CN207860425U - Novel industrial unmanned aerial vehicle body structure - Google Patents
Novel industrial unmanned aerial vehicle body structure Download PDFInfo
- Publication number
- CN207860425U CN207860425U CN201721788096.8U CN201721788096U CN207860425U CN 207860425 U CN207860425 U CN 207860425U CN 201721788096 U CN201721788096 U CN 201721788096U CN 207860425 U CN207860425 U CN 207860425U
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- main case
- reinforcing plate
- carbon pipe
- vehicle body
- aerial vehicle
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Abstract
The utility model is related to a kind of novel industrial unmanned aerial vehicle body structures, belong to unmanned plane equipment technical field.It includes the main case made of high intensity carbon fiber material, there are six circular holes for the setting of main case circumference, cavity is provided in main case, cavity inner wall is provided with reinforcement structure along circular hole, reinforcement structure includes reinforcing plate and reinforcement carbon pipe, reinforce carbon pipe to be fixed on main case cavity inner wall by reinforcing plate, it is the pipe that high intensity carbon fiber material makes to reinforce carbon pipe, and the circular hole by stretching out main case is connected with horn fixing piece；Between reinforcing plate and main case, reinforces being all made of high intensity glue between carbon pipe and main case and be fixed.The utility model realizes the simplification of manufacture craft relative to the main case being integrated by split type main case and reinforcement structure, reduces enterprise practical production cost；And horn is opposite with main case when bending, and reinforcement structure stress is simple and convenient if wrecking only needs to change reinforcement structure.
Description
Technical field
The utility model is related to a kind of novel industrial unmanned aerial vehicle body structures, belong to unmanned plane equipment technical field.
Background technology
Existing unmanned aerial vehicle body mostly uses integral cast, and complex process, high rejection rate is caused to increase the production of enterprise
Cost.In addition, unmanned aerial vehicle body, due to be connected with horn fixing piece, main case requires to bear the folding force of sufficient intensity,
But the fuselage resistance to compression limitation of integral cast, after often fractureing the case where maintenance difficult occur, customer experience is poor.
Utility model content
In view of the foregoing defects the prior art has, the utility model proposes a kind of new novel industrial unmanned plane machines
Body structure by reinforcing plate and reinforces carbon pipe, reduces manufacturing process, enhance the intensity of main case.
The utility model is realized using technical solution below：Novel industrial unmanned plane described in the utility model
Airframe structure, including the main case made of high intensity carbon fiber material, the setting of main case circumference is there are six circular hole, in main case
It is provided with cavity, cavity inner wall is provided with reinforcement structure along circular hole, and reinforcement structure includes reinforcing plate and reinforces carbon pipe, reinforces carbon
Pipe is fixed on by reinforcing plate on main case cavity inner wall, and it is the pipe that high intensity carbon fiber material makes to reinforce carbon pipe, is passed through
The circular hole for stretching out main case is connected with horn fixing piece；Between reinforcing plate and main case, reinforce adopting between carbon pipe and main case
It is fixed with high intensity glue.
Further, be provided with transition shoulder between the circular hole and main case, transition shoulder connect with main case one
Side is frustum cone structure, transition shoulder and the round hyperboloid that the side of circular hole to connect is inner wide and outer narrow.
Further, the circular hole is in axial alignment along the center of circle of main case, and 60 ° of interval is evenly distributed.
Further, the round pie structural top where the main case offers window, and cavity is provided in main case,
Cavity is carried out by window built in control unit, and the main case top perimeter where window is provided with bolt hole, in addition increases
One cover board, cover board are lived window aperture seal by bolt hole.
Further, the reinforcement carbon pipe is vertically fixed in reinforcing plate, and reinforcing plate is provided with carbon pipe contact position is reinforced
Through-hole, through-hole are matched with carbon pipe is reinforced.
Further, the reinforcement carbon pipe and reinforcing plate are integrated casting and forming.
Further, the overall dimensions of the reinforcing plate are more than the diameter of the circular hole of main case, the reinforcement carbon pipe range of stretching
Height of the degree more than the transition shoulder of main case.
Further, the arc-shaped setting of the reinforcing plate, the radian of outwardly convex is consistent with the crooked radian of main case,
The two realization fits closely.
The utility model has the beneficial effects that：Using novel industrial unmanned aerial vehicle body structure described in the utility model,
The simplification of manufacture craft is realized by split type main case and reinforcement structure relative to the main case being integrated, is reduced
Enterprise practical production cost；And horn is opposite with main case when bending, and reinforcement structure stress only needs to change reinforcement if wrecked
Structure, it is simple and convenient.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model.
In figure：1 is main case, and 2 be horn fixing piece, and 3 be reinforcing plate, and 4 be reinforcement carbon pipe.
Specific implementation mode
In order to make the utility model aim, technical solution be more clearly understood, with reference to embodiment, to the utility model
It is described in further detail.
As shown in Figure 1, main case 1 is the round pie structure that high intensity carbon fiber material makes, on the circumference of main case 1
There are six circular holes for setting, transition shoulder are provided between circular hole and main case 1, the side that transition shoulder connects with main case 1 is
Frustum cone structure, transition shoulder and the round hyperboloid that the side of circular hole to connect is inner wide and outer narrow.Six circular holes are along main case 1
The center of circle is in axial alignment, and 60 ° of interval is evenly distributed.Round pie structural top where main case 1 offers window, main case 1
It is inside provided with cavity, cavity is carried out by window built in control unit, and 1 top perimeter of main case where window is provided with spiral shell
Keyhole, in addition increases a cover board, and cover board is lived window aperture seal by bolt hole.
Main case 1 is made using high-strength carbon fiber integration, and intensity and toughness are all relatively good, and meet weight
Light advantage provides possibility for main case 1 is applied to unmanned plane occasion.
The cavity of main case 1 is provided with the reinforcement carbon pipe being connected with horn fixing piece 2 outward along circular hole, reinforces carbon pipe 4
It is fixed on 1 cavity inner wall of main case by reinforcing plate 3.It will be seen from figure 1 that reinforcing carbon pipe 4 is vertically fixed on reinforcing plate 3
On, reinforcing plate 3 is provided with through-hole with 4 contact position of carbon pipe is reinforced.Between reinforcing plate 3 and main case 1, reinforce carbon pipe 4 and main case 1
Between be all made of high intensity glue and be fixed.Reinforcing plate 3 is square, and the center is provided with through-hole, through-hole with reinforce carbon pipe 4 into
Row matching.Reinforce carbon pipe 4 and reinforcing plate 3 is integrated casting and forming.Reinforce the circle that carbon pipe 4 makes for high intensity carbon fiber material
Pipe, the circular hole by stretching out main case 1 are connected with horn fixing piece 2.Threaded hole is additionally provided in reinforcing plate 3, threaded hole passes through
Bolt is fixed on main case 1.
The overall dimensions of reinforcing plate 3 are more than the diameter of the circular hole of main case 1, and 4 length of reinforcement carbon pipe of stretching is more than host
The height of the transition shoulder of shell 1 ensures to reinforce carbon pipe 4 and 1 fixation of main case and can be realized with horn fixing piece 2 closely
Connection.
The radian of the arc-shaped setting of reinforcing plate, outwardly convex is consistent with the crooked radian of main case 1, when close, two
Person realizes and fits closely, fixedly more secured.
The utility model includes main case 1, horn fixing piece 2, reinforcing plate 3 and reinforces carbon pipe 4, six rotor unmanned aircrafts
Complete machine is made of high intensity carbon fiber material, and intensity and toughness are all relatively good, light-weight.The reinforcement carbon pipe 4 is fixed on master
On casing 1；The reinforcing plate 3 main case 1 and reinforces carbon pipe 4 fixed to one piece by high intensity glue；The horn fixing piece 2
It is fixed on and reinforces on carbon pipe 4；The reinforcement carbon plate 3, main case 1 and reinforcement carbon pipe 4 are fixed on one piece, form box like structure,
To improve intensity.
The above is only the preferred embodiment of the present invention and oneself, not with the utility model be limitation, it is all this
Impartial modifications, equivalent substitutions and improvements etc., should be included in the utility model made by within the spirit and principle of utility model
Patent covering scope in.
Claims (8)
1. a kind of novel industrial unmanned aerial vehicle body structure, including the main case made of high intensity carbon fiber material (1), host
The setting of shell (1) circumference is there are six circular hole, and main case (1) is interior to be provided with cavity, which is characterized in that cavity inner wall is arranged along circular hole
There are reinforcement structure, reinforcement structure to include reinforcing plate (3) and reinforce carbon pipe (4), reinforce carbon pipe (4) and be fixed on by reinforcing plate (3)
On main case (1) cavity inner wall, it is the pipe that high intensity carbon fiber material makes to reinforce carbon pipe (4), by stretching out main case (1)
Circular hole be connected with horn fixing piece (2)；Between reinforcing plate (3) and main case (1), reinforce between carbon pipe (4) and main case (1)
High intensity glue is all made of to be fixed.
2. novel industrial unmanned aerial vehicle body structure according to claim 1, which is characterized in that the circular hole and main case
(1) transition shoulder is provided between, the side that transition shoulder connects with main case (1) is frustum cone structure, transition shoulder and circular hole
The side to connect be inner wide and outer narrow round hyperboloid.
3. novel industrial unmanned aerial vehicle body structure according to claim 2, which is characterized in that the circular hole is along main case
(1) the center of circle is in axial alignment, and 60 ° of interval is evenly distributed.
4. novel industrial unmanned aerial vehicle body structure according to claim 1 or 2, which is characterized in that the main case (1)
The round pie structural top at place offers window, is provided with cavity in main case (1), cavity carries out control unit by window
It is built-in, main case (1) top perimeter where window is provided with bolt hole, in addition increases a cover board, cover board passes through bolt
Window aperture seal is lived in hole.
5. novel industrial unmanned aerial vehicle body structure according to claim 4, which is characterized in that the reinforcement carbon pipe (4)
It is vertically fixed in reinforcing plate (3), reinforcing plate (3) is provided with through-hole, through-hole and reinforcement carbon pipe with carbon pipe (4) contact position is reinforced
(4) it is matched.
6. novel industrial unmanned aerial vehicle body structure according to claim 1 or 5, which is characterized in that the reinforcement carbon pipe
(4) and reinforcing plate (3) is integrated casting and forming.
7. novel industrial unmanned aerial vehicle body structure according to claim 2, which is characterized in that the reinforcing plate (3)
Overall dimensions are more than the diameter of the circular hole of main case (1), and reinforcement carbon pipe (4) length of stretching is more than the transition bench of main case (1)
The height of rank.
8. novel industrial unmanned aerial vehicle body structure according to claim 6, which is characterized in that the reinforcing plate (3) is in
Arc is arranged, and the radian of outwardly convex is consistent with the crooked radian of main case (1), and the two realization fits closely.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721788096.8U CN207860425U (en) | 2017-12-19 | 2017-12-19 | Novel industrial unmanned aerial vehicle body structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721788096.8U CN207860425U (en) | 2017-12-19 | 2017-12-19 | Novel industrial unmanned aerial vehicle body structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207860425U true CN207860425U (en) | 2018-09-14 |
Family
ID=63465565
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721788096.8U Active CN207860425U (en) | 2017-12-19 | 2017-12-19 | Novel industrial unmanned aerial vehicle body structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207860425U (en) |
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2017
- 2017-12-19 CN CN201721788096.8U patent/CN207860425U/en active Active
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