CN203268313U - Novel unmanned aerial vehicle - Google Patents
Novel unmanned aerial vehicle Download PDFInfo
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- CN203268313U CN203268313U CN 201320203767 CN201320203767U CN203268313U CN 203268313 U CN203268313 U CN 203268313U CN 201320203767 CN201320203767 CN 201320203767 CN 201320203767 U CN201320203767 U CN 201320203767U CN 203268313 U CN203268313 U CN 203268313U
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- main body
- machine body
- main machine
- camera assembly
- pick
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- 239000012780 transparent material Substances 0.000 claims abstract description 4
- 239000002131 composite material Substances 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims 1
- 238000003780 insertion Methods 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
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Abstract
The utility model provides a novel unmanned aerial vehicle which is characterized in that the novel unmanned aerial vehicle is provided with a cylindrical hollow main machine body; the main machine body is provided with a plurality of rotary wing supporting rods symmetrically distributed relative to the main machine body, the end part of each rotary wing supporting rod is provided with a rotary wing, the main machine body or the rotary wing supporting rods are internally provided with a power source for being connected with and driving the rotary wings; the lower surface of the main machine body is provided with a camera shooting hole covered by a transparent material; the part, which is corresponding to the camera shooting hole is provided with a video camera assembly; the main machine body is internally provided with a controller used for connecting and controlling the power source and the video camera assembly; the main machine body and the rotary wing supporting rods are of a shell with an integrated structure. By adopting a mode that the video camera assembly is arranged in the main machine body and a mode that the main machine body and the rotary wing supporting rods are integrally molded, a linear shell with good aerodynamic performance can be manufactured.
Description
Technical field
The utility model belongs to a kind of flight equipment, relates in particular to a kind of depopulated helicopter equipment.
Background technology
Depopulated helicopter is to begin at present practical gradually a kind of flight equipment, loads pick up camera on depopulated helicopter, and fire-fighting, military affairs, the police service field of being applied to monitors to realize the cruise shooting in needs zones or to specify.It is little that depopulated helicopter has floor area, and landing is flexible, can hover, and the multiple advantage such as is convenient to control.
Present depopulated helicopter is single shaft single-blade form or the common oar form of single shaft the most generally, is rotor a top that comprises the mechanical framework of driving machine (electrical motor or combustion engine), the below lifting pick up camera of mechanical framework.The shortcoming of this structure be aerodynamic performance this structure that has more is damaged due to pick up camera, cause integrally-built overbalance, increased the difficulty of controlling.
The utility model content
The utility model provides a kind of novel unmanned plane, its objective is to solve the shortcoming that prior art exists, and makes the aerodynamic performance of depopulated helicopter better.
The technical scheme that its technical matters that solves the utility model adopts is:
A kind of novel unmanned plane is characterized in that:
Has the hollow main body of tubular;
Main body is provided with several rotor poles, and rotor pole is symmetrical with respect to main body, and the end of each rotor pole arranges rotor;
Be provided with the propulsion source that connects and drive rotor in main body or rotor pole;
The lower surface of main body is provided with the shooting hole that transparent material covers, and in main body, corresponding shooting hole site is provided with the pick up camera assembly;
Be provided with the controller that connects and control above-mentioned propulsion source and pick up camera assembly in main body.
Described main body and rotor pole are the integrated shell that composite material is made.
Described main body is the stream line pattern cylindrical body, between the outside face of the outside face of main body and rotor pole for being connected smoothly.
Slot is set on main body, and the photographed data registration card is electrically connected to the pick up camera assembly after inserting slot.
Described main body is the stream line pattern cylindrical body, between main body and rotor pole for being connected smoothly.
The main body upper surface is provided with the camera control panel, establishes the control button that is electrically connected to and can controls the pick up camera assembly with the pick up camera assembly on the camera control panel.
Usefulness of the present utility model is:
The utility model has adopted the pick up camera assembly has been arranged on mode in main body, therefore can realize on housing being exceptionally all the surface of smooth change except Rotary-Wing Department, the mode of taking main body and rotor pole to be integrated, can make the fleetline housing, reduced the attaching parts between main body and rotor pole, thereby reduced weight and installation difficulty, therefore had good aerodynamic performance.
Description of drawings
Fig. 1 is the utility model structural representation.
The specific embodiment
The utility model embodiment as shown in Figure 1:
The utility model is a kind of unmanned plane of helicopter form, its main body 1 is along the hollow housing form of the strip shape tubular of axis face symmetry, main body 1 is provided with 6 rotor poles 2, rotor pole 2 is symmetrical with respect to main body, also namely with respect to the both sides of the middle axial plane of main body 1, three rotor poles 2 are arranged respectively, and the rotor pole 2 of both sides is symmetrical arranged.The rotor pole of designed varying number as required in other embodiments.
The present embodiment also is provided with two with respect to the leg 5 of the axis face symmetry of main body 1 below main body 1.
The end of each rotor pole 2 arranges rotor 4, is provided with a motor 3 that drives rotor in the rotor pole 2 of each rotor 4 belows, and power supply 10 is located in main body 1 and is connected to provide power can drive rotor 4 with each motor 3.
In other embodiments, propulsion source also can be provided in a side of the combustion engine in main body 1, and combustion engine connects by deceleration system and drives rotor 4.
The close head lower surface of main body 1 is provided with shooting hole 6(that transparent material (for example glass) covers also can be made as head fleetline glass-faced surface), the minimum power system that comprises camera and drive camera of pick up camera assembly 7() be arranged in main body 1 near head and corresponding to the position in shooting hole 6.The upper surface of main body 1 is provided with camera control panel 8, establishes the control button (can control by this control panel 8 when unmanned plane is positioned at ground and adjust pick up camera assembly 7) that is electrically connected to and can controls pick up camera assembly 7 with pick up camera assembly 7 on camera control panel 8.Slot 12 is set on main body 1, and photographed data registration card 9 is electrically connected to (this set can not taken unmanned plane apart and just obtain data in pick up camera) with pick up camera assembly 7 after inserting slots 12.
Be provided with the controller 11(that connects and control said motor 3 and pick up camera assembly 7 in main body 1 and comprise remote signal receiver and CPU).
When using, the utility model sends remote signal by ground remote control equipment, processed by CPU after remote signal receiver reception by controller 11, CPU can control motor 3 and then control rotor 4 and the flight of control unmanned plane, and CPU controls shooting and the rotation of the camera of pick up camera assembly 7.
Claims (5)
1. novel unmanned plane is characterized in that:
Has the hollow main body of tubular;
Main body is provided with several rotor poles, and rotor pole is symmetrical with respect to main body, and the end of each rotor pole arranges rotor;
Be provided with the propulsion source that connects and drive rotor in main body or rotor pole;
The lower surface of main body is provided with the shooting hole that transparent material covers, and in main body, corresponding shooting hole site is provided with the pick up camera assembly;
Be provided with the controller that connects and control above-mentioned propulsion source and pick up camera assembly in main body.
2. novel unmanned plane as claimed in claim 1, it is characterized in that: described main body and rotor pole are the integrated shell that composite material is made.
3. novel unmanned plane as claimed in claim 2, it is characterized in that: described main body is the stream line pattern cylindrical body, between the outside face of the outside face of main body and rotor pole for being connected smoothly.
4. novel unmanned plane as claimed in claim 1, is characterized in that: slot is set on main body, is electrically connected to the pick up camera assembly after photographed data registration card insertion slot.
5. novel unmanned plane as claimed in claim 1, it is characterized in that: the main body upper surface is provided with the camera control panel, establishes the control button that is electrically connected to and can controls the pick up camera assembly with the pick up camera assembly on the camera control panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320203767 CN203268313U (en) | 2013-04-22 | 2013-04-22 | Novel unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320203767 CN203268313U (en) | 2013-04-22 | 2013-04-22 | Novel unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203268313U true CN203268313U (en) | 2013-11-06 |
Family
ID=49498771
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320203767 Expired - Fee Related CN203268313U (en) | 2013-04-22 | 2013-04-22 | Novel unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203268313U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103171763A (en) * | 2013-04-22 | 2013-06-26 | 王麒麟 | Novel unmanned plane |
| CN104986321A (en) * | 2015-07-10 | 2015-10-21 | 哈瓦国际航空技术（深圳）有限公司 | Integrated aircraft body |
| CN106218883A (en) * | 2016-09-05 | 2016-12-14 | 广州市丹爵通讯科技有限公司 | A kind of unmanned plane with high-definition camera ability for oil exploration |
| WO2017166724A1 (en) * | 2016-03-30 | 2017-10-05 | 乐视控股（北京）有限公司 | Aircraft apron device, aircraft, and aircraft parking system |
-
2013
- 2013-04-22 CN CN 201320203767 patent/CN203268313U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103171763A (en) * | 2013-04-22 | 2013-06-26 | 王麒麟 | Novel unmanned plane |
| CN104986321A (en) * | 2015-07-10 | 2015-10-21 | 哈瓦国际航空技术（深圳）有限公司 | Integrated aircraft body |
| CN104986321B (en) * | 2015-07-10 | 2017-06-06 | 哈瓦国际航空技术（深圳）有限公司 | A kind of integrated flight device body |
| WO2017166724A1 (en) * | 2016-03-30 | 2017-10-05 | 乐视控股（北京）有限公司 | Aircraft apron device, aircraft, and aircraft parking system |
| CN106218883A (en) * | 2016-09-05 | 2016-12-14 | 广州市丹爵通讯科技有限公司 | A kind of unmanned plane with high-definition camera ability for oil exploration |
| CN106218883B (en) * | 2016-09-05 | 2018-09-21 | 嘉兴维特拉电气科技有限公司 | A kind of unmanned plane with high-definition camera ability for oil exploration |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: XIAMEN RUIHANG PRECISION TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: WANG QILIN Effective date: 20131226 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 361009 XIAMEN, FUJIAN PROVINCE TO: 361010 XIAMEN, FUJIAN PROVINCE |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20131226 Address after: Two road, Huli District of Xiamen city in Fujian province 361010 Fang Hu Xi No. 1-3 (office building) room 326 Patentee after: XIAMEN RUIHANG PRECISION TECHNOLOGY CO., LTD. Address before: Xianglian Siming District of Xiamen city in Fujian province 361009 No. 33 room 2907 Patentee before: Wang Qilin |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131106 Termination date: 20160422 |