CN203294306U - Shell of unmanned aerial vehicle - Google Patents
Shell of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203294306U CN203294306U CN2013202239959U CN201320223995U CN203294306U CN 203294306 U CN203294306 U CN 203294306U CN 2013202239959 U CN2013202239959 U CN 2013202239959U CN 201320223995 U CN201320223995 U CN 201320223995U CN 203294306 U CN203294306 U CN 203294306U
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- unmanned plane
- tail
- protective cover
- shell
- fuselage
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Abstract
The utility model discloses a shell of an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The shell of the unmanned aerial vehicle is suitable for being installed on a body of the unmanned aerial vehicle and comprises a head, a body, wings and a tail, wherein the outer surface of the head, the outer surface of the body, the outer surfaces of the wings and the outer surface of the tail are joined to form a streamline structure. The included angle between the symmetry plane of the tail and the horizontal plane of the body ranges from 85 degrees to 95 degrees. Through the technical scheme, the shell of the unmanned aerial vehicle is good in wind resistance, so that the unmanned aerial vehicle is small in resistance and less in energy consumption in the flight process.
Description
Technical field
The utility model relates to the unmanned plane technical field, particularly a kind of unmanned plane shell.
Background technology
Robot airplane, be called for short unmanned plane (UAV, Unmanned Aerial Vehicle), is a kind of new ideas aircraft that is in developing rapidly, and it has advantages of maneuverability, reaction is quick, nobody flies, operation requirements is low.Unmanned plane, by carrying multiclass sensor, can be realized image real-time Transmission, high-risk regional detecting function, is that the strong of satellite remote sensing and traditional air remote sensing supplements.At present, the range of use of unmanned plane has been widened military affairs, scientific research, civilian three large fields, specifically in electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, the field application such as Crop Estimation, drug law enforcement anti-smuggling, border patrol, public security anti-terrorism are very wide.
At present, generally shell is not set or only is provided with simple and crude shell on the body of unmanned plane.
In realizing process of the present utility model, utility model people finds that there is following problem at least in prior art:
Shell is not set and only is provided with the helicopter wind resistance of simple and crude shell poor, in the unmanned plane during flying process, resistance is excessive, and the flight energy consumption is very high.
The utility model content
The purpose of this utility model is to provide the high unmanned plane shell of a kind of wind resistance to reduce the resistance in the unmanned plane during flying process, reduces the flight energy consumption.
To achieve these goals, the utility model embodiment provides a kind of unmanned plane shell, this unmanned plane shell is applicable to be arranged on the body of unmanned plane, and comprise head, fuselage, wing and tail, the outside face of the outside face of this head, the outside face of this fuselage, this wing and the outside face of this tail are connected the formation streamlined structure, and the angle between the horizontal surface at the plane of symmetry of this tail and this fuselage place is 85 to 95 degree.
Preferably, as an embodiment of the present utility model, the surface of this head, fuselage, wing and tail is equipped with carbon fiber layer or glass layer or 7075 aluminium alloy layers or titanium alloy layer.
Alternatively, the surface of this head, fuselage, wing and tail is equipped with the first protective cover and is positioned at the second protective cover on this first protective cover, and this first protective cover is carbon fiber layer or glass layer, and this second protective cover is 7075 aluminium alloy layers or titanium alloy layer.
In another embodiment of the present utility model, the upper end of this tail is provided with a groove, and this unmanned plane shell also comprises the protective case that is complementary with this groove, and this groove is applicable to accommodating data transmitter-receiver.
Preferably, the surface of this protective case is provided with carbon fiber layer or glass layer or 7075 aluminium alloy layers or titanium alloy layer.
Alternatively, this protective case surface is provided with the first protective cover and the second protective cover that is positioned on this first protective cover, and this first protective cover is carbon fiber layer or glass layer, and this second protective cover is 7075 aluminium alloy layers or titanium alloy layer.
Equally preferably, this protective case is circular.
In another embodiment of the present utility model, this head, this fuselage, this wing and this tail structure that is formed in one.
The beneficial effect that the technical scheme that the utility model embodiment provides is brought is:
Form streamlined structure because the outside face of the outside face of the outside face of the outside face of the head of unmanned plane shell, fuselage, wing and tail is connected, can reduce the resistance in the unmanned plane during flying process, reduce the energy consumption of flying.In addition, the angle between the horizontal surface at the plane of symmetry of tail and fuselage place is the 85-95 degree, can improve unmanned plane during flying stability on the one hand, can strengthen on the other hand unmanned plane and fly the naked eyes discernibility of rear head far away and tail.
Description of drawings
In order to be illustrated more clearly in the technical scheme in the utility model embodiment, in below describing embodiment, the accompanying drawing of required use is briefly described, apparently, accompanying drawing in the following describes is only embodiment more of the present utility model, for those of ordinary skills, under the prerequisite of not paying creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the schematic diagram of the unmanned plane shell that provides of the utility model embodiment;
Fig. 2 is the section drawing of unmanned plane shell shown in Figure 1.
The specific embodiment
, for making the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing, the utility model embodiment is described in further detail.
The utility model embodiment provides a kind of unmanned plane shell, this unmanned plane shell is applicable to be arranged on the body of unmanned plane, as depicted in figs. 1 and 2, this unmanned plane shell comprises head 11, fuselage 12, wing 13 and tail 14, the outside face of the outside face of the outside face of the outside face of this head 11, this fuselage 12, this wing 13 and this tail 14 is connected the formation streamlined structure, and the angle α between the horizontal surface at the plane of symmetry of this tail and this fuselage place is 85 to 95 degree.
Wherein, angle α is that 90 degree are best, can guarantee that the unmanned plane during flying windage is minimum.
Preferably, the surface of this head 11, fuselage 12, wing 13 and tail 14 is equipped with carbon fiber layer or glass layer or 7075 aluminium alloy layers or titanium alloy layer.Little, the withstand voltage height of this carbon fiber layer proportion.This glass layer resistance to effect of heat is strong, mechanical strength is high.This 7075 aluminium alloy layer intensity is high, resistance to abrasion good.This titanium alloy layer tissue is stable, resistance to abrasion is high, oxidation resistance is strong.
Alternatively; the surface of this head 11, fuselage 12, wing 13 and tail 14 is equipped with the first protective cover and is positioned at the second protective cover on this first protective cover; this first protective cover is carbon fiber layer or glass layer, and this second protective cover is 7075 aluminium alloy layers or titanium alloy layer.
In an embodiment of the present utility model, the upper end of this tail 14 is provided with a groove (figure does not look), and this unmanned plane shell also comprises the protective case 16 that is complementary with this groove, and this groove is applicable to accommodating data transmitter-receiver.Cooperatively interacting of this groove and this protective case 16 can avoid the data transmitter-receiver to be subject to the impact of environment on the basis that does not affect data transmission reception accuracy.
In another embodiment of the present utility model; this protective case 16 can be with reference to the design of head 11, fuselage 12, wing 13 and tail 14 in the unmanned plane shell, and the surface of this protective case 16 can be provided with carbon fiber layer or glass layer or 7075 aluminium alloy layers or titanium alloy layer.Alternatively, the surface of this protective case 16 can be provided with the first protective cover and the second protective cover that is positioned on this first protective cover, and this first protective cover is carbon fiber layer or glass layer, and this second protective cover is 7075 aluminium alloy layers or titanium alloy layer.
Preferably, this protective case 16 is circular.Circular design can improve signal emission and the received power of data transmitter-receiver.Understandably, this protective case 16 also can be triangle, semicircle, ellipse or square etc., but circle is best mode.
In an embodiment more of the present utility model, this head 11, fuselage 12, wing 13 and tail 14 structure that is formed in one.Integrated formed structure can avoid head, fuselage, wing and tail joining place each other the phenomenon of cracking to occur, and this structure can compress manufacturing cost, and is also very convenient when assembling casing and volume.
As from the foregoing, because the outside face of the outside face of the outside face of the outside face of the head of unmanned plane shell, fuselage, wing and tail is connected, form streamlined structure, can reduce the resistance in the unmanned plane during flying process, reduce the energy consumption of flying.In addition, the angle between the horizontal surface at the plane of symmetry of tail and fuselage place is the 85-95 degree, can improve unmanned plane during flying stability on the one hand, can strengthen on the other hand unmanned plane and fly the naked eyes discernibility of rear head far away and tail.
Above this is only preferred embodiment of the present utility model, not in order to limit the utility model, all within spirit of the present utility model and principle, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
Claims (8)
1. unmanned plane shell, comprise head, fuselage, wing and tail, it is characterized in that, the outside face of the outside face of described head, the outside face of described fuselage, described wing and the outside face of described tail are connected the formation streamlined structure, and the angle between the horizontal surface at the plane of symmetry of described tail and described fuselage place is 85 to 95 degree.
2. unmanned plane shell as claimed in claim 1, is characterized in that, the surface of described head, fuselage, wing and tail is equipped with carbon fiber layer or glass layer or 7075 aluminium alloy layers or titanium alloy layer.
3. unmanned plane shell as claimed in claim 1; it is characterized in that; the surface of described head, fuselage, wing and tail is equipped with the first protective cover and is positioned at the second protective cover on described the first protective cover; described the first protective cover is carbon fiber layer or glass layer, and described the second protective cover is 7075 aluminium alloy layers or titanium alloy layer.
4. unmanned plane shell as claimed in claim 1, is characterized in that, the upper end of described tail is provided with a groove, and described unmanned plane shell also comprises the protective case that is complementary with described groove, and described groove is applicable to accommodating data transmitter-receiver.
5. unmanned plane shell as claimed in claim 4, is characterized in that, the surface of described protective case is provided with carbon fiber layer or glass layer or 7075 aluminium alloy layers or titanium alloy layer.
6. unmanned plane shell as claimed in claim 4; it is characterized in that; the surface of described protective case is provided with the first protective cover and the second protective cover that is positioned on described the first protective cover; described the first protective cover is carbon fiber layer or glass layer, and described the second protective cover is 7075 aluminium alloy layers or titanium alloy layer.
7. unmanned plane shell as claimed in claim 4, is characterized in that, described protective case is circular.
8. unmanned plane shell as claimed in claim 1, is characterized in that, described head, described fuselage, described wing and the described tail structure that is formed in one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013202239959U CN203294306U (en) | 2013-04-27 | 2013-04-27 | Shell of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013202239959U CN203294306U (en) | 2013-04-27 | 2013-04-27 | Shell of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203294306U true CN203294306U (en) | 2013-11-20 |
Family
ID=49570338
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013202239959U Expired - Fee Related CN203294306U (en) | 2013-04-27 | 2013-04-27 | Shell of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203294306U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818956A (en) * | 2016-05-12 | 2016-08-03 | 辽宁壮龙无人机科技有限公司 | Fuel oil power multi-rotor-wing plant protection unmanned aerial vehicle hood |
| CN106863941A (en) * | 2016-12-30 | 2017-06-20 | 易瓦特科技股份公司 | Fixed-wing unmanned plane body and its manufacture method |
-
2013
- 2013-04-27 CN CN2013202239959U patent/CN203294306U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818956A (en) * | 2016-05-12 | 2016-08-03 | 辽宁壮龙无人机科技有限公司 | Fuel oil power multi-rotor-wing plant protection unmanned aerial vehicle hood |
| CN106863941A (en) * | 2016-12-30 | 2017-06-20 | 易瓦特科技股份公司 | Fixed-wing unmanned plane body and its manufacture method |
| CN106863941B (en) * | 2016-12-30 | 2019-03-12 | 易瓦特科技股份公司 | Fixed-wing unmanned plane body and its manufacturing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131120 Termination date: 20180427 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |