CN207758990U - A kind of easy-to-dismount multi-rotor unmanned aerial vehicle - Google Patents
A kind of easy-to-dismount multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN207758990U CN207758990U CN201721826902.6U CN201721826902U CN207758990U CN 207758990 U CN207758990 U CN 207758990U CN 201721826902 U CN201721826902 U CN 201721826902U CN 207758990 U CN207758990 U CN 207758990U
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Abstract
The utility model discloses a kind of easy-to-dismount multi-rotor unmanned aerial vehicles, including shell, dismantle spiral cover, stepped stem, flabellum, intermediate bar and micromotor, two outer surface of described shell or so is connected with the small end face of stepped stem, the large end face of the stepped stem is connected directly with circular sleeve, intermediate bar is installed in the circular sleeve, and intermediate bar is axially moved in the outer end face of extension bar, the extension bar is fixedly linked with connecting rod, one end of the connecting rod is installed with micromotor, it is connected by shaft between the micromotor and flabellum, the housing lower surface is installed with upper support bar, described upper support bar one end is equipped with lower support bar, the lower support bar is fixedly connected with pedestal vertical pole, the shell is connected with stepped stem by dismantling spiral cover.The utility model realizes a kind of easy-to-dismount unmanned plane, has the advantages that simple in structure, easy to use, using effect is good.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of easy-to-dismount multi-rotor unmanned aerial vehicle.
Background technology
Science and technology is constantly progressive so that unmanned plane starts largely universal, popularization.For importance, the use of unmanned plane,
It is small to arrive people’s lives greatly to national defense and military, sciemtifec and technical sphere.Unmanned plane is promoted the use of for the development of human society,
It is unquestionably a huge advance, many facilities is brought to daily life.But any one product,
Can not possibly be without any defect in use, for unmanned plane, structure is complex, and parts are more, so that nobody
The dismounting of machine is more troublesome, especially when people, which are used outside unmanned plane, carries out recreation, because unmanned plane volume is larger, and institute
To carry nor easily.Therefore it is directed to unmanned plane drawbacks described above, the utility model proposes a kind of easy-to-dismount more
Rotor wing unmanned aerial vehicle.
Utility model content
The purpose of this utility model is to provide a kind of easy-to-dismount multi-rotor unmanned aerial vehicles, to solve in above-mentioned background technology
The problem of proposition.
To achieve the above object, the utility model provides the following technical solutions：A kind of easy-to-dismount multi-rotor unmanned aerial vehicle, packet
Include shell, dismounting spiral cover, stepped stem, flabellum, intermediate bar and micromotor, two outer surface of described shell or so and stepped stem it is small
End face is connected, and large end face and the circular sleeve of the stepped stem are connected directly, and is equipped with intermediate bar in the circular sleeve, and in
Between bar axially moved in the outer end face of extension bar, the extension bar is fixedly linked with connecting rod, one end of the connecting rod
It is installed with micromotor, is connected by shaft between the micromotor and flabellum, the housing lower surface is fixedly mounted
There are upper support bar, described upper support bar one end that lower support bar is installed, the lower support bar is fixedly connected with pedestal vertical pole.
Preferably, the shell is connected with stepped stem by dismantling spiral cover.
Preferably, the shell, stepped stem and dismounting spiral cover surface are both provided with screw thread.
Preferably, both the intermediate bar and extension bar pass through the groove of intermediate bar one end and the buckle phase of extension bar one end
Connection.
Preferably, the lower support bar is boring structure, and is moved freely between upper support bar and lower support bar.
Preferably, the both ends of the pedestal vertical pole are equipped with resilient sleeve.
Compared with prior art, the utility model has the beneficial effects that：
1, the utility model is by the installing and dismounting spiral cover between shell and stepped stem, by rotating dismounting rotation counterclockwise
Lid, can detach stepped stem, and then achieve the purpose that dismounting from shell；
2, the utility model is additionally provided with extension bar and buckle simultaneously, and by pressing buckle with strength, intermediate bar may be implemented
With the separation of extension bar, have the advantages that simple in structure, easy to use, using effect is good.
Description of the drawings
Fig. 1 is a kind of easy-to-dismount multi-rotor unmanned aerial vehicle overall structure diagram of the utility model；
Fig. 2 is a kind of easy-to-dismount multi-rotor unmanned aerial vehicle partial schematic diagram of the utility model；
Fig. 3 is a kind of shell of easy-to-dismount multi-rotor unmanned aerial vehicle of the utility model, dismantles the connection of spiral cover and stepped stem
Schematic diagram.
In figure：1- shells；2- dismantles spiral cover；3- stepped stems；4- flabellums；5- shafts；6- circular sleeves；7- intermediate bars；8-
Micromotor；9- upper support bars；10- lower support bars；11- pedestal vertical poles；12- resilient sleeves；13- connecting rods；14- extension bars；
15- is buckled；16- screw threads.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of easy-to-dismount multi-rotor unmanned aerial vehicle, including
Shell 1, dismounting spiral cover 2, stepped stem 3, flabellum 4, intermediate bar 7 and micromotor 8,1 or so two outer surface of the shell and ladder
The small end face of bar 3 is connected, and large end face and the circular sleeve 6 of the stepped stem 3 are connected directly, and are equipped in the circular sleeve 6
Intermediate bar 7, and intermediate bar 7 is axially moved in the outer end face of extension bar 14, the extension bar 14 and 13 stationary phase of connecting rod
Even, one end of the connecting rod 13 is installed with micromotor 8, passes through 5 phase of shaft between the micromotor 8 and flabellum 4
Even, 1 lower surface of the shell is installed with upper support bar 9, and 9 one end of the upper support bar is equipped with lower support bar 10, described
Lower support bar 10 is fixedly connected with pedestal vertical pole 11.
The shell 1 is connected by dismounting spiral cover 2 with stepped stem 3 and shell 1, stepped stem 3 and 2 surface of dismounting spiral cover are equal
It is provided with screw thread 16, by rotating dismounting spiral cover 2 counterclockwise, stepped stem 3 can be detached from shell 1, and then reach dismounting
Purpose；15 phase of buckle that both the intermediate bar 7 and extension bar 14 pass through the groove and 14 one end of extension bar of 7 one end of intermediate bar
Connection, by pressing buckle 15 with strength, may be implemented the separation of intermediate bar 7 and extension bar 14；10 inside of the lower support bar is
Hollow-core construction, and moved freely between upper support bar 9 and lower support bar 10, to which the occupancy of unmanned plane can be reduced when carrying
Space；The both ends of the pedestal vertical pole 11 are equipped with resilient sleeve 12, and when unmanned plane lands, resilient sleeve 12 can be to avoid nothing
It is man-machine directly to collide with ground, to be played a certain protective role to the overall structure of unmanned plane.
Operation principle：The utility model is led to by the installing and dismounting spiral cover 2 between shell 1 and stepped stem 3
Rotation dismounting spiral cover 2 counterclockwise is crossed, stepped stem 3 can be detached from shell 1, and then achieve the purpose that dismounting,
The utility model is additionally provided with extension bar 14 and buckle 15 simultaneously, by pressing buckle 15 with strength, intermediate bar 7 may be implemented and stretch
The separation of rod 14 has the advantages that simple in structure, easy to use, using effect is good.
It should be noted that herein, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also include other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of easy-to-dismount multi-rotor unmanned aerial vehicle, including shell（1）, dismounting spiral cover（2）, stepped stem（3）, flabellum（4）, it is intermediate
Bar（7）And micromotor（8）, it is characterised in that：The shell（1）Two outer surfaces of left and right and stepped stem（3）Small end face be connected,
The stepped stem（3）Large end face and circular sleeve（6）It is connected directly, the circular sleeve（6）Intermediate bar is inside installed（7）,
And intermediate bar（7）In extension bar（14）Outer end face axially moved, the extension bar（14）With connecting rod（13）Stationary phase
Even, the connecting rod（13）One end be installed with micromotor（8）, the micromotor（8）With flabellum（4）Between pass through
Shaft（5）It is connected, the shell（1）Lower surface is installed with upper support bar（9）, the upper support bar（9）One end is equipped with
Lower support bar（10）, the lower support bar（10）With pedestal vertical pole（11）It is fixedly connected.
2. a kind of easy-to-dismount multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The shell（1）With rank
Ladder bars（3）By dismantling spiral cover（2）It is connected.
3. a kind of easy-to-dismount multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The shell（1）, ladder
Bar（3）And dismounting spiral cover（2）Surface is both provided with screw thread（16）.
4. a kind of easy-to-dismount multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The intermediate bar（7）With
Extension bar（14）The two passes through intermediate bar（7）The groove and extension bar of one end（14）The buckle of one end（15）It is connected.
5. a kind of easy-to-dismount multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The lower support bar（10）
For boring structure, and upper support bar（9）With lower support bar（10）Between move freely.
6. a kind of easy-to-dismount multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The pedestal vertical pole（11）
Both ends resilient sleeve is installed（12）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721826902.6U CN207758990U (en) | 2017-12-25 | 2017-12-25 | A kind of easy-to-dismount multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721826902.6U CN207758990U (en) | 2017-12-25 | 2017-12-25 | A kind of easy-to-dismount multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207758990U true CN207758990U (en) | 2018-08-24 |
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ID=63187950
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721826902.6U Active CN207758990U (en) | 2017-12-25 | 2017-12-25 | A kind of easy-to-dismount multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207758990U (en) |
-
2017
- 2017-12-25 CN CN201721826902.6U patent/CN207758990U/en active Active
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