CN208248495U - A kind of rotor enwraped type unmanned plane - Google Patents
A kind of rotor enwraped type unmanned plane Download PDFInfo
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- CN208248495U CN208248495U CN201721489682.2U CN201721489682U CN208248495U CN 208248495 U CN208248495 U CN 208248495U CN 201721489682 U CN201721489682 U CN 201721489682U CN 208248495 U CN208248495 U CN 208248495U
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- China
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- unmanned plane
- protective cover
- accommodating cavity
- propeller
- rotor
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Abstract
The utility model belongs to unmanned plane field, provide a kind of rotor enwraped type unmanned plane, control unit including body, propeller, power supply, the power unit of driving propeller rotation and control unmanned plane during flying, the power unit, control unit are electrically connected to a power source, and the propeller and power unit are installed on inside body.Being mounted on inside body using propeller makes unmanned plane not encounter barrier because of propeller in flight course and aircraft bombing, substantially avoid the unstability of propeller outside in flight course, shape can be allowed more beautiful, also make unmanned plane safer awing, people will not be accidentally injured.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of rotor enwraped type unmanned plane.
Background technique
Flying saucer unmanned plane protection design is incomplete currently on the market, and volume is big, and weight weight lacks anticollision device, collision-prevention device,
Protective cover venthole is larger in flight course, and barrier, which encounters propeller, in flight course leads to aircraft bombing, is also easy to accidentally injure people.
Utility model content
The purpose of this utility model is to provide a kind of rotor enwraped type unmanned planes, it is intended to solve existing unmanned plane and fly
Barrier encounters the problem of propeller leads to aircraft bombing in the process.
The utility model is realized in this way a kind of rotor enwraped type unmanned plane, including body, propeller, power supply, drive
The power unit of dynamic propeller rotation and the control unit for controlling unmanned plane during flying, the power unit, control unit and electricity
Source electrical connection, the propeller and power unit are installed on inside body.
Wherein, the body includes body rack and body fuselage, and the body rack is distributed in body, the spiral
Paddle is mounted on power unit, and the propeller quantity is 4, and the power unit quantity is 4, the power unit installation
On body rack.
Wherein, the body is equipped with accommodating cavity, and the accommodating cavity is located at body center, the accommodating cavity and body rack
It is connected, described control unit, power supply are installed in accommodating cavity.
Wherein, the arc groove that the accommodating cavity is equipped with, the diameter of the arc groove are less than the diameter on the outside of accommodating cavity.
Wherein, GPS positioning module is equipped in the accommodating cavity, the GPS positioning module is electrically connected with control unit.
Wherein, it is additionally provided with accommodating chamber in the accommodating cavity, the camera shooting of adjustable shooting angle is installed in the accommodating chamber
Head assembly, the CCD camera assembly are mounted in accommodating chamber.
Wherein, the accommodating cavity is equipped with unmanned plane pedestal, and the unmanned plane pedestal is mounted below accommodating cavity, the nothing
Man-machine pedestal is Triangulum.
It wherein, further include upper protective cover and lower protective cover, the upper protective cover and lower protective cover are respectively arranged in outside body
A through-hole is respectively equipped on shell upper and lower, the upper protective cover and lower protective cover, the upper protective cover through-hole and lower protective cover are logical
Hole is adapted with accommodating cavity outer respectively, and the upper protective cover and lower protective cover are adapted with body fuselage respectively.
Wherein, the upper protective cover, lower protective cover are respectively equipped with venthole.
Wherein, the body includes that periphery is equipped with anti-collision ring, and the anti-collision ring is adapted with body fuselage.
After the above technical solution is adopted, propeller is mounted on inside body makes unmanned plane will not be because of in flight course
Propeller encounters barrier and aircraft bombing, substantially avoids the unstability of propeller outside in flight course, can allow shape
It is more beautiful, also make unmanned plane safer awing, people will not be accidentally injured.
Detailed description of the invention
Fig. 1 is a kind of rotor enwraped type unmanned plane perspective view of the explosion of the utility model.
Fig. 2 is protective cover stereoscopic schematic diagram on a kind of rotor enwraped type unmanned plane of the utility model.
Fig. 3 is protective cover stereoscopic schematic diagram under a kind of rotor enwraped type unmanned plane of the utility model.
Fig. 4 is a kind of rotor enwraped type unmanned plane body positive stereoscopic diagram of the utility model.
Fig. 5 is a kind of rotor enwraped type unmanned plane body reverse side stereoscopic schematic diagram of the utility model.
Fig. 6 is a kind of rotor enwraped type unmanned plane body schematic cross-sectional view of the utility model.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only used to explain
The utility model is not used to limit the utility model.
As shown in Fig. 1-6 figure, a kind of rotor enwraped type unmanned plane provided by the embodiment of the utility model, including body 3, spiral shell
Revolve the control of paddle 232, power supply (not shown), the power unit 231 of driving propeller rotation and control unmanned plane during flying
Unit (not shown), the power unit 231, control unit are electrically connected to a power source, the propeller 232 and power unit
231 are installed on 3 the inside of body.
Specifically, the propeller 232 is mounted on power unit 231, and the propeller 232 has 4 propellers
232, the symmetrical front and rear, left and right four direction of the propeller 232, the propeller 232 is in sustained height plane, described
Front and back propeller 232 rotates counterclockwise, and the left-and-right spiral paddle 232 rotates clockwise, 231 quantity of power unit with
Propeller 232 is adapted.
After the above technical solution is adopted, the power unit 231 is electrically connected with control unit, and keeps propeller 232 normal
Rotation and unmanned plane normal flight, are electrically connected to a power source using control unit, provide electric energy, the propeller for unmanned plane during flying
232 and power unit 231 be installed on the inside of body 3, when unmanned plane during flying, propeller 232, power unit 231 are installed in machine
3 the inside of body, substantially avoids the unstability of propeller 232 outside, will not encounter barrier because of propeller in flight course
And aircraft bombing, keep unmanned plane during flying safer.
As shown in Fig. 1-6 figure, the body 3 includes body rack 23 and body fuselage 13, and the body rack 23 is uniformly distributed
In in body 3, the propeller 232 is mounted on power unit 231, and 232 quantity of propeller is 4, the power list
First 231 quantity are 4, and the power unit 231 is mounted on body rack 23.Specifically, the body rack 23 is symmetrical
Distribution front and rear, left and right four direction one end is connected with body fuselage 13, and 23 other end of body rack is connected with accommodating cavity 4
It connects.
After the above technical solution is adopted, propeller 232 is mounted on power unit 231,232 quantity of propeller is
4,231 quantity of power unit of the driving propeller rotation is 4, it is ensured that propeller 232 can normally rotate, and will drive spiral shell
The power unit 231 of rotation paddle rotation is mounted on body rack 23, is made full use of internal body space, is made the volume of unmanned plane more
It is small, so that unmanned plane is seemed more beautiful.
As shown in Fig. 1-6 figure, the body 3 is equipped with accommodating cavity 4, and the accommodating cavity 4 is located at 3 center of body, the appearance
It sets chamber 4 to be connected with body rack 23, described control unit, power supply are installed in accommodating cavity 4.After the above technical solution is adopted,
The accommodating cavity 4 is located at 3 center of body, and the accommodating cavity 4 is connected with body rack 23, keeps body rack 23 symmetrical
In body 3, described control unit, power supply are installed in accommodating cavity 4, make the center of gravity of unmanned plane at center, and center of gravity is under,
It is more steady when making unmanned plane during flying.
As shown in Fig. 1-6 figure, the diameter of the arc groove 54 that the accommodating cavity 4 is equipped with, the arc groove 54 is less than accommodating cavity 4
The diameter in outside.Specifically, the arc groove 54 is 232 rotary wind runner of propeller.After the above technical solution is adopted, holding
It sets chamber 4 and is equipped with the arc groove 54 for reducing diameter, make the weight of unmanned plane, reduce the resistance of flight, the arc groove 54
For 232 rotary wind runner of propeller, making accommodating cavity 4 not influences to also provide the rotation of propeller 232 while propeller 232 rotates
Distinguished and admirable road, it is safer when making unmanned plane during flying, it is not influenced by external air flow.
As shown in Fig. 1-6 figure, GPS positioning module 24, the GPS positioning module 24 and control are equipped in the accommodating cavity 4
Unit electrical connection.After the above technical solution is adopted, the GPS positioning module 24 is electrically connected with control unit, and is GPS positioning module
24 provide electric energy, it is ensured that can work normally, unmanned plane is made to have positioning function, the GPS positioning module 24 is mounted on accommodating cavity 4
It is interior, make the center of gravity of unmanned plane on accommodating cavity 4, it is more steady for making unmanned plane during flying.
As shown in Fig. 1-6 figure, it is additionally provided with accommodating chamber 44 in the accommodating cavity 4, is equipped in the accommodating chamber 44 adjustable
The CCD camera assembly 14 of shooting angle, the CCD camera assembly 14 are mounted in accommodating chamber 44.Specifically, institute
Accommodating chamber 44 is stated to be provided with below accommodating cavity.After the above technical solution is adopted, adjustable shooting is installed in the accommodating chamber 44
The CCD camera assembly 14 of angle makes unmanned plane that can carry out each orientation shooting to affairs by adjusting angle in flight, makes user
More preferably, the CCD camera assembly 14 is mounted in accommodating chamber 44 experience effect, and the accommodating chamber 44 is provided with appearance
It sets below chamber, it is easy to disassemble, make the center of gravity of unmanned plane under, when flight is more steady.
As shown in Fig. 1-6 figure, the accommodating cavity 4 is equipped with unmanned plane pedestal 34, and the unmanned plane pedestal 34 is mounted on appearance
4 lower section of chamber is set, the unmanned plane pedestal 34 is Triangulum.After the above technical solution is adopted, it is mounted on using unmanned plane pedestal 34
4 lower section of accommodating cavity prevents unmanned plane from encountering barrier in landing and makes a mess of the detachable camera group being mounted on accommodating chamber 44
Part 14 makes unmanned plane reduce landing impulse force in landing, safer when so that unmanned plane is landed using Triangulum, steady.
It further include upper protective cover 1 and lower protective cover 2 as shown in Fig. 1-6 figure, the upper protective cover 1 and lower protective cover 2 are distinguished
It is installed on 13 upper and lower of body fuselage, a through-hole, the upper protective cover are respectively equipped on the upper protective cover 1 and lower protective cover 2
Through-hole 11 and lower protective cover through-hole 21 are adapted with 4 outer of accommodating cavity respectively, the upper protective cover 1 and lower protective cover 2 respectively with
Body fuselage 13 is adapted.Specifically, the upper protective cover 1 and lower protective cover 2 are all made of plastic material, the lower protective cover
2 are equipped with clamp 32, and the clamp 32 is connected with body fuselage 13.
After the above technical solution is adopted, the upper protective cover 1 and lower protective cover 2 are respectively arranged in about 13 body fuselage
Side, makes unmanned plane seem more beautiful, a through-hole, the upper protection is respectively equipped on the upper protective cover 1 and lower protective cover 2
Cover through-hole 11 and lower protective cover through-hole 21 are adapted with 4 outer of accommodating cavity respectively, and when use need to only pass through upper protective cover through-hole 11
Upper protective cover 1, lower protective cover 2 can be mounted on body 3 with lower protective cover through-hole 21, the upper protective cover 1, lower protective cover
2 are adapted with body fuselage 13 respectively, also make unmanned plane weight lighter, reduce the resistance of flight, set on the lower protective cover 2
There is clamp 32, the clamp 32 is connected with body 3, avoids lower 2 center of gravity of protective cover not easily to fall off awing downwards, avoids spiral shell
It revolves paddle 232 and encounters barrier aircraft bombing in rotation, make in-flight safer.
As shown in Fig. 1-6 figure, the upper protective cover, lower protective cover are respectively equipped with venthole.Specifically, the upper protection
Cover venthole 11 and lower protective cover venthole 22 are irregular shape, the upper protective cover venthole 11 and lower protective cover venthole
22 shapes are adapted.After the above technical solution is adopted, the upper protective cover venthole 21 prevents from using with lower protective cover venthole 22
Finger is put into when in use at family, is avoided propeller 232 and is encountered barrier in flight and aircraft bombing, when unmanned plane during flying, institute
It states protective cover venthole 11 and lower protective cover venthole 22 can ensure that air smooth flow, keep unmanned plane during flying more stable.
As shown in Fig. 1-6 figure, the body 3 includes that periphery is equipped with anti-collision ring 131, the anti-collision ring 131 and body fuselage
13 are adapted.After the above technical solution is adopted, enable unmanned plane encounter barrier in flight course to flick, protection unmanned plane flies
Row, avoids unmanned plane and awing collides aircraft bombing, and in the present embodiment, the anti-collision ring 131 uses foam, both mitigates
The weight of itself, can also achieve the effect that anticollision.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Made any modifications, equivalent replacements, and improvements etc., should be included in the utility model within the spirit and principle of utility model
Protection scope within.
Claims (7)
1. a kind of rotor enwraped type unmanned plane, it is characterised in that: rotated including body, propeller, power supply, driving propeller dynamic
Power unit and the control unit for controlling unmanned plane during flying, the power unit, control unit are electrically connected to a power source, the spiral
Paddle and power unit are installed on inside body；The body includes body rack and body fuselage, and the body rack is distributed in
In body, the propeller is mounted on power unit, and the propeller quantity is 4, and the power unit quantity is 4,
The power unit is mounted on body rack；The body is equipped with accommodating cavity, and the accommodating cavity is located at body center, described
Accommodating cavity is connected with body rack, and described control unit, power supply are installed in accommodating cavity；The arc that the accommodating cavity is equipped with
Slot, the diameter of the arc groove are less than the diameter on the outside of accommodating cavity.
2. a kind of rotor enwraped type unmanned plane as described in claim 1, it is characterised in that: fixed equipped with GPS in the accommodating cavity
Position module, the GPS positioning module are electrically connected with control unit.
3. a kind of rotor enwraped type unmanned plane as claimed in claim 2, it is characterised in that: be additionally provided with receiving in the accommodating cavity
Chamber, the CCD camera assembly of adjustable shooting angle is equipped in the accommodating chamber, and the CCD camera assembly is mounted at
In accommodating chamber.
4. a kind of rotor enwraped type unmanned plane as claimed in claim 3, it is characterised in that: the accommodating cavity is equipped with unmanned plane
Pedestal, the unmanned plane pedestal are mounted below accommodating cavity, and the unmanned plane pedestal is Triangulum.
5. a kind of rotor enwraped type unmanned plane as claimed in claim 4, it is characterised in that: further include upper protective cover and lower protection
Cover, the upper protective cover and lower protective cover are respectively arranged in body fuselage upper and lower, divide on the upper protective cover and lower protective cover
Not She You a through-hole, the upper protective cover through-hole and lower protective cover through-hole be adapted with accommodating cavity outer respectively, the upper protection
Cover and lower protective cover are adapted with body fuselage respectively.
6. a kind of rotor enwraped type unmanned plane as claimed in claim 5, it is characterised in that: the upper protective cover, lower protective cover
It is respectively equipped with venthole.
7. a kind of rotor enwraped type unmanned plane as described in claim 1, it is characterised in that: the body includes periphery equipped with anti-
Circle is hit, the anti-collision ring is adapted with body fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721489682.2U CN208248495U (en) | 2017-11-09 | 2017-11-09 | A kind of rotor enwraped type unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721489682.2U CN208248495U (en) | 2017-11-09 | 2017-11-09 | A kind of rotor enwraped type unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208248495U true CN208248495U (en) | 2018-12-18 |
Family
ID=64619520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721489682.2U Active CN208248495U (en) | 2017-11-09 | 2017-11-09 | A kind of rotor enwraped type unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208248495U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115158681A (en) * | 2022-08-30 | 2022-10-11 | 南京开天眼无人机科技有限公司 | Protective mesh enclosure for flight rotor wing, application and forming process thereof |
-
2017
- 2017-11-09 CN CN201721489682.2U patent/CN208248495U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115158681A (en) * | 2022-08-30 | 2022-10-11 | 南京开天眼无人机科技有限公司 | Protective mesh enclosure for flight rotor wing, application and forming process thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190411 Address after: 514400 Industrial Park of Shuizhai Town, Wuhua County, Meizhou City, Guangdong Province Patentee after: Guangdong brightness fine horse science and technology Group Co., Ltd Address before: 518100 F7 Building 201, F518 Creative Park, 1065 Baoyuan Road, Xixiang Street, Baoan District, Shenzhen City, Guangdong Province Patentee before: Shenzhen territory intelligent Polytron Technologies Inc |