horn
20 layering on horn mounting surface 11 folds.Pass through it is this layering fold form so that no matter the Design of length of horn 20
How long, folding can not also clash after abutting on horn mounting surface 10, ensure that the length of horn 20.
In other embodiments, more than two horns, such as three or four are installed on each horn mounting surface
Horn, the first end of adjacent horn have to spacing be present in vertical direction.So when storing unmanned plane frame, horn can
To abut at various height on horn mounting surface, realize that layering of the horn on horn mounting surface folds.
With continued reference to Fig. 3, two horns 20, two horns 20 are only installed in the present embodiment, on horn mounting surface 11
The center of first end 21 be in horizontal direction (Fig. 3 Y-direction) and space D 2 be present, the setting of space D 2 by horn 20 length
Degree determines.Specifically, in the present embodiment, the first end 21 of two horns 20 is separately positioned on horn mounting surface 11 in level side
Upward both ends, space D 2 are the length of horn mounting surface 11 in the horizontal direction, and the length of such horn 20 can be designed as
The length of horn mounting surface 11 in the horizontal direction, this is also the maximum length of horn 20.If to the length requirement of horn 20
In the case of not high, the space D 2 of the first end 21 of horn 20 in the horizontal direction might be less that horn mounting surface 11 in level
Length on direction, the length of such horn 20 can be designed as being less than the length of horn mounting surface 11 in the horizontal direction.
In other embodiments, more than two horns, such as three or four horns, phase are installed on horn mounting surface
Spacing in the horizontal direction be present in horn mounting surface in the first end of adjacent horn.In order to obtain the maximum length of horn, adjacent machine
The first end of arm is located at the both ends of horn mounting surface in the horizontal direction respectively, and the first end of adjacent horn is in the horizontal direction
Spacing is equal to the length of horn mounting surface in the horizontal direction.The length of so each horn can be designed as horn mounting surface
Length in the horizontal direction.In the case that if length requirement to horn is not high, the first end of horn is in the horizontal direction
Spacing might be less that the length of horn mounting surface in the horizontal direction, the length of such horn can be less than horn mounting surface
Length in the horizontal direction.
In other embodiments, if installing more than two horns on horn mounting surface, adjacent machine can be set
The spacing of the first end of arm in vertical direction is equal, and the first end of adjacent horn is respectively positioned at horn mounting surface in level side
Upward both ends, i.e., the spacing of the first end of adjacent horn in the horizontal direction are equal.In this manner it is ensured that installed in horn
After on horn mounting surface, overall center of gravity can be located at the center of horn mounting surface.
Referring to figs. 2 and 3 in vertical direction (Fig. 3 X-direction), on the second end 22 of the horn 20 in lowest part
It is provided with undercarriage 24.Wherein, undercarriage 24 is raised vertically down.Undercarriage 24 is being taken off and dropped in unmanned plane
The cushioning effect between unmanned plane frame and ground is played when falling, avoids unmanned plane from facing unmanned plane machine in takeoff and landing
The impact of frame is too big.
In the present embodiment, fuselage 10 is arranged to cuboid, and fuselage 10 has two relative horn mounting surfaces 11, horn
Mounting surface 11 is two relative sides of fuselage 10.Because fuselage 10 has four sides, fuselage 10, which can also be set, to be had
Four horn mounting surfaces 11.
In other embodiments, fuselage is not limited to the shape of cuboid, could be arranged to six arris cylinders or eight arris
Cylinder.If fuselage is six arris cylinders, fuselage can have two either four or six horn mounting surfaces；If fuselage
For eight arris cylinders, fuselage can have two either four or six or eight horn mounting surfaces.Similarly, with such
Push away.
With reference to figure 1 and Fig. 3 is combined, motor 23 has been set on the second end 22 of each horn 20.Wherein motor 23 is all
Installed in the upside at the second end 22 of horn 20, (Fig. 3 X-direction) is higher than the upper table of fuselage 10 to motor 23 in vertical direction
Face.The top installation propeller blade of motor 23, because motor 23 is higher than the upper surface of fuselage 10, propeller in vertical direction
Blade is in vertical direction also above the upper surface of fuselage 10.So, after the expansion of horn 20, propeller blade is also in fuselage 10
Top, can thus select larger propeller blade, unmanned plane it is more efficient；After the folding of horn 20, propeller
Blade can be located above fuselage 10, and propeller blade can not have to pull down from motor 23, and unmanned plane is more convenient to carry.
With reference to figure 1 and Fig. 2 is combined, the groove 13 for accommodating motor 23 is provided with horn mounting surface 11, groove 13
It is open towards the outside of fuselage 10.In the present embodiment, a total of four grooves 13 on fuselage 10, after the folding of horn 20, four
Individual motor 23 is corresponded and is contained in four grooves 13.Wherein, two grooves 13 are set positioned at the head of battery installation section 12
Both sides.After thering is battery socket, battery socket to occupy the segment space among fuselage due to the head of battery installation section 12,
Because the position closer from battery socket is easily influenceed by battery current, it is impossible to which arrangement is to electromagnetism than more sensitive electronics device
Part, therefore the both sides on the head of battery installation section 12 are cut off as groove 13, for storing the motor 23 on horn 20, so may be used
To make full use of the space of fuselage 10.Two other grooves 13 set the afterbody being located in fuselage 10, by the afterbody of fuselage 10
Both sides are cut off, and for storing motor 23 and nose-gear 24, can so reduce the volume after unmanned plane frame 1 is stored, more sharp
In portable.
With reference to figure 1, the first end 21 of each horn 20 is connected by spring rotary shaft 14 with horn mounting surface 11.Spring turns
Axle 14 ensures that horn 20 only has one degree of freedom, i.e., is rotated around spring rotary shaft 14.When horn 20 deploys, when horn 20 is spread out over
After the maximum anglec of rotation of spring rotary shaft 14, horn 20 can the automatic outwards expansion under the drive of spring rotary shaft 14.Horn 20 is opened up
When reaching maximum position, spring rotary shaft 14 still has larger power horn 20 is outwards deployed, and ensures that horn 20 flies in unmanned plane
It is unlikely to rotate automatically during row.If unmanned plane horn 20 in flight course bumps against barrier, horn 20 can be to receipts
Receiving direction is rotated a bit, and so as to play a part of damping, such horn 20 so will not be severed easily.When unmanned aerial vehicle to obstacle
After thing, as long as long as the angle of revolution of horn 20 no more than the maximum anglec of rotation of spring rotary shaft 14 itself, horn 20 still may be used
To self expand to maximum position in the presence of spring rotary shaft 14.
With reference to figure 1, battery installation section 12 is provided with fuselage 10, for installing battery.Battery is arranged on battery installation section
After 12, electrically connected with the battery socket positioned at the head of battery installation section 12, so as to provide electric energy for motor 23.
The utility model embodiment also provides a kind of unmanned plane, and it includes above-mentioned unmanned plane frame 1.
Although the utility model discloses as above, the utility model is not limited to this.Any those skilled in the art,
Do not depart from spirit and scope of the present utility model, can make various changes or modifications, therefore the scope of protection of the utility model
It should be defined by claim limited range.
Claims (12)
- A kind of 1. frame of unmanned plane, it is characterised in that including：Fuselage, the fuselage have relative horn mounting surface, the horn mounting surface and horizontal plane；Horn, the horn have first end and the second end, and the first end of the horn pivotably connects with the horn mounting surface Connect；At least two horns are installed, the first end of the adjacent horn is in vertical direction on the horn mounting surface Spacing be present.
- 2. frame as claimed in claim 1, it is characterised in that the first end of the adjacent horn exists in the horizontal direction Spacing.
- 3. frame as claimed in claim 2, it is characterised in that the first end of the adjacent horn in vertical direction between The spacing of first end away from equal, the adjacent horn in the horizontal direction is equal.
- 4. frame as claimed in claim 1, it is characterised in that second of the horn in lowest part in vertical direction Undercarriage is provided with end.
- 5. frame as claimed in claim 4, it is characterised in that the undercarriage is raised vertically down.
- 6. frame as claimed in claim 1, it is characterised in that the fuselage is arranged to cuboid, and the fuselage has two The relative horn mounting surface.
- 7. frame as claimed in claim 6, it is characterised in that two horns are provided with the horn mounting surface.
- 8. frame as claimed in claim 1, it is characterised in that be provided with motor on the second end of the horn；The motor It is higher than the fuselage in vertical direction.
- 9. frame as claimed in claim 8, it is characterised in that be provided with the horn mounting surface for accommodating the motor Groove, the opening of the groove is towards the outside of the fuselage.
- 10. frame as claimed in claim 1, it is characterised in that the first end of the horn passes through spring rotary shaft and the machine Arm mounting surface connects.
- 11. frame as claimed in claim 1, it is characterised in that battery installation section is provided with the fuselage, for installing electricity Pond.
- 12. a kind of unmanned plane, it is characterised in that including the frame as any one of claim 1-11.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720799484.XU CN206939046U (en) | 2017-07-04 | 2017-07-04 | The frame and unmanned plane of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720799484.XU CN206939046U (en) | 2017-07-04 | 2017-07-04 | The frame and unmanned plane of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206939046U true CN206939046U (en) | 2018-01-30 |
Family
ID=61366883
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720799484.XU Expired - Fee Related CN206939046U (en) | 2017-07-04 | 2017-07-04 | The frame and unmanned plane of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206939046U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108545190A (en) * | 2018-06-15 | 2018-09-18 | 芜湖万户航空航天科技有限公司 | Miniature drone |
| WO2019227445A1 (en) * | 2018-05-31 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Rack and unmanned aerial vehicle |
| CN113002768A (en) * | 2021-02-26 | 2021-06-22 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle horn rapid disassembly structure reaches unmanned aerial vehicle including it |
-
2017
- 2017-07-04 CN CN201720799484.XU patent/CN206939046U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019227445A1 (en) * | 2018-05-31 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Rack and unmanned aerial vehicle |
| JP2021523850A (en) * | 2018-05-31 | 2021-09-09 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Racks and drones |
| JP7074894B2 (en) | 2018-05-31 | 2022-05-24 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッド | Racks and drones |
| CN108545190A (en) * | 2018-06-15 | 2018-09-18 | 芜湖万户航空航天科技有限公司 | Miniature drone |
| CN113002768A (en) * | 2021-02-26 | 2021-06-22 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle horn rapid disassembly structure reaches unmanned aerial vehicle including it |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180130 Termination date: 20200704 |