CN208198805U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN208198805U CN208198805U CN201820808412.1U CN201820808412U CN208198805U CN 208198805 U CN208198805 U CN 208198805U CN 201820808412 U CN201820808412 U CN 201820808412U CN 208198805 U CN208198805 U CN 208198805U
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- Prior art keywords
- horn
- jacking block
- holder mounting
- fuselage
- unmanned plane
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model relates to gyroplane technical field more particularly to unmanned planes.Unmanned plane includes fuselage, fuselage has box body structure, box body structure has box top, box top is center plate, is equipped with flight control assemblies, section board, image transmission, data transmission device on central plate, central plate is also connect with holder mounting plate, holder mounting plate protrudes from the space of box body structure, holder mounting plate is equipped with holder mounting base, and holder mounting base is equipped with holder mounting hole, and holder mounting base is used to install the holder at least partially across holder mounting hole.The utility model is able to solve the not compact technical problem of housing construction existing in the prior art.
Description
Technical field
The utility model relates to gyroplane technical field more particularly to unmanned planes.
Background technique
In the prior art, the horn of military unmanned air vehicle is generally not foldable, and volume is larger when carrying, not portable.
Moreover, electron speed regulator, section board, the receiver etc. that use are the existing finished products purchased on the market, therefore aircraft is integrated
Spend lower, interior layout is more chaotic, and the signal interference between interior of aircraft component is more serious.Electron speed regulator setting
In fuselage main body, cause the size of fuselage main body larger, correspondingly, the space inside horn is then wasted.
And the unmanned plane does not give the setting reserved space of holder, so being still difficult to install holder.
Utility model content
The purpose of this utility model is to provide unmanned planes, not compact to solve housing construction existing in the prior art
Technical problem.
Unmanned plane, including fuselage, fuselage have box body structure, and box body structure has box top, and box top is center plate, central plate
On flight control assemblies, section board, image transmission, data transmission device be installed, central plate also connects with holder mounting plate
It connects, holder mounting plate protrudes from the space of box body structure, and holder mounting plate is equipped with holder mounting base, and holder mounting base is equipped with cloud
Platform mounting hole, holder mounting base are used to install the holder at least partially across holder mounting hole.
The unmanned plane, by the box body structure of fuselage, setting holder mounting plate outstanding is arranged on holder mounting plate
Holder mounting base can reduce the space that holder occupies fuselage interior.For the integrated installation wound of each original part of fuselage interior
Condition is made.Moreover, flight control assemblies, section board, image transmission, data transmission device are all mounted on central plate
On, the integrated level of unmanned plane can be improved, reduce overall quality, reduce the volume of unmanned plane.
Preferred technical solution, supplementary features are that box body structure has side wall, are equipped with horn pivot on the outside of side wall
Joint chair, the horn pin joint seat on the side wall of the same side are respectively provided with different height, so that horn is when being stowed away, the same side
Side wall outside more horns can arrange along the vertical direction.
There is the horn pin joint seat of different height by being arranged, enable with the horn of horn pin joint seat pivot joint when packing up
It is enough arranged above and below, horn can be made when packing up, it can be as close as possible to the side wall of fuselage, to reduce fuselage when packing up
Shape width, while a possibility that horn is broken off when packing up is also reduced, improve the portability of unmanned plane.
Further preferred technical solution, supplementary features are, pivot joint assembly is equipped on horn pin joint seat, and pivot joint is total
It is articulated on horn pin joint seat at including drive-connecting shaft, compressed spring, upper jacking block and lower jacking block, drive-connecting shaft, upper jacking block and lower jacking block
One of connect with horn, the other of upper jacking block and lower jacking block are connect with horn pin joint seat, compressed spring, lower jacking block and
Upper jacking block is successively sleeved on drive-connecting shaft from one end of drive-connecting shaft to the other end, the third of the first end face of upper jacking block and lower jacking block
End face abuts, and one of first end face and third end face have with lug boss, another in first end face and third end face
Person has recessed portion.
The program makes upper jacking block and lower jacking block by opposite top by setting pivot joint assembly using compressed spring
Tightly, while in the third end face of the first end face of upper jacking block and lower jacking block, lug boss and recessed portion is respectively set, can utilize convex
The cooperation in portion and recessed portion is played, under the holding out against of spring, lug boss is fallen into recessed portion, and elastic potential energy is in the shape of minimum energy
State, the two keep relative stability.Naturally, the horn and horn pin joint seat that connect respectively with upper jacking block and lower jacking block can also be kept
The position, so that horn can keep the angle of a spontaneous fixation relative to fuselage.
Technical solution still further preferably, supplementary features are, the first end face of upper jacking block have upper recessed portion and
Upper projecting portion, the angle between upper recessed portion and upper projecting portion are the first angle, and the second end face of lower jacking block has lower concave portion
And lower convex portion, the angle between lower concave portion and lower convex portion are the second angle, the first angle and the second corner dimension are identical,
Upper recessed portion, upper projecting portion, lower concave portion and lower convex portion are provided as that the same of lower concave portion can be embedded in upper projecting portion
When lower convex portion be embedded in upper recessed portion.
The program by the way that upper recessed portion and upper projecting portion are arranged in first end face, on third end face setting lower concave portion and
Lower convex portion can make upper recessed portion, lower convex portion and upper projecting portion, lower concave portion match respectively, be capable of forming at least
The combination of two pairs of lug boss and recessed portion, to improve in the case where there is compressed spring to hold out against, upper jacking block and lower jacking block exist
Bond strength when certain relative angles, to improve horn and horn pin joint seat holding relative angle, i.e. horn and fuselage
The reliability for the angle for keeping some opposite.
Preferred technical solution, supplementary features are, further include horn, at least partially hollow structure of horn, machine
Electron speed regulator is installed in arm.
By the way that horn is arranged to hollow structure, electron speed regulator is accommodated in hollow structure, the sky in fuselage can be saved
Between, advantageously reduce the volume of fuselage.Meanwhile so that electron speed regulator at work in fuselage flight control assemblies, point
Battery plate, image transmission, data transmission device distance increase, reduce the operation of electron speed regulator to flight control assemblies,
The electromagnetic interference of section board, image transmission, data transmission device.
Further preferred technical solution, supplementary features are that horn has horn upper housing and horn lower cover, machine
Arm upper housing includes horn top surface and horn side, and through-hole is provided on horn lower cover, and bolt passes through through-hole and horn upper casing
Body is threadedly coupled and fixes horn lower cover and horn upper housing.
Horn is arranged to above structure, the weight for mitigating horn can be conducive to, meanwhile, upper housing includes horn top surface
With horn side, electron speed regulator can be first mounted on horn lower cover, when this installation process carries out, around have no and appoint
What other entity causes to hinder to installation process, and then electron speed regulator and horn lower cover are co-mounted on horn again
In shell.So the assembling speed of horn can be improved.
Preferred technical solution, supplementary features are, further include horn, horn, a left side before horn includes left front horn, is right
Horn and horn behind the right side, the free end of left back horn and horn behind the right side are provided with undercarriage, the outside of the bottom surface of box body structure afterwards
It is provided with supporting fuselage seat.
By the outside for the bottom surface that undercarriage and box body mechanism is arranged in horn after left back horn and the right side, fuselage branch is set
Seat is supportted, the biggish triangular support of area can be formed, to improve stability when unmanned plane landing.
Preferred technical solution, supplementary features are, further include battery compartment, and battery compartment is removably mounted at
The rear portion of fuselage, battery compartment and holder mounting base are located at the opposite both ends of fuselage.
By the way that battery compartment to be arranged in the rear portion of fuselage, i.e., the opposite both ends of fuselage are located at holder mounting base,
It can use battery compartment and holder form trim to fuselage weight, the lift of each propeller is allowed to keep relatively uniform
Output, to improve flying quality.Battery compartment is removably mounted on fuselage simultaneously, is also convenient in battery
When electricity exhausts, battery is rapidly removed, replaces the battery of full electricity.
Further preferred technical solution, supplementary features are that battery compartment and box body structure are carried out by movable buckle
Connection.
It is clamped using movable buckle, it may be convenient to carry out the replacement of battery.
Preferred technical solution, supplementary features are, further include upper housing and lower case, and upper housing passes through self-tapping screw
It is connect with fuselage and lower case.
It is connect by self-tapping screw with fuselage by setting upper housing and lower case, and by the two, it may be convenient to real
It now dismantles, and the equipment in fuselage is protected not to be contaminated.
Detailed description of the invention
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is schematic perspective view of the unmanned plane of embodiment one after horn expansion, does not show that holder, spiral shell in figure
Revolve paddle etc.；
Fig. 2 is the bottom view of Fig. 1；
Fig. 3 is structural schematic diagram of the unmanned plane of embodiment one after horn is packed up, and does not show that holder, propeller in figure
Deng；
Fig. 4 is the schematic perspective view of the box body structure in embodiment one；
Fig. 5 is the three-dimensional disassembly diagram of horn before left front horn or the right side in embodiment one；
Fig. 6 is the three-dimensional disassembly diagram of horn behind left back horn or the right side in embodiment one；
Fig. 7 is the three-dimensional disassembly diagram of the pivot joint assembly in embodiment one；
Fig. 8 is the schematic perspective view from a direction of the upper housing in embodiment one；
Fig. 9 is the schematic perspective view from another direction of the upper housing in embodiment one.
Icon: 10- fuselage；11-central plates；12-holder mounting plates；13-holder mounting bases；14- holder mounting hole；
15- horn pin joint seat；16-supporting fuselage seats；21-horn upper housings；22-horn lower covers；221-through-holes；23-rise and fall
Frame；The upper jacking block of 31-；Jacking block under 32-；33- compressed spring；34- drive-connecting shaft；35- outer sleeve；40- battery compartment；51- upper housing；
511- threaded hole；52- lower case.
Specific embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
Field those of ordinary skill every other embodiment obtained without making creative work belongs to practical
Novel protected range.
Embodiment one
As shown in figs. 1-9, unmanned plane, including fuselage 10, fuselage 10 have box body structure, and box body structure has box top,
Box top is center plate 11, is equipped with flight control assemblies, section board, image transmission, data transmission device on central plate 11,
Central plate 11 is also connect with holder mounting plate 12, and holder mounting plate 12 protrudes from the space of box body structure, on holder mounting plate 12
Equipped with holder mounting base 13, holder mounting base 13 is equipped with holder mounting hole 14, and holder mounting base 13 is at least partly worn for installing
Cross the holder of holder mounting hole 14.The concrete shape of box body structure constructs, as shown in Figure 4.
The unmanned plane, by the box body structure of fuselage 10, setting holder mounting plate 12 outstanding, holder mounting plate 12
Upper setting holder mounting base 13 can reduce the space inside holder occupancy fuselage 10.For each original part inside fuselage 10
Integrated installation creates condition.Moreover, flight control assemblies, section board, image transmission, data transmission device are all pacified
On central plate 11, the integrated level of unmanned plane can be improved, reduce overall quality, reduce the volume of unmanned plane.
Particularly, box body structure has side wall, is equipped with horn pin joint seat 15 on the outside of side wall, on the side wall of the same side
Horn pin joint seat 15 be respectively provided with different height so that horn receive to box body structure side wall when, the side of the same side
More horns outside wall can arrange along the vertical direction.
There is the horn pin joint seat 15 of different height by being arranged, so that the horn being pivotally connected with horn pin joint seat 15 is being packed up
When can be arranged above and below, horn can be made when packing up, can be as close as possible to the side wall of fuselage 10, to reduce when packing up
10 shape width of fuselage, while also reducing a possibility that horn is broken off when packing up, improve the portability of unmanned plane.
Further particularly, as shown in fig. 7, being equipped with pivot joint assembly on horn pin joint seat 15, pivot joint assembly includes pivot
Spindle 34, compressed spring 33, upper jacking block 31 and lower jacking block 32, drive-connecting shaft 34 are articulated on horn pin joint seat 15, upper 31 He of jacking block
One of lower jacking block 32 is connect with horn, and the other of upper jacking block 31 and lower jacking block 32 are connect with horn pin joint seat 15, pressure
Contracting spring 33, lower jacking block 32 and upper jacking block 31 are successively sleeved on drive-connecting shaft 34 from one end of drive-connecting shaft 34 to the other end, upper top
The third end face of the first end face of block 31 and lower jacking block 32 abuts, and one of first end face and third end face are raised with having
Portion, the other of first end face and third end face have recessed portion.In addition, in order to improve between upper jacking block 31 and lower jacking block 32
The clean level in space grind first end in order to avoid external particle etc. enters between first end face and third end face
The surface in face and third end face is set with outer sleeve 35 also in the outside of upper jacking block 31 and lower jacking block 32 and spring.In Fig. 7,
In order to clearly show the structure of upper jacking block 31 and lower jacking block 32, outer sleeve 35 uses transparent processing, that is, passes through the shape of wire frame
Formula is indicated.
The program makes upper jacking block 31 and lower jacking block 32 opposite by setting pivot joint assembly using compressed spring 33
Hold out against, while in the third end face of the first end face of upper jacking block 31 and lower jacking block 32, lug boss and recessed portion, energy is respectively set
The cooperation of lug boss and recessed portion is enough utilized, under the holding out against of spring, lug boss is fallen into recessed portion, and elastic potential energy is in energy
Minimum state, the two keep relative stability.Naturally, horn and the horn pivot joint being connect respectively with upper jacking block 31 and lower jacking block 32
Seat 15 can also keep the position, so that horn can keep the angle of a spontaneous fixation relative to fuselage 10.
Further particularly, the first end face of upper jacking block 31 have upper recessed portion and upper projecting portion, upper recessed portion with
Angle between upper projecting portion is the first angle, and the second end face of lower jacking block 32 has lower concave portion and lower convex portion, lower recess
Angle between portion and lower convex portion is the second angle, and the first angle and the second corner dimension are identical, upper recessed portion, upper protrusion
Portion, lower concave portion and lower convex portion are provided as can be while upper projecting portion be embedded in lower concave portion in lower convex portion insertion
Recessed portion.
The program by the way that upper recessed portion and upper projecting portion are arranged in first end face, on third end face setting lower concave portion and
Lower convex portion can make upper recessed portion, lower convex portion and upper projecting portion, lower concave portion match respectively, be capable of forming at least
The combination of two pairs of lug boss and recessed portion, to improve upper jacking block 31 and lower top in the case where there is compressed spring 33 to hold out against
Bond strength of the block 32 in certain relative angles, to improve horn and the holding relative angle of horn pin joint seat 15, i.e. machine
Arm keeps the reliability of some opposite angle with fuselage 10.
It particularly, further include horn, at least partially hollow structure of horn is equipped with electron speed regulator in horn.
By the way that horn is arranged to hollow structure, electron speed regulator is accommodated in hollow structure, can be saved in fuselage 10
Space advantageously reduces the volume of fuselage 10.Meanwhile so that electron speed regulator controls dress with the flight in fuselage 10 at work
It sets, the increase of the distance of section board, image transmission, data transmission device, the operation for reducing electron speed regulator controls flight
The electromagnetic interference of device, section board, image transmission, data transmission device.
Further particularly, as shown in Figure 5 and Figure 6, horn has horn upper housing 21 and horn lower cover 22, horn
Upper housing 21 includes horn top surface and horn side, is provided with through-hole 221 on horn lower cover 22, bolt pass through through-hole 221 with
Horn upper housing 21 is threadedly coupled and fixes horn lower cover 22 and horn upper housing 21.
Horn is arranged to above structure, the weight for mitigating horn can be conducive to, meanwhile, upper housing 51 includes horn top
Electron speed regulator can be first mounted on horn lower cover 22 by face and horn side, and when this installation process carries out, surrounding is simultaneously
No any other entity causes to hinder to installation process, is then again co-mounted to electron speed regulator and horn lower cover 22
In horn upper housing 21.So the assembling speed of horn can be improved.
Particularly, horn behind horn, left back horn and the right side before horn includes left front horn, is right, left back horn and it is right after
The free end of horn is provided with undercarriage 23, and supporting fuselage seat 16 is provided on the outside of the bottom surface of box body structure.
By the outside for the bottom surface that undercarriage 23 and box body mechanism is arranged in horn after left back horn and the right side, fuselage is set
Support base 16 can form the biggish triangular support of area, to improve stability when unmanned plane landing.
It particularly, further include battery compartment 40, battery compartment 40 is removably mounted at the rear portion of fuselage 10, battery
Storehouse 40 and holder mounting base 13 are located at the opposite both ends of fuselage 10.
By the way that battery compartment 40 to be arranged in the rear portion of fuselage 10, i.e., the opposite of fuselage 10 is located at holder mounting base 13
Both ends, can use battery compartment 40 and holder form trim to 10 weight of fuselage, so that the lift of each propeller can be with
Relatively uniform output is kept, to improve flying quality.Battery compartment 40 is removably mounted at fuselage simultaneously
It on 10, is also convenient in dead battery capability, battery is rapidly removed, replace the battery of full electricity.
Further particularly, battery compartment 40 and box body structure are attached by movable buckle.
It is clamped using movable buckle, it may be convenient to carry out the replacement of battery.
It particularly, further include upper housing 51 and lower case 52, upper housing 51 passes through self-tapping screw and fuselage 10 and lower casing
Body 52 connects.Specifically, lower case 52 and machine can be turned in the setting threaded hole 511 of the inner wall of upper housing 51, self-tapping screw
The connecting hole of body 10 screws in the threaded hole 511 of 51 inner wall of upper housing, upper housing 51, fuselage 10, lower case 52 is connected.
It is connect by self-tapping screw with fuselage 10 by setting upper housing 51 and lower case 52, and by the two, Ke Yifang
Just realization disassembly, and the equipment in fuselage 10 is protected not to be contaminated.
It is in the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
For ease of description the utility model and simplify description, rather than the device or element of indication or suggestion meaning must have it is specific
Orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In addition, term " first ", " second ", " third " are used for description purposes only, it is not understood to indicate or imply phase
To importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection；It can be mechanical connection, be also possible to be electrically connected；Can be directly connected, can also indirectly connected through an intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
The concrete meaning of language in the present invention.
Finally, it should be noted that the above various embodiments is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should
Understand: it is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of
Technical characteristic is equivalently replaced, such as:
(1) in embodiment one, show in figure and be provided with two upper recessed portions and two in the first end face of upper jacking block
Corresponding matching is done in lower convex portion, the setting of third end face, indeed, it is possible to according to the specific needs of rotational angle, first
One upper recessed portion and lower concave portion are only set on end face, do corresponding matching on third end face.
And these are modified or replaceed, various embodiments of the utility model technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (10)
1. unmanned plane, which is characterized in that including fuselage, the fuselage has box body structure, and the box body structure has box top, institute
Stating box top is center plate, and flight control assemblies, section board, image transmission, data transmission dress are equipped on the central plate
It sets, the central plate is also connect with holder mounting plate, and the holder mounting plate protrudes from the space of the box body structure, the cloud
Platform mounting plate is equipped with holder mounting base, and the holder mounting base is equipped with holder mounting hole, and the holder mounting base is for installing
At least partially across the holder of the holder mounting hole.
2. unmanned plane according to claim 1, which is characterized in that the box body structure has a side wall, the side wall it is outer
Side is equipped with horn pin joint seat, and the horn pin joint seat on the side wall of the same side is respectively provided with different height, so that
Horn is obtained when being stowed away, the more horns outside the side wall of the same side can arrange along the vertical direction.
3. unmanned plane according to claim 2, which is characterized in that be equipped with pivot joint assembly, institute on the horn pin joint seat
Stating pivot joint assembly includes drive-connecting shaft, compressed spring, upper jacking block and lower jacking block, and the drive-connecting shaft is articulated in the horn pin joint seat
On, the compressed spring, the lower jacking block and the upper jacking block are successively sleeved on institute to the other end from one end of the drive-connecting shaft
It states on drive-connecting shaft, one of the upper jacking block and the lower jacking block are connect with the horn, the upper jacking block and the lower top
The other of block is connect with the horn pin joint seat, and the third end face of the first end face of the upper jacking block and the lower jacking block is supported
It connects, one of the first end face and the third end face are with lug boss, the first end face and the third end
The other of face has recessed portion.
4. unmanned plane according to claim 3, which is characterized in that the first end face of the upper jacking block have upper recessed portion and
Upper projecting portion, the angle between the upper recessed portion and the upper projecting portion are the first angle, the second end face of the lower jacking block
With lower concave portion and lower convex portion, the angle between the lower concave portion and the lower convex portion is the second angle, described
One angle is identical with second corner dimension, the upper recessed portion, the upper projecting portion, the lower concave portion and it is described under it is convex
The portion of rising is provided as the lower convex portion to be embedded on described while the upper projecting portion is embedded in the lower concave portion
Recessed portion.
5. unmanned plane according to claim 1, which is characterized in that it further include horn, at least partially sky of the horn
Core structure is equipped with electron speed regulator in the horn.
6. unmanned plane according to claim 5, which is characterized in that the horn has horn upper housing and horn lower cover
Body, the horn upper housing include horn top surface and horn side, through-hole are provided on the horn lower cover, bolt passes through institute
Through-hole is stated to be threadedly coupled with the horn upper housing and fix the horn lower cover and the horn upper housing.
7. unmanned plane according to claim 1, which is characterized in that further include horn, the horn includes left front horn, the right side
The free end of horn is provided with undercarriage behind horn behind preceding horn, left back horn and the right side, the left back horn and the right side, described
Supporting fuselage seat is provided on the outside of the bottom surface of box body structure.
8. unmanned plane according to claim 1, which is characterized in that further include battery compartment, the battery compartment is with dismountable
Mode is mounted on the rear portion of the fuselage, and the battery compartment and the holder mounting base are located at opposite two of the fuselage
End.
9. unmanned plane according to claim 8, which is characterized in that the battery compartment and the box body structure pass through active card
Button is attached.
10. unmanned plane according to claim 1 to 9, which is characterized in that further include upper housing and lower case, institute
Upper housing is stated to connect by self-tapping screw with the fuselage and the lower case.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820808412.1U CN208198805U (en) | 2018-05-25 | 2018-05-25 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820808412.1U CN208198805U (en) | 2018-05-25 | 2018-05-25 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208198805U true CN208198805U (en) | 2018-12-07 |
Family
ID=64516606
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820808412.1U Active CN208198805U (en) | 2018-05-25 | 2018-05-25 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208198805U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077596A (en) * | 2019-05-27 | 2019-08-02 | 广西云瑞科技有限公司 | A kind of four axis unmanned plane during flying platform of multipurpose and unmanned plane |
| CN112918676A (en) * | 2021-03-25 | 2021-06-08 | 中国十七冶集团有限公司 | Continuation of journey construction robot of easy dismouting power |
-
2018
- 2018-05-25 CN CN201820808412.1U patent/CN208198805U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077596A (en) * | 2019-05-27 | 2019-08-02 | 广西云瑞科技有限公司 | A kind of four axis unmanned plane during flying platform of multipurpose and unmanned plane |
| CN110077596B (en) * | 2019-05-27 | 2024-04-26 | 广西云瑞科技有限公司 | Multipurpose four-axis unmanned aerial vehicle flight platform and unmanned aerial vehicle |
| CN112918676A (en) * | 2021-03-25 | 2021-06-08 | 中国十七冶集团有限公司 | Continuation of journey construction robot of easy dismouting power |
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