CN206782074U - A kind of amphibious multi-rotor unmanned aerial vehicle - Google Patents
A kind of amphibious multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN206782074U CN206782074U CN201720687593.2U CN201720687593U CN206782074U CN 206782074 U CN206782074 U CN 206782074U CN 201720687593 U CN201720687593 U CN 201720687593U CN 206782074 U CN206782074 U CN 206782074U
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- fuselage
- water
- navigation
- control assembly
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Abstract
The utility model discloses a kind of amphibious multi-rotor unmanned aerial vehicle, including fuselage, flying power system, surface navigation dynamical system, ground control terminal；Fuselage bottom is ship shape, and fuselage roof is provided with cover；Flying power system includes horn, fly brushless electric tune, control assembly, lithium battery group, and horn is arranged on back, and horn end is provided with the waterproof flight brushless electric machine that can install rotor；Surface navigation dynamical system includes keg float, PTO, detachable connecting rod, and keg float is arranged on the both sides of underbelly by detachable connecting rod, and PTO is arranged on the afterbody of fuselage；PTO promotes fuselage to be navigated by water in water, control assembly, PTO control under change the direction navigated by water in water of fuselage.The utility model is simple in construction, can in the air fly and, when barrier is met in navigation, can also drop to the water surface in surface navigation after directly being taken off from the water surface across obstacle and continue to navigate by water.
Description
Technical field
The utility model belongs to unmanned plane manufacturing technology field, and in particular to a kind of amphibious multi-rotor unmanned aerial vehicle.
Background technology
Unmanned plane is the not manned vehicle manipulated using radio robot and the presetting apparatus provided for oneself, nobody
Machine welcomes the fast growth phase at the beginning of 21 century, and progressively extend to civil area from military domain.Nowadays, civilian unmanned plane has been
It is used widely in emergency management and rescue, environment measuring, power-line patrolling, the multiple fields such as mapping, agricultural plant protection of taking photo by plane.Prior art
The unmanned plane overwhelming majority can only fly in the air, the unmanned plane that can in the air fly while can navigate by water on the water apply compared with
It is few.In the case of especially for hydrologic monitoring, water quality exploration, in the unmanned plane course of work, not only it is required in the water surface certainly
By navigating by water, while being capable of across obstacle, therefore exploitation one kind can fly in the air while and can is enough navigated on the water freely
Capable unmanned plane is extremely necessary.
Utility model content
For problem above, the utility model provides a kind of amphibious multi-rotor unmanned aerial vehicle, simple in construction, can be in sky
Middle flight can also in surface navigation, when barrier is met in navigation, drop to after directly being taken off from the water surface across obstacle the water surface after
Continuation of the journey row work.
The technical solution of the utility model is as follows：A kind of amphibious multi-rotor unmanned aerial vehicle, including fuselage, flying power system
System, surface navigation dynamical system, ground control terminal；Fuselage is made up of composite and expanded material, and fuselage bottom is ship shape,
Fuselage interior is hollow structure, and fuselage roof is provided with cover, and cover is connected by bolt with fuselage；Flying power system includes
Horn, flight is brushless electric tune, control assembly, lithium battery group, horn are arranged on back, and horn is at least provided with 4, horn
End is provided with the waterproof flight brushless electric machine that can install rotor, and waterproof flight brushless electric machine is adjusted by the brushless electricity that flies and control
Component is connected, and the brushless electricity that flies is adjusted to be connected with lithium battery group, and the brushless electricity that flies adjusts the rotational speed regulation for realizing waterproof brushless electric machine, lithium
Battery pack is connected with control assembly, and lithium battery group provides power supply for control assembly；Surface navigation dynamical system includes keg float, power
Output device, detachable connecting rod, keg float are arranged on the both sides of underbelly by detachable connecting rod, keg float at least provided with
Two, it is ensured that unmanned plane is more steady reliable in underwater exercise, and PTO is arranged on the afterbody of fuselage；Power output fills
Put including quant, rudder for ship, steering wheel, navigation brushless electric machine, navigation it is brushless electricity adjust, quant with navigation brushless electric machine be connected, navigation nothing
Brush motor connects with navigating by water brushless electric adjust, and navigates by water brushless electricity tune and is connected with control assembly, navigates by water brushless electricity and adjust and lithium battery group company
Connect, navigate by water brushless electricity and adjust the rotational speed regulation for realizing navigation brushless electric machine, quant promotes fuselage to be navigated by water in water, and rudder for ship passes through steering wheel
Be connected with control assembly, rudder for ship control assembly, steering wheel control under change the direction navigated by water in water of fuselage.
Further, control terminal in ground includes switching switch, joystick, antenna, power switch, ground control terminal
Communicated with the control assembly in flying power system by antenna using 2.4GHZ radio signals, set in ground control terminal
There is switching to switch, switching switch can be achieved flying power system and carry out manual switching, joystick with surface navigation dynamical system
For controlling unmanned plane during flying speed, direction, power switch is used to start, closes ground control terminal.
Further, flying power system is located at the top of fuselage, and surface navigation dynamical system is the bottom of fuselage, is flown
Control assembly in dynamical system is arranged on fuselage interior, and the PTO in surface navigation dynamical system passes through control group
Part is controlled.
Further, detachable connecting rod one end is provided with tapped metal connecting piece, and fuselage both sides set outer spiral shell
Line post, detachable connecting rod are connected by metal connecting piece with the external thread column on fuselage, and detachable connecting rod other end can
Keg float is connected, detachable connecting rod can disassemble from the external thread column of fuselage both sides.
Brief description of the drawings
Fig. 1 is the utility model tail structure schematic diagram.
Fig. 2 is the utility model top structure schematic diagram.
Fig. 3 is the utility model side structure schematic diagram.
Fig. 4 is the utility model control principle block diagram.
Fig. 5 is that the utility model ground controls terminal structure schematic diagram.
Embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.
As shown in Figure 1, Figure 2, Figure 3, Figure 4, a kind of amphibious multi-rotor unmanned aerial vehicle, including fuselage 1, flying power system
2nd, surface navigation dynamical system 3, ground control terminal 4；Fuselage 1 is made up of composite and expanded material, and the bottom of fuselage 1 is ship
Shape, the inside of fuselage 1 are hollow structure, and the top of fuselage 1 is provided with cover 101, and cover 304 is connected by bolt with fuselage 1；Flight
Dynamical system 2 includes horn 201, fly brushless electric tune, control assembly, lithium battery group, and horn 201 is arranged on the top of fuselage 1, machine
Arm 201 is provided with 4, and horn 201 is provided with the waterproof flight brushless electric machine 202 that can install rotor, waterproof flight brushless electric machine
202 are connected by the brushless electricity tune that flies with control assembly, and the brushless electricity that flies is adjusted to be connected with lithium battery group, and brushless electric adjust of flying is realized
The rotational speed regulation of waterproof brushless electric machine, lithium battery group are connected with control assembly, and lithium battery group provides power supply for control assembly；The water surface
Navigating power system 3 includes keg float 301, detachable connecting rod 302, PTO 303, and keg float 301 is by detachable
Connecting rod 302 is arranged on the both sides of the bottom of fuselage 1, and keg float 301 is at least provided with two, it is ensured that unmanned plane is more flat in underwater exercise
Steady reliable, PTO 3 is arranged on the afterbody of fuselage 1；PTO 3 includes quant 3031, rudder for ship 3032, rudder
Machine, navigation brushless electric machine, navigation is brushless, and electricity is adjusted, and quant 3031 is connected with navigation brushless electric machine, navigation brushless electric machine and navigation nothing
The electric tune connection of brush, navigation is brushless, and electricity tune is connected with control assembly, and navigation is brushless, and electricity tune is connected with lithium battery group, navigates by water brushless electric tune
The rotational speed regulation of navigation brushless electric machine is realized, quant 3031 promotes fuselage 1 to be navigated by water in water, and rudder for ship 3032 passes through steering wheel and control
Component connects, rudder for ship 3032 control assembly, steering wheel control under change the direction navigated by water in water of fuselage.
As shown in figure 5, ground control terminal 4 includes switching switch 401, joystick 402, antenna 403, power switch
404, ground control terminal 4 is led to using 2.4GHZ radio signals by antenna 403 and the control assembly in flying power system 2
Letter, ground control and switching switch 401 are provided with terminal 4, and switching switch 401 can realize flying power system 2 and surface navigation
Dynamical system 3 carries out manual switching, and joystick 402 is used to control unmanned plane during flying speed, direction, and power switch 404 is used for
Start, close ground control terminal 4.
As shown in figure 1, flying power system 2 is located at the top of fuselage 1, surface navigation dynamical system 3 is located under fuselage 1
Portion, the control assembly in flying power system 2 are arranged on inside fuselage 1, the PTO in surface navigation dynamical system 3
303 are controlled by control assembly.
Detachable one end of connecting rod 302 is provided with tapped metal connecting piece, and the both sides of fuselage 1 set external thread column,
Detachable connecting rod 302 is connected by metal connecting piece with the external thread column on fuselage 1, the detachable other end of connecting rod 302
Keg float 301 can be connected, detachable connecting rod 302 can disassemble from the external thread column of the both sides of fuselage 1.
When unmanned plane needs to drop to the water surface：Operating personnel drive into unmanned plane to above the water surface, fuselage 1, surface navigation
Keg float 302 in dynamical system 3 is fallen into the water surface, ground is controlled the switching switch 401 in terminal 4 switch to surface navigation and moved
Force system 3, unmanned plane during flying dynamical system 2 are closed automatically, and PTO 303 works, and PTO 303 promotes machine
Body 1 is in surface navigation.
When barrier is met when unmanned plane is in surface navigation：Ground is directly controlled the switching in terminal 4 to open by operating personnel
Close 401 and switch to flying power system 2, unmanned plane surface navigation dynamical system 3 is stopped, and PTO 303 stops
Work, flying power system 2 works, and unmanned plane takes off from the water surface, after avoiding obstacles, can select to drop to again the water surface or
Fly in the air.
Above is exemplary description is carried out to the utility model, it is clear that realization of the present utility model is not by above-mentioned side
The limitation of formula, if employ technical solutions of the utility model progress various improvement, or it is not improved will be of the present utility model
Design and technical scheme directly apply to other occasions, in the scope of protection of the utility model.
Claims (4)
1. a kind of amphibious multi-rotor unmanned aerial vehicle, including fuselage, flying power system, surface navigation dynamical system, ground control
Terminal processed；
Characterized in that, fuselage is made up of composite and expanded material, fuselage bottom is ship shape, and fuselage interior is hollow knot
Structure, fuselage roof are provided with cover, and cover is connected by bolt with fuselage；
Flying power system includes horn, fly brushless electric tune, control assembly, lithium battery group, and horn is arranged on back, machine
For arm at least provided with 4, horn end is provided with the waterproof flight brushless electric machine that can install rotor, and waterproof flight brushless electric machine leads to
Cross the brushless electricity tune that flies to be connected with control assembly, the brushless electricity that flies is adjusted to be connected with lithium battery group, and brushless electric adjust of flying realizes waterproof
The rotational speed regulation of brushless electric machine, lithium battery group are connected with control assembly, and lithium battery group provides power supply for control assembly；
Surface navigation dynamical system includes keg float, PTO, detachable connecting rod, and keg float is set by detachable connecting rod
Put in the both sides of underbelly, keg float is at least provided with two, it is ensured that unmanned plane is more steady reliable in underwater exercise, and power is defeated
Go out the afterbody that device is arranged on fuselage；
PTO includes quant, rudder for ship, steering wheel, navigation brushless electric machine, navigation is brushless, and electricity is adjusted, and quant is with navigating by water brushless electricity
Machine connects, and navigation brushless electric machine connects with navigating by water brushless electric adjust, and navigates by water brushless electricity tune and is connected with control assembly, navigates by water brushless electricity and adjust
It is connected with lithium battery group, navigates by water brushless electricity and adjust the rotational speed regulation for realizing navigation brushless electric machine, quant promotes fuselage to be navigated by water in water,
Rudder for ship is connected by steering wheel with control assembly, rudder for ship control assembly, steering wheel control under change the side navigated by water in water of fuselage
To.
2. a kind of amphibious multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that ground control terminal includes
Switch switch, joystick, antenna, power switch, ground control terminal is using 2.4GHZ radio signals by antenna with flying
Control assembly communication in action Force system, ground, which controls, is provided with switching switch in terminal, it is dynamic to switch the achievable flight of switch
Force system carries out manual switching with surface navigation dynamical system, and joystick is used to control unmanned plane during flying speed, direction, power supply
Switch for starting, closing ground control terminal.
3. a kind of amphibious multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that flying power system is located at
The top of fuselage, surface navigation dynamical system are the bottom of fuselage, and the control assembly in flying power system is arranged in fuselage
Portion, the PTO in surface navigation dynamical system are controlled by control assembly.
A kind of 4. amphibious multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that detachable connecting rod one end
Be provided with tapped metal connecting piece, fuselage both sides set external thread column, detachable connecting rod by metal connecting piece with
External thread column connection on fuselage, detachable connecting rod other end can connect keg float, and detachable connecting rod can be from fuselage both sides
External thread column on disassemble.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720687593.2U CN206782074U (en) | 2017-06-14 | 2017-06-14 | A kind of amphibious multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720687593.2U CN206782074U (en) | 2017-06-14 | 2017-06-14 | A kind of amphibious multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206782074U true CN206782074U (en) | 2017-12-22 |
Family
ID=60715764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720687593.2U Expired - Fee Related CN206782074U (en) | 2017-06-14 | 2017-06-14 | A kind of amphibious multi-rotor unmanned aerial vehicle |
Country Status (1)
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| CN (1) | CN206782074U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109358654A (en) * | 2018-11-16 | 2019-02-19 | 江苏科技大学 | A kind of empty amphibious search and rescue support unmanned vehicle system of water |
| CN110626514A (en) * | 2019-10-29 | 2019-12-31 | 中国石油大学(华东) | Amphibious four-rotor unmanned aerial vehicle with multiple perch structures |
| JP2021020672A (en) * | 2019-07-26 | 2021-02-18 | 国立大学法人信州大学 | Movable body, investigation and survey apparatus and investigation and survey method |
| WO2021129001A1 (en) * | 2019-12-27 | 2021-07-01 | 浙江大学 | Underwater and aerial robot |
| CN113799562A (en) * | 2021-10-14 | 2021-12-17 | 上海海事大学 | Water-air amphibious unmanned ship capable of crossing obstacles and control method |
-
2017
- 2017-06-14 CN CN201720687593.2U patent/CN206782074U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109358654A (en) * | 2018-11-16 | 2019-02-19 | 江苏科技大学 | A kind of empty amphibious search and rescue support unmanned vehicle system of water |
| CN109358654B (en) * | 2018-11-16 | 2022-03-29 | 江苏科技大学 | Water-air amphibious search and rescue support unmanned aerial vehicle system |
| JP2021020672A (en) * | 2019-07-26 | 2021-02-18 | 国立大学法人信州大学 | Movable body, investigation and survey apparatus and investigation and survey method |
| JP7086144B2 (en) | 2019-07-26 | 2022-06-17 | 国立大学法人信州大学 | Mobiles, exploration surveyors and exploration survey methods |
| CN110626514A (en) * | 2019-10-29 | 2019-12-31 | 中国石油大学(华东) | Amphibious four-rotor unmanned aerial vehicle with multiple perch structures |
| CN110626514B (en) * | 2019-10-29 | 2021-01-15 | 中国石油大学(华东) | Amphibious four-rotor unmanned aerial vehicle with multiple perch structures |
| WO2021129001A1 (en) * | 2019-12-27 | 2021-07-01 | 浙江大学 | Underwater and aerial robot |
| US11926414B2 (en) | 2019-12-27 | 2024-03-12 | Zhejiang University | Underwater and aerial vehicle |
| CN113799562A (en) * | 2021-10-14 | 2021-12-17 | 上海海事大学 | Water-air amphibious unmanned ship capable of crossing obstacles and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171222 Termination date: 20190614 |
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| CF01 | Termination of patent right due to non-payment of annual fee |