CN204776010U - Many rotors unmanned vehicles - Google Patents
Many rotors unmanned vehicles Download PDFInfo
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- CN204776010U CN204776010U CN201520376929.4U CN201520376929U CN204776010U CN 204776010 U CN204776010 U CN 204776010U CN 201520376929 U CN201520376929 U CN 201520376929U CN 204776010 U CN204776010 U CN 204776010U
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- cantilever
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Abstract
The utility model relates to a many rotors unmanned vehicles, including the frame, fly to control board, brushless motor, rotor and landing chassis, the frame with fly to control the board for the center is central symmetrical structure, the frame includes that therefrom just a plurality of cantilevers of evenly distributed of type extension are dispersed all around to the mind -set, the end of every cantilever all is equipped with a brushless motor, the brushless motor top is connected with the rotor, the frame still includes buffer stop, buffer stop is circular and links to each other with every cantilever is terminal respectively, it is equipped with host computer and battery to fly to control the board top, it still is equipped with a protection casing to fly to control the board top, it is equipped with the landing chassis to fly to control the board below, the landing chassis includes four pillars and a foot rest, four pillar tops all with the board rigid coupling flies to control, the bottom all with the foot rest rigid coupling, it still is equipped with linkage to fly to control the board below, last the hanging of linkage is equipped with the medical kit, linkage bonds with the medical kit, the utility model discloses a many rotors unmanned vehicles has anticollision and rain -proof function.
Description
Technical field
The utility model relates to a kind of unmanned vehicle, particularly relates to a kind of many rotor unmanned aircrafts, belongs to unmanned air vehicle technique field.
Background technology
Unmanned vehicle as the term suggests i.e. unpiloted aircraft, wherein many rotor unmanned aircrafts with its maneuverability, reaction fast, the advantage such as unmanned flight, operation requirements be low and being widely used.Such as, unmanned plane loads as camera, image real-time Transmission, high-risk areas detecting function can be realized, be widely used in the fields such as fire-fighting, military affairs, traffic, police service, exploration and meteorology, to realize cruise shooting to designated area and supervision; Unmanned plane loads medicine-chest, can realize spraying insecticide at a distance, on a large scale, be widely used in the field such as agricultural, forestry.At present, unmanned vehicle is carry out manufacturing and designing based on the flight theory of helicopter mostly, can realize vertical lift and high-altitude hovering, thus meet the requirement of taking photo by plane and monitoring.
But current many rotor unmanned aircrafts do not assemble protective equipment substantially, if misoperation or easily hit the accidents such as wall and damage rotor when having strong wind; And the equipment such as main motor do not possess rainproof function, in case of rainy day easily drenches destruction circuit.
Utility model content
The technical problems to be solved in the utility model is: propose a kind of crashproof and rainproof many rotor unmanned aircrafts.
The utility model is the technical scheme solving the problems of the technologies described above proposition: a kind of many rotor unmanned aircrafts, comprise frame, fly to control plate, brushless motor, rotor and landing pad, it is characterized in that: described frame flies to be centrosymmetric centered by control plate structure by described, described frame comprises from center to the extension of surrounding divergence form and the multiple cantilever of well-distributed, the end of each cantilever is equipped with a brushless motor, rotor is connected with above described brushless motor, described frame also comprises anticollision device, described anticollision device is circular and is connected with each cantilevered distal end respectively, described flying is provided with main frame and battery above control plate, described flying also is provided with a protective cover above control plate, described flying is provided with landing pad below control plate, described landing pad comprises four pillars and a foot rest, four described pillar tops are all with to fly to control plate affixed, bottom is all affixed with foot rest, described flying also is provided with suspension gear below control plate, described suspension gear is linked with medicine-chest, described suspension gear is bonding with medicine-chest.
Being improved to technique scheme: be equipped with strut bar between described foot rest and each cantilever, described strut bar one end is fixedly connected with cantilever, and the other end is fixedly connected with foot rest.
Being improved to technique scheme: described protective cover is semisphere.
Being improved to technique scheme: described cantilever is four and distributes in " ten " font to fly to control centered by plate.
Being improved to technique scheme: described cantilever is six.
Being improved to technique scheme: described cantilever is eight.
Being improved to technique scheme: the inclination angle of described rotor and described frame place plane is 3 to 8 °.
Being improved to technique scheme: described anticollision device detouchable is fixed on cantilever.
The beneficial effects of the utility model are:
1, frame is provided with circular anticollision device, making unmanned vehicle bump against wall in time when flying, also can not cause the damage of rotor, make unmanned plane still can normal flight when trees or other objects.
2, fly also to be provided with protective cover above control plate, make to fly to control the equipment such as main frame on plate and battery and be protected, effectively prevent from being soaked with rain.
3, suspension gear and medicine-chest adopt simple bonding way to be connected, and make to change medicine-chest more convenient, are convenient to handling.
4, be equipped with strut bar between foot rest and each cantilever, a part of load of cantilever shared on foot rest, thus alleviates the load of cantilever, but also add the rigidity of whole fuselage.
5, the inclination angle of rotor and frame place plane is 3 to 8 °, enhances the wind resistance of unmanned vehicle.
Accompanying drawing explanation
Be described further of the present utility model below in conjunction with accompanying drawing.
Fig. 1 is the perspective view of the utility model embodiment one.
Detailed description of the invention
Embodiment one
Many rotor unmanned aircrafts of the present embodiment comprise frame 1 as shown in Figure 1, fly to control plate 2, brushless motor 3, rotor 4 and landing pad 5, frame 1 comprises from center to the extension of surrounding divergence form and is " ten " font well-distributed four cantilevers 11, each cantilever 11 is equipped with a brushless motor 3, one group of rotor 4 is connected with above brushless motor, frame 1 also comprises circular anticollision device 12, anticollision device 12 is connected with each cantilever 11 end and detachable respectively, fly to be provided with main frame 21 above control plate 2, fly also to be provided with a semisphere protective cover 7 above control plate 2, fly also to be provided with suspension gear 8 below control plate 2, suspension gear 8 is linked with medicine-chest 9, suspension gear 8 is bonding with medicine-chest 9.
Landing pad 5 is positioned at and flies below control plate 2, landing pad 5 comprises four pillars 51 and a foot rest 52, four pillar 51 tops are all with to fly to control plate 2 affixed, bottom is all affixed with foot rest 52, strut bar 6 is equipped with between foot rest 52 and each cantilever 11, strut bar 6 one end is fixedly connected with cantilever 11, and the other end is fixedly connected with foot rest 52.
In the present embodiment, rotor 4 is 3 ° with the inclination angle of frame 1 place plane.
Embodiment two
Other structure of many rotor unmanned aircrafts of the present embodiment is identical with embodiment one, and difference is that in the present embodiment, rotor 4 has six and is uniformly distributed, and rotor 4 is 8 ° with the inclination angle of frame 1 place plane.
Embodiment three
Other structure of many rotor unmanned aircrafts of the present embodiment is identical with embodiment one, and difference is that in the present embodiment, rotor 4 has eight and is uniformly distributed, and rotor 4 is 5 ° with the inclination angle of frame 1 place plane.
Many rotor unmanned aircrafts of the present utility model are not limited to the various embodiments described above, and all employings are equal to the technical scheme of replacing and being formed, and all drop on the protection domain of the utility model requirement.
Claims (8)
1. rotor unmanned aircraft more than a kind, comprise frame, fly to control plate, brushless motor, rotor and landing pad, it is characterized in that: described frame flies to be centrosymmetric centered by control plate structure by described, described frame comprises from center to the extension of surrounding divergence form and the multiple cantilever of well-distributed, the end of each cantilever is equipped with a brushless motor, rotor is connected with above described brushless motor, described frame also comprises anticollision device, described anticollision device is circular and is connected with each cantilevered distal end respectively, described flying is provided with main frame and battery above control plate, described flying also is provided with a protective cover above control plate, described flying is provided with landing pad below control plate, described landing pad comprises four pillars and a foot rest, four described pillar tops are all with to fly to control plate affixed, bottom is all affixed with foot rest, described flying also is provided with suspension gear below control plate, described suspension gear is linked with medicine-chest, described suspension gear is bonding with medicine-chest.
2. many rotor unmanned aircrafts according to claim 1, it is characterized in that: be equipped with strut bar between described foot rest and each cantilever, described strut bar one end is fixedly connected with cantilever, and the other end is fixedly connected with foot rest.
3. many rotor unmanned aircrafts according to claim 1, is characterized in that: described protective cover is semisphere.
4. many rotor unmanned aircrafts according to claim 1, is characterized in that: described cantilever is four and to fly the distribution in " ten " font centered by control plate.
5. many rotor unmanned aircrafts according to claim 1, is characterized in that: described cantilever is six.
6. many rotor unmanned aircrafts according to claim 1, is characterized in that: described cantilever is eight.
7. many rotor unmanned aircrafts according to claim 1, is characterized in that: the inclination angle of described rotor and described frame place plane is 3 to 8 °.
8. many rotor unmanned aircrafts according to claim 1, is characterized in that: described anticollision device detouchable is fixed on cantilever.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520376929.4U CN204776010U (en) | 2015-06-03 | 2015-06-03 | Many rotors unmanned vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520376929.4U CN204776010U (en) | 2015-06-03 | 2015-06-03 | Many rotors unmanned vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204776010U true CN204776010U (en) | 2015-11-18 |
Family
ID=54516112
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520376929.4U Expired - Fee Related CN204776010U (en) | 2015-06-03 | 2015-06-03 | Many rotors unmanned vehicles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204776010U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105836147A (en) * | 2016-03-21 | 2016-08-10 | 飞智控（天津）科技有限公司 | Rotor wing unmanned aerial vehicle protection device |
| CN106956768A (en) * | 2017-05-02 | 2017-07-18 | 锐合防务技术（北京）有限公司 | Aircraft |
| CN108058823A (en) * | 2018-01-26 | 2018-05-22 | 湖州职业技术学院 | A kind of unmanned plane rotor protective device |
| CN109927905A (en) * | 2019-04-19 | 2019-06-25 | 代连朋 | A kind of mine drug delivery unmanned plane |
-
2015
- 2015-06-03 CN CN201520376929.4U patent/CN204776010U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105836147A (en) * | 2016-03-21 | 2016-08-10 | 飞智控（天津）科技有限公司 | Rotor wing unmanned aerial vehicle protection device |
| CN106956768A (en) * | 2017-05-02 | 2017-07-18 | 锐合防务技术（北京）有限公司 | Aircraft |
| CN108058823A (en) * | 2018-01-26 | 2018-05-22 | 湖州职业技术学院 | A kind of unmanned plane rotor protective device |
| CN108058823B (en) * | 2018-01-26 | 2024-05-10 | 湖州职业技术学院 | Unmanned aerial vehicle rotor wing protection device |
| CN109927905A (en) * | 2019-04-19 | 2019-06-25 | 代连朋 | A kind of mine drug delivery unmanned plane |
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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: 20151118 Termination date: 20160603 |