CN204956909U - Portable unmanned aerial vehicle - Google Patents
Portable unmanned aerial vehicle Download PDFInfo
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- CN204956909U CN204956909U CN201520492653.6U CN201520492653U CN204956909U CN 204956909 U CN204956909 U CN 204956909U CN 201520492653 U CN201520492653 U CN 201520492653U CN 204956909 U CN204956909 U CN 204956909U
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Abstract
The utility model discloses a portable unmanned aerial vehicle, including fuselage, a 2 -8 horn rotation axis, a 2 -8 horn, 4 -16 piece paddle, a 2 -8 paddle rotary part, its characterized in that: every horn one end is fixed on the fuselage through a rotation axis, and a 2 -8 horn symmetric distribution is on the fuselage, every horn other end installation paddle rotary part, every paddle tail end is equipped with the round hole, installs two paddles on every paddle rotary part. The utility model discloses to compare the operation simpler with four rotor unmanned aerial vehicle of other brands with equal -volume and performance, takes in more easily, more conveniently carries. It is long wide similar with A4 paper in folding back, and though be go out at ordinary times or go out that the tourism can all follow one's bent put individual knapsack, suitcase and che nei into, also can be lightly freely even holding. The injury of external force is avoided to better protection horn, blade and the foot rest of folding state ability simultaneously.
Description
Technical field
The utility model relates to a kind of Portable unmanned machine.
Background technology
Along with developing rapidly of unmanned plane industry, unmanned plane will enter in the daily life of ordinary consumer, work, amusement as camera.And four rotor wing unmanned aerial vehicles were all fixed horns in the past, small product size was comparatively large, and take up space, particularly thin and sharp blade allows most people fear especially when high speed operation, product does not have affinity.Therefore, in order to make unmanned plane have more affinity, its product should consider design factor and the speciality of fashional consumption level product, makes it to be presented in face of everybody with a kind of image having more affinity.Except profile fashion is attractive in appearance, the powerful and unmanned plane of compact more can meet the needs of people's daily life.
Utility model content
The purpose of this utility model provides a kind of Collapsible mobile four rotor wing unmanned aerial vehicle, have simple to operate, easily receive, the feature be convenient for carrying, after the utility model is folding, its length and width are similar to A4 paper, no matter be to go out at ordinary times or out on tours arbitraryly can put individual knapsack, baggage container and Che Nei into, also can be freely light even hand-held.Simultaneously folding state can better protect horn, blade and foot rest from the injury of external force.
The technical solution of the utility model is:
Collapsible mobile four rotor wing unmanned aerial vehicle, comprises fuselage, a 2-8 S. A., a 2-8 horn, 4-16 sheet blade, a 2-8 blade turning unit; It is characterized in that: each horn one end is fixed on fuselage by a S. A., and 2-8 horn is symmetrically distributed on fuselage; Each horn other end installs blade turning unit, and every sheet blade tail end is provided with circular hole, and each blade turning unit installs two panels blade.
The utility model also comprises two foot rests, four foot rest bases, and each foot rest is fixed on fuselage bottom by two foot rest bases.
Described S. A. is made up of fuselage turning unit and horn turning unit, and fuselage turning unit is fixed on fuselage, and horn turning unit is fixed on horn, and horn turning unit by limitation locking in fuselage turning unit.
Multiple horns of fuselage homonymy are upper and lower state straggly.
Described blade turning unit comprises motor, press strip, Fast detachable unit; Motor is arranged on the horn other end, each motor is installed two panels blade, and blade is arranged on the blade spindle that on motor, two ends are outstanding, and two panels blade is pushed down through the threaded column of motor center by press strip, and the threaded column of Fast detachable unit and motor center screws and locked by press strip.
Two described foot rests are small one and large one, and little foot rest passes inside large foot rest, and latter two foot rest folding is in same level, and the inwall of each foot rest base is designed to C-type clamp, limits the expansion of foot rest or folding angle by foot rest base.
After the utility model is folding, its length and width are similar to A4 paper, no matter be to go out at ordinary times or out on tours arbitraryly can put individual knapsack, baggage container and Che Nei into, and also can be freely light even hand-held.Simultaneously folding state can better protect horn, blade and foot rest from the injury of external force.
Accompanying drawing explanation
Fig. 1 is deployed condition schematic diagram of the present utility model;
Fig. 2 is folded state schematic diagram of the present utility model;
Fig. 3 is expanded angle of the present utility model and horn hand of rotation schematic diagram;
Fig. 4 is the upper and lower layout schematic diagram straggly of horn of the present utility model;
Fig. 5 is that blade of the present utility model launches and fast removable member dismounting partial schematic diagram;
Fig. 6 is the partial schematic diagram after blade of the present utility model folds;
Fig. 7 is foot rest of the present utility model and fuselage connection diagram;
Fig. 8 is foot rest of the present utility model and foot rest base partial schematic diagram;
Fig. 9 is foot rest expanded angle schematic diagram of the present utility model.
Figure 10 is bottom upward schematic diagram of the present utility model.
Detailed description of the invention:
For making the technical solution of the utility model, object and advantage clearly, below in conjunction with accompanying drawing, the utility model is described in further detail.
The utility model provides a kind of Portable unmanned machine, as shown in Figure 1, Figure 2, shown in Fig. 4, Fig. 5, Fig. 6, Fig. 7, Figure 10, the utility model comprises fuselage 1, four S. A.s, four horns, 3, eight blades, 8, four blade turning units (5,6,7), two foot rests (12,13), four foot rest bases 11; It is characterized in that: each horn 3 one end is fixing on the fuselage 1 by a S. A., and four horns 3 are distributed in both sides before and after fuselage 1, and symmetrical distribution, two horns 3 of fuselage 1 homonymy are in upper and lower state straggly; Described S. A. is made up of fuselage turning unit 2 and horn turning unit 4, and fuselage turning unit 2 is fixing, and horn turning unit 4 is fixed on horn 3 on the fuselage 1, and horn turning unit 4 by limitation locking in fuselage turning unit 2; Each horn 3 other end installs blade turning unit, and every sheet blade 8 tail end is provided with circular hole, and each blade turning unit installs two panels blade 8; Described blade turning unit comprises motor 5, press strip 6, Fast detachable unit 7, motor 5 is arranged on horn 3 one end, two panels blade 8 installed by each motor 5, blade 8 is arranged on the blade spindle 10 that on motor 5, two ends are outstanding, two panels blade 8 is pushed down through the threaded column 9 at motor 5 center by press strip 6, and Fast detachable unit 7 screws with the threaded column 9 at motor 5 center and locked by press strip 6; Each foot rest is fixed two foot rest bases 11, each foot rest is fixed on bottom fuselage 1 by two foot rest bases 11; Described two foot rests (12,13) are small one and large one, and little left foot frame 12 passes inside large right crus of diaphragm frame 13; Latter two foot rest folding is in same level.The inwall of each foot rest base 11 is designed to C-type clamp, limits the expansion of foot rest or folding angle by foot rest base 11.
The utility model provides a kind of foldable integral design example scheme of Collapsible mobile four rotor wing unmanned aerial vehicle, as depicted in figs. 1 and 2, described in upper one, the utility model defines one group of storage mode, this group storage mode makes product after storage, reach small size, regular state, make product not need to carry out any fitting operation, only need easily to rotate after each parts launch and just can carry out flight operation.
In embodiment of the present utility model, horn 3 is connected by one group of S. A. with fuselage 1, this group S. A. comprises fuselage turning unit 2 and horn turning unit 4 forms, this group S. A. does not need the nuisance operation of the devices such as the button of other outside or buckle horn just can be helped to fold and launch, and be designed with limitation locking structure, only need apply its direction that just can prolong power of certain application force to horn to rotate, and as shown in Figure 3 at the position strong fix of 120 °.Ensure the convenience that user uses, also ensure product launch after can stable flight and folding after minimum volume all around;
As shown in Figure 2 and Figure 4, the utility model is in the folding embodiment of arranging of horn 3, and two horns are upper and lower straggly folding, utilize the gauge of fuselage 1 itself, do not increase remaining volumetric spaces after folding, reach effectively folding object, after making it folding, size is compacter;
In the utility model, the Fast Installation of blade and folding embodiment are as Fig. 5, shown in Fig. 6, the circular hole of the blade 8 tail end blade spindle 10 outstanding with two ends on motor 5 is corresponding installs after, press strip 6 passes the threaded column 9 at motor 5 center, then the threaded column 9 at Fast detachable unit 7 and motor 5 center is screwed locking; Blade 8 can not firmly be locked by press strip 6 and Fast detachable unit 7, but plays relatively-stationary effect to blade 8; Blade 8 is when naturally being compressed, and the effect being subject to external force also can to fold into very easily above horn 3 and to stablize its position, after folding as shown in Figure 6;
In the utility model, one piece of contrarotation nut is equipped with and motor 5 center threaded column 9 screws locking in Fast detachable unit 7 center of blade turning unit the top, not easily gets loose; The diameter of Fast detachable unit 7 is comparatively large, and be convenient to user and grasp, user also need not can carry out fast assembling-disassembling replacing to blade 8 by any instrument;
The embodiment that in the utility model, foot rest is folding as shown in Fig. 7, Fig. 8, Fig. 9, Figure 10,
As shown in Figure 9, the activity point of view of foot rest, at 0 °-110 °, can balance landing when the span of two foot rests ensures landing;
As shown in Figure 7 and Figure 8, foot rest base 11 guarantees that foot rest is firmly connected with fuselage 1, and is realized the expansion of foot rest by the position, axle center on foot rest base 11 and packed up; The C-type clamp design of foot rest base 11 inwall simultaneously guarantees that foot rest is launching and is being in firm positioning states after packing up and can not rocks; Foot rest exquisiteness is small and exquisite simultaneously, can represent compacter folding effect after folding.
As shown in Figure 10, left foot frame 12 is little, and right crus of diaphragm frame 13 is large, and time folding, left foot frame 12 passes inside right crus of diaphragm frame 13; Latter two foot rest folding in same level, and then ensures the minimum size of folding rear complete machine.
These are only better embodiment of the present utility model, not in order to limit the utility model, all do in this in spirit of the present utility model and principle any amendment, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (7)
1. Portable unmanned machine, comprises fuselage, a 2-8 S. A., a 2-8 horn, 4-16 sheet blade, a 2-8 blade turning unit; It is characterized in that: each horn one end is arranged on fuselage by a horn S. A., and 2-8 horn is symmetrically distributed on fuselage; Each horn other end installs blade turning unit, and every sheet blade tail end is provided with circular hole, and each blade turning unit installs two panels blade.
2. Portable unmanned machine according to claim 1, is characterized in that: also comprise two foot rests, four foot rest bases, each foot rest is fixed on fuselage bottom by two foot rest bases.
3. Portable unmanned machine according to claim 1 and 2, it is characterized in that: described S. A. is made up of fuselage turning unit and horn turning unit, fuselage turning unit is fixed on fuselage, horn turning unit is fixed on horn, and horn turning unit by limitation locking in fuselage turning unit.
4. Portable unmanned machine according to claim 3, is characterized in that: multiple horns of fuselage homonymy are upper and lower state straggly.
5. Portable unmanned machine according to claim 1 and 2, is characterized in that: described blade turning unit comprises motor, press strip, Fast detachable unit; Motor is arranged on the horn other end, each motor is installed two panels blade, and blade is arranged on the blade spindle that on motor, two ends are outstanding, and two panels blade is pushed down through the threaded column of motor center by press strip, and the threaded column of Fast detachable unit and motor center screws and locked by press strip.
6. Portable unmanned machine according to claim 1 and 2, is characterized in that: two described foot rests are small one and large one, and little foot rest passes inside large foot rest; Latter two foot rest folding is in same level, and the inwall of each foot rest base is designed to C-type clamp, limits the expansion of foot rest or folding angle by foot rest base.
7. Portable unmanned machine according to claim 1 and 2, is characterized in that: described S. A. is 4, horn is 4, blade is 8, blade turning unit is 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520492653.6U CN204956909U (en) | 2015-07-09 | 2015-07-09 | Portable unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520492653.6U CN204956909U (en) | 2015-07-09 | 2015-07-09 | Portable unmanned aerial vehicle |
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| CN204956909U true CN204956909U (en) | 2016-01-13 |
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| CN201520492653.6U Active CN204956909U (en) | 2015-07-09 | 2015-07-09 | Portable unmanned aerial vehicle |
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| CN106564582A (en) * | 2016-04-27 | 2017-04-19 | 重庆零度智控智能科技有限公司 | Unmanned aerial vehicle |
| CN106672210A (en) * | 2017-02-21 | 2017-05-17 | 上海未来伙伴机器人有限公司 | Quick disassembly propeller and unmanned aerial vehicle adopting same |
| CN106697256A (en) * | 2016-12-26 | 2017-05-24 | 歌尔科技有限公司 | Unmanned aerial vehicle |
| CN106741839A (en) * | 2016-12-27 | 2017-05-31 | 歌尔科技有限公司 | A kind of unmanned plane |
| CN107097942A (en) * | 2017-05-06 | 2017-08-29 | 安徽省先胜农业发展有限公司 | A kind of light foldable unmanned plane |
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| CN107235139A (en) * | 2017-03-29 | 2017-10-10 | 深圳市科卫泰实业发展有限公司 | Portable many rotor unmanned aircrafts |
| CN108163182A (en) * | 2018-02-24 | 2018-06-15 | 高琴 | A kind of folding deinsectization unmanned plane |
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| WO2018119620A1 (en) * | 2016-12-27 | 2018-07-05 | 深圳市大疆创新科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN108622367A (en) * | 2017-03-22 | 2018-10-09 | 比亚迪股份有限公司 | Unmanned plane horn folding device and unmanned plane |
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| ES2706658A1 (en) * | 2018-07-31 | 2019-03-29 | Casanova Ignacio Recarte | Flying vehicle (Machine-translation by Google Translate, not legally binding) |
| CN110733624A (en) * | 2019-01-23 | 2020-01-31 | 杭州零零科技有限公司 | Unmanned flight system and control system for unmanned flight system |
| US10604248B2 (en) | 2017-05-10 | 2020-03-31 | Coretronic Intelligent Robotics Corporation | Rotating apparatus |
| CN111212782A (en) * | 2018-06-26 | 2020-05-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN111717378A (en) * | 2020-07-08 | 2020-09-29 | 济南职业学院 | Four rotor unmanned aerial vehicle |
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| CN113277064A (en) * | 2021-07-02 | 2021-08-20 | 宁波阿瑞斯自动化技术有限公司 | Many rotor unmanned aerial vehicle of emergency rescue |
| EP3954606A1 (en) * | 2018-11-30 | 2022-02-16 | SZ DJI Technology Co., Ltd. | Foldable unmanned aerial vehicle |
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| WO2018214224A1 (en) * | 2017-05-22 | 2018-11-29 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160523 Address after: 518000 Guangdong city of Shenzhen province Qianhai Shenzhen Hong Kong cooperation zone before Bay Road No. 1 building 201 room A (located in Shenzhen Qianhai business secretary Co. Ltd.) Patentee after: Universal aircraft technology (Shenzhen) Co., Ltd. Address before: 430205, Wuhan 58, Optics Valley Road, East Lake Development Zone, Hubei Province, 1 Fuxing medical park, 10 floor, room 6 Patentee before: Wuhan Gao De unmanned plane Science and Technology Ltd. |
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| CP03 | Change of name, title or address |
Address after: 518066 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee after: Puzhou Technology (Shenzhen) Co.,Ltd. Address before: 518000 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee before: PRODRONE TECHNOLOGY (SHENZHEN) Co.,Ltd. |
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| CP03 | Change of name, title or address |