CN207607631U - Three axis connecting rod unmanned planes non-stop layer plate framework fuselage - Google Patents
Three axis connecting rod unmanned planes non-stop layer plate framework fuselage Download PDFInfo
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- CN207607631U CN207607631U CN201721794749.3U CN201721794749U CN207607631U CN 207607631 U CN207607631 U CN 207607631U CN 201721794749 U CN201721794749 U CN 201721794749U CN 207607631 U CN207607631 U CN 207607631U
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- fuselage body
- frame fuselage
- mounting hole
- connecting rod
- stop layer
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Abstract
The utility model belongs to inorganic people's technical field, more particularly to a kind of three axis connecting rod unmanned planes non-stop layer plate framework fuselage.Side plate including bottom plate and along floor peripheral setting, the side plate, which joins end to end, constitutes frame fuselage body, the mounting hole for installing horn is provided on the frame fuselage body, 6 mounting holes are provided on the frame fuselage body, the rear and front end of the frame fuselage body is each provided with 2 mounting holes, the side of the frame fuselage body is each provided with 1 mounting hole, the midpoint of the central point line of 2 mounting holes of frame fuselage body side and each mounting hole the line of the distal center point of fixed horn make the angle between adjacent connection lines be 60 °.The utility model is designed reasonably, scientific arrangement make unmanned plane more stablize in flight, and large-scale promotion is suitble to use.
Description
Technical field
The utility model belongs to inorganic people's technical field, more particularly to a kind of three axis connecting rod unmanned plane non-stop layer plate frameworks
Fuselage.
Background technology
UAV, abbreviation unmanned plane are a kind of new concept weapon equipments being in rapidly developing, with machine
Dynamic flexible, rapid reaction, unmanned flight, operation require low advantage.Shadow may be implemented by carrying multiclass sensor in unmanned plane
It is the strong supplement of satellite remote sensing and traditional air remote sensing as real-time Transmission, high-risk areas detecting function.At present, unmanned plane
Use scope has widened military affairs, scientific research, civilian three big field, specifically electric power, communication, meteorology, agricultural, ocean, exploration,
Photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the fields application such as public security anti-terrorism it is very wide.
Existing unmanned plane mostly uses center harden structure, and central plate is connected by upper and lower two pieces of connecting plates, be which is provided with more
For connecting horn and electronic equipment, above structure is arranged in the application of unmanned plane for a assembly hole and connector, often as it can be seen that
If but if horn is the structure design of connecting rod form, the structure of central plate can then hinder the normal folding of horn, meanwhile,
Fastness is greatly lowered, and unmanned plane is in flight course, it is easy to flight is occurred and the technical problems such as be had some setbacks.
Utility model content
The utility model can not apply the horn structure of three axis connecting rods for the frame fuselage of above-mentioned center harden structure
Technical problem proposes a kind of reasonable design, simple in structure, easy to process and three axis of three axis link mechanisms of setting can be facilitated to connect
Bar unmanned plane non-stop layer plate framework fuselage.
In order to achieve the above object, the technical solution adopted in the utility model is that the utility model provides a kind of three axis company
Bar unmanned plane non-stop layer plate framework fuselage, including bottom plate and the side plate along floor peripheral setting, the side plate join end to end
Frame fuselage body is constituted, the mounting hole for installing horn, the frame fuselage sheet are provided on the frame fuselage body
6 mounting holes are provided on body, the rear and front end of the frame fuselage body is each provided with 2 mounting holes, the frame fuselage
The side of ontology is each provided with 1 mounting hole, the midpoint of the central point line of 2 mounting holes of frame fuselage body side
With each mounting hole the line of distal center point of fixed horn make the angle between adjacent connection lines be 60 °.
Preferably, the frame fuselage body includes the rectangular portion of the rectangular setting in cross section and cross section is in rule
The polygon portion of polygon setting, the polygon portion are overlapped with the short side of rectangular portion, and it is remote that the mounting hole is separately positioned on rectangular portion
The long side face and polygon portion in short side face, rectangular portion short side face both sides from polygon portion one end are far from rectangular portion short side one end both sides
Edge surface on.
Preferably, the number of edges of the shape of the cross section in the polygon portion is even number.
Preferably, the shape of the cross section in the polygon portion is 8 side shapes.
Compared with prior art, it is with good effect the advantages of the utility model,
1, the utility model provides a kind of three axis connecting rod unmanned planes non-stop layer plate framework fuselage, by cancelling central plate
Structure setting is changed to add side plate on the periphery along bottom plate, and horn is made to be mounted on side plate, meanwhile, by being reasonably laid out, really
Determine the installation site of horn, and then ensure the stability of unmanned plane during flying, the utility model is designed reasonably, scientific arrangement make nothing
It is man-machine more to stablize in flight, it is suitble to large-scale promotion to use.
Description of the drawings
It is required in being described below to embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment
The attached drawing used is briefly described, it should be apparent that, the accompanying drawings in the following description is some embodiments of the utility model,
For those of ordinary skill in the art, without having to pay creative labor, it can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the structural schematic diagram for the three axis connecting rod unmanned plane non-stop layer plate framework fuselages that embodiment 1 provides；
Fig. 2 is the vertical view for the three axis connecting rod unmanned plane non-stop layer plate framework fuselage fitting machine arm states that embodiment 1 provides
Figure；
In above each figure, 1, bottom plate；2, frame fuselage body；21, short side face；22, long side face；23, edge surface；3, it installs
Hole；31, mounting base；4, horn.
Specific implementation mode
It is below in conjunction with the accompanying drawings and real in order to be more clearly understood that the above objects, features, and advantages of the utility model
Example is applied to be described further the utility model.It should be noted that in the absence of conflict, embodiments herein and reality
The feature applied in example can be combined with each other.
Many details are elaborated in the following description in order to fully understand the utility model, still, this practicality
Novel to implement using different from other modes described here, therefore, the utility model is not limited to be described below
The limitation of the specific embodiment of specification.
Embodiment 1, as shown in Figure 1 and Figure 2, the present embodiment provides a kind of three axis connecting rod unmanned planes non-stop layer plate framework machines
The main purpose of body, the invention aims to solve the problem that the structure of existing central plate cannot be satisfied three axis connecting rod horn normal uses
Technical problem, for this purpose, the three axis connecting rod unmanned plane non-stop layer plate framework fuselages that the present embodiment is provided include bottom plate 1 and edge
The side plate of floor peripheral setting, side plate, which joins end to end, constitutes frame fuselage body 2, and frame fuselage body 2 is sleeved on outside bottom plate 1,
And be detachably connected between bottom plate 1, in order to ensure the stability of unmanned plane during flying, it is arranged on frame fuselage body 2 useful
In the mounting hole (not shown) of installation horn, in order to ensure the stability of unmanned plane during flying, while being revolved for three axis connecting rods 6
The unmanned plane of the wing, for this purpose, in the present embodiment, 6 mounting holes are provided on frame fuselage body 2, wherein frame fuselage sheet
The rear and front end of body 2 is each provided with 2 mounting holes, and 1 mounting hole, six peaces are each provided in the side of frame fuselage body 2
The midpoint that the position in dress hole will meet the central point line of 2 mounting holes of 2 side of frame fuselage body is consolidated with each mounting hole
Angle between the line and adjacent connection lines of the distal center point of fixed horn is 60 °, i.e. 6 mounting holes fixed horn
The central point of end and the central point line of 2 mounting holes of 2 side of frame fuselage body completely justify 6 deciles by one, and
The length of line is consistent, i.e., for the central point of the end of 6 horns all on circle, such setting can be such that unmanned plane is flying
When row, keep stablizing, meanwhile, the frame fuselage body being made of side, the structure relative to central plate is more stable.
The horn 4 of three axis connecting rods folds for convenience, meanwhile, the volume of frame fuselage body 2 is reduced as far as possible, at this
In embodiment, frame fuselage body 2 includes that the rectangular portion of the rectangular setting in cross section and cross section are arranged in regular polygon
Polygon portion, regular polygon refers to the polygon of regular shape, in the present embodiment, the side of the shape of the cross section in polygon portion
Number is even number, and polygon portion is overlapped with the short side of rectangular portion, in this way, mounting hole is separately positioned on rectangular portion far from polygon portion one end
The edge surface of long side face 22 and polygon portion far from rectangular portion short side one end both sides in short side face 21,21 both sides of rectangular portion short side face
On 23, pass through above-mentioned setting, it is only necessary to which the mounting base 3 in short side face 21 is arranged to angle of inclination, you can realize decile, when
So, can also the short side face 21 of rectangular portion be directly arranged to multidirectional face, still, designed so long in frame fuselage body
Spend it is equal in the case of just affect the volume of entire frame fuselage body, be unfavorable for that other equipment are installed, meanwhile, also not side
Just it folds, for this purpose, in the present embodiment, short side face 21 is horizontal plane.
For more convenient folding, reduces difficulty of processing and ensure the aesthetics of fuselage, in the present embodiment, polygon portion
The shape of cross section is 8 side shapes, wherein the angle between edge surface 23 and horizontal plane is 130 degree, such design, it is ensured that energy
Enough realize quickly folds.
By above-mentioned setting, unmanned plane is not only made more to stablize in flight, meanwhile, horn 4 can also fixed
It is secured, extend the service life of unmanned plane.
The above descriptions are merely preferred embodiments of the present invention, is not to make other forms to the utility model
Limitation, any person skilled in the art is changed or is modified as possibly also with the technology contents of the disclosure above equivalent
The equivalent embodiment of variation is applied to other fields, but every without departing from the content of the technical scheme of the utility model, according to this reality
With novel technical spirit to any simple modification, equivalent variations and remodeling made by above example, it is new to still fall within this practicality
The protection domain of type technical solution.
Claims (4)
1. a kind of three axis connecting rod unmanned planes non-stop layer plate framework fuselage, which is characterized in that including bottom plate and along floor peripheral
The side plate of setting, the side plate, which joins end to end, constitutes frame fuselage body, is provided on the frame fuselage body for installing
The mounting hole of horn is provided with 6 mounting holes on the frame fuselage body, and the rear and front end of the frame fuselage body is respectively set
It is equipped with 2 mounting holes, the side of the frame fuselage body is each provided with 1 mounting hole, and the 2 of frame fuselage body side
The midpoint of the central point line of a mounting hole and each mounting hole the line of the distal center point of fixed horn make adjacent connection lines
Between angle be 60 °.
2. three axis connecting rod unmanned plane according to claim 1 non-stop layer plate framework fuselage, which is characterized in that the frame
Fuselage body include the rectangular setting in cross section rectangular portion and cross section be in regular polygon setting polygon portion, it is described more
Edge is overlapped with the short side of rectangular portion, and the mounting hole is separately positioned on short side face of the rectangular portion far from polygon portion one end, rectangle
In the edge surface of long side face and polygon portion far from rectangular portion short side one end both sides of portion short side face both sides.
3. three axis connecting rod unmanned plane according to claim 2 non-stop layer plate framework fuselage, which is characterized in that described polygon
The number of edges of the shape of the cross section in portion is even number.
4. three axis connecting rod unmanned plane according to claim 2 non-stop layer plate framework fuselage, which is characterized in that described polygon
The shape of the cross section in portion is 8 side shapes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721794749.3U CN207607631U (en) | 2017-12-20 | 2017-12-20 | Three axis connecting rod unmanned planes non-stop layer plate framework fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721794749.3U CN207607631U (en) | 2017-12-20 | 2017-12-20 | Three axis connecting rod unmanned planes non-stop layer plate framework fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207607631U true CN207607631U (en) | 2018-07-13 |
Family
ID=62799523
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721794749.3U Expired - Fee Related CN207607631U (en) | 2017-12-20 | 2017-12-20 | Three axis connecting rod unmanned planes non-stop layer plate framework fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207607631U (en) |
-
2017
- 2017-12-20 CN CN201721794749.3U patent/CN207607631U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180713 Termination date: 20191220 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |