CN208515811U - A kind of foldable six rotor wing unmanned aerial vehicle - Google Patents
A kind of foldable six rotor wing unmanned aerial vehicle Download PDFInfo
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- CN208515811U CN208515811U CN201721459142.XU CN201721459142U CN208515811U CN 208515811 U CN208515811 U CN 208515811U CN 201721459142 U CN201721459142 U CN 201721459142U CN 208515811 U CN208515811 U CN 208515811U
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Abstract
A kind of foldable six rotor wing unmanned aerial vehicle, including body, horn, motor, wing, laterally folded seat, longitudinal folding seat, laterally folded seat one end connects horn, one end connects body, horn can be made to be folded in body two sides, the laterally folded seat one end for wherein connecting the second horn and the 6th horn is connected to body one end, the second horn and the 6th horn can be made to be folded in body two sides i.e. upper space, connect third horn, laterally folded seat one end of 5th horn is connected to underpart, it can make third horn, 5th horn is folded in middle space below the 6th horn, longitudinal folding seat is separately connected body longitudinal direction both ends and horn, horn can be made to be folded in below body, wherein the first horn is turned down to body lower section to middle space below body, 4th horn turns down the bottom space below body to body lower section, bottom space is in middle level Space lower part.
Description
Technical field
The utility model relates to unmanned plane field, especially a kind of six rotor wing unmanned aerial vehicle field of Collapsible mobile.
Background technique
In unmanned plane class industry, how to transport and carry multi-rotor unmanned aerial vehicle is always a problem, and majority can be rolled over now
Folded unmanned plane is mostly that can only fold horn.However, folded wing mostly be to be folded in unmanned plane foot prop two sides, folded height according to
It is old constant, it is even higher, in this way, volume after folding is still very big, it has not been convenient to transport.
Summary of the invention
The purpose of this utility model is to provide a kind of foldable six rotor wing unmanned aerial vehicles, can reduce unmanned plane volume, side
Just it transports.
The technical solution of the utility model is achieved in that
A kind of foldable six rotor wing unmanned aerial vehicle, including body (7), horn, motor, wing, the horn and motor and
Body (7) connection, the motor connect with horn and wing respectively, it is characterised in that: further include laterally folded seat (10) with
And longitudinal folding seat (11), described laterally folded seat one end connect horn, one end connects body (7), horn can be made along machine
Body (7) rotates horizontally that horn is made to be folded in the body (7) two sides, wherein connecting the second horn (2) and the 6th horn (6)
Laterally folded seat one end be connected to the body (7) one end, second horn (2) and the 6th horn (6) can be made to be folded in
Body two sides connect third horn (3), laterally folded seat one end of the 5th horn (5) is connected to the body (7) lower part, energy
The third horn (3), the 5th horn (5) is set to be folded in middle space below the body (7), the longitudinal folding seat point
Not Lian Jie body (7) and horn, the horn can be made to be rotated vertically downward along body (7) to making horn be folded in the machine
Below body, wherein the longitudinal folding seat for connecting first horn (1) can make the first horn (1) to fold below body described
Middle space below body, the longitudinal folding seat for connecting the 4th horn (4) can be such that the 4th horn (4) turns over to body lower section
Folding bottom space below the body, bottom space space lower part in middle level.
Preferably, the longitudinal folding seat includes that the first noumenon (16) and the second ontology (27) and the first horn are fixed
Structure (17), the first noumenon (16) and the second ontology (27) are connected by the first horn fixed structure (17), and described the
One ontology (16) and body (7) connection, second ontology (27) connect with horn, when the first horn fixed structure of release
(17), second ontology (27) can longitudinally be turned over downwards most 180 ° along the first noumenon (16).
Preferably, the laterally folded seat includes third ontology (26) and the 4th ontology (19), the second horn fixed knot
Structure (18), the 4th ontology (19) include external screw thread fixed structure, and the second horn fixed structure (18) is solid comprising internal screw thread
Determine structure, third ontology (26) is capable of fixing horn, and when unclamping the second horn fixed structure (18), third ontology (26) can be along the
Four ontologies (19) rotate horizontally 0 ° -120 °.
It preferably, further include foldable GPS support rod (14), foldable compass support rod (15), the foldable GPS branch
Strut (14), foldable compass support rod (15) can be folded to the upper space of body upper along body longitudinal direction.
Preferably, the wing energy horizontal direction horn direction rotates, and makes wing-folding to horn two sides.
Preferably, 4 Quick Release foot rest bases (8), (12) are respectively symmetrically installed on the horn of laterally folded seat connection, including
2 short foot prop Quick Release foot rest base (8) and 2 long foot prop Quick Release foot rest base (12), the short foot prop Quick Release foot rest base (8), long foot
Frame Quick Release foot rest base (12) seat is that detachable limit mechanical structured member can be by long foot prop (9), short foot prop when folding unmanned plane
(13) fast quick-detach reduces folding volume.
Preferably, the body (7) uses carbon fibre material, horn, wing, laterally folded seat, longitudinal folding seat, length
Foot prop, short foot prop use aluminum alloy materials, compare other materials, and carbon fibre material and aluminum alloy materials can guarantee that unmanned plane is firm
Under the premise of reduce weight as far as possible.
Preferably, the short foot prop Quick Release foot rest base (8), long foot prop Quick Release foot rest base (12) limit foot prop comprising fast-assembling
5th ontology (20), fast-assembling limit scaffold fixing structure (21), fast-assembling limit foot prop position restrainer tool structure (22), fast-assembling position-limit foot
The 6th ontology (23) of frame.Fast-assembling limit the 5th ontology (20) of foot prop is fixed on the horn of laterally folded seat connection, is passed through
Fastened by screw, fast-assembling limit the 5th ontology (20) of foot prop are limited by fast-assembling limit scaffold fixing structure (21) and the fast-assembling
Position the 6th ontology (23) of foot prop connection, limits the fast-assembling position-limit foot by fast-assembling limit foot prop position restrainer tool structure (22)
The position of the 6th ontology (23) of frame, guarantees the stability of entire foot prop.
The utility model has the following beneficial effects: foldable six rotor using the utility model design scheme is inorganic, layering
Horn, while folded wing, GPS support rod, compass support rod are folded, the folding space of unmanned plane, structure is preferably utilized
Simply, folding convenient.After folding, the occupied space of unmanned plane is greatly reduced, makes unmanned plane is more convenient carry, transport.
Detailed description of the invention
Fig. 1 is six rotation unmanned plane schematic perspective view in the utility model
Fig. 2 is that six rotation unmanned planes fold preceding top view in the utility model
Fig. 3 be in the utility model six rotation unmanned planes fold after top view
Fig. 4 is that six rotation unmanned planes fold front view in the utility model
Fig. 5 is that six rotation unmanned planes fold lateral side view in the utility model
Fig. 6 is longitudinal folding seat figure in the utility model
Fig. 7 is laterally folded seat figure in the utility model
Fig. 8 is that fast-assembling limit foot rest base is stated in the utility model
Wherein, title corresponding to the appended drawing reference in attached drawing are as follows:
1-the first horn, the 2-the second horn, 3-third horns, the 4-the four horn, the 5-the five horn, the 6-the six machine
Arm, 7-bodies, 8-short foot prop Quick Release foot rest bases, 9-long foot props, 10-laterally folded seats, 11-longitudinal folding seats, 12-is long
Foot prop Quick Release foot rest base, 13-short foot props, 14-foldable GPS support rods, the foldable compass support rod of 15-, 16-longitudinal foldings
Folded seat the first noumenon, 27-longitudinal folding the second ontologies of seat, 17-longitudinal folding the first horn of seat fixed structures, 18-laterally roll over
Folded the second horn of seat fixed structure, 26-laterally folded seat third ontologies, 19-laterally folded the 4th ontologies of seat, 20-fast-assemblings
The 5th ontology of foot prop is limited, 21-fast-assemblings limit scaffold fixing structure, and 22-fast-assemblings limit foot prop position restrainer tool structure, and 23-is fast
Dress limit the 6th ontology of foot prop.
Specific embodiment
The utility model is described in further detail below with reference to embodiment.
Embodiment
As described in Fig. 1 to 8, a kind of foldable six rotor wing unmanned aerial vehicle, including body (7), horn, motor, the horn
It is connect with motor and body, the motor is connect with horn and wing respectively, further includes such as seat laterally folded in Fig. 7 and Fig. 6
(10) and longitudinal folding seat (11), laterally folded seat one end connects horn, and one end is connected to body (7), can make horn along
Horn rotates horizontally that horn is made to be folded in the body (7) two sides, wherein connecting the second horn (2) and the 6th horn (6)
Laterally folded seat one end be connected to the body (7) one end, second horn (2) and the 6th horn (6) can be made to be folded in
The upper space of body two sides connects third horn (3), laterally folded seat one end of the 5th horn (5) is connected to the body
(7) lower part can make third horn (3), the 5th horn (5) be folded in two sides middle space below the horn (6), longitudinal folding
Seat is separately connected body (7) and horn, and horn can be made to be folded along a longitudinal seat and rotate that horn is made to be folded in institute vertically downward
It states below body, wherein the longitudinal folding seat for connecting first horn (1) can make the first horn (1) exist to fold below body
Middle space below body, the longitudinal folding seat for connecting the 4th horn (4) can be such that the 4th horn (4) turns over to body lower section
Folding bottom space below body, bottom space space lower part in middle level.Wing also can horizontal direction horn direction rotate, make
Wing-folding is to horn two sides.Wherein body (7) can use carbon fibre material, horn, wing, laterally folded seat, longitudinal folding
Folded seat, long foot prop, short foot prop use aluminum alloy materials.
Wherein longitudinal folding seat includes the first noumenon (27) and the second ontology (16) and the first horn fixed structure (17),
The first noumenon (27) and the second ontology (16) are connected by the first horn fixed structure (17), the first noumenon (16)
With body (7) by screw connection, second ontology (16) connects with horn, when the first horn fixed structure (17) of release,
Second ontology (27) can be turned over downwards 180 ° maximum to the first noumenon (16).
Laterally folded seat third ontology (26) and the 4th ontology (19), the second horn fixed structure (18), described second
Horn fixed structure (18) includes internal screw thread, and the 4th ontology (19) includes external thread structure.Third ontology (26) passes through
Screw hole location is connect with the 4th ontology (19).Third ontology (26) connects horn, and the 4th ontology (19) connects body, when unclamping the
Two horn fixed structures (18), third ontology (26) can rotate horizontally 0 ° -120 ° along the 4th ontology (19).
Foldable unmanned plane further includes foldable GPS support rod (14), foldable compass support rod (15), foldable GPS
Support rod (14), foldable compass support rod (15) can be along the upper spaces of body longitudinal direction rotary folding to body upper.
Such as Fig. 1,4 Quick Release foot rest bases (8), (12), including 2 are symmetrically installed on the horn of 4 laterally folded seat connections
A short foot prop Quick Release foot rest base (8) and 2 long foot prop Quick Release foot rest base (12).The short foot prop Quick Release foot rest base (8), long foot prop
Quick Release foot rest base (12) is detachable limit mechanical structured member, when folding unmanned plane, can by short foot prop Quick Release foot rest base (8),
The fast quick-detach of long foot prop Quick Release foot rest base (12) reduces folding volume.
Such as Fig. 8, fast-assembling limit the 5th ontology (20) of foot prop is fixed on the second horn (2), third horn (3), the 5th horn
(5), on the 6th horn (6), it is firm to be fixed by screw.5th ontology (20) limits scaffold fixing structure by fast-assembling
(21) it is connect with fast-assembling limit the 6th ontology (23) of foot prop, passes through fast-assembling limit foot prop position restrainer tool structure (22) limit
The position of fixed fast-assembling limit the 6th ontology (23) of foot prop, guarantees the stability of entire foot prop.
In the present embodiment, portable six rotor wing unmanned aerial vehicle of a kind of novel foldable, folding mode are different from common six
Rotor wing unmanned aerial vehicle, using the folding mode of layered stereoscopic formula, 6 horns are divided into, in, the folding of three layers of bottom, make full use of sky
Between.The body, foot prop also have removable unloading functions.The length of the body: 1500mm, wide: 1350mm is high: 600mm.It folds
The length of the body afterwards: 650mm, wide: 430mm is high: 350mm.After visible fold, sky shared by the body is substantially reduced
Between, it is more convenient transport and carries.
The content being not described in detail in this specification is the prior art well known to professional and technical personnel in the art.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Made any modifications, equivalent replacements, and improvements etc., should be included in the utility model within the spirit and principle of utility model
Protection scope within.
Claims (8)
1. a kind of foldable six rotor wing unmanned aerial vehicle, including body (7), horn, motor, wing, the horn and motor and machine
Body (7) connection, the motor connect with horn and wing respectively, it is characterised in that: further include laterally folded seat (10) and
Longitudinal folding seat (11), described laterally folded seat one end connect horn, and one end connects body (7), horn can be made along body
(7) it rotates horizontally to making horn be folded in the body (7) two sides, wherein connecting the second horn (2) and the 6th horn (6)
Laterally folded seat one end is connected to the body (7) one end, and second horn (2) and the 6th horn (6) can be made to be folded in machine
Body two sides, connection third horn (3), the 5th horn (5) laterally folded seat one end be connected to the body (7) lower part, can make
The third horn (3), the 5th horn (5) are folded in middle space below the body (7), the longitudinal folding seat difference
Body (7) and horn are connected, the horn can be made to rotate vertically downward along body (7) to make horn be folded in the body
Lower section, wherein the longitudinal folding seat for connecting the first horn (1) can make the first horn (1) to fold below body under the body
The middle space of side, the longitudinal folding seat of the 4th horn (4) of connection can make the 4th horn (4) to fold below body in the machine
Bottom space below body, bottom space space lower part in middle level.
2. foldable six rotor wing unmanned aerial vehicle as described in claim 1 a kind of, it is characterised in that: the longitudinal folding seat includes
The first noumenon (16) and the second ontology (27) and the first horn fixed structure (17), the first noumenon (16) and the second ontology
(27) it is connected by the first horn fixed structure (17), the first noumenon (16) and body (7) connection, second ontology
(27) it is connected with horn, when unclamping the first horn fixed structure (17), second ontology (27) can be along the first noumenon (16)
Longitudinal direction is turned over downwards most 180 °.
3. foldable six rotor wing unmanned aerial vehicle as described in claim 1 a kind of, it is characterised in that: the laterally folded seat includes
Third ontology (26) and the 4th ontology (19), the second horn fixed structure (18), the 4th ontology (19) include external screw thread
Fixed structure, the second horn fixed structure (18) include internal screw thread fixed structure, and third ontology (26) passes through screw hole location and the
Four ontologies (19) connection, third ontology (26) are capable of fixing horn, when the second horn fixed structure (18) of release, third ontology (26)
0 ° -120 ° can be rotated horizontally along the 4th ontology (19).
4. a kind of foldable six rotor wing unmanned aerial vehicle as described in claim 1, it is characterised in that: including foldable GPS support rod
(14), foldable compass support rod (15), the foldable GPS support rod (14), foldable compass support rod (15) can be along machines
Body longitudinal direction is folded to the upper space of body upper.
5. foldable six rotor wing unmanned aerial vehicle of one kind as described in one of claim 1-4, it is characterised in that: the wing energy water
It puts down to horn direction and rotates, make wing-folding to horn two sides.
6. foldable six rotor wing unmanned aerial vehicle of one kind as described in one of claim 1-4, it is characterised in that: connect in laterally folded seat
4 Quick Release foot rest bases (8), (12) are respectively symmetrically installed, including 2 short foot prop Quick Release foot rest base (8) and 2 long on the horn connect
Foot prop Quick Release foot rest base (12), the short foot prop Quick Release foot rest base (8), long foot prop Quick Release foot rest base (12) are detachable position restrainer
Long foot prop (9), short foot prop (13) fast quick-detach can be reduced folding volume when folding unmanned plane by tool structural member.
7. a kind of foldable six rotor wing unmanned aerial vehicle as claimed in claim 6, it is characterised in that: the body (7) uses carbon
Fibrous material, horn, wing, laterally folded seat, longitudinal folding seat, long foot prop, short foot prop use aluminum alloy materials, compare other
Material, carbon fibre material and aluminum alloy materials can guarantee reduces weight under the premise of unmanned plane is firm as far as possible.
8. a kind of foldable six rotor wing unmanned aerial vehicle as claimed in claim 6, it is characterised in that the short foot prop Quick Release foot rest base
(8), long foot prop Quick Release foot rest base (12) limits scaffold fixing structure comprising fast-assembling limit the 5th ontology (20) of foot prop, fast-assembling
(21), fast-assembling limit foot prop position restrainer tool structure (22), fast-assembling limit the 6th ontology (23) of foot prop, fast-assembling limit foot prop the
Five ontologies (20) are fixed on the horn of laterally folded seat connection, are fixed by screw, the fast-assembling limits the 5th ontology of foot prop
(20) it limits the 6th ontology (23) of foot prop with the fast-assembling by fast-assembling limit scaffold fixing structure (21) to connect, by described fast
Dress limit foot prop position restrainer tool structure (22) limits the position of fast-assembling limit the 6th ontology (23) of foot prop, guarantees entire foot prop
Stability.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721314363 | 2017-10-12 | ||
| CN2017213143638 | 2017-10-12 |
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| Publication Number | Publication Date |
|---|---|
| CN208515811U true CN208515811U (en) | 2019-02-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201721459142.XU Active CN208515811U (en) | 2017-10-12 | 2017-11-06 | A kind of foldable six rotor wing unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110065617A (en) * | 2019-05-10 | 2019-07-30 | 苏州臻迪智能科技有限公司 | Folding unmanned plane structure and unmanned plane |
| CN110723273A (en) * | 2019-07-02 | 2020-01-24 | 翔升（上海）电子技术有限公司 | Arm locking device and aircraft |
-
2017
- 2017-11-06 CN CN201721459142.XU patent/CN208515811U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110065617A (en) * | 2019-05-10 | 2019-07-30 | 苏州臻迪智能科技有限公司 | Folding unmanned plane structure and unmanned plane |
| CN110723273A (en) * | 2019-07-02 | 2020-01-24 | 翔升（上海）电子技术有限公司 | Arm locking device and aircraft |
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