CN207773428U - A kind of Portable unmanned machine - Google Patents
A kind of Portable unmanned machine Download PDFInfo
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- CN207773428U CN207773428U CN201721055081.0U CN201721055081U CN207773428U CN 207773428 U CN207773428 U CN 207773428U CN 201721055081 U CN201721055081 U CN 201721055081U CN 207773428 U CN207773428 U CN 207773428U
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- tripod
- portable unmanned
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Abstract
The utility model discloses a kind of Portable unmanned machines, including：Dish-shaped primary structural component has the main part for constituting dish-shaped periphery, and the engine department for protruding from main part at dish middle part is constituted positioned at main part side；Positioned at the main part other side, the cover portion for the cabin for protruding from main part is installed；There is certain thickness, periphery edge to be uniformly distributed at least three horns for being equipped with and flexing outward on main part periphery, and horn end is equipped with the blade and motor as power；Wherein, the inner fovea part in body peripheral edge is stretched into horn one end, and horizontally rotates with main body and connect；Horn is fixed on a turned position by a fixing piece；Main part be peripherally provided with by inner fovea part with the matched groove of horn shape, the notch end correspond to main part have with the matched recess portion of motor, be respectively used to accommodating horizontally rotate horn and motor to the groove.By upper, complete machine is flying saucer shape after the application folds, and fuselage arrangements of components is close, and space availability ratio is high, compacter.
Description
Technical field
The utility model is related to air vehicle technique fields, and in particular to a kind of Portable unmanned machine.
Background technology
Unmanned plane, that is, air-robot can replace the mankind to complete aerial work, and can form aerial platform, in conjunction with
Other component expands application.Currently, unmanned plane take photo by plane and entertain, agricultural, security protection, the fields such as electric power have shown wide hair
Exhibition foreground.
In existing load-carrying UAV system same in the market, it is polygonal shape to fold unmanned plane shape, even if folding
Poststack, occupied space is also bigger when transport, low space utilization.
Therefore, there is an urgent need for a kind of Portable unmanned machines to solve the above problems at present.
Utility model content
In view of this, the application provides a kind of Portable unmanned machine, after the horn folding of the Portable unmanned machine of the application
Complete machine is flying saucer shape, and body parts arrangement is close, and space availability ratio is high, and complete machine is compacter.
A kind of Portable unmanned machine of the application, including：
Dish-shaped primary structural component has the main part for constituting dish-shaped periphery, is located at main part side and constitutes dish middle part
Protrude from the engine department of main part；
Positioned at the main part other side, the cover portion for the cabin for protruding from main part is installed；
There is certain thickness, periphery edge to be uniformly distributed at least three machines for being equipped with and flexing outward on the main part periphery
Arm, horn end are equipped with the blade and motor as power；
Wherein, the inner fovea part in the body peripheral edge is stretched into described horn one end, and horizontally rotates with main body and connect；Pass through
Horn is fixed on a turned position by one fixing piece；
The main part is peripherally provided with by the inner fovea part and is corresponded to the matched groove of horn shape, the notch end
Main part have with the matched recess portion of the motor, be respectively used to accommodating horizontally rotate the horn and electricity to the groove
Machine.
By upper, the horn of the unmanned plane of the application may be implemented to be arranged in after rotating horn along horn rotary shaft
In the groove for housing the horn after rotary folding that one be arranged on unmanned plane primary structural component matches with the horn, folding
Poststack complete machine is flying saucer shape, and body parts arrangement is close, and space availability ratio is high, and machine shape size is compacter, when transport
Occupied space smaller, to be conducive to the convenient loading packing to unmanned plane and carrying.
Preferably, foot stool installing structure, the engine department and the cover portion are provided in the engine department and the cover portion
One bottom as unmanned plane is selected, removably in installing tripod on foot stool installing structure.
By upper, the Portable unmanned machine of the application by being provided with foot stool installing structure on engine department and the cover portion,
The engine department and the cover portion select one bottom as unmanned plane, removably in installing tripod on foot stool installing structure.
The voluntarily selection for being conducive to the different use demand of user is provided with thrust paddle or pulling force paddle on same unmanned plane, facilitates nobody
Machine uses, and is conducive to economize on resources.
Preferably, the foot stool installing structure includes：It is set on the surface of the engine department and the cover portion, inwardly prolongs
At least three hole slots stretched, and the direction convergence that extends internally；
The tripod, which corresponds to the mounting structure, has the insertion end that can be inserted into the hole slot.
Preferably, the hole slot engages with the insertion end or thread fiting mode assembles.
By upper, it is advantageously implemented the fast assembling-disassembling of tripod.Wherein, the tripod can also take folded form, that is, carry
When, it need not dismantle, need to only be folded.
Preferably, the inner fovea part in the body peripheral edge is stretched into described horn one end, and horizontally rotates with main body and connect；It is logical
It crosses a fixing piece and horn is fixed on certain turned position；
The main part is peripherally provided with by the inner fovea part and is corresponded to the matched groove of horn shape, the notch end
Main part have with the matched recess portion of the motor, be respectively used to accommodating horizontally rotate the horn and electricity to the groove
Machine.
By upper, the application may be implemented to be arranged in unmanned plane primary structural component after rotating horn along horn rotary shaft
In the groove for housing the horn after rotary folding that the one of upper setting matches with the horn, to be conducive to convenient pair
The loading packing of unmanned plane and carrying.
Preferably, inner fovea part described in main part has the vertical axis of horn one end described in rolling assembling, the fixing piece
For the vertical goat's horn bolt detachably installed.
By upper, the application can limit the rotating range of the horn and to rotary folding by the way that positioning limiting fixator is arranged
The horn afterwards is fixed.
Preferably, the engine department or/and the cover portion have hand-held through-hole close to outer circumference.
By upper, user can carry out the unmanned plane by the through-hole being arranged in the unmanned plane shell or the groove
It is hand-held to carry.
Preferably, there is the external components mounting portion outwardly protruded at the engine department or/and the cover portion center.
By upper, the external components mounting portion is conducive to the external components such as accommodating camera, battery.
Preferably, the external components mounting portion is equipped with camera.
By upper, be conducive to take photo by plane during unmanned plane during flying.By upper, be conducive to navigate during unmanned plane during flying
It claps.Also load (camera) can be selected when user selects pulling force paddle or thrust paddle to install according to different application range and scene
Mounting means is installed on engine department or/and the cover portion, i.e., the external components mounting portion for being both mountable to back may be used also
It is installed on the external components mounting portion (side of tripod installation) of underbelly, in general, is mounted on underbelly mounting portion
Location application range is wider, is suitable for various in working at height, looks down ground installation equipment and personnel etc., but in special circumstances
Under, for example when similar detection inspection tunnel upper wall situation, load is mounted on top mounting portion and is just particularly important.User can be with
According to oneself need be selectively mounted to engine department or/and the cover portion.
Preferably, the unmanned plane is in its horizontal section central symmetry.
By upper, be conducive to improve the stability during unmanned plane during flying.Wherein, asymmetry can also be selected as needed
Design.
In conclusion the horn of the Portable unmanned machine of the application may be implemented after rotating horn along horn rotary shaft
One be arranged on unmanned plane primary structural component is arranged in be used to house the horn after rotary folding with what the horn matched
Groove in, complete machine is flying saucer shape after folding, and the arrangement of body parts part is close, and space availability ratio is high, and machine shape size is more
Step up to gather, occupied space smaller when transport, to be conducive to the convenient loading packing to unmanned plane and carrying.And simultaneously, this Shen
Please by the way that positioning limiting fixator is arranged, the rotating range of the horn can be limited and the horn after rotary folding is consolidated
It is fixed.Meanwhile the application Portable unmanned machine on engine department and the cover portion by being provided with foot stool installing structure, the cabin
Portion and the cover portion select one bottom as unmanned plane, removably in installing tripod on foot stool installing structure.Be conducive to use
The voluntarily selection of the different use demand in family is provided with thrust paddle or pulling force paddle on same unmanned plane, convenient to make to unmanned plane
With, and be conducive to economize on resources.Through-hole or groove are additionally provided on the unmanned plane shell of the application in order to be carried out to unmanned plane
It is hand-held.It is more convenient to carry carrying.
Description of the drawings
Fig. 1 is the front view of Portable unmanned machine (thrust paddle) structure provided by the embodiments of the present application；
Fig. 2 is the stereogram of Portable unmanned machine provided by the embodiments of the present application (pulling force paddle) structure；
Solid when Fig. 3 is Portable unmanned machine (not installing tripod) horn unfolded state provided by the embodiments of the present application is shown
It is intended to；
Solid when Fig. 4 is Portable unmanned machine (not installing tripod) horn folded state provided by the embodiments of the present application is shown
It is intended to；
Fig. 5 is the enlarged diagram of horn provided by the embodiments of the present application and the junction of unmanned plane primary structural component；
Fig. 6 A are the decomposition diagram of foot stool installing structure provided by the embodiments of the present application (thread fiting mode assembly)；
Fig. 6 B are the signal after the assembly of foot stool installing structure provided by the embodiments of the present application (thread fiting mode assembly)
Figure；
Fig. 7 A are the decomposition diagram of foot stool installing structure provided by the embodiments of the present application (snap-fit)；
Fig. 7 B are the schematic diagram after the assembly of foot stool installing structure provided by the embodiments of the present application (snap-fit)；
Fig. 8 A are the vertical view of the clamping structure of foot stool installing structure provided by the embodiments of the present application (snap-fit)；
Fig. 8 B are the upward view of the clamping structure of foot stool installing structure provided by the embodiments of the present application (snap-fit)；
Fig. 8 C are the side view of the clamping structure of foot stool installing structure provided by the embodiments of the present application (snap-fit).
Specific implementation mode
The utility model is further described below in conjunction with the drawings and specific embodiments.
Embodiment one
As shown in figures 1-8, Portable unmanned machine provided by the present application, including：Dish-shaped primary structural component has and constitutes dish
The main part 10 on periphery constitutes the engine department 20 for protruding from main part at dish middle part positioned at main part side；Positioned at main part
The other side is equipped with the cover portion 30 for the cabin for protruding from main part；The main part periphery has certain thickness, periphery edge equal
Even distributing installation has at least three horns 40 flexed outward, horn end to be equipped with the blade 50 and motor as power
60；Foot stool installing structure 70 is provided on the engine department and the cover portion, the engine department and the cover portion select one conduct
The bottom of unmanned plane, removably in installation tripod 120 on foot stool installing structure.
Wherein, the tripod 120 includes but not limited to：Prop stand, parallel bars tripod or annular tripod；Wherein, the list
Tripod, quantity are at least 30, and one end is set on primary structural component or shell.
The parallel bars tripod, including 4 prop stands and two cross bar connected to it；Wherein, one end of two adjacent prop stands
It is set on the primary structural component or shell, the other end is as illustrated in figures 7 a-b, hinged by ball head universal and a cross bar；
One end of another two adjacent prop stand is set on the primary structural component or shell, and the other end as illustrated in figures 7 a-b, passes through bulb
Universal joint is hinged with another cross bar.
The annular tripod, including at least three prop stand and an annulus connected to it；Wherein, the one of the prop stand
End is set on the primary structural component or shell, and the other end as illustrated in figures 7 a-b, passes through ball head universal 130 and the circle
Ring is hinged.
Wherein, prop stand adapts to various landform, and parallel bars tripod adapts to relatively flat landform, and stationarity when landing is better than
Prop stand, annular tripod adapt to level terrain, and stationarity when landing is better than aforementioned two kinds of tripods.User can be according to specific
It is selected.
Wherein, the foot stool installing structure includes：It is set on the surface of the engine department and the cover portion, extends internally
At least three hole slots, and extend internally direction convergence；The tripod, which corresponds to the mounting structure, has the pluggable hole slot
Insertion end.
Wherein, the hole slot engages with tripod insertion end or thread fiting mode assembles.It is advantageously implemented foot as a result,
The fast assembling-disassembling of frame.Wherein, when hole slot and tripod insertion end are that thread fiting mode assembles, as shown in Fig. 6 A, 6B, wherein
Fig. 6 A show the schematic diagram of foot stool installing structure and tripod separated position.Wherein, Fig. 6 B show that tripod is tied with tripod installation
Schematic diagram after the connection of structure spiral.Wherein, the foot stool installing structure includes：One insertion end for being sheathed on the tripod
Outer wall is provided with external screw thread, and the set 71 and one that through-hole 711 is provided on wall be assemblied in it is described be set to the engine department and
The female helical structure of the settings of one of hole slot end on the surface of the cover portion and 71 screw-thread fits of the set 72；Its
In, it is provided with internal thread at the wall for the through-hole 711 being arranged on the set 71, by being inserted into and the matched spiral shell of 711 size of through-hole
Bolt is simultaneously tightened, and can closely connect the tripod for being inserted into the set 71 with the set 71.And further by it is described set 71 with it is described
Helical structure 72 is threadedly coupled the connection that tripod and unmanned plane engine department or cover portion can be achieved.
Wherein, when the hole slot and tripod insertion end are snap-fit, as illustrated in figures 7 a-b, the tripod installation knot
Structure includes：It is assemblied in the clamping structure 73 at the hole slot end of the engine department and the cover portion, is set to the tripod insertion end
The projecting shaft 74 of both sides, wherein the diameter that width and the projecting shaft 74 are provided on the wall of the clamping structure 73 matches
Card slot, wherein the card slot include perforation one end open rising part 731, horizontal component 732, fovea superior slot part 733
And recessed slot part 734.Wherein, the top that the connection structure is fixed in an one end is provided in the clamping structure 73
Spring 735.Wherein, the projecting shaft 74 can be through towards stretching outside the both sides of the insertion end of tripod, the projecting shaft
The two side of the tripod can also be the quantity being set on tripod lateral wall respectively to the axis stretched out outside tripod wall
Quantity for 2 projecting shaft, the card slot corresponds to 2.The engaging principle of the snap-in structure is：The foot of projecting shaft 74 will be provided with
Frame insertion end is inserted into the clamping structure 73, wherein the projecting shaft 74 is opened by the rising part 731 of clamping structure 73
The card slot is stretched at mouthful end, and is moved to horizontal component 732 all the way up, (in the process, the insertion end of tripod by from
The elastic force of spring), the tripod is rotated, makes its projecting shaft 74 along 732 transverse shifting of the horizontal component, finally in the bullet of spring
The projecting shaft 74 is pressed on into the recessed slot part 734 under the action of power.To complete the clamping of tripod and clamping structure 73.
When needing to dismantle tripod, tripod is moved up, so that projecting shaft 74 is moved upward to the horizontal component 732, rotates institute
Tripod is stated, its projecting shaft 74 is made to laterally move to rising part 731 along the horizontal component 732, further by projecting shaft 74
It is stretched out from the opening of rising part 731 and detaches it with clamping structure 73.By upper, by above-mentioned tripod quick-disassembly structure, favorably
In being rapidly assembled and disassembled for realization tripod.Wherein, the tripod can also take folded form.That is, when carrying, need not tear open
It unloads, need to only be folded.
Wherein, as in Figure 3-5, the inner fovea part in the body peripheral edge is stretched into described horn one end, and horizontal with main body
Rotation connection；Horn is fixed on certain turned position by a fixing piece；The main part is peripherally arranged by the inner fovea part
Have with the matched groove of horn shape, the notch end correspond to main part have with the matched recess portion of the motor, be respectively used to
It is accommodating to horizontally rotate the horn and motor to the groove.The application may be implemented to rotate horn along horn as a result,
One be arranged on unmanned plane primary structural component is arranged in after axis rotation to be used to house rotary folding with what the horn matched
In the groove of horn afterwards, to be conducive to the convenient loading packing to unmanned plane and carrying.
Wherein, inner fovea part described in main part has the vertical axis 80 of horn one end described in rolling assembling, the fixing piece
For the vertical goat's horn bolt 90 detachably installed.The application, can be to the rotation of the horn by the way that positioning limiting fixator is arranged as a result,
Turn range limit and the horn after rotary folding is fixed.
Wherein, the engine department or/and the cover portion have hand-held through-hole 100 close to outer circumference.User can as a result,
To carry out hand-held carrying to the unmanned plane by the through-hole being arranged in the unmanned plane shell or the groove.
Wherein, there is the external components mounting portion 110 outwardly protruded at the engine department or/and the cover portion center.By
This, the external components mounting portion is conducive to the external components such as accommodating camera, battery.
Wherein, it is additionally provided with flight control system HY-01 or PLC controller in the engine department or/and the cover portion,
Other stronger flight control systems of business specific aim can also be selected according to customer requirement.Wherein, flight control system is installed
In Portable unmanned machine integral central position.It is additionally provided with battery in the engine department or/and the cover portion, battery passes through inside
Circuit board is powered to motor.
Wherein, as shown in Figs. 1-2, the external components peace outwardly protruded at the engine department or/and the cover portion center
Dress portion 11 is equipped with camera.Be conducive to take photo by plane during unmanned plane during flying as a result,.
Wherein, the unmanned plane is its horizontal section central symmetry (also can non complete symmetry).Be conducive to improve nothing as a result,
Stability in man-machine flight course.
Wherein, the propeller includes：Propeller blade and propeller fixing sleeve；Wherein, the propeller blade
It is fixedly connected on the side of the propeller fixing sleeve；The propeller fixing sleeve is sheathed on institute by a propeller quick-disassembly structure
It states on the output shaft of motor.
Wherein, the propeller quick-disassembly structure includes：
It is set to the buckle being connect in the propeller fixing sleeve and with the propeller fixing sleeve inner wall by spring；Its
In, the output shaft of the motor is equipped with and the overhead kick being clasped.By above-mentioned propeller quick-disassembly structure, it is advantageously implemented
The fast assembling-disassembling of propeller.Wherein, propeller can need not also be dismantled, and directly be folded to it by foldable structure.
Wherein, the Portable unmanned machine further includes：Remote controler, with the flight control system HY-01 or PLC
Controller wireless signal connects.The remote control to Portable unmanned machine can be realized by the way that remote controler is arranged.
For the technical solution of further instruction the application, now by the operation principle explanation of the application Portable unmanned machine
It is as follows：
As shown in figure 4, when needing to pack unmanned plane or carry, the horn of unmanned plane is revolved along horn rotary shaft
Be arranged in after turning be arranged on unmanned plane primary structural component one with the horn match for after housing rotary folding
In the groove of horn；Meanwhile the dismounting of the propeller of unmanned plane either being folded, tripod is dismantled or folded, to be conducive to
Convenient loading packing and carrying to unmanned plane.And through-hole or groove are additionally provided on the unmanned plane shell of the application in order to right
Unmanned plane is held.It is more convenient to carry carrying.
Due to being both provided with foot stool installing structure on the engine department and cover portion of the application.Since the propeller is towards main knot
The side of component is arranged.
As shown in Figure 1, when the tripod is set on the engine department, the propeller is set as thrust paddle；By distant
Flight control system HY-01 either PLC controller and passes through flight control system HY-01 or PLC described in control device remote control
Controller further controls the rotation of the output shaft of motor, and the rotation of propeller is further driven by motor output shaft.With production
Raw upward thrust makes unmanned plane take off.Wherein, using thrust paddle mounting means, propeller is dried downwards, and lower section hides without horn
Gear, energy loss is few, can effectively promote the unmanned plane cruise time, and actual measurement probably promotes 10%-15% cruise duration.
As shown in Fig. 2, when the tripod is set in the cover portion, the propeller is set as pulling force paddle.By being remotely controlled
Flight control system HY-01 described in device remote control either PLC controller and pass through flight control system HY-01 or PLC control
Device processed further controls the rotation of the output shaft of motor, and the rotation of propeller is further driven by motor output shaft.To generate
Upward pulling force makes unmanned plane take off.Pulling force paddle mounting means, machine gravity is relatively low, and paddle plane is above center of gravity, when flight more
Easy to operate, flight is more steady, and underbelly free space is more, can in vivo dispose a greater variety of loads.
In conclusion the Portable unmanned machine of application on engine department and the cover portion by being provided with tripod installation knot
Structure, the engine department and the cover portion select one bottom as unmanned plane, removably in installation foot on foot stool installing structure
Frame.The voluntarily selection for being conducive to the different use demand of user is provided with thrust paddle or pulling force paddle on same unmanned plane, convenient
Unmanned plane is used, and is conducive to economize on resources.Wherein, using thrust paddle mounting means, propeller is dried downwards, and lower section is inorganic
Arm blocks, and energy loss is few, can effectively promote the unmanned plane cruise time, and actual measurement probably promotes 10%-15% cruise duration；Pulling force
Paddle mounting means, machine gravity is relatively low, and above center of gravity, when flight is easier to operate to paddle plane, and flight is more steady, and fuselage
Lower part free space is more, can in vivo dispose a greater variety of loads.When user selects pulling force paddle or thrust paddle to install
It can select load (camera) mounting means according to different application range and scene, that is, be installed on back mounting portion (foot
The opposite side of frame installation side) or lower part mounting portion (side of tripod installation), in general, installed mounted on underbelly
Portion position application range is wider, is suitable for various in working at height, looks down ground installation equipment and personnel etc., but in special feelings
Under condition, for example when similar detection inspection tunnel upper wall situation, load is mounted on top mounting portion and is just particularly important.And horn
It may be implemented to be arranged in be arranged on unmanned plane primary structural component one and the machine after rotating horn along horn rotary shaft
Arm match for housing in the groove of the horn after rotary folding, to be conducive to the convenient loading packing to unmanned plane and
It carries.Meanwhile the application by be arranged positioning limiting fixator, can to the rotating range of the horn limit and to rotary folding after
The horn is fixed.Through-hole or groove are additionally provided on the unmanned plane shell of the application in order to carry out hand to unmanned plane
It holds.It is more convenient to carry carrying.And the machine shell water resistance is preferable, can fly in the rain, even if fuselage interior is intake accidentally,
Droplet can also flow downwardly to the discharge of minimum point osculum along shell shape.
In addition, dish-shaped primary structural component is round disk like in the utility model embodiment, it can be appreciated that dish middle part is rectangle
Equal regular polygons, or/and, dish-shaped edge is the regular polygons such as rectangle,.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model.In short, all
Within the spirit and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in this practicality
Within novel protection domain.
Claims (9)
1. a kind of Portable unmanned machine, which is characterized in that including：
Dish-shaped primary structural component has the main part for constituting dish-shaped periphery, is located at the protrusion that main part side constitutes dish middle part
In the engine department of main part；
Positioned at the main part other side, the cover portion for the cabin for protruding from main part is installed；
There is an appointed thickness, periphery edge to be uniformly distributed at least three machines for being equipped with and flexing outward on the main part periphery
Arm, horn end are equipped with the blade and motor as power；
Wherein, the inner fovea part in the body peripheral edge is stretched into described horn one end, and horizontally rotates with main body and connect；It is solid by one
Determine part and horn is fixed on a turned position；
The main part is peripherally provided with by the inner fovea part and corresponds to main body with the matched groove of horn shape, the notch end
Portion have with the matched recess portion of the motor, be respectively used to accommodating horizontally rotate the horn and motor to the groove.
2. Portable unmanned machine according to claim 1, which is characterized in that be provided in the engine department and the cover portion
Foot stool installing structure, the engine department and the cover portion select one bottom as unmanned plane, removably install and tie in tripod
Tripod is installed on structure.
3. Portable unmanned machine according to claim 2, which is characterized in that the foot stool installing structure includes：It is set to
On the surface of the engine department and the cover portion, at least three hole slots to extend internally, and the direction convergence that extends internally；
The tripod, which corresponds to the mounting structure, has the insertion end that can be inserted into the hole slot.
4. Portable unmanned machine according to claim 3, which is characterized in that the hole slot and the insertion end be engage,
Or thread fiting mode assembly.
5. Portable unmanned machine according to claim 1, which is characterized in that inner fovea part described in main part has rolling assembling
The vertical axis of described horn one end, the fixing piece are the vertical limited post detachably installed.
6. Portable unmanned machine according to claim 1, which is characterized in that the engine department or/and the cover portion are close
Outer circumference has hand-held through-hole.
7. Portable unmanned machine according to claim 1, which is characterized in that the engine department or/and the cover portion center
Locate that there is the external components mounting portion outwardly protruded.
8. Portable unmanned machine according to claim 7, which is characterized in that the external components mounting portion is equipped with camera shooting
Head.
9. according to claim 1-8 any one of them Portable unmanned machines, which is characterized in that the unmanned plane is in its horizontal cutting
Face central symmetry.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721055081.0U CN207773428U (en) | 2017-08-22 | 2017-08-22 | A kind of Portable unmanned machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721055081.0U CN207773428U (en) | 2017-08-22 | 2017-08-22 | A kind of Portable unmanned machine |
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| Publication Number | Publication Date |
|---|---|
| CN207773428U true CN207773428U (en) | 2018-08-28 |
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ID=63218295
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721055081.0U Active CN207773428U (en) | 2017-08-22 | 2017-08-22 | A kind of Portable unmanned machine |
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| Country | Link |
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| CN (1) | CN207773428U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109279015A (en) * | 2018-10-26 | 2019-01-29 | 珠海银通无人机科技有限公司 | A kind of 20 kilograms of load-carrying of novel unmanned plane |
| CN111377049A (en) * | 2020-03-31 | 2020-07-07 | 马鞍山元辰网络科技有限公司 | Portable foldable unmanned aerial vehicle and working method thereof |
-
2017
- 2017-08-22 CN CN201721055081.0U patent/CN207773428U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109279015A (en) * | 2018-10-26 | 2019-01-29 | 珠海银通无人机科技有限公司 | A kind of 20 kilograms of load-carrying of novel unmanned plane |
| CN111377049A (en) * | 2020-03-31 | 2020-07-07 | 马鞍山元辰网络科技有限公司 | Portable foldable unmanned aerial vehicle and working method thereof |
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