CN204297077U - A kind of six rotor wing unmanned aerial vehicles - Google Patents
A kind of six rotor wing unmanned aerial vehicles Download PDFInfo
- Publication number
- CN204297077U CN204297077U CN201420657241.9U CN201420657241U CN204297077U CN 204297077 U CN204297077 U CN 204297077U CN 201420657241 U CN201420657241 U CN 201420657241U CN 204297077 U CN204297077 U CN 204297077U
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- CN
- China
- Prior art keywords
- wing unmanned
- unmanned aerial
- rotor wing
- arm support
- control unit
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Abstract
The utility model discloses a kind of six rotor wing unmanned aerial vehicles, comprise six screw propellers, rigidity arm support and master control unit, described six screw propellers connect firmly in rigidity arm support mechanism by six independently motor drivings, described master control unit organization establishes is in the positive lower end of rigidity arm support, described six rotor wing unmanned aerial vehicles can realize the hovering that accuracy rating is 1 meter aloft, can the long-time object observing of actv. dynamic, and manipulation flexibly, this battery module is 10000mAh, can to fly 10km in the flying power be thirty minutes long, maximum speed is 10m/s, the pardon of flying height is 0-1000m, can adaptive temperature scope it be-10 °-45 °, its take-off weight 3kg, payload capacity is 1kg, the place that the equipment such as video camera observe the mankind not easily observe in detail can be carried.
Description
Technical field
The utility model relates to airmanship field, is specially a kind of six rotor wing unmanned aerial vehicles.
Background technology
Society's fast speed development, mechanization is more and more common, the peasant in rural area is also more and more tending towards mechanization production with planting, improve efficiency, so there is farmland centralized management and plantation, centralization improves plantation efficiency, the growing state of observation crops has just used unmanned plane observation, arboreal growth situation in mountain has also used unmanned plane observation, traditional fixed-wing unmanned plane freedom of motion is not enough, be difficult to anxious stopping, independently cannot stop row aloft, and there is the restriction of flying height, be difficult to reach monitoring crops, orchard, the actual conditions of mountain forest trees, more clear in order to obtain, crops accurately, tree information, we propose a kind of six rotor wing unmanned aerial vehicles.
Utility model content
The purpose of this utility model is to provide a kind of six rotor wing unmanned aerial vehicles, this six rotor wing unmanned aerial vehicle can vertical takeoff and landing, using six screw propellers as engine installation, powerful power is provided, has four screw propellers can control to fold, make its narrowed width of flying, be more conducive to flight, and the flight of six-freedom degree can be realized, be convenient to flexible control, propose to obtain the information such as crops, trees more accurately to solve in above-mentioned background technology.
For achieving the above object, the utility model provides following technical scheme: electrical motor 2 is connected with rigid support 3, screw propeller 1, body 4 is connected with rigid support 3, hinge 5, strut bar 6 is connected with hinge 5, foot rest 7, fix screw propeller 8, fixing screw propeller 9, be fixed on to ensure the stable fixed performance of fixing screw propeller on hinge 5, rotatable screw propeller 10, rotatable screw propeller 11, rotatable screw propeller 12, rotatable screw propeller 13 all can rotate.A kind of six rotor wing unmanned aerial vehicles, comprise six screw propellers, rigidity arm support and master control unit, described six screw propellers connect firmly by six independently motor drivings in rigidity arm support mechanism, and described master control unit organization establishes is in the positive lower end of rigidity arm support.
Preferably, described six screw propellers are M shape distribution.
Preferably, pipeline is established in described rigidity arm support.
Preferably, described master control unit comprises attitude sensor module, motor drive module, main control module, Radio control module and power module.
Preferably, described six screw propellers can realize the flight of aerial six-freedom degree.
Preferably, having four screw propellers can complete with body in described six screw propellers is horizontally rotating of the center of circle.
Compared with prior art, the beneficial effects of the utility model are: this six rotor wing unmanned aerial vehicle six screw propellers are little, there is flight safety, power is powerful, control the features such as flexible, there are four screw propellers can control to fold, make its narrowed width of flying, be more conducive to flight, and the flight of six-freedom degree can be realized, master control unit comprises the position situation that attitude measurement system, motor drive module, main control module, wireless communication module and power module energy actv. detect six rotor wing unmanned aerial vehicles, realizes long-distance flight, distance control.
Fig. 1 is the utility model six wing unmanned plane structural representation:
Fig. 2 has four rotatable schematic diagrams of screw propeller in six screw propellers:
Fig. 3 is for being the utility model master control unit schematic diagram:
In figure: screw propeller 1, electrical motor 2, rigid support 3, body 4, hinge 5, strut bar 6 foot rest 7, fixing screw propeller 8, fixing screw propeller 9, rotatable screw propeller 10, rotatable screw propeller 11, rotatable screw propeller 12, rotatable screw propeller 13.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Described in composition graphs 1, the utility model provides a kind of technical scheme: a kind of six rotor wing unmanned aerial vehicles, at least comprise four rotatable screw propellers, rigidity arm support and master control unit, in described six screw propellers, two screw propellers be connected with foot lever connect firmly on fuselage, to ensure the stationarity of fuselage.By six independently motor drivings in rigidity arm support mechanism, described master control unit organization establishes is in the positive lower end of rigidity arm support.
Described six wing unmanned plane versions as shown in Figure 2, the screw propeller intersected in rigidity by six forms, fixing screw propeller 8 and fixing screw propeller 9 are fixed on fuselage to keep the stationarity of fuselage, rotating screw 10, rotating screw 11, rotating screw 12 and rotating screw 13 can rotate around fuselage, and rotating screw 10, rotating screw 11, rotating screw 12, rotating screw 13 all move to self adjacent fixing screw propeller, maximum angle rotates to parallel with fixing screw propeller.
Six wing unmanned plane during flyings are more steady, six electrical motors can start flight simultaneously, rotating screw 10 rotating screw 11 rotating screw 12 rotating screw 13 rotates, the width of fuselage can be changed by rotating screw, fuselage is narrowed change of flight width, can more easily by narrower place, rotor blade rotates the mass distribution density that can change six wing unmanned planes, and then can change the heading of six wing unmanned planes.
Due to six wing unmanned plane symmetrical configuration, tendency motion and the just direction that seesaws different, by change rotating screw come controlling party to.Described six rotor wing unmanned aerial vehicles can realize the hovering that accuracy rating is 1 meter aloft, can the long-time object observing of actv. dynamic, and manipulation flexibly, this battery module is 10000mAh, can to fly 10km in the flying power be thirty minutes long, maximum speed is 10m/s, the pardon of flying height is 0-1000m, can adaptive temperature scope be-10 °-45 °, its take-off weight 3kg, payload capacity is 1kg, can carry the place that the equipment such as video camera observe the mankind not easily observe in detail.
The above; be only the utility model preferably detailed description of the invention; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; be equal to according to the technical solution of the utility model and utility model design thereof and replace or change, all should be encompassed within protection domain of the present utility model.
Claims (1)
1. six rotor wing unmanned aerial vehicles, is characterized in that: comprise six screw propellers, rigidity arm support and master control unit; Described six screw propellers connect firmly in rigidity arm support mechanism by six independently motor drivings; Described master control unit organization establishes is in the body of six wing unmanned planes; Four rotating screws are had to complete horizontally rotating around body in six screw propellers; Described master control unit comprises attitude measurement system, motor drive module, main control module, wireless communication module and power module; Described wireless communication module can this six rotor wing unmanned aerial vehicle of Long-distance Control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420657241.9U CN204297077U (en) | 2014-11-05 | 2014-11-05 | A kind of six rotor wing unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420657241.9U CN204297077U (en) | 2014-11-05 | 2014-11-05 | A kind of six rotor wing unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204297077U true CN204297077U (en) | 2015-04-29 |
Family
ID=53102640
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420657241.9U Expired - Fee Related CN204297077U (en) | 2014-11-05 | 2014-11-05 | A kind of six rotor wing unmanned aerial vehicles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204297077U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104925251A (en) * | 2015-07-04 | 2015-09-23 | 苏州科锐恒机械科技有限公司 | Low-altitude flight device |
| CN106275446A (en) * | 2015-06-01 | 2017-01-04 | 深圳市大疆创新科技有限公司 | Fixed structure and apply the flight equipment of this fixed structure |
| CN106794897A (en) * | 2016-05-18 | 2017-05-31 | 深圳市创客工场科技有限公司 | A kind of multi-rotor unmanned aerial vehicle |
-
2014
- 2014-11-05 CN CN201420657241.9U patent/CN204297077U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275446A (en) * | 2015-06-01 | 2017-01-04 | 深圳市大疆创新科技有限公司 | Fixed structure and apply the flight equipment of this fixed structure |
| CN106275446B (en) * | 2015-06-01 | 2020-05-05 | 深圳市大疆创新科技有限公司 | Fixed knot constructs and uses this fixed knot to construct flight equipment |
| CN104925251A (en) * | 2015-07-04 | 2015-09-23 | 苏州科锐恒机械科技有限公司 | Low-altitude flight device |
| CN106794897A (en) * | 2016-05-18 | 2017-05-31 | 深圳市创客工场科技有限公司 | A kind of multi-rotor unmanned aerial vehicle |
| CN106794897B (en) * | 2016-05-18 | 2019-12-13 | 深圳市创客工场科技有限公司 | Multi-rotor unmanned aerial vehicle |
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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: 20150429 Termination date: 20151105 |
|
| EXPY | Termination of patent right or utility model |