CN202717030U - Eight-axis rotor craft - Google Patents
Eight-axis rotor craft Download PDFInfo
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- CN202717030U CN202717030U CN 201220363839 CN201220363839U CN202717030U CN 202717030 U CN202717030 U CN 202717030U CN 201220363839 CN201220363839 CN 201220363839 CN 201220363839 U CN201220363839 U CN 201220363839U CN 202717030 U CN202717030 U CN 202717030U
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- flight controller
- arms
- rotors
- hold
- secondary hold
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Abstract
The utility model relates to an eight-axis rotor craft, which comprises a flight controller, a support frame arranged on the flight controller and eight rotors, wherein the eight rotors are arranged on the support frame and uniformly distributed around the flight controller 10. The eight-axis rotor craft is high in stability and flexibility, and can be folded to facilitate carrying and transportation.
Description
Technical field
The utility model relates to aircraft, particularly a kind of eight axle rotor crafts.
Background technology
Rotor craft has been widely used in the unmanned vehicle technical field, common rotor craft has three axle list (two) rotors, four axle list (two) rotors, six axle rotors etc., but above-mentioned rotor craft is due to the restriction of rotor, and its stability and alerting ability are not high; Simultaneously not collapsible, be inconvenient to carry and transport.
Summary of the invention
The utility model provides a kind of eight axle rotor crafts for the deficiencies in the prior art.
The technical scheme that the utility model adopts is as follows:
A kind of eight axle rotor crafts is characterized in that, comprising:
Flight controller;
Be located at the bracing frame on flight controller;
Eight rotors, described eight rotors are located on support frame as described above, and are uniformly distributed in around described flight controller.
A kind of eight axle rotor crafts as above, wherein, support frame as described above comprises eight hold-down arms of corresponding described eight rotors, described eight hold-down arms evenly are fixed on described flight controller, are M shape.
A kind of eight axle rotor crafts as above, wherein, described eight hold-down arms are hinged with described flight controller respectively.
A kind of eight axle rotor crafts as above, wherein, support frame as described above comprises eight master arms and four secondary hold-down arms of corresponding described eight rotors, the corresponding secondary hold-down arm of every two master arms, described every two master arms are connected with an end of corresponding secondary hold-down arm respectively, the other end of described corresponding secondary hold-down arm is connected with flight controller, and described four secondary hold-down arms are criss-cross.
A kind of eight axle rotor crafts as above, wherein, described every two master arms are hinged with an end of corresponding secondary hold-down arm respectively, and the other end and the flight controller of described corresponding secondary hold-down arm are hinged.
A kind of eight axle rotor crafts as above wherein, are provided with electronic compass and gyroscope in described flight controller.
A kind of eight axle rotor crafts as above, wherein, described flight controller is provided with camera.
The utlity model has following beneficial effect:
1, the utlity model has eight rotors, improved stability and the alerting ability of rotor craft;
2, the utility model is controlled rotation direction and the velocity of rotation of eight rotors by flight controller, can control easily rotor craft lifting, advance, retreat, left and action to the right, further improved stability and the alerting ability of rotor craft;
3, hold-down arm of the present utility model can fold, and is convenient for carrying and transports.
Description of drawings
Describe the utility model in detail below in conjunction with the drawings and specific embodiments:
Fig. 1 is the structural representation of the utility model one embodiment;
Fig. 2 is the structural representation of the utility model one embodiment;
Fig. 3 is folded state schematic diagram embodiment illustrated in fig. 1;
Fig. 4 is folded state schematic diagram embodiment illustrated in fig. 2.
Wherein, the arrow in Fig. 1 and Fig. 2 represents the hand of rotation of rotor.
The specific embodiment
For technological means, creation characteristic that the utility model is realized, reach purpose and effect is easy to understand, below in conjunction with concrete diagram, further set forth the utility model.
As Fig. 1 and as shown in Figure 2, a kind of eight axle rotor crafts comprise flight controller 10, bracing frame 20 and eight rotors 30 that driven by motor.Bracing frame 20 is located on flight controller 10, and eight rotors 30 are located on bracing frame 20, and are uniformly distributed in around flight controller 10.Owing to having eight rotors, improved stability and the alerting ability of rotor craft.
Eight axle rotor crafts can adopt not only light intensity but also higher carbon fiber composite material, and aircraft weight is lightened again very high load-carrying capacity simultaneously.
10 can arrange electronic compass and gyroscope in flight controller, can provide enough safety control for rotor craft, simultaneously, also camera can be set, and scout and rescue is offered help for unmanned.
Particularly, as the hand of rotation of each rotor 30 such as Fig. 1 and when shown in Figure 2, and the rotating speed of each rotor 30 is identical, increases simultaneously each rotor 30 rotating speeds, and aircraft is lift-off just; Otherwise, each rotor 30 rotating speeds that slow down simultaneously, rotor craft is landing just.
As the hand of rotation of each rotor 30 such as Fig. 1 and when shown in Figure 2, control the rotating speed of each rotor 30 by flight controller 10, thereby obtain the rotor 30 of different rotation rates, that so just can realize rotor craft advances, retreats, waits flight operation left, to the right.
Particularly, as shown in Figure 1, bracing frame 20 comprises eight hold-down arms 21 of corresponding eight rotors 30, and described eight hold-down arms 21 evenly are fixed on flight controller 10, are M shape.
In order to be convenient for carrying and to transport, eight hold-down arms 21 are hinged with flight controller 10 respectively, and eight axle rotor crafts can be folded, and so greatly saved the space, and can play the effect of protection aircraft; State after folding please refer to accompanying drawing 3.
Certainly, bracing frame 20 also can be realized by another structure, particularly, as shown in Figure 2, bracing frame 20 comprises eight master arms 22 and four secondary hold-down arms 23 of corresponding eight rotors 30, the corresponding secondary hold-down arm 23 of every two master arms 22, and every two master arms 22 are connected with an end of corresponding secondary hold-down arm 23 respectively, the other end of corresponding secondary hold-down arm 23 is connected with flight controller 10, and four secondary hold-down arms 23 are criss-cross.
In order to be convenient for carrying and to transport, every two master arms 22 are hinged with an end of corresponding secondary hold-down arm 23 respectively, and the other end of corresponding secondary hold-down arm 23 and flight controller 10 are hinged, and rotor craft can be folded, so greatly save the space, and can play the effect of protection aircraft; State after folding please refer to accompanying drawing 4.
Above demonstration and described groundwork of the present utility model, principal character and advantage of the present utility model.The technical personnel of the industry should be understood; the utility model is not restricted to the described embodiments; that describes in above-described embodiment and specification sheets just illustrates principle of the present utility model; the utility model also has various changes and modifications under the prerequisite that does not break away from the utility model spirit and scope, and these changes and improvements all fall in claimed the utility model scope.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (7)
1. an axle rotor craft, is characterized in that, comprising:
Flight controller;
Be located at the bracing frame on flight controller;
Eight rotors, described eight rotors are located on support frame as described above, and are uniformly distributed in around described flight controller.
2. a kind of eight axle rotor crafts according to claim 1, is characterized in that, support frame as described above comprises eight hold-down arms of corresponding described eight rotors, and described eight hold-down arms evenly are fixed on described flight controller, are M shape.
3. a kind of eight axle rotor crafts according to claim 2, is characterized in that, described eight hold-down arms are hinged with described flight controller respectively.
4. a kind of eight axle rotor crafts according to claim 1, it is characterized in that, support frame as described above comprises eight master arms and four secondary hold-down arms of corresponding described eight rotors, the corresponding secondary hold-down arm of every two master arms, described every two master arms are connected with an end of corresponding secondary hold-down arm respectively, the other end of described corresponding secondary hold-down arm is connected with flight controller, and described four secondary hold-down arms are criss-cross.
5. a kind of eight axle rotor crafts according to claim 4, is characterized in that, described every two master arms are hinged with an end of corresponding secondary hold-down arm respectively, and the other end and the flight controller of described corresponding secondary hold-down arm are hinged.
6. the described a kind of eight axle rotor crafts of according to claim 1 ~ 5 any one, is characterized in that, is provided with electronic compass and gyroscope in described flight controller.
7. a kind of eight axle rotor crafts according to claim 6, is characterized in that, described flight controller is provided with camera.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220363839 CN202717030U (en) | 2012-07-25 | 2012-07-25 | Eight-axis rotor craft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220363839 CN202717030U (en) | 2012-07-25 | 2012-07-25 | Eight-axis rotor craft |
Publications (1)
Publication Number | Publication Date |
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CN202717030U true CN202717030U (en) | 2013-02-06 |
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CN 201220363839 Expired - Fee Related CN202717030U (en) | 2012-07-25 | 2012-07-25 | Eight-axis rotor craft |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103963969A (en) * | 2014-04-30 | 2014-08-06 | 中国科学院长春光学精密机械与物理研究所 | Aircraft with multiple layers of rotary wings of circumferentially distributed rotary planes |
CN104085529A (en) * | 2014-07-31 | 2014-10-08 | 山东创惠电子科技股份有限公司 | Eight-rotor-wing unmanned plane system |
CN104584330A (en) * | 2014-07-28 | 2015-04-29 | 深圳市大疆创新科技有限公司 | Wire connetion seat, energy supplying assembly using same, and aircraft |
CN104787318A (en) * | 2015-04-20 | 2015-07-22 | 吴李海 | Multi-rotor unmanned aerial vehicle with function of loaded long-time flying |
WO2015117512A1 (en) * | 2014-02-08 | 2015-08-13 | 杨华东 | Multi-axis flight unit |
CN105912023A (en) * | 2016-05-31 | 2016-08-31 | 王翔 | Portable multifunctional unmanned aerial vehicle and control system and control method thereof |
WO2016138604A1 (en) * | 2015-03-04 | 2016-09-09 | 珠海羽人飞行器有限公司 | Agricultural aircraft |
CN107069361A (en) * | 2017-05-10 | 2017-08-18 | 中科新松有限公司 | A kind of power distribution device and unmanned plane |
CN108469829A (en) * | 2018-03-05 | 2018-08-31 | 黄相贤 | A kind of the stable type control mode and control algolithm of unmanned plane |
-
2012
- 2012-07-25 CN CN 201220363839 patent/CN202717030U/en not_active Expired - Fee Related
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015117512A1 (en) * | 2014-02-08 | 2015-08-13 | 杨华东 | Multi-axis flight unit |
CN103963969A (en) * | 2014-04-30 | 2014-08-06 | 中国科学院长春光学精密机械与物理研究所 | Aircraft with multiple layers of rotary wings of circumferentially distributed rotary planes |
CN104584330A (en) * | 2014-07-28 | 2015-04-29 | 深圳市大疆创新科技有限公司 | Wire connetion seat, energy supplying assembly using same, and aircraft |
US10374331B2 (en) | 2014-07-28 | 2019-08-06 | SZ DJI Technology Co., Ltd. | Wire connector, and power supply assembly and aerial vehicle using the wire connector |
CN104085529A (en) * | 2014-07-31 | 2014-10-08 | 山东创惠电子科技股份有限公司 | Eight-rotor-wing unmanned plane system |
WO2016138604A1 (en) * | 2015-03-04 | 2016-09-09 | 珠海羽人飞行器有限公司 | Agricultural aircraft |
CN104787318A (en) * | 2015-04-20 | 2015-07-22 | 吴李海 | Multi-rotor unmanned aerial vehicle with function of loaded long-time flying |
CN105912023A (en) * | 2016-05-31 | 2016-08-31 | 王翔 | Portable multifunctional unmanned aerial vehicle and control system and control method thereof |
CN105912023B (en) * | 2016-05-31 | 2019-12-13 | 南京禾谱航空科技有限公司 | portable multifunctional unmanned aerial vehicle |
CN107069361A (en) * | 2017-05-10 | 2017-08-18 | 中科新松有限公司 | A kind of power distribution device and unmanned plane |
CN108469829A (en) * | 2018-03-05 | 2018-08-31 | 黄相贤 | A kind of the stable type control mode and control algolithm of unmanned plane |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130206 Termination date: 20130725 |