CN209427018U - A kind of empty amphibious aircraft of novel photoelectric mixing water - Google Patents
A kind of empty amphibious aircraft of novel photoelectric mixing water Download PDFInfo
- Publication number
- CN209427018U CN209427018U CN201822093382.3U CN201822093382U CN209427018U CN 209427018 U CN209427018 U CN 209427018U CN 201822093382 U CN201822093382 U CN 201822093382U CN 209427018 U CN209427018 U CN 209427018U
- Authority
- CN
- China
- Prior art keywords
- sealed compartment
- fuselage
- mixing water
- novel photoelectric
- amphibious aircraft
- Prior art date
- 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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- 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
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses a kind of empty amphibious aircraft of novel photoelectric mixing water, including fuselage, fuselage has sealed compartment and four floating drums, four floating drums are evenly arranged on four angles of fuselage lower end surface, steering engine and rudder are installed on floating drum, the inside of sealed compartment is equipped with control device, the lower end of sealed compartment is equipped with PODDED PROPULSOR, PODDED PROPULSOR and steering engine are electrically connected with control device, control device can receive external control signal to control PODDED PROPULSOR work, solar panel is equipped on the upper surface of fuselage, solar panel and the battery being mounted on inside sealed compartment are electrically connected, several uniformly distributed cradling pieces on fuselage lower end surface, the end of cradling piece be equipped with motor and and the propeller that is driven by motor, motor and solar panel are electrically connected with control device.The utility model utilizes solar panel and lithium battery hybrid power supply, can long-distance flight, while can also stop, navigate by water and landing on the water.
Description
Technical field
The utility model relates to aircraft device technical fields, and in particular to a kind of empty amphibious flight of novel photoelectric mixing water
Device.
Background technique
Nowadays the electronic unmanned vehicle of quadrotor is more more and more universal, relative to traditional unmanned vehicle, has unique
Advantage, energy conservation and environmental protection, high-efficient low energy consumption, and structure is simple, and noise is small, safe and reliable (explosion and fuel leakage will not occur),
Manipulation is simple, can freely hover.Currently, the application of quadrotor unmanned vehicle is concentrated mainly on aerial aspect, such as aviation is taken the photograph
Shadow, agricultural protection, cruise detection, fire control and disaster rescue etc..
However the generally existing short slab of the unmanned vehicle of pure electric vehicle, endurance is short, and voyage is small, can not navigate by water and stop on the water
It stays, therefore, it is difficult to complete particular task that is relatively remote, having the water surface to be detained navigation demand.Therefore, one kind can effectively improve boat
Shi Hangcheng, and the aircraft that can navigate by water landing on the water is necessary.
Summary of the invention
Problem to be solved in the utility model is: a kind of empty amphibious aircraft of novel photoelectric mixing water is provided, using too
It is positive can solar panel and lithium battery hybrid power supply, can long-distance flight, while can also stop, navigate by water and landing on the water.
The utility model in order to solve the above problem provided by technical solution are as follows: a kind of novel photoelectric mixing water is empty amphibious to fly
Row device, including fuselage, the fuselage have sealed compartment and four floating drums, and four floating drums are evenly arranged on the fuselage lower end surface
Four angles on, steering engine and rudder are installed, the inside of the sealed compartment is equipped with control device, described close on the floating drum
The lower end of batten down is equipped with PODDED PROPULSOR, and the PODDED PROPULSOR and steering engine are electrically connected with the control device, the control
Device processed can receive external control signal to control PODDED PROPULSOR work, be equipped with too on the upper surface of the fuselage
Positive energy solar panel, the solar panel and the battery being mounted on inside sealed compartment are electrically connected, on the fuselage lower end surface
Several cradling pieces of cloth, the end of the cradling piece are equipped with motor and and by the motor-driven propeller, the motors
It is electrically connected with the control device with solar panel.
Preferably, the control device includes flight control panel and remote control signal receiver, the remote control signal receiver
It receives the wireless signal that remote control issues and is input to the flight control panel, flight control panel is according to the wireless signal received
It is controlled, makes flight directive.
Preferably, four electronics tune connecting respectively by water proof wire with four propellers are installed in the sealed compartment
The lithium battery of fast device and offer energy.Electron speed regulator is used to control the speed of propeller, and the signal of electron speed regulator is by leading
Line is transferred to flight control panel, and by the revolving speed of flight control panel control motor, to control the speed of propeller.Battery is nothing
Man-machine offer energy, while the solar energy storage that solar panels are absorbed is in the battery.
Preferably, the cradling piece has 4 and is arranged on the lower end surface of the fuselage in right-angled intersection.
Preferably, small-sized high definition water-proof CCD camera is installed outside the sealed compartment.Pass through small-sized high definition water-proof CCD camera
It can work, real-time image acquisition and can pass back at staff in the sky, under the water surface, a variety of environment in land.
Preferably, carrying platform is installed outside the sealed compartment.Small device can be carried by carrying platform to carry out
Sampling.
Preferably, the cradling piece is equipped with metallic channel.Waterproof machine and watertight connector can be placed by metallic channel
Water proof wire keeps device more neat and artistic.
Preferably, the solar panel is monocrystalline silicon high-efficient bendable solar panel.
Preferably, the sealing cabin is equipped with the movement position in the orientation of available unmanned plane, real-time report unmanned plane
Beidou navigation module.
Compared with prior art, the utility model has the advantages that: the empty amphibious flight of the utility model novel photoelectric mixing water
Device can work normally in the sky, can also be navigated by water on the water.Using being used in mixed way for solar energy and electric energy, effectively improve winged
The endurance voyage of row device；Buoyance in water is provided using removable floating drum, it can be on the water surface freely by the PODDED PROPULSOR of installation
Movement can also be swum on the water surface, this greatly expands quadrotor for a long time to realize stop waterborne, navigation, landing
The working range of unmanned plane.The operation that the utilization of its intelligent control module simultaneously largely reduces staff is difficult
Degree.
Detailed description of the invention
Attached drawing described herein is used to provide a further understanding of the present invention, and constitutes one of the utility model
Point, the exemplary embodiment of the utility model and the description thereof are used to explain the utility model, does not constitute to the utility model
Improper restriction.
Fig. 1 is the overall structure diagram of the utility model；
Fig. 2 is the bottom view of the utility model；
Fig. 3 is the main view of the utility model；
Attached drawing mark: 1, propeller, 2, waterproof machine, 3, rudder, 4, motor support base, 5, floating drum, 6, PODDED PROPULSOR,
7, solar panel, 8, cradling piece, 9, carrying platform, 10, metallic channel, 11, sealed compartment, 12, small-sized high definition water-proof CCD camera,
13, fuselage.
Specific embodiment
The embodiments of the present invention is described in detail below in conjunction with accompanying drawings and embodiments, whereby to the utility model
How applied technology method solves technical problem and reaches the realization process of technical effect to fully understand and implement.
Specific embodiment of the utility model is as shown in figures 1 and 3, a kind of empty amphibious aircraft of novel photoelectric mixing water,
Including fuselage 13, fuselage 13 has sealed compartment 11 and four floating drums 5, and four floating drums 5 are evenly arranged on four of 13 lower end surface of fuselage
On angle, steering engine and rudder 3 are installed on floating drum 5, the inside of sealed compartment 11 is equipped with control device, the lower end peace of sealed compartment 11
Equipped with PODDED PROPULSOR 6, PODDED PROPULSOR 6 and steering engine are electrically connected with control device, and control device can receive external control
Signal processed is equipped with solar panel 7, solar battery on the upper surface of fuselage 13 to control the work of PODDED PROPULSOR 6
Plate 7 and the battery being mounted on inside sealed compartment 11 are electrically connected, several uniformly distributed cradling pieces 8 on 13 lower end surface of fuselage, cradling piece 8
End be equipped with motor and and the propeller 1 that is driven by motor, motor and solar panel 7 are electrically connected with control device.
Control device includes flight control panel and remote control signal receiver, and remote control signal receiver receives what remote control issued
Wireless signal is simultaneously input to flight control panel, and flight control panel is controlled according to the wireless signal received, is made flight and is referred to
It enables.
It is installed with four electron speed regulators connecting respectively by water proof wire with four propellers in sealed compartment 11 and mentions
For the lithium battery of energy.Electron speed regulator is used to control the speed of propeller, and the signal of electron speed regulator is given by wire transmission
Flight control panel, and by the revolving speed of flight control panel control motor, to control the speed of propeller.Battery provides for unmanned plane
Energy, while the solar energy storage that solar panels are absorbed is in the battery.
Cradling piece 8 has 4 and is arranged on the lower end surface of fuselage 13 in right-angled intersection.
Small-sized high definition water-proof CCD camera 12 is installed outside sealed compartment 11.It can be in sky by small-sized high definition water-proof CCD camera 12
In, work under the water surface, a variety of environment in land, real-time image acquisition and can pass back at staff.
Carrying platform 9 is installed outside sealed compartment 11.Small device can be carried by carrying platform to be sampled.
Cradling piece 8 is equipped with metallic channel 10.It is led by the waterproof that metallic channel 10 can place waterproof machine and watertight connector
Line keeps device more neat and artistic.
The beneficial effects of the utility model are: the empty amphibious aircraft of the utility model novel photoelectric mixing water can be in the sky
It works normally, can also be navigated by water on the water.Using being used in mixed way for solar energy and electric energy, the endurance boat of aircraft is effectively improved
Journey；There is provided buoyance in water using removable floating drum, by the PODDED PROPULSOR of installation can the free movement on the water surface, to realize
Stop waterborne, navigation, landing, can also swim on the water surface, this greatly expands the work of quadrotor drone for a long time
Range.The utilization of its intelligent control module largely reduces the operation difficulty of staff simultaneously.
Only the most preferred embodiment of the utility model is described above, but is not to be construed as the limit to claim
System.The utility model is not only limited to above embodiments, and specific structure is allowed to vary.It is all in the utility model independent right
It is required that protection scope in made various change in scope of protection of the utility model.
Claims (9)
1. a kind of empty amphibious aircraft of novel photoelectric mixing water, it is characterised in that: including fuselage, the fuselage has sealed compartment
With four floating drums, four floating drums are evenly arranged on four angles of the fuselage lower end surface, be equipped on the floating drum steering engine and
Rudder, the inside of the sealed compartment are equipped with control device, and the lower end of the sealed compartment is equipped with PODDED PROPULSOR, described to hang
Cabin propeller and steering engine are electrically connected with the control device, and the control device can receive external control signal to control
PODDED PROPULSOR processed works, and is equipped with solar panel, the solar panel and installation on the upper surface of the fuselage
Battery inside sealed compartment is electrically connected, several uniformly distributed cradling pieces on the fuselage lower end surface, the end peace of the cradling piece
It is electrically connected with the control device equipped with motor and by the motor-driven propeller, the motor and solar panel
It connects.
2. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the control dress
It sets including flight control panel and remote control signal receiver, the remote control signal receiver receives the wireless signal of remote control sending simultaneously
It is input to the flight control panel, flight control panel is controlled according to the wireless signal received, makes flight directive.
3. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the sealed compartment
It is inside installed with four electron speed regulators connecting respectively by water proof wire with four propellers and the lithium battery of energy is provided.
4. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the cradling piece
There are 4 and is arranged on the lower end surface of the fuselage in right-angled intersection.
5. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the sealed compartment
Outside is equipped with small-sized high definition water-proof CCD camera.
6. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the sealed compartment
Outside is equipped with carrying platform.
7. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 4, it is characterised in that: the cradling piece
It is equipped with metallic channel.
8. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the solar energy
Solar panel is monocrystalline silicon high-efficient bendable solar panel.
9. the empty amphibious aircraft of a kind of novel photoelectric mixing water according to claim 1, it is characterised in that: the sealed compartment
Body be equipped with the orientation of available unmanned plane, real-time report unmanned plane movement position Beidou navigation module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822093382.3U CN209427018U (en) | 2018-12-13 | 2018-12-13 | A kind of empty amphibious aircraft of novel photoelectric mixing water |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822093382.3U CN209427018U (en) | 2018-12-13 | 2018-12-13 | A kind of empty amphibious aircraft of novel photoelectric mixing water |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209427018U true CN209427018U (en) | 2019-09-24 |
Family
ID=67971726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822093382.3U Expired - Fee Related CN209427018U (en) | 2018-12-13 | 2018-12-13 | A kind of empty amphibious aircraft of novel photoelectric mixing water |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209427018U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110775265A (en) * | 2019-10-28 | 2020-02-11 | 上海交通大学 | Oil-electricity hybrid driving amphibious aircraft and control method thereof |
| CN111634415A (en) * | 2020-06-09 | 2020-09-08 | 王大祥 | High-endurance water environment monitoring device for regional lake |
-
2018
- 2018-12-13 CN CN201822093382.3U patent/CN209427018U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110775265A (en) * | 2019-10-28 | 2020-02-11 | 上海交通大学 | Oil-electricity hybrid driving amphibious aircraft and control method thereof |
| CN111634415A (en) * | 2020-06-09 | 2020-09-08 | 王大祥 | High-endurance water environment monitoring device for regional lake |
| CN111634415B (en) * | 2020-06-09 | 2021-08-27 | 王大祥 | High-endurance water environment monitoring device for regional lake |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190924 Termination date: 20201213 |