CN208102331U - A kind of multi-rotor unmanned aerial vehicle - Google Patents
A kind of multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN208102331U CN208102331U CN201820649532.1U CN201820649532U CN208102331U CN 208102331 U CN208102331 U CN 208102331U CN 201820649532 U CN201820649532 U CN 201820649532U CN 208102331 U CN208102331 U CN 208102331U
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- blade body
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- aerial vehicle
- unmanned aerial
- unmanned plane
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model discloses a kind of multi-rotor unmanned aerial vehicles, by fixing seat are fixedly connected with rotor wing unmanned aerial vehicle fuselage cradle with flight support frame after improvement integral；Instrument and equipment frame is connected to the upper end of fixing seat, is fixed with solar cell module at the top of instrument and equipment frame, and the position that solar cell module is arranged in the unmanned plane is moderate, not will increase the volume of unmanned plane, inside and outside structure is more reasonable.On the other hand, the inside of blade body connecting pin is formed with blade body connection clamp, and it is hemisphere shape that blade body, which connects clamp, and side is formed with V-arrangement card slot；The end of rotor blade body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot and V-arrangement latch；The end of rotor blade body is connected at clamp and V-arrangement card slot by connection card chamber with the blade body that V-arrangement latch can be directly clamped among inside blade body connecting pin, thus is seemed when docking combination and be quickly easy.
Description
Technical field
The utility model relates to unmanned plane related fieldss, are especially a kind of multi-rotor unmanned aerial vehicle.
Background technique
Currently, the application of unmanned plane is seen everywhere；Some unmanned planes using solar powered, i.e. solar energy unmanned plane refer to
Solar energy is the UAV of power, is converted solar energy into electrical energy and is stored in energy-storage battery by photovoltaic cell, white
It is worked using system each on solar panel maintenance machine and is charged to energy-storage battery on machine；Pass through release energy storage at night
The electric energy stored in battery maintains the operating of entire UAV system.
It is found by retrieval, the utility model of patent No. CN201520729203.4 discloses a kind of solar energy continuation of the journey nothing
It is man-machine, it is provided with solar power generation panel on unmanned plane, can be charged using the battery that solar energy is unmanned plane, effectively extension nothing
Man-machine cruise duration.Solar power generation panel is mounted in holster shell, and is located at the upper end of holster shell.Battery installation
In the inside of holster shell, and it is located at the centre of holster shell.The inner end of bracket is mounted in holster shell, and bracket position
In the centre of holster shell.Electron speed regulator is mounted on the upper end of bracket, and is located at the centre of bracket.Propeller is mounted on nothing
In brush motor, and it is located at the upper end of brushless motor.Brushless motor is rack-mount, and is located at the outer end of bracket.Flight
Control panel is mounted on the inside of holster shell, and is located at the lower end of holster shell.There are four supporting leg settings, is separately fixed at machine
On four angles of rack enclosure bottom end.
The disclosure of the invention of patent No. CN201610969012.4 is a kind of anti-interference to take photo by plane nobody with solar powered
Machine, including mainframe, filming apparatus and solar components mounting platform, this, which has, solar powered anti-interference takes photo by plane nobody
Machine improves the cruising ability of unmanned plane, has simultaneously by way of solar panel absorption solar energy is added and is converted into electric energy
Effect reduces to the replacement to battery, reduces to burden caused by environment, while by solar panel mounting base
Lower section adds the mode of bird-scaring unit, in the high dry running of unmanned plane, can prevent the invasion of birds, avoid causing to endanger to unmanned plane
Evil, and by way of adding luminosity sensor and solar components control device, sunlight is perceived by luminosity sensor
Power regulates and controls the position of solar panel by solar components control device, so that solar panel pair
The use of solar energy more has efficiency.
It is found by retrieval, the utility model of patent No. CN201620833919.3 discloses a kind of multi-rotor unmanned aerial vehicle
Undercarriage and multi-rotor unmanned aerial vehicle；The undercarriage of multi-rotor unmanned aerial vehicle provided by the utility model, including it is respectively arranged at nobody
The mounting plate that multiple undercarriage booms, the fixed device of multiple undercarriages and two parallel intervals of machine fuselage two sides are arranged, main peace
The upper mounting plate shelved is fixedly connected with fuselage, and the fixed device of undercarriage is mounted on the lower surface of the lower installation board of main mounting rack,
It is provided with motor, retarder and driving gear between upper mounting plate and lower installation board, is equipped in the fixed device of undercarriage driven
One end of gear, undercarriage boom is connected with driven gear, and driven gear is meshed with driving gear.
However, existing some unmanned planes can using solar powered, however in existing solar energy unmanned plane for
The position of solar cell module and assembling seem cumbersomeness and inconvenience；In other words it is arranged too in existing solar energy unmanned plane
So that unmanned plane volume increases, structure becomes complicated for meeting after positive energy battery component；It certainly will influence the beauty of unmanned plane；However, nothing
It is man-machine to provide power using propeller, during the tour of unmanned plane, due to be easy to touch building or trees or its
His facility can damage the rotor of unmanned plane when encountering, however existing unmanned plane undercarriage itself lacks anti-contact function；It is existing
The most unmanned plane rotor blades having are overall structure, are not easy to dismantle, and when transport can occupy biggish parking space.
Utility model content
Therefore, in order to solve above-mentioned deficiency, the utility model provides a kind of multi-rotor unmanned aerial vehicle herein, has and changes as follows
Into；Firstly, this patent rotor wing unmanned aerial vehicle fuselage cradle is fixedly connected with flight support frame by fixing seat it is integral；So make
The structure of the unmanned plane is simpler, and being capable of quick assembling；Meanwhile instrument and equipment frame is connected to the upper end of fixing seat, instrument
It is fixed with solar cell module at the top of device equipment frame, the position that solar cell module is arranged in the unmanned plane is moderate,
The volume of unmanned plane is not will increase, inside and outside structure is more reasonable.On the other hand, after the utility model improves, blade
The inside of body connecting pin is formed with blade body connection clamp, and it is hemisphere shape that blade body, which connects clamp, and side is formed with V-arrangement card
Slot；The end of rotor blade body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot and V-arrangement latch；Rotation
The end of wing blade body can be directly clamped among the blade body connection card inside blade body connecting pin by connection card chamber and V-arrangement latch
At head and V-arrangement card slot, thus seems when docking combination and be quickly easy.
The utility model is realized in this way constructing a kind of multi-rotor unmanned aerial vehicle, it is characterised in that：The multi-rotor unmanned aerial vehicle
Including rotor wing unmanned aerial vehicle fuselage cradle, flight support frame, fixed connecting base, instrument and equipment frame, unmanned plane rotor blade component；Its
In, rotor wing unmanned aerial vehicle fuselage cradle is fixedly connected with flight support frame by fixed connecting base integral；The connection of instrument and equipment frame
Solar cell module is installed at the top of the upper end of fixed connecting base, instrument and equipment frame；Unmanned plane rotor blade component packet
Include rotor fixing seat and rotor blade body；Rotor fixing seat has the fixing end connecting with unmanned plane runner assembly and blade
Body connecting pin, fixing end and blade body connecting pin use monolithic molding；
The inside of blade body connecting pin is formed with blade body connection clamp, and it is hemisphere shape, side that blade body, which connects clamp,
Face is formed with V-arrangement card slot；The end of rotor blade body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot
With V-arrangement latch.
This patent has following improve compared with existing same type unmanned plane；Firstly, this patent passes through fixing seat for rotor
Unmanned aerial vehicle body frame is fixedly connected integral with flight support frame；So make the structure of the unmanned plane simpler, Er Qieneng
Enough quick assemblings；Meanwhile instrument and equipment frame is connected to the upper end of fixing seat, is fixed with solar battery at the top of instrument and equipment frame
Component, after assembly as Figure 1-Figure 2, the position that solar cell module is arranged in the unmanned plane are moderate, not will increase nothing
Man-machine volume, inside and outside structure are more reasonable.On the other hand, after the utility model improves, blade body connecting pin
Inside is formed with blade body connection clamp, and it is hemisphere shape that blade body, which connects clamp, and side is formed with V-arrangement card slot；Rotor
The end of leaf body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot and V-arrangement latch；As shown, rotation
The end of wing blade body can be directly clamped among the blade body connection card inside blade body connecting pin by connection card chamber and V-arrangement latch
At head and V-arrangement card slot, thus seems when docking combination and be quickly easy.
As an improvement of the above technical solution, a kind of multi-rotor unmanned aerial vehicle, it is characterised in that：Rotor wing unmanned aerial vehicle fuselage
Frame has two groups of undercarriage booms and two groups of undercarriage connecting rod compositions；The both ends of undercarriage connecting rod form the anticollision contact upwarped
Block, the end of anticollision contact block are provided with induction sensory package.The utility model rotor wing unmanned aerial vehicle fuselage cradle structure is simple, operation
Convenient, low in cost, fastener is few, and adaptability is relatively broad.With preferable wind resistance.On the other hand, undercarriage connecting rod
Both ends form the anticollision contact block upwarped.When unmanned plane is during tour, the both ends of undercarriage connecting rod form the anticollision upwarped
Contact block so that the anticollision contact block upwarped is more outward compared with rotor, during flight cruise even to touch building or
When trees or other facilities, the anticollision contact block upwarped can be touched first, therefore can prevent the rotor of unmanned plane from touching.Together
When, the end of anticollision contact block can be provided with induction sensory package, touch building during flight cruise
When object or trees or other facilities, the anticollision contact block upwarped can be touched first, incuded sensory package at this time and be able to sense of touch, will believe
It number is transmitted to UAV system, control unmanned plane is flown away from, then making unmanned plane have contact collision prevention function by the undercarriage.
As an improvement of the above technical solution, a kind of multi-rotor unmanned aerial vehicle, it is characterised in that：The end of rotor blade body
Sealant is filled between the inner wall of blade body connecting pin on the outside of portion.So when the end of rotor blade body insertion blade body connection
Behind the inside at end, then sealant can make the end of rotor blade body realize sealing, prevent dust from immersing.
The utility model has the following advantages that：The utility model provides a kind of multi-rotor unmanned aerial vehicle by improving herein, such as
Shown in Fig. 1-Fig. 5, have the advantages that as follows improve and；
Advantage 1：The multi-rotor unmanned aerial vehicle includes that rotor wing unmanned aerial vehicle fuselage cradle, flight support frame, fixed connecting base, instrument are set
Standby frame, unmanned plane rotor blade component；Wherein, rotor wing unmanned aerial vehicle fuselage cradle and flight support frame are fixed by fixed connecting base
It connects integral；Instrument and equipment frame is connected to the upper end of fixed connecting base, is equipped with solar battery at the top of instrument and equipment frame
Component；Unmanned plane rotor blade component includes rotor fixing seat and rotor blade body；Rotor fixing seat has and unmanned plane
The fixing end of runner assembly connection and blade body connecting pin, fixing end and blade body connecting pin use monolithic molding；Blade body connects
The inside for connecing end is formed with blade body connection clamp, and it is hemisphere shape that blade body, which connects clamp, and side is formed with V-arrangement card slot；
The end of rotor blade body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot and V-arrangement latch.
This patent has following improve compared with existing same type unmanned plane；Firstly, this patent passes through fixing seat for rotor
Unmanned aerial vehicle body frame is fixedly connected integral with flight support frame；So make the structure of the unmanned plane simpler, Er Qieneng
Enough quick assemblings；Meanwhile instrument and equipment frame is connected to the upper end of fixing seat, is fixed with solar battery at the top of instrument and equipment frame
Component, after assembly as Figure 1-Figure 2, the position that solar cell module is arranged in the unmanned plane are moderate, not will increase nothing
Man-machine volume, inside and outside structure are more reasonable.On the other hand, after the utility model improves, blade body connecting pin
Inside is formed with blade body connection clamp, and it is hemisphere shape that blade body, which connects clamp, and side is formed with V-arrangement card slot；Rotor
The end of leaf body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot and V-arrangement latch；As shown, rotation
The end of wing blade body can be directly clamped among the blade body connection card inside blade body connecting pin by connection card chamber and V-arrangement latch
At head and V-arrangement card slot, thus seems when docking combination and be quickly easy.
Advantage 2：A kind of multi-rotor unmanned aerial vehicle described in the utility model, rotor wing unmanned aerial vehicle fuselage cradle have two groups of undercarriage framves
Arm and two groups of undercarriage connecting rod compositions；The both ends of undercarriage connecting rod form the anticollision contact block upwarped, the end of anticollision contact block
It is provided with induction sensory package.The utility model rotor wing unmanned aerial vehicle fuselage cradle structure is simple, easy to operate, low in cost, fastening
Part is few, and adaptability is relatively broad.With preferable wind resistance.On the other hand, the both ends of undercarriage connecting rod form the anticollision upwarped
Contact block.When unmanned plane is during tour, the both ends of undercarriage connecting rod form the anticollision contact block upwarped, so that is upwarped is anti-
Hit contact block more outward compared with rotor, when during flight cruise even to touch building or trees or other facilities, on
The anticollision contact block stuck up can be touched first, therefore can prevent the rotor of unmanned plane from touching.Meanwhile it can be in anticollision contact block
End is provided with induction sensory package, when during flight cruise even to touch building or trees or other facilities,
The anticollision contact block upwarped can be touched first, incuded sensory package at this time and be able to sense of touch, transmit a signal to UAV system, control
Unmanned plane processed is flown away from, then making unmanned plane have contact collision prevention function by the undercarriage.
Advantage 3：The end outside of a kind of multi-rotor unmanned aerial vehicle described in the utility model, rotor blade body is connect with blade body
Sealant is filled between the inner wall at end（Such as spongy layer）.So when in the insertion blade body connecting pin of the end of rotor blade body
Behind portion, then sealant can make the end of rotor blade body realize sealing, prevent dust from immersing.
Detailed description of the invention
Fig. 1-is the whole implementation schematic diagram of multi-rotor unmanned aerial vehicle described in the utility model；
Fig. 2 is the utility model Instrumental equipment frame separated position implementation diagram；
Fig. 3 is that unmanned plane rotor blade component corresponds to schematic diagram in the utility model；
Fig. 4 is rotor fixing seat and rotor blade body seperated schematic diagram in the utility model；
Fig. 5 is rotor fixing seat and rotor blade body combination diagram in the utility model.
Wherein：Rotor wing unmanned aerial vehicle fuselage cradle 1, flight support frame 2, fixed connecting base 3, instrument and equipment frame 4, unmanned plane rotor
Paddle components 5, solar cell module 6, undercarriage boom 7, two groups of undercarriage connecting rods 8 form, and anticollision contact block 9, induction passes
Feel component 10, rotor fixing seat 11, rotor blade body 12, fixing end 13, blade body connecting pin 14, blade body connection clamp
15, V-arrangement card slot 16, connection card chamber 17, V-arrangement latch 18.
Specific embodiment
The utility model is described in detail below in conjunction with attached drawing 1- Fig. 5, to the skill in the utility model embodiment
Art scheme is clearly and completely described, it is clear that and the described embodiments are only a part of the embodiments of the utility model, and
The embodiment being not all of.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creativeness
Every other embodiment obtained, fall within the protection scope of the utility model under the premise of labour.
The utility model provides a kind of multi-rotor unmanned aerial vehicle by improving herein, as Figure 1-Figure 5, can be according to as follows
Mode is practiced；The multi-rotor unmanned aerial vehicle includes rotor wing unmanned aerial vehicle fuselage cradle 1, flight support frame 2, fixed connecting base 3, instrument
Equipment frame 4, unmanned plane rotor blade component 5；Wherein, by fixed connecting base 3 by rotor wing unmanned aerial vehicle fuselage cradle 1 and flight support
Frame 2 is fixedly connected integral；Instrument and equipment frame 4 is connected to the upper end of fixed connecting base 3, and the top of instrument and equipment frame 4 is equipped with
Solar cell module 6；Unmanned plane rotor blade component 5 includes rotor fixing seat 11 and rotor blade body 12；Rotor is solid
Reservation 11 has the fixing end 13 connecting with unmanned plane runner assembly and blade body connecting pin 14, and fixing end 13 is connected with blade body
End 14 uses monolithic molding；
The inside of blade body connecting pin 14 is formed with blade body connection clamp 15, and it is hemisphere that blade body, which connects clamp 15,
Shape, side are formed with V-arrangement card slot 16；The end of rotor blade body 12, which is formed with, connect clamp 15 and V-arrangement card slot with blade body
16 corresponding connection card chambers 17 and V-arrangement latch 18.
This patent has following improve compared with existing same type unmanned plane；Firstly, this patent will be revolved by fixing seat 3
Wing unmanned aerial vehicle body frame 1 is fixedly connected integral with flight support frame 2；So make the structure of the unmanned plane simpler, and
And it being capable of quick assembling；Meanwhile instrument and equipment frame 4 is connected to the upper end of fixing seat 3, the top of instrument and equipment frame 4 is fixed with too
Positive energy battery component 6, after assembly as Figure 1-Figure 2, the position that solar cell module 6 is arranged in the unmanned plane is moderate,
The volume of unmanned plane is not will increase, inside and outside structure is more reasonable.On the other hand, after the utility model improves, blade
The inside of body connecting pin is formed with blade body connection clamp, and it is hemisphere shape that blade body, which connects clamp, and side is formed with V-arrangement card
Slot；The end of rotor blade body is formed with connection card chamber corresponding with blade body connection clamp and V-arrangement card slot and V-arrangement latch；Such as
Shown in figure, the end of rotor blade body can be directly clamped among the paddle inside blade body connecting pin by connection card chamber and V-arrangement latch
Leaf body connects at clamp and V-arrangement card slot, thus seems when docking combination and be quickly easy.
A kind of multi-rotor unmanned aerial vehicle described in the utility model, rotor wing unmanned aerial vehicle fuselage cradle 1 have two groups of 7 Hes of undercarriage boom
Two groups of undercarriage connecting rods 8 form；The both ends of undercarriage connecting rod 8 form the anticollision contact block 9 upwarped, the end of anticollision contact block 9
It is provided with induction sensory package 10.The utility model rotor wing unmanned aerial vehicle 1 structure of fuselage cradle is simple, easy to operate, low in cost, tightly
Firmware is few, and adaptability is relatively broad.With preferable wind resistance.On the other hand, the both ends formation of undercarriage connecting rod upwarps anti-
Hit contact block.When unmanned plane is during tour, the both ends of undercarriage connecting rod form the anticollision contact block upwarped, so that upwarp
Anticollision contact block more outward compared with rotor, when during flight cruise even to touch building or trees or other facilities,
The anticollision contact block upwarped can be touched first, therefore can prevent the rotor of unmanned plane from touching.Meanwhile it can be in anticollision contact block
End be provided with induction sensory package, touch building or trees or other facilities during flight cruise
When, the anticollision contact block upwarped can be touched first, incuded sensory package at this time and be able to sense of touch, transmit a signal to unmanned plane system
System, control unmanned plane is flown away from, then making unmanned plane have contact collision prevention function by the undercarriage.
A kind of multi-rotor unmanned aerial vehicle described in the utility model, end outside and the blade body connecting pin 14 of rotor blade body 12
Inner wall between fill sealant（Such as the sealant of sponge material）；So when blade body is inserted into the end of rotor blade body 12
Behind the inside of connecting pin 14, then sealant can make the end of rotor blade body 12 realize sealing, prevent dust from immersing.
The foregoing description of the disclosed embodiments can be realized professional and technical personnel in the field or using originally practical new
Type.Various modifications to these embodiments will be readily apparent to those skilled in the art, and determine herein
The General Principle of justice can be realized in other embodiments without departing from the spirit or scope of the present utility model.Cause
This, the present invention will not be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The widest scope consistent with features of novelty.
Claims (3)
1. a kind of multi-rotor unmanned aerial vehicle, it is characterised in that：The multi-rotor unmanned aerial vehicle includes rotor wing unmanned aerial vehicle fuselage cradle（1）, rotor
Support frame（2）, fixed connecting base（3）, instrument and equipment frame（4）, unmanned plane rotor blade component（5）；Wherein, by being fixedly connected
Seat（3）By rotor wing unmanned aerial vehicle fuselage cradle（1）With flight support frame（2）It is fixedly connected integral；Instrument and equipment frame（4）It is connected to solid
Determine attachment base（3）Upper end, instrument and equipment frame（4）Top solar cell module is installed（6）；Unmanned plane rotor blade group
Part（5）Including rotor fixing seat（11）With rotor blade body（12）；Rotor fixing seat（11）With with unmanned plane rotating group
The fixing end of part connection（13）With blade body connecting pin（14）, fixing end（13）With blade body connecting pin（14）Using integral into
Shape；
Wherein, blade body connecting pin（14）Inside be formed with blade body connection clamp（15）, blade body connection clamp（15）For
Hemisphere shape, side are formed with V-arrangement card slot（16）；Rotor blade body（12）End be formed with and connect clamp with blade body
（15）With V-arrangement card slot（16）Corresponding connection card chamber（17）With V-arrangement latch（18）.
2. a kind of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The rotor wing unmanned aerial vehicle fuselage cradle（1）Tool
There are two groups of undercarriage booms（7）With two groups of undercarriage connecting rods（8）Composition；Undercarriage connecting rod（8）Both ends form the anticollision that upwarps
Contact block（9）, anticollision contact block（9）End be provided with induction sensory package（10）.
3. a kind of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：In rotor blade body（12）End on the outside of
With blade body connecting pin（14）Inner wall between fill sealant.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820649532.1U CN208102331U (en) | 2018-05-03 | 2018-05-03 | A kind of multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820649532.1U CN208102331U (en) | 2018-05-03 | 2018-05-03 | A kind of multi-rotor unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN208102331U true CN208102331U (en) | 2018-11-16 |
Family
ID=64113634
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820649532.1U Expired - Fee Related CN208102331U (en) | 2018-05-03 | 2018-05-03 | A kind of multi-rotor unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113353255A (en) * | 2021-05-31 | 2021-09-07 | 四川省天域航通科技有限公司 | Quick assembly disassembly device of unmanned aerial vehicle paddle |
-
2018
- 2018-05-03 CN CN201820649532.1U patent/CN208102331U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113353255A (en) * | 2021-05-31 | 2021-09-07 | 四川省天域航通科技有限公司 | Quick assembly disassembly device of unmanned aerial vehicle paddle |
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Granted publication date: 20181116 |