CN111824413A - Amphibious manned unmanned aerial vehicle - Google Patents
Amphibious manned unmanned aerial vehicle Download PDFInfo
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- CN111824413A CN111824413A CN201910320926.1A CN201910320926A CN111824413A CN 111824413 A CN111824413 A CN 111824413A CN 201910320926 A CN201910320926 A CN 201910320926A CN 111824413 A CN111824413 A CN 111824413A
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- unmanned aerial
- aerial vehicle
- amphibious
- carbon fiber
- fiber composite
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- 239000002131 composite material Substances 0.000 claims abstract description 53
- 239000011521 glass Substances 0.000 claims abstract description 30
- 239000000835 fiber Substances 0.000 claims abstract description 14
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 39
- 239000004917 carbon fiber Substances 0.000 claims description 39
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 39
- 230000003139 buffering effect Effects 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 3
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 claims description 3
- 230000007613 environmental effect Effects 0.000 claims description 3
- 238000007789 sealing Methods 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000003340 mental effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/008—Amphibious sea planes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
- B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention discloses an amphibious manned unmanned aerial vehicle, which comprises: the parachute device comprises a machine body, a power device, a parachute device, a buffer moving device, a control system and a machine cabin door. Amphibious unmanned aerial vehicle both can fly in the air but also can sail on water, and the organism is two hemispheric aviation organic glass panorama windows and the carbon-fibre composite host computer body, and two hemispheric aviation organic glass panorama windows divide two upper and lower parts fixed connection in the middle of the carbon-fibre composite host computer body. The power device comprises a motor, a propeller, a generator and a power supply, the propeller is fixedly arranged on a motor shaft, and the propeller can change the power direction to control the running direction in flying or navigating through multi-directional rotation. When the parachute device is emergently landed, the parachute is automatically opened, and the parachute device can be opened through the manual opening device under the power failure state. The amphibious manned unmanned aerial vehicle improves the safety of the manned unmanned aerial vehicle and enlarges the application range of the manned unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of manned unmanned aerial vehicles, in particular to an amphibious manned unmanned aerial vehicle
Background
Manned unmanned aerial vehicle is limited to the flight in sky now, can't navigate in water, lacks the manned unmanned aerial vehicle that can fly in the sky and can navigate in water again.
The manned unmanned aerial vehicle safety measure is not enough nowadays, can't give other people the sense of security, and the engine burst trouble loses the unable passenger safety of protection when needing to force to land during the flight.
The unmanned aerial vehicle travelling comfort of people now is not enough with the sight, and along with the material life is better and better, unmanned aerial vehicle's appearance is not only the instrument of solving the trip problem, especially the product that will satisfy people's mental needs, and unmanned aerial vehicle of people still is past traditional aircraft development at present, only realizes taking the people overhead to be far away not enough.
Disclosure of Invention
The invention provides an amphibious manned unmanned aerial vehicle, which solves the problems that the existing manned unmanned aerial vehicle is only limited to flying in the air, a yacht is only limited to sailing on water, and safety measures and ornamental value are insufficient.
In order to solve the above problems, the present invention provides the following technical solutions:
amphibious manned unmanned aerial vehicle includes: the parachute device comprises a machine body, a power device, a parachute device, a buffer moving device, a control system and a machine cabin door.
According to amphibious manned unmanned aerial vehicle, characterized by: the amphibious unmanned aerial vehicle can fly in the air and also can sail on water.
According to amphibious manned unmanned aerial vehicle, characterized by: the aircraft organic glass panorama window comprises an aircraft organic glass panorama window body, a carbon fiber composite main machine body, a main frame body and a power supply, wherein the aircraft organic glass panorama window body is in a hemispherical shape, and the two hemispherical aircraft organic glass panorama window bodies are fixedly connected between the upper portion and the lower portion of the main machine body.
According to amphibious manned unmanned aerial vehicle, characterized by: the aviation organic glass panoramic window is divided into an upper layer and a lower layer, and the aerial organic glass panoramic window can reach the upper layer space and the lower layer space by lifting up and down through the built-in seat.
According to amphibious manned unmanned aerial vehicle, characterized by: the carbon fiber composite main machine body is in a ring shape.
According to amphibious manned unmanned aerial vehicle, characterized by: the carbon fiber composite main machine body is provided with eight round holes, and each round hole is internally provided with a set of power device.
According to amphibious manned unmanned aerial vehicle, characterized by: the power device comprises a motor, a propeller, a generator and a power supply, wherein the propeller is fixedly arranged on a motor shaft, the power supply is arranged and sealed in the carbon fiber composite material main body, and the power supply is connected with the motor through an electric wire which is hermetically connected with the carbon fiber composite material main body.
According to amphibious manned unmanned aerial vehicle, characterized by: when the propeller works, kinetic energy can be transmitted to the generator through the transmission belt and converted into electric energy to charge the power supply.
According to amphibious manned unmanned aerial vehicle, characterized by: the motor is a waterproof motor.
According to amphibious manned unmanned aerial vehicle, characterized by: the propeller can change the power direction to control the driving direction by multi-directional rotation when flying or navigating.
According to amphibious manned unmanned aerial vehicle, characterized by: the parachute device is unmanned aerial vehicle parachute and carbon-fibre composite roof, and the unmanned aerial vehicle parachute passes through the carbon-fibre composite component connection locking on the carbon-fibre composite roof, and the parachute is automatic to be opened during emergency landing, and the manual opening device of accessible opens under the power failure state, and manual opening device installs under the carbon-fibre composite roof.
According to amphibious manned unmanned aerial vehicle, characterized by: the buffering mobile device comprises a buffering mechanism, eight carbon fiber composite material telescopic foot frames and eight spherical bottom wheels, wherein the buffering mechanism is arranged at the bottom of the aviation organic glass panoramic window, the eight carbon fiber composite material telescopic foot frames are arranged at the bottom of the buffering mechanism, and the eight carbon fiber composite material telescopic foot frames are respectively provided with one spherical bottom wheel.
According to amphibious manned unmanned aerial vehicle, characterized by: the eight carbon fiber composite material telescopic foot frames can be stretched through the control system.
The control system includes: control terminal, lighting device, big dipper positioner, under-deck environmental control system. And an independent power supply in the carbon fiber composite material main body supplies electric energy to the control system through a wire in sealing connection.
According to amphibious manned unmanned aerial vehicle, characterized by: the upper layer and the lower layer of the aviation organic glass panoramic window are respectively provided with a cabin door.
The invention has the beneficial effects that:
1. the application range is wide, not only can fly in the sky, can also sail on water.
2. The safety is high, and the safety of personnel in the parachute device and the buffer moving device can be greatly ensured under the emergency condition.
3. The ornamental value is high, the aviation organic glass panoramic window is divided into an upper layer and a lower layer, and the large-area glass enables passengers to enjoy the scenery outside the glass without shielding. When the vehicle sails on water, the lower-layer aviation organic glass panoramic window is positioned underwater, and passengers can view underwater scenery in a glance.
Drawings
Fig. 1 is a schematic structural diagram provided by the present invention.
Figure 2 is a top plan view of the present invention.
In the attached drawing, 1 is an aviation organic glass panoramic window; 2 is a carbon fiber composite material top plate; 3 is a buffer mechanism; 4 is a carbon fiber composite material main machine body; 5 is a carbon fiber composite material telescopic foot rest; 6 is a spherical bottom wheel; 7 is a power device; 8 is an unmanned aerial vehicle parachute; 9 is a control system; 10 is a cabin door.
Detailed Description
The invention will be further described with reference to the following figures and specific examples:
the invention relates to an amphibious manned unmanned aerial vehicle, which comprises an aviation organic glass panoramic window 1, a carbon fiber composite top plate 2, a buffer mechanism 3, a carbon fiber composite main body 4, a carbon fiber composite telescopic foot stand 5, a spherical bottom wheel 6, a power device 7, an unmanned aerial vehicle parachute 8, a control system 9 and a cabin door 10, as shown in figure 1.
Amphibious manned unmanned aerial vehicle includes: the parachute device comprises a machine body, a power device, a parachute device, a buffer moving device, a control system and a machine cabin door.
According to amphibious manned unmanned aerial vehicle, characterized by: the amphibious manned unmanned aerial vehicle can sail on water.
According to amphibious manned unmanned aerial vehicle, characterized by: the aircraft organic glass panoramic window comprises two hemispherical aviation organic glass panoramic windows 1 and a carbon fiber composite main machine body 4, wherein the two hemispherical aviation organic glass panoramic windows 1 are fixedly connected between the carbon fiber composite main machine body 4 in an upper part and a lower part.
According to amphibious manned unmanned aerial vehicle, characterized by: the aviation organic glass panoramic window 1 is divided into an upper layer and a lower layer, and can reach the upper layer and the lower layer of space through the up-down lifting of the seat in the aircraft.
According to amphibious manned unmanned aerial vehicle, characterized by: the carbon fiber composite main body 4 is in a ring shape.
According to amphibious manned unmanned aerial vehicle, characterized by: the carbon fiber composite main body 4 is provided with eight round holes, and each round hole is internally provided with a set of power device 7.
According to amphibious manned unmanned aerial vehicle, characterized by: the power device 7 comprises a motor, a propeller, a generator and a power supply, the propeller is fixedly arranged on a motor shaft, the power supply is arranged and sealed in the carbon fiber composite material main machine body 4, and the power supply is connected with the motor through an electric wire which is hermetically connected with the carbon fiber composite material main machine body 4.
According to amphibious manned unmanned aerial vehicle, characterized by: when the propeller works, kinetic energy can be transmitted to the generator through the transmission belt and converted into electric energy to charge the power supply.
According to amphibious manned unmanned aerial vehicle, characterized by: the motor is a waterproof motor.
According to amphibious manned unmanned aerial vehicle, characterized by: the propeller can change the power direction to control the driving direction by multi-directional rotation when flying or navigating.
According to amphibious manned unmanned aerial vehicle, characterized by: the parachute device is unmanned aerial vehicle parachute 8 and carbon-fibre composite roof 2, and unmanned aerial vehicle parachute 8 passes through the carbon-fibre composite component connection locking on carbon-fibre composite roof 2, and the parachute is automatic to be opened during emergency landing, and the manual opening device of accessible opens under the power failure state, and manual opening device installs under carbon-fibre composite roof 2.
According to amphibious manned unmanned aerial vehicle, characterized by: the buffering mobile device comprises a buffering mechanism 3, eight carbon fiber composite material telescopic foot rests 5 and eight spherical bottom wheels 6, wherein the buffering mechanism 3 is installed at the bottom of the aviation organic glass panoramic window 1, the eight carbon fiber composite material telescopic foot rests 5 are installed at the bottom of the buffering mechanism 3, and the eight carbon fiber composite material telescopic foot rests 5 are respectively provided with one spherical bottom wheel 6.
According to amphibious manned unmanned aerial vehicle, characterized by: the eight carbon fiber composite material telescopic foot frames 5 can be telescopic through a control system.
The control system 9 includes: control terminal, lighting device, big dipper positioner, under-deck environmental control system. And an independent power supply in the carbon fiber composite material main body supplies electric energy to the control system through a wire in sealing connection.
According to amphibious manned unmanned aerial vehicle, characterized by: the upper layer and the lower layer of the aviation organic glass panoramic window are respectively provided with a cabin door 10.
As shown in fig. 1, the following description is further provided in conjunction with the first embodiment:
the unmanned aerial vehicle parachute 8 is
The fiber material is folded and fixed on the carbon fiber composite material top plate 2 in a normal flying state.
When the machine is weightless, the parachute is automatically opened by the electronic system of the equipment, and the parachute can be opened through the independent manual switch under the condition that the power supply fails, and the independent manual switch is arranged below the carbon fiber composite material top plate 2.
The above description is a preferred embodiment of the present invention, and various modifications or improvements made to the solution of the present invention by those skilled in the art without departing from the design concept of the present invention shall fall within the protection scope of the present invention.
Claims (15)
1. Amphibious manned unmanned aerial vehicle includes: the parachute device comprises a machine body, a power device, a parachute device, a buffer moving device, a control system and a machine cabin door.
2. An amphibious drone according to claim 1, characterised in that: according to amphibious manned unmanned aerial vehicle, characterized by: the amphibious unmanned aerial vehicle can fly in the air and also can sail on water.
3. An amphibious drone according to claim 1, characterised in that: the aircraft organic glass panorama window comprises an aircraft organic glass panorama window body, a carbon fiber composite main machine body, a main frame body and a power supply, wherein the aircraft organic glass panorama window body is in a hemispherical shape, and the two hemispherical aircraft organic glass panorama window bodies are fixedly connected between the upper portion and the lower portion of the main machine body.
4. An amphibious drone according to claim 1, characterised in that: the aviation organic glass panoramic window is divided into an upper layer and a lower layer, and the aerial organic glass panoramic window can reach the upper layer space and the lower layer space by lifting up and down through the built-in seat.
5. An amphibious drone according to claim 1, characterised in that: the carbon fiber composite main machine body is in a ring shape.
6. An amphibious drone according to claim 1, characterised in that: the carbon fiber composite main machine body is provided with eight round holes, and each round hole is internally provided with a set of power device.
7. An amphibious drone according to claim 1, characterised in that: according to amphibious manned unmanned aerial vehicle, characterized by: the power device comprises a motor, a propeller, a generator and a power supply, wherein the propeller is fixedly arranged on a motor shaft, the power supply is arranged and sealed in the carbon fiber composite material main body, and the power supply is connected with the motor through an electric wire which is hermetically connected with the carbon fiber composite material main body.
8. An amphibious drone according to claim 1, characterised in that: according to amphibious manned unmanned aerial vehicle, characterized by: when the propeller works, kinetic energy can be transmitted to the generator through the transmission belt and converted into electric energy to charge the power supply.
9. An amphibious drone according to claim 1, characterised in that: the motor is a waterproof motor.
10. An amphibious drone according to claim 1, characterised in that: the propeller can change the power direction to control the driving direction by multi-directional rotation when flying or navigating.
11. An amphibious drone according to claim 1, characterised in that: according to amphibious manned unmanned aerial vehicle, characterized by: the parachute device is unmanned aerial vehicle parachute and carbon-fibre composite roof, and the unmanned aerial vehicle parachute passes through the carbon-fibre composite component connection locking on the carbon-fibre composite roof, and the parachute is automatic to be opened during emergency landing, and the manual opening device of accessible opens under the power failure state, and manual opening device installs under the carbon-fibre composite roof.
12. An amphibious drone according to claim 1, characterised in that: according to amphibious manned unmanned aerial vehicle, characterized by: the buffering mobile device comprises a buffering mechanism, eight carbon fiber composite material telescopic foot frames and eight spherical bottom wheels, wherein the buffering mechanism is arranged at the bottom of the aviation organic glass panoramic window, the eight carbon fiber composite material telescopic foot frames are arranged at the bottom of the buffering mechanism, and the eight carbon fiber composite material telescopic foot frames are respectively provided with one spherical bottom wheel.
13. An amphibious drone according to claim 1, characterised in that: according to amphibious manned unmanned aerial vehicle, characterized by: the eight carbon fiber composite material telescopic foot frames can be stretched through the control system.
14. An amphibious drone according to claim 1, characterised in that: the control system includes: control terminal, lighting device, big dipper positioner, under-deck environmental control system. And an independent power supply in the carbon fiber composite material main body supplies electric energy to the control system through a wire in sealing connection.
15. An amphibious drone according to claim 1, characterised in that: the upper layer and the lower layer of the aviation organic glass panoramic window are respectively provided with a cabin door.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910320926.1A CN111824413A (en) | 2019-04-21 | 2019-04-21 | Amphibious manned unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910320926.1A CN111824413A (en) | 2019-04-21 | 2019-04-21 | Amphibious manned unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN111824413A true CN111824413A (en) | 2020-10-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910320926.1A Pending CN111824413A (en) | 2019-04-21 | 2019-04-21 | Amphibious manned unmanned aerial vehicle |
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| Country | Link |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022261864A1 (en) * | 2021-06-16 | 2022-12-22 | 深圳市大疆创新科技有限公司 | Control method and apparatus for unmanned aerial vehicle system, and unmanned aerial vehicle system and storage medium |
-
2019
- 2019-04-21 CN CN201910320926.1A patent/CN111824413A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022261864A1 (en) * | 2021-06-16 | 2022-12-22 | 深圳市大疆创新科技有限公司 | Control method and apparatus for unmanned aerial vehicle system, and unmanned aerial vehicle system and storage medium |
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Application publication date: 20201027 |