CN111874244A - Novel unmanned aerial vehicle paddle safety cover - Google Patents
Novel unmanned aerial vehicle paddle safety cover Download PDFInfo
- Publication number
- CN111874244A CN111874244A CN202010739928.7A CN202010739928A CN111874244A CN 111874244 A CN111874244 A CN 111874244A CN 202010739928 A CN202010739928 A CN 202010739928A CN 111874244 A CN111874244 A CN 111874244A
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- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- main body
- spokes
- annular main
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
Abstract
The invention provides a novel unmanned aerial vehicle blade protective cover which comprises an annular main body, an installation support and a bottom net, wherein the installation support is arranged on the annular main body; the mounting support comprises spokes and a motor connecting piece; the number of the spokes is odd, and the spokes are uniformly distributed on the surface of the motor connecting piece by taking the motor connecting piece as the center; the annular main body is arranged on a circle formed by the outer ends of the spokes in a matching way; the bottom layer net is arranged on the lower end face of the annular main body and filled between every two adjacent spokes. Compared with the prior art, the unmanned aerial vehicle with the large blades solves the contradiction between the requirement of reliable safety protection of the unmanned aerial vehicle with the large blades and the limited power redundancy of the unmanned aerial vehicle, and ensures that the blades of the unmanned aerial vehicle can be prevented from being interfered by objects from the lower part and the horizontal direction in the flying process under the condition of not causing overlarge flying resistance of the unmanned aerial vehicle as much as possible.
Description
Technical Field
The invention belongs to the field of mechanical design of unmanned aerial vehicles, and particularly relates to a novel unmanned aerial vehicle paddle protective cover.
Background
Nowadays, unmanned aerial vehicle is more extensive in the application in each field, and in order to realize some more complicated tasks, unmanned aerial vehicle has to develop towards bigger volume, and the bulky means bigger quality, and in order to realize bigger load, unmanned aerial vehicle's paddle also need constantly to be increaseed, and the motor needs higher rotational speed, and this has also brought very big potential safety hazard, and unmanned aerial vehicle injures people's incident and frequently takes place.
Therefore, it is an urgent problem to those skilled in the art to develop a structure capable of reliably protecting the blades of the unmanned aerial vehicle.
Disclosure of Invention
In order to solve the problems, the invention discloses a novel unmanned aerial vehicle blade protective cover.
In order to achieve the purpose, the invention provides the following technical scheme:
a novel unmanned aerial vehicle blade protection cover comprises an annular main body, an installation support and a bottom net; the mounting support comprises spokes and a motor connecting piece; the number of the spokes is odd, and the spokes are uniformly distributed on the surface of the motor connecting piece by taking the motor connecting piece as the center; the annular main body is arranged on a circle formed by the outer ends of the spokes in a matching way; the bottom layer net is arranged on the lower end face of the annular main body and filled between every two adjacent spokes.
Further, the number of spokes is 5.
Further, a circle of protrusions are arranged on the outer side of the annular main body along the circumferential direction; the protrusion is a protrusion with a wide outer part and a narrow inner part.
Further, the annular main body comprises an upper layer main body and a lower layer main body which are distributed up and down; the upper layer main body and the lower layer main body are both annular and are fixed through nylon columns.
Further, the annular main body and the spokes are made of light and deformation-resistant materials; the bottom layer web is made of a material that is fine and has high tensile strength.
Further, the annular body and the spokes are made of carbon plate.
The novel unmanned aerial vehicle blade protective cover provided by the invention has the following characteristics:
1. the annular main body adopts a double-layer design, and is not easy to deform when being collided compared with the existing layer;
2. the mounting support is connected with the peripheral annular main body by 5 spokes to seal the protective cover, so that the spokes are mainly pulled when the unmanned aerial vehicle horizontally flies and collides with an obstacle, and possible instability of the protective cover under the condition of pressure is solved; meanwhile, the odd spokes avoid the resonance of the unmanned aerial vehicle under the influence of the airflow of the blades;
3. the sectional area of the spokes in the horizontal direction is smaller than that of 3 spokes due to the selection of 5 spokes and larger than that of 7 spokes, so that the unmanned aerial vehicle has excellent aerodynamic performance and is not easy to cause great damage to other objects when the unmanned aerial vehicle crashes, and the 5 spokes enable the bottom net woven on the spokes to be uniformly distributed so that the bottom net can provide protection at the edge of the protective cover compared with 3 spokes, turbulence generated by the 7 spokes near the spokes is smaller, the bottom net can timely limit the rotation of the blades when the blades fall down abnormally, and the damage to ground personnel and property is reduced;
4. the motor connecting piece has the function of connecting spoke, connecting unmanned aerial vehicle horn pipe clamp concurrently for unmanned aerial vehicle's the maintenance of being convenient for rationally assembled, and processing is simple.
Therefore, compared with the prior art, the unmanned aerial vehicle with the large blades solves the contradiction between the requirement of reliable safety protection of the unmanned aerial vehicle with the large blades and the limited power redundancy of the unmanned aerial vehicle, and ensures that the blades of the unmanned aerial vehicle can be prevented from being interfered by objects from the lower part and the horizontal direction in the flying process under the condition of not causing overlarge flying resistance of the unmanned aerial vehicle as much as possible.
Drawings
FIG. 1 is a schematic structural view of the present invention;
list of reference numerals: the device comprises an annular main body 1, an upper layer main body 11, a lower layer main body 12, a nylon column 13, a mounting support 2, spokes 21, a motor connecting piece 22, a bottom layer net 3, a propeller assembly 4 and a pipe clamp 5.
Detailed Description
The technical solutions provided by the present invention will be described in detail below with reference to specific examples, and it should be understood that the following specific embodiments are only illustrative of the present invention and are not intended to limit the scope of the present invention.
As shown in fig. 1, the invention is a structural schematic diagram of the novel unmanned aerial vehicle blade protective cover, and the novel unmanned aerial vehicle blade protective cover comprises an annular main body 1, a mounting support 2 and a bottom net 3.
The mounting support 2 is used for supporting a motor and propeller assembly 4 and a pipe clamp 5 which are arranged on a machine arm, and comprises spokes 21 and a motor connecting piece 22; the number of the spokes 21 is 5, and the spokes are uniformly distributed on the surface of the motor connecting piece 22 by taking the motor connecting piece 22 as a center.
The annular main body 1 is arranged on a circle formed by the outer ends of the spokes 21 in a matching way, and a circle of protrusions are arranged on the outer side of the annular main body 1 along the circumferential direction; the protrusion is a protrusion with a wide outer part and a narrow inner part; the annular main body 1 comprises an upper layer main body 11 and a lower layer main body 12 which are distributed up and down; the upper layer main body 11 and the lower layer main body 12 are both annular and are fixed by nylon columns 13.
The bottom layer net 3 is arranged on the lower end face of the annular main body 1 and is filled between every two adjacent spokes 21.
The above annular body 1 and the spokes 21 are made of carbon plate.
Finally, it should be noted that the above embodiments are only used for illustrating the technical solutions of the present invention and not for limiting the technical solutions, and those skilled in the art should understand that modifications or equivalent substitutions can be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions, and all the modifications and equivalent substitutions should be covered by the claims of the present invention.
Claims (6)
1. The utility model provides a novel unmanned aerial vehicle paddle safety cover which characterized in that: comprises an annular main body (1), a mounting support (2) and a bottom layer net (3); the mounting support (2) comprises spokes (21) and a motor connecting piece (22); the number of the spokes (21) is odd, and the spokes are uniformly distributed on the surface of the motor connecting piece (22) by taking the motor connecting piece (22) as the center; the annular main body (1) is arranged on a circle formed by the outer ends of the spokes (21) in a matching way; the bottom layer net (3) is arranged on the lower end face of the annular main body (1) and filled between every two adjacent spokes (21).
2. The novel unmanned aerial vehicle paddle safety cover of claim 1, characterized in that: the number of the spokes (21) is 5.
3. The novel unmanned aerial vehicle paddle safety cover of claim 1, characterized in that: a circle of bulges are arranged on the outer side of the annular main body (1) along the circumferential direction; the protrusions are protrusions with wide outer parts and narrow inner parts.
4. The novel unmanned aerial vehicle paddle safety cover of claim 3, characterized in that: the annular main body (1) comprises an upper layer main body (11) and a lower layer main body (12) which are distributed up and down; the upper layer main body (11) and the lower layer main body (12) are both annular and are fixed through nylon columns (13).
5. The novel unmanned aerial vehicle paddle safety cover of claim 1, characterized in that: the annular main body (1) and the spokes (21) are made of light and deformation-resistant materials; the bottom layer net (3) is made of a material which is fine and has high tensile strength.
6. The novel unmanned aerial vehicle paddle safety cover of claim 5, characterized in that: the annular body (1) and the spokes (21) are made of carbon plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010739928.7A CN111874244A (en) | 2020-07-28 | 2020-07-28 | Novel unmanned aerial vehicle paddle safety cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010739928.7A CN111874244A (en) | 2020-07-28 | 2020-07-28 | Novel unmanned aerial vehicle paddle safety cover |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111874244A true CN111874244A (en) | 2020-11-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010739928.7A Pending CN111874244A (en) | 2020-07-28 | 2020-07-28 | Novel unmanned aerial vehicle paddle safety cover |
Country Status (1)
| Country | Link |
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| CN (1) | CN111874244A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105438457A (en) * | 2015-11-30 | 2016-03-30 | 湖北易瓦特科技股份有限公司 | Rotor unmanned aerial vehicle for dual-propeller obstacle avoiding |
| US20160221671A1 (en) * | 2015-01-08 | 2016-08-04 | Vantage Robotics, Llc | Unmanned aerial vehicle with propeller protection and high impact-survivability |
| CN206367591U (en) * | 2016-12-25 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of many rotor mechanisms of unmanned plane |
| CN107108025A (en) * | 2016-12-15 | 2017-08-29 | 深圳市大疆创新科技有限公司 | A kind of propeller protective cover and unmanned plane |
| CN206569265U (en) * | 2017-03-17 | 2017-10-20 | 普宙飞行器科技（深圳）有限公司 | A kind of safe fast-demounting blade protective cover and unmanned plane |
| CN209336995U (en) * | 2018-09-10 | 2019-09-03 | 清远市飞凡创丰科技有限公司 | A kind of collapsible plant protection drone with safeguard function |
-
2020
- 2020-07-28 CN CN202010739928.7A patent/CN111874244A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160221671A1 (en) * | 2015-01-08 | 2016-08-04 | Vantage Robotics, Llc | Unmanned aerial vehicle with propeller protection and high impact-survivability |
| CN105438457A (en) * | 2015-11-30 | 2016-03-30 | 湖北易瓦特科技股份有限公司 | Rotor unmanned aerial vehicle for dual-propeller obstacle avoiding |
| CN107108025A (en) * | 2016-12-15 | 2017-08-29 | 深圳市大疆创新科技有限公司 | A kind of propeller protective cover and unmanned plane |
| CN206367591U (en) * | 2016-12-25 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of many rotor mechanisms of unmanned plane |
| CN206569265U (en) * | 2017-03-17 | 2017-10-20 | 普宙飞行器科技（深圳）有限公司 | A kind of safe fast-demounting blade protective cover and unmanned plane |
| CN209336995U (en) * | 2018-09-10 | 2019-09-03 | 清远市飞凡创丰科技有限公司 | A kind of collapsible plant protection drone with safeguard function |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20201103 |
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| RJ01 | Rejection of invention patent application after publication |