CN206265286U - A kind of portable folding multi-rotor unmanned aerial vehicle - Google Patents
A kind of portable folding multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN206265286U CN206265286U CN201621095135.1U CN201621095135U CN206265286U CN 206265286 U CN206265286 U CN 206265286U CN 201621095135 U CN201621095135 U CN 201621095135U CN 206265286 U CN206265286 U CN 206265286U
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- transverse arm
- foot stool
- connector
- connecting plate
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Abstract
The utility model discloses a kind of portable folding multi-rotor unmanned aerial vehicle, including fuselage, laterally folded component and longitudinal folding component, the laterally folded component is connected with fuselage, the longitudinal folding component is connected with laterally folded component, and fuselage is made up of casing, head, cover, rear lid case and electronic component link；Laterally folded component includes foot stool fold mechanism and transverse arm fold mechanism, the foot stool fold mechanism is connected with transverse arm fold mechanism, the foot stool fold mechanism is made up of foot stool and foot stool connector, and transverse arm fold mechanism is made up of side connecting plate, upper junction plate, guide pad one, " Z " type bar, transverse arm connector and transverse arm；Longitudinal folding component includes lower triangular connecting plate, upper triangle connection element, guide pad two, " one " word bar, trailing arm connector, trailing arm and flight motor mount, press close to the double folding method of fuselage by laterally folded component and longitudinal folding member collapses, realize multi-rotor unmanned aerial vehicle farthest to fold, be convenient for carrying transport.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, and specifically, the utility model is related to a kind of portable folding many
Rotor wing unmanned aerial vehicle.
Background technology
Multi-rotor unmanned aerial vehicle on the market has much now, has many uses too general, such as personal consumption tourism is taken photo by plane, business
Video display are taken photo by plane, logistics distribution, security are speedily carried out rescue work, most of general size smart with big boundary, and this kind of product is in order to conveniently take as far as possible
Band, the very little for deliberately designing so, on the one hand loses the relative stability energy of unmanned plane, on the other hand loses again
Cruising time；But it is actual to carry and inconvenient, it is outgoing to find a view when taking photo by plane, otherwise a tooth dance tooth pawl is portable, or extremely
Awkward tying with a rope round the neck and hands is carried, or being exactly the exclusive toy of car cluster, as the regionality very strong unmanned plane of limitation, basic band is not
Go out；Also part unmanned plane, for convenience of carrying, specially designs especially small, as a result with toy for children one also to cater to consumer
As.
Utility model content
The utility model provides a kind of portable folding multi-rotor unmanned aerial vehicle, by double folding method, realize many rotors without
Man-machine folding, is convenient for carrying transport.
To achieve these goals, the technical scheme that the utility model is taken is：A kind of many rotors of portable folding nobody
Machine, including fuselage, laterally folded component and longitudinal folding component, wherein the laterally folded component is connected with fuselage, it is described vertical
It is connected with laterally folded component to foldable assembly, the fuselage is by casing, head, cover, rear lid case and electronic component link
Composition, the head is connected with casing, and the cover is connected with casing, and the rear lid case is connected with the rear end of casing, the electricity
Subcomponent link is located between casing and cover, and the electronic component link is connected with casing, is provided with the casing
Battery tank tower, the cover both sides are provided with laterally folded component mounting hole, and the laterally folded component is in fuselage interior and electronics
Element link is connected, and fuselage is then stretched out from laterally folded component mounting hole, and the rear lid case is provided with buckle, and rear lid case leads to
Buckle and casing clamping are crossed, for self-contained battery tank tower.
Preferably, the laterally folded component includes foot stool fold mechanism and transverse arm fold mechanism, wherein the foot stool is rolled over
Folded mechanism is connected with transverse arm fold mechanism.
Preferably, the foot stool fold mechanism is made up of foot stool and foot stool connector, and the foot stool connector connects with foot stool
Connect；The transverse arm fold mechanism is made up of side connecting plate, upper junction plate, guide pad one, " Z " type bar, transverse arm connector and transverse arm,
Wherein described side connecting plate is provided with two, and the side connecting plate is connected by screw with electronic component link, the upper company
Fishplate bar is connected with two side connecting plates respectively by screw, and the guide pad one is connected with one of side connecting plate by screw
Connect, and the two ends of the guide pad one are provided with pilot hole one, " Z " the type bar is connected with pilot hole one, and can be slided along pilot hole one
Dynamic, the transverse arm connector lower end is connected by rotary pair with two side connecting plates, and the transverse arm is socketed with transverse arm connector.
Preferably, the foot stool lower end outside is provided with lower triangular connecting plate folded slot, and middle outside is provided with transverse arm folded slot,
Upper end outside is provided with transverse arm connector folded slot, and the foot stool connector upper end is arranged with two folding ears, and in the folding
Folded ear inner side is provided with foot stool folded piece one.
Preferably, two chutes one collinearly are provided with the side connecting plate, " Z " the type bar upper end is provided with toggle one, and
The toggle one stretches out upper junction plate, is arranged with stage clip one in " Z " type bar lower end in addition, and lock is provided with " Z " type bar lower end side
Bar one, and after the two ends of the locking bar one are installed with " Z " type bar in the chute one that is located just on side connecting plate, the transverse arm connects
Fitting upper end is provided with locked groove one, and the transverse arm connector lower end is provided with foot stool folded piece two, the transverse arm connector lower end and pin
Frame connector upper end is connected by rotary pair, and the rotary pair is coaxial with the rotary pair that side connecting plate is formed with transverse arm connector
Line.
Preferably, the longitudinal folding component includes lower triangular connecting plate, upper triangle connection element, guide pad two, " one " word
Bar, trailing arm connector, trailing arm and flight motor mount, wherein the lower triangular connecting plate passes through screw and upper triangle connection element
Connection, the upper triangle connection element is socketed with transverse arm, and the guide pad two passes through screw connection with lower triangular connecting plate, and described
The two ends of guide pad two are provided with pilot hole two, and " one " the word bar is connected with pilot hole two, and can be slided along pilot hole two, described vertical
Arm connector is connected with lower triangular connecting plate and upper triangle connection element by rotary pair, described trailing arm one end and trailing arm connector set
Connect, other end is socketed with flight motor mount.
Preferably, the lower triangular connecting plate is provided with two the first holes, is collinearly provided with lower triangular connecting plate in addition
Two chutes two, are arranged with stage clip two on " one " the word bar, " one " the word boom end is provided with locking bar two, and the locking bar two
In the chute two being located just on lower triangular connecting plate after being installed with " one " word bar, it is provided with the upper end of the locking bar two dials in addition
Button two, and the toggle two stretches out triangle connection element, the trailing arm connector is provided with the second hole, and the trailing arm connector
Rotary pair is formed by the second hole and the first hole, locked groove two is provided with the trailing arm connector in addition.
The utility model presses close to the double folding method of fuselage by laterally folded component and longitudinal folding member collapses, realizes
The folding of multi-rotor unmanned aerial vehicle, is convenient for carrying transport, and the foldable structure to multi-rotor unmanned aerial vehicle done brand-new design, uses
The beneficial effect of above technical scheme is：The second hole being provided with by trailing arm connector be provided with lower triangular connecting plate
One rotary pair for being formed, realizes the foldable of trailing arm, and the trailing arm connector is provided with locked groove two in addition, is driven by toggle two
Dynamic locking bar two pins trailing arm connector, realizes the stability of structure after trailing arm launches；The transverse arm connector lower end passes through back
Turn pair to be connected with two side connecting plates, and the transverse arm connector lower end is connected with foot stool connector upper end by rotary pair,
And the rotary pair coaxial line that the rotary pair is formed with transverse arm connector and side connecting plate, realize transverse arm and indulging of be connected with transverse arm
To the foldable of foldable assembly, the foot stool connector upper end is arranged with two folding ears in addition, and is folded in ear described
Side is provided with foot stool folded piece one, and the transverse arm connector lower end is provided with foot stool folded piece two, it is ensured that folded into and pin in transverse arm
When frame is fitted, can by the active force between foot stool folded piece two and foot stool folded piece one, drive foot stool continue to fold into it is perpendicular
Straight state is fitted with fuselage, is realized multi-rotor unmanned aerial vehicle and is farthest folded.
Brief description of the drawings
Fig. 1 is that portable folding multi-rotor unmanned aerial vehicle launches assembling structure schematic diagram；
Fig. 2 is portable folding multi-rotor unmanned aerial vehicle fold assembling structural representation；
Fig. 3 is fuselage explosive view；
Fig. 4 is laterally folded component and foot stool assembling structure schematic diagram；
Fig. 5 is laterally folded component and foot stool explosive view；
Fig. 6 is longitudinal folding component explosive view；
Fig. 7 is upper triangle connection element structural representation；
Fig. 8 is transverse arm connecting-piece structure schematic diagram；
Fig. 9 is trailing arm connecting-piece structure schematic diagram；
Figure 10 is the partial enlarged drawing of the installation site of stage clip one；
Figure 11 is the partial enlarged drawing of the installation site of stage clip two；
Wherein：
1st, fuselage；2nd, laterally folded component；3rd, longitudinal folding component；10th, casing；11st, head；12nd, cover；12-1, horizontal stroke
To foldable assembly mounting hole；13rd, rear lid case；13-1, buckle；14th, battery tank tower；15th, electronic component link；20th, foot stool；
20-1, lower triangular connecting plate folded slot；20-2, transverse arm folded slot；20-3, transverse arm connector folded slot；21st, foot stool connector；
21-1, folding ear；21-2, foot stool folded piece one；22nd, side connecting plate；22-1, chute one；23rd, upper junction plate；24th, guide pad
One；25th, " Z " type bar；25-1, toggle one；25-2, locking bar one；25-3, stage clip one；26th, transverse arm connector；26-1, locked groove one；
26-2, foot stool folded piece two；27th, transverse arm；30th, lower triangular connecting plate；30-1, the first hole；30-2, chute two；31st, upper triangle connects
Fitting；32nd, guide pad two；33rd, " one " word bar；33-1, locking bar two；33-2, toggle two；33-3, stage clip two；34th, trailing arm connection
Part；34-1, the second hole；34-2, locked groove two；35th, trailing arm；36th, flight motor mount.
Specific embodiment
Below against accompanying drawing, by the description to embodiment, specific embodiment of the present utility model is made further in detail
Thin explanation, it is therefore an objective to help those skilled in the art have to design of the present utility model, technical scheme it is more complete, accurate and
Deep understanding, and contribute to it to implement.
As shown in Figure 1 to 11, the utility model is a kind of portable folding multi-rotor unmanned aerial vehicle, by double folding
Method, realizes the folding of multi-rotor unmanned aerial vehicle, is convenient for carrying transport, improves its portability.
Specifically, as shown in Figure 1 to 11, including machine 1, laterally folded component 2 and longitudinal folding component 3, wherein institute
State laterally folded component 2 to be connected with fuselage 1, the longitudinal folding component 3 is connected with laterally folded component 2, as shown in figure 3, institute
State fuselage 1 to be made up of casing 10, head 11, cover 12, rear lid case 13 and electronic component link 15, the head 11 and casing
10 connections, the cover 12 is connected with casing 10, and the rear lid case 13 is connected with the rear end of casing 10, the electronic component connection
Frame 15 is located between casing 10 and cover 12, and the electronic component link 15 is connected with casing 10, is set in the casing 10
There is battery tank tower 14, the both sides of the cover 12 are provided with laterally folded component mounting hole 12-1, and the laterally folded component 2 is in fuselage
1 inside is connected with electronic component link 15, then stretches out fuselage 1, the bonnet from laterally folded component mounting hole 12-1
Shell 13 is provided with buckle 13-1, and rear lid case 13 passes through buckle 13-1 and the clamping of casing 10, for self-contained battery tank tower 14.
As shown in Figure 4, Figure 5, the laterally folded component 2 includes foot stool fold mechanism and transverse arm fold mechanism, wherein institute
Foot stool fold mechanism is stated to be connected with transverse arm fold mechanism.
The foot stool fold mechanism is made up of foot stool 20 and foot stool connector 21, and the foot stool connector 21 connects with foot stool 20
Connect；As shown in figure 5, the transverse arm fold mechanism is by side connecting plate 22, upper junction plate 23, guide pad 1, " Z " type bar 25, horizontal stroke
Arm connector 26 and transverse arm 27 are constituted, and as shown in Figure 4, Figure 5, wherein the side connecting plate 22 is provided with two, and the side connects
Plate 22 is connected by screw with electronic component link 15, the upper junction plate 23 by screw respectively with two side connecting plates 22
Connection, the guide pad 1 is provided with one of side connecting plate 22 by screw connection, and the two ends of the guide pad 1
Pilot hole one, " Z " the type bar 25 is connected with pilot hole one, and can be slided along pilot hole one, transverse arm connector as shown in Figure 8
26 lower ends are connected by rotary pair with two side connecting plates 22, and the transverse arm 27 is socketed with transverse arm connector 26.
As shown in Figure 4, Figure 5, the lower end outside of the foot stool 20 is provided with lower triangular connecting plate folded slot 20-1, and middle outside sets
There is transverse arm folded slot 20-2, upper end outside is provided with transverse arm connector folded slot 20-3, and the upper end of foot stool connector 21 symmetrically sets
There are two folding ear 21-1, and the 21-2 of foot stool folded piece one is provided with the inside of the folding ear 21-1.
Two 22-1 of chute one collinearly are provided with the side connecting plate 22, the upper end of " Z " type bar 25 is provided with the 25- of toggle one
1, and the 25-1 of the toggle one stretches out upper junction plate 23, the 25-3 of stage clip one is arranged with the lower end of " Z " type bar 25 in addition, in " Z " type
Side is located just at after the lower end side of bar 25 is provided with the 25-2 of locking bar one, and the 25-2 two ends of the locking bar one are installed with " Z " type bar 25
In the 22-1 of chute one on connecting plate 22, the upper end of transverse arm connector 26 as shown in Figure 8 is provided with the 26-1 of locked groove one, and the transverse arm connects
The lower end of fitting 26 is provided with the 26-2 of foot stool folded piece two, and the lower end of transverse arm connector 26 is with the upper end of foot stool connector 21 by revolution
Pair connection, and the rotary pair coaxial line that the rotary pair is formed with transverse arm connector 26 and side connecting plate 22.
As shown in fig. 6, the longitudinal folding component 3 includes lower triangular connecting plate 30, upper triangle connection element 31, guide pad two
32nd, " one " word bar 33, trailing arm connector 34, trailing arm 35 and flight motor mount 36, as shown in Figure 1 and Figure 2, wherein under described
Triangular connecting plate 30 is connected by screw with upper triangle connection element 31 as shown in Figure 7, the upper triangle connection element 31 and transverse arm
27 sockets, the guide pad 2 32 is provided with and is led with lower triangular connecting plate 30 by screw connection, and the two ends of the guide pad 2 32
To hole two, " one " the word bar 33 is connected with pilot hole two, and can be slided along pilot hole two, trailing arm connector as shown in Figure 9
34 are connected with lower triangular connecting plate 30 and upper triangle connection element 31 by rotary pair, the one end of the trailing arm 35 and trailing arm connector 34
Socket, other end is socketed with flight motor mount 36.
As shown in fig. 6, the lower triangular connecting plate 30 is provided with two the first hole 30-1, in addition in lower triangular connecting plate 30
On be collinearly provided with two 30-2 of chute two, the 33-3 of stage clip two, the end of " one " word bar 33 are arranged with " one " the word bar 33
It is provided with the 33-1 of locking bar two, and is located just on lower triangular connecting plate 30 after the 33-1 of the locking bar two is installed with " one " word bar 33
In the 30-2 of chute two, the 33-2 of toggle two is provided with the 33-1 upper ends of the locking bar two in addition, and the 33-2 of the toggle two stretches out three
Angle connector 31, trailing arm connector 34 as shown in Figure 9 is provided with the second hole 34-1, and the trailing arm connector 34 passes through second
Hole 34-1 and the first hole 30-1 forms rotary pair, is provided with the 34-2 of locked groove two on the trailing arm connector 34 in addition.
Specific works mode is illustrated with specific embodiment below：
Embodiment：
When we go out to need to carry this unmanned plane, us are carried for convenience needs the unmanned plane before not dismantling
Put and folded, because the 33-2 of toggle two is provided with the 33-1 upper ends of the locking bar two, and the 33-2 of the toggle two stretches out three
Angle connector 31, the 33-2 of toggle two is stirred along the 30-2 of chute two on lower triangular connecting plate 30 towards guide pad 2 32, by
In the 33-3 of stage clip two is arranged with " one " the word bar 33, the end of " one " word bar 33 is provided with the 33-1 of locking bar two, makes and toggle
Overcome under the guide effect of the pilot holes two of the 33-1 of locking bar two on the 30-2 of chute two and guide pad 2 32 of two 33-2 connections as
The elastic force of the 33-3 of stage clip two shown in Figure 11 is exited from the 34-2 of locked groove two on trailing arm connector 34, then manually by trailing arm 35
Folded towards near the direction of transverse arm 27, due to being provided with two the first hole 30-1 on the lower triangular connecting plate 30, trailing arm connects
Fitting 34 is provided with the second hole 34-1, and the trailing arm connector 34 forms revolution by the second hole 34-1 and the first hole 30-1
Pair, so trailing arm 35 can form rotary pair around by the second hole 34-1 and the first hole 30-1 together with flight motor mount 36
It is rotated by 90 °, realizes the folding of trailing arm 35 and flight motor mount 36.
After the completion of action folding as above, because the upper end of " Z " type bar 25 is provided with the 25-1 of toggle one, and the toggle one
25-1 stretches out upper junction plate 23, is arranged with the 25-3 of stage clip one in the lower end of " Z " type bar 25 in addition, is set in the lower end side of " Z " type bar 25
There are the 25-2 of locking bar one, and the 25-2 two ends of the locking bar one with the cunning being located just at after the installation of " Z " type bar 25 on side connecting plate 22
In the 22-1 of groove one, the upper end of transverse arm connector 26 is provided with the 26-1 of locked groove one, so by the 25-1 of toggle one along side connecting plate 22
On the 22-1 of chute one stirred towards guide pad 1, make the 25-2 of locking bar one that is connected with " Z " type bar 25 in the 22-1 of chute one and
The 25-3 of stage clip one as shown in Figure 10 is overcome under the guide effect of the pilot hole one on guide pad 1 from transverse arm connector 26
The 26-1 of locked groove one in exit, then manually by transverse arm 27 towards near fuselage 1 direction fold, due to the transverse arm connector
26 lower ends are connected with the upper end of foot stool connector 21 by rotary pair, and the rotary pair is with transverse arm connector 26 and the shape of side connecting plate 22
Into rotary pair coaxial line, with transverse arm 27 with the longitudinal folding component 3 folded up around by transverse arm connector 26
The rotary pair rotation formed with side connecting plate 22, until the lower triangular connecting plate 30 in the longitudinal folding component 3 and foot stool 20
The lower triangular connecting plate folded slot 20-1 contacts that lower end outside is provided with, the transverse arm 27 is provided with transverse arm folding with the centre of foot stool 20 outside
Folded groove 20-2 contacts, the transverse arm connector 26 is provided with transverse arm connector folded slot 20-3 and contacts with the upper end of foot stool 20 outside, by
Ear 21-1 are folded in being arranged with two in the upper end of foot stool connector 21, and foot stool is provided with the inside of the folding ear 21-1
The 21-2 of folded piece one, is provided with the 26-2 of foot stool folded piece two, now transverse arm connector 26 in the lower end of transverse arm connector 26 in addition
On the 26-2 of foot stool folded piece two contacted with the 21-2 of foot stool folded piece one folded on the inside of ear 21-1, when we continue hand foldable
When, the folding ear 21-1 shapes that now foot stool 20 can be with transverse arm 27 together on by transverse arm connector 26 and foot stool connector 21
Into the secondary rotation of rotation, until foot stool 20 rotates to vertical state, complete the folding of whole multi-rotor unmanned aerial vehicle, finally fold
Come as shown in Fig. 2 now trailing arm 35 be in the parastate of transverse arm 27, transverse arm 27 fits completely with foot stool 20, foot stool 20 and machine
Body 1 is fitted completely, and what is so folded is more thorough, and profile is more upright regular, it is easier to deposits in knapsack, is easy to carry.
When we need to launch the trailing arm 35 of unmanned plane, as long as going to launch trailing arm 35 manually, launch in trailing arm 35
During, in the presence of the 33-3 of stage clip two, the 33-1 of locking bar two always with the contact slide of trailing arm connector 34, until trailing arm 35 is complete
Complete to launch, the 33-1 of the locking bar two snaps in the 34-2 of locked groove two on trailing arm connector 34 under the elastic force effect of the 33-3 of stage clip two
In, realize the locking to trailing arm 35；Then the transverse arm 27 of unmanned plane is launched, during transverse arm 27 launches, with transverse arm 27
Expansion, when the 26-2 of foot stool folded piece two on transverse arm connector 26 is to folding the 21-2's of foot stool folded piece one on the inside of ear 21-1
After active force is released, foot stool 20 launches, and continues with the expansion of transverse arm 27, in the presence of the 25-3 of stage clip one, the 25-2 of locking bar one
Always with the contact slide of transverse arm connector 26, until transverse arm 27 is fully deployed, bullets of the 25-2 of the locking bar one in the 25-3 of stage clip one
Snapped under power effect in the 26-1 of locked groove one on transverse arm connector 26, realize the locking to transverse arm 27, finally launched such as Fig. 1 institutes
Show, it is ensured that the stability of whole multi-rotor unmanned aerial vehicle structure.
The utility model is exemplarily described above in association with accompanying drawing, it is clear that the utility model is implemented not
Limited by aforesaid way, as long as employ the various unsubstantialities that method design of the present utility model and technical scheme are carried out
Improvement；Or it is not improved, above-mentioned design of the present utility model and technical scheme are directly applied into other occasions, at this
Within the protection domain of utility model.
Claims (7)
1. a kind of portable folding multi-rotor unmanned aerial vehicle, it is characterised in that：Including fuselage, laterally folded component and longitudinal folding group
Part, wherein the laterally folded component is connected with fuselage, the longitudinal folding component is connected with laterally folded component, the fuselage
It is made up of casing, head, cover, rear lid case and electronic component link, the head is connected with casing, the cover and casing
Connection, the rear lid case is connected with the rear end of casing, and the electronic component link is located between casing and cover, and the electricity
Subcomponent link is connected with casing, and battery tank tower is provided with the casing, and the cover both sides are provided with laterally folded component peace
Dress hole, the laterally folded component is connected in fuselage interior with electronic component link, then from laterally folded component mounting hole
In stretch out fuselage, the rear lid case is provided with buckle, rear lid case by buckle and casing clamping, for self-contained battery tank tower.
2. a kind of portable folding multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：Described laterally folded group
Part includes foot stool fold mechanism and transverse arm fold mechanism, wherein the foot stool fold mechanism is connected with transverse arm fold mechanism.
3. a kind of portable folding multi-rotor unmanned aerial vehicle according to claim 2, it is characterised in that：The foot stool folding machine
Structure is made up of foot stool and foot stool connector, and the foot stool connector is connected with foot stool；The transverse arm fold mechanism by side connecting plate,
Upper junction plate, guide pad one, " Z " type bar, transverse arm connector and transverse arm composition, wherein the side connecting plate is provided with two, and institute
Side connecting plate is stated to be connected with electronic component link by screw, the upper junction plate by screw respectively with two side connecting plates
Connection, the guide pad one passes through screw connection with one of side connecting plate, and the two ends of the guide pad one are provided with pilot hole
One, " Z " the type bar is connected with pilot hole one, and can be slided along pilot hole one, and the transverse arm connector lower end passes through rotary pair
It is connected with two side connecting plates, the transverse arm is socketed with transverse arm connector.
4. a kind of portable folding multi-rotor unmanned aerial vehicle according to claim 3, it is characterised in that：Outside the foot stool lower end
Side is provided with lower triangular connecting plate folded slot, and middle outside is provided with transverse arm folded slot, and upper end outside is provided with transverse arm connector folded slot,
The foot stool connector upper end is arranged with two folding ears, and is provided with foot stool folded piece one on the inside of the folding ear.
5. a kind of portable folding multi-rotor unmanned aerial vehicle according to claim 3, it is characterised in that：On the side connecting plate
Two chutes one collinearly are provided with, " Z " the type bar upper end is provided with toggle one, and the toggle one stretches out upper junction plate, exists in addition
" Z " type bar lower end is arranged with stage clip one, and locking bar one, and the two ends of the locking bar one are provided with " Z " in the side of " Z " type bar lower end
Type bar is located just in the chute one on side connecting plate after installing, and the transverse arm connector upper end is provided with locked groove one, the transverse arm
Connector lower end is provided with foot stool folded piece two, and the transverse arm connector lower end is connected with foot stool connector upper end by rotary pair,
And the rotary pair coaxial line that the rotary pair is formed with transverse arm connector and side connecting plate.
6. a kind of portable folding multi-rotor unmanned aerial vehicle according to any one of claim 1,3, it is characterised in that：It is described
Longitudinal folding component include lower triangular connecting plate, upper triangle connection element, guide pad two, " one " word bar, trailing arm connector, trailing arm and
Flight motor mount, wherein the lower triangular connecting plate is connected by screw with upper triangle connection element, the upper triangle joint
Part is socketed with transverse arm, and the guide pad two is provided with and is led with lower triangular connecting plate by screw connection, and the two ends of the guide pad two
To hole two, " one " the word bar is connected with pilot hole two, and can be slided along pilot hole two, and the trailing arm connector connects with lower triangle
Fishplate bar and upper triangle connection element are by rotary pair connection, described trailing arm one end and the socket of trailing arm connector, other end and flight
Motor mount is socketed.
7. a kind of portable folding multi-rotor unmanned aerial vehicle according to claim 6, it is characterised in that：The lower triangle joint
Plate is provided with two the first holes, is collinearly provided with two chutes two on lower triangular connecting plate in addition, is arranged on " one " the word bar
There is a stage clip two, be located just at down after " one " the word boom end is provided with locking bar two, and the locking bar two is installed with " one " word bar
In chute two on triangular connecting plate, toggle two is provided with the upper end of the locking bar two in addition, and the toggle two stretches out triangle
Connector, the trailing arm connector is provided with the second hole, and the trailing arm connector forms revolution by the second hole with the first hole
Pair, is provided with locked groove two on the trailing arm connector in addition.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621095135.1U CN206265286U (en) | 2016-09-30 | 2016-09-30 | A kind of portable folding multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621095135.1U CN206265286U (en) | 2016-09-30 | 2016-09-30 | A kind of portable folding multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206265286U true CN206265286U (en) | 2017-06-20 |
Family
ID=59037307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621095135.1U Expired - Fee Related CN206265286U (en) | 2016-09-30 | 2016-09-30 | A kind of portable folding multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206265286U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379514A (en) * | 2016-09-30 | 2017-02-08 | 深圳市高智尚创新科技有限公司 | Portable foldable multi-rotor unmanned aerial vehicle |
| WO2019024541A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市道通智能航空技术有限公司 | Arm and unmanned aerial vehicle |
-
2016
- 2016-09-30 CN CN201621095135.1U patent/CN206265286U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379514A (en) * | 2016-09-30 | 2017-02-08 | 深圳市高智尚创新科技有限公司 | Portable foldable multi-rotor unmanned aerial vehicle |
| CN106379514B (en) * | 2016-09-30 | 2019-08-20 | 深圳市高智尚创新科技有限公司 | A kind of portable folding multi-rotor unmanned aerial vehicle |
| WO2019024541A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市道通智能航空技术有限公司 | Arm and unmanned aerial vehicle |
| CN109383739A (en) * | 2017-08-04 | 2019-02-26 | 深圳市道通智能航空技术有限公司 | A kind of horn and unmanned plane |
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