CN103171763A - Novel unmanned plane - Google Patents
Novel unmanned plane Download PDFInfo
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- CN103171763A CN103171763A CN2013101404667A CN201310140466A CN103171763A CN 103171763 A CN103171763 A CN 103171763A CN 2013101404667 A CN2013101404667 A CN 2013101404667A CN 201310140466 A CN201310140466 A CN 201310140466A CN 103171763 A CN103171763 A CN 103171763A
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- main body
- rotor
- unmanned plane
- pick
- camera assembly
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- 239000012780 transparent material Substances 0.000 claims abstract description 4
- 239000002131 composite material Substances 0.000 claims description 3
- 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 invention provides a novel unmanned plane which is characterized by being provided with a barrel-shaped hollow main unit body, wherein a plurality of rotor wing supporting rods are arranged on the main unit body and are symmetrically arranged relative to the main unit body; rotor wings are arranged at the ends of the rotor wing supporting rods; power sources connected with and driving the rotor wings are arranged in the main unit body or the rotor wing supporting rods; a camera hole covered by a transparent material is formed in the lower surface of the main unit body; a camera assembly is arranged in the main unit body and corresponds to the camera hole; and a controller connected with and used for controlling the power sources and the camera assembly is arranged in the main unit body. The main unit body and the rotor wing supporting rods form a shell with an integrated structure. According to the novel unmanned plane, the camera assembly is arranged in the main unit body, and the main unit body and the rotor wing supporting rods are integrated, so that the streamline-type shell is high in aerodynamic performance.
Description
Technical field
The invention belongs to a kind of flight equipment, relate 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.
Summary of the invention
The invention provides a kind of novel unmanned plane, its objective is to solve the shortcoming that prior art exists, make the aerodynamic performance of depopulated helicopter better.
The technical solution adopted for the present invention to solve the technical problems 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 invention is:
The present invention 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 structural representation of the present invention.
The specific embodiment
The embodiment of the present invention as shown in Figure 1:
The present invention 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).
Pass through ground remote control equipment when the present invention uses and send remote signal, 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. as claimed in claim novel unmanned plane, it is characterized in that: described main body and rotor pole are the integrated shell that composite material is made.
3. as claimed in claim novel unmanned plane, 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. as claimed in claim novel unmanned plane, it is characterized in that: slot is set on main body, and the photographed data registration card is electrically connected to the pick up camera assembly after inserting slot.
5. as claimed in claim novel unmanned plane, 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 |
|---|---|---|---|
| CN2013101404667A CN103171763A (en) | 2013-04-22 | 2013-04-22 | Novel unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101404667A CN103171763A (en) | 2013-04-22 | 2013-04-22 | Novel unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103171763A true CN103171763A (en) | 2013-06-26 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013101404667A Pending CN103171763A (en) | 2013-04-22 | 2013-04-22 | Novel unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN103171763A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015000277A1 (en) * | 2013-07-01 | 2015-01-08 | 昊翔电能运动科技(昆山)有限公司 | Multi-axial flying machine |
| WO2015109700A1 (en) * | 2014-01-24 | 2015-07-30 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body, and manufacturing method therefor |
| CN105872334A (en) * | 2016-05-06 | 2016-08-17 | 上海航天测控通信研究所 | Aviation support integrated compact camera |
| CN107683243A (en) * | 2015-06-01 | 2018-02-09 | 元基渊 | Fire-fighting unmanned plane is used in fire extinguishing |
| CN109050892A (en) * | 2013-11-13 | 2018-12-21 | 深圳市大疆创新科技有限公司 | More rotor unmanned aircrafts |
| CN111661327A (en) * | 2019-03-05 | 2020-09-15 | 上海科技大学 | Many rotors of flexible fuselage flight device |
| US11338912B2 (en) | 2012-11-15 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
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| CN101381002A (en) * | 2008-10-24 | 2009-03-11 | 华北电力大学 | Flying robot for detecting transmission line insulator |
| CN101559832A (en) * | 2008-03-25 | 2009-10-21 | 尤洛考普特公司 | Fast hybrid helicopter with large range |
| CN202080435U (en) * | 2011-05-12 | 2011-12-21 | 张思远 | Ranked dual-rotor vertically-lifted unmanned aerial vehicle (UAV) |
| US20120083945A1 (en) * | 2010-08-26 | 2012-04-05 | John Robert Oakley | Helicopter with multi-rotors and wireless capability |
| CN302133121S (en) * | 2012-06-13 | 2012-10-17 | 王麒麟 | Drone |
| CN203268313U (en) * | 2013-04-22 | 2013-11-06 | 王麒麟 | Novel unmanned aerial vehicle |
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2013
- 2013-04-22 CN CN2013101404667A patent/CN103171763A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101559832A (en) * | 2008-03-25 | 2009-10-21 | 尤洛考普特公司 | Fast hybrid helicopter with large range |
| CN101381002A (en) * | 2008-10-24 | 2009-03-11 | 华北电力大学 | Flying robot for detecting transmission line insulator |
| US20120083945A1 (en) * | 2010-08-26 | 2012-04-05 | John Robert Oakley | Helicopter with multi-rotors and wireless capability |
| CN202080435U (en) * | 2011-05-12 | 2011-12-21 | 张思远 | Ranked dual-rotor vertically-lifted unmanned aerial vehicle (UAV) |
| CN302133121S (en) * | 2012-06-13 | 2012-10-17 | 王麒麟 | Drone |
| CN203268313U (en) * | 2013-04-22 | 2013-11-06 | 王麒麟 | Novel unmanned aerial vehicle |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11338912B2 (en) | 2012-11-15 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
| WO2015000277A1 (en) * | 2013-07-01 | 2015-01-08 | 昊翔电能运动科技(昆山)有限公司 | Multi-axial flying machine |
| CN109050892A (en) * | 2013-11-13 | 2018-12-21 | 深圳市大疆创新科技有限公司 | More rotor unmanned aircrafts |
| WO2015109700A1 (en) * | 2014-01-24 | 2015-07-30 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body, and manufacturing method therefor |
| CN107683243A (en) * | 2015-06-01 | 2018-02-09 | 元基渊 | Fire-fighting unmanned plane is used in fire extinguishing |
| CN107683243B (en) * | 2015-06-01 | 2020-08-04 | 元基渊 | Fire-fighting unmanned aerial vehicle for fire extinguishment |
| CN105872334A (en) * | 2016-05-06 | 2016-08-17 | 上海航天测控通信研究所 | Aviation support integrated compact camera |
| CN111661327A (en) * | 2019-03-05 | 2020-09-15 | 上海科技大学 | Many rotors of flexible fuselage flight device |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| ASS | Succession or assignment of patent right |
Owner name: XIAMEN RUIHANG PRECISION TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: WANG QILIN Effective date: 20140928 |
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| 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 |
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| TA01 | Transfer of patent application right |
Effective date of registration: 20140928 Address after: Two road, Huli District of Xiamen city in Fujian province 361010 Fang Hu Xi No. 1-3 (office building) room 326 Applicant after: XIAMEN RUIHANG PRECISION TECHNOLOGY CO., LTD. Address before: Xianglian Siming District of Xiamen city in Fujian province 361009 No. 33 room 2907 Applicant before: Wang Qilin |
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130626 |