CN114524092A - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN114524092A CN114524092A CN202011235947.2A CN202011235947A CN114524092A CN 114524092 A CN114524092 A CN 114524092A CN 202011235947 A CN202011235947 A CN 202011235947A CN 114524092 A CN114524092 A CN 114524092A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- wing
- horn
- battery
- wings
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 claims abstract description 11
- 238000004806 packaging method and process Methods 0.000 abstract description 3
- 230000007547 defect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 241000120551 Heliconiinae Species 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
Images
Classifications
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- 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
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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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/293—Foldable or collapsible rotors or rotor supports
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/244—Secondary casings; Racks; Suspension devices; Carrying devices; Holders characterised by their mounting method
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Toys (AREA)
Abstract
The invention discloses an unmanned aerial vehicle, which comprises a vehicle body, wings and a battery, wherein the vehicle body is provided with a mounting space for mounting the battery; the battery is detachably mounted in the battery mounting space; the wing is rotatably arranged on the fuselage and can be folded in the battery installation space after the battery is detached from the fuselage. Compared with the prior art, the unmanned aerial vehicle can rotate the wings to the battery installation space when not in use, so that the size of the unmanned aerial vehicle is greatly reduced, and the problems of packaging and transportation of the existing unmanned aerial vehicle are effectively solved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with rotatable wings.
Background
The existing unmanned aerial vehicle has the defects that the whole size of the unmanned aerial vehicle is large due to long wings, so that the unmanned aerial vehicle is inconvenient to package and transport.
In view of the above problems, the existing solutions include: 1. the wings are detachably arranged on the unmanned aerial vehicle body, and when the unmanned aerial vehicle is not in use, the wings are detached from the unmanned aerial vehicle body so as to reduce the size, but the wings need to be detached and arranged for many times, so that the electric connection between the wings and the unmanned aerial vehicle body is influenced, and the stability of the unmanned aerial vehicle is reduced; 2. the rotary wing is adopted, the wing is rotationally attached to the position near the fuselage in a non-use state so as to reduce the volume, but the folded wing still occupies a certain space.
Therefore, it is necessary to improve the existing structure of the unmanned aerial vehicle and provide an unmanned aerial vehicle which is convenient to package and transport.
Disclosure of Invention
One of the purposes of the invention is to overcome the defects of the prior art and provide an unmanned aerial vehicle convenient for packaging and transportation.
The invention discloses a specific scheme of an unmanned aerial vehicle, which comprises the following steps:
an unmanned aerial vehicle comprises a body, wings and a battery, wherein the body is provided with a battery installation space; the battery is detachably mounted in the battery mounting space; the wing is rotatably arranged on the fuselage and can be folded in the battery installation space after the battery is detached from the fuselage.
Further, the wings at least comprise two symmetrically arranged front wings and two symmetrically arranged rear wings.
In the optimization scheme of this embodiment, the front wings are installed at the same height of the fuselage, the rear wings are installed at another height of the fuselage, and the front wings and the rear wings can be overlapped up and down after being folded into the battery installation space.
Optionally, the front wing comprises a horn and a motor installed below the horn, the rear wing comprises a horn and a motor installed above the horn, and the height of the front wing installed on the fuselage is lower than the height of the two rear wings installed on the fuselage.
Optionally, the front wing comprises a horn and a motor installed above the horn, the rear wing comprises a horn and a motor installed below the horn, and the height of the front wing installed on the fuselage is higher than the height of the two rear wings installed on the fuselage.
Furthermore, a landing device is installed at the bottom of the fuselage, and support frames are arranged on the two symmetrically arranged front wings and/or the two symmetrically arranged rear wings.
Further, the cloud platform is installed to unmanned aerial vehicle's fuselage front end.
Further, two obstacle avoidance fisheye lenses which are symmetrically arranged are installed above the unmanned aerial vehicle body.
Compared with the prior art, the unmanned aerial vehicle can rotate the wings of the unmanned aerial vehicle to the battery installation space in the non-use state, so that the size of the unmanned aerial vehicle is greatly reduced, and the problems of packaging and transportation of the existing unmanned aerial vehicle are effectively solved.
Drawings
Fig. 1 is a schematic diagram of a drone of a preferred embodiment of the present invention.
Fig. 2 is a schematic diagram of the drone of fig. 1 with the battery removed.
Fig. 3 is a schematic view of the wing of fig. 2 rotated into the battery receiving space.
Fig. 4 is another perspective view of fig. 1.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The invention will be further explained in detail with reference to the drawings and the specific embodiments.
Example 1
Fig. 1 to 4 are schematic views of a drone according to a preferred embodiment of the present invention. The unmanned aerial vehicle 100 in this embodiment includes a fuselage 1, a front wing 2, a rear wing 3, a battery 4, an obstacle avoidance fisheye lens 5, a cradle head 6, and a landing device 7.
Fuselage 1 constitutes unmanned aerial vehicle 100's main part, is equipped with on it to be used for battery installation space, specifically is the breach department on the fuselage 1, in addition, still installs key components and parts such as sensor, control circuit on the fuselage.
The front wing 2 comprises two parts, which are symmetrically installed on the fuselage 1, and the front wing 2 comprises a horn 21, a motor 22 and a rotating blade (not shown in the figure), wherein one end of the horn 21 is rotatably connected to the fuselage 1. In the present embodiment, the motor 22 is mounted below the horn 21, and a rotary blade (not shown in the figure) is mounted on a power output shaft of the motor 22; two front wings 2 are arranged at the lower position of the fuselage 1 and are at the same height.
The rear wing 3 comprises two, symmetrically installed on the fuselage 1, and the rear wing 3 comprises a horn 31, a motor 32, a rotating blade (not shown in the figure) and a support rod 33, wherein one end of the horn 31 is rotatably connected to the fuselage 1. In the present embodiment, the motor 32 is installed above the horn 31, the rotating blade (not shown in the figure) is installed on the power output shaft of the motor 32, and the support rod 33 is installed below the horn 31 to form a three-point support with the land buffer 7 for landing of the drone 100; two rear wings 3 are arranged at the upper position of the fuselage 1 and are at the same height. Referring to fig. 3, after the front wing 2 and the rear wing 3 are folded into the battery installation space, the front wing 2 is located below the rear wing 3; in addition, because the motor 22 of the front wing 2 is installed below the horn 21, and the motor 32 of the rear wing 3 is installed above the horn 31, no space needs to be reserved for the motors (22, 32) between the horn 21 of the front wing 2 and the horn 31 of the rear wing 3, and then the two horns (21, 31) can be attached together, so that the overall structure of the folded front wing 2 and the folded rear wing 3 is more compact.
The battery 4 is a rechargeable battery, which is detachably mounted in a battery mounting space on the body 1.
Obstacle avoidance fisheye lenses 5 are symmetrically arranged on the body 1 and face upward, and are used for detecting obstacles above the body 1.
The cradle head 6 is installed in front of the body 1 for mounting a camera to implement aerial photography.
Example 2
This example is substantially the same as example 2, except that: the front wing 2 is arranged at the upper position of the fuselage 1, and the motor 22 of the front wing 2 is arranged above the horn 21; the rear wing 3 is arranged at a position lower than the fuselage 1, and the motor 32 of the rear wing 3 is arranged below the horn 31. Through the arrangement, the whole structure of the folded front wing 2 and the folded rear wing 3 is more compact.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (8)
1. The utility model provides an unmanned aerial vehicle, includes fuselage, wing and battery, its characterized in that:
the machine body is provided with a battery installation space;
the battery is detachably mounted in the battery mounting space;
the wing is rotatably arranged on the fuselage and can be folded in the battery installation space after the battery is detached from the fuselage.
2. A drone according to claim 1, characterised in that:
the wings at least comprise two symmetrically arranged front wings and two symmetrically arranged rear wings.
3. A drone according to claim 2, characterized in that:
the front wing is installed at the same height of the fuselage, the rear wing is installed at the other height of the fuselage, and the front wing and the rear wing can be overlapped up and down after being folded into the battery installation space.
4. A drone according to claim 3, characterised in that:
the front wing comprises a horn and a motor arranged below the horn, the rear wing comprises a horn and a motor arranged above the horn, and the height of the front wing arranged on the fuselage is lower than the height of the two rear wings arranged on the fuselage.
5. A drone according to claim 3, characterised in that:
the front wing comprises a horn and a motor arranged above the horn, the rear wing comprises a horn and a motor arranged below the horn, and the front wing is arranged on the fuselage and is higher than the two rear wings.
6. A drone according to claim 2, characterized in that:
and the landing device is arranged at the bottom of the fuselage, and the two symmetrically arranged front wings and/or the two symmetrically arranged rear wings are provided with supporting frames.
7. A drone according to claim 1, characterised in that:
the cloud platform is installed to unmanned aerial vehicle's fuselage front end.
8. A drone according to claim 1, characterised in that:
two obstacle avoidance fisheye lenses symmetrically arranged are installed above the unmanned aerial vehicle body.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011235947.2A CN114524092A (en) | 2020-11-09 | 2020-11-09 | Unmanned plane |
| PCT/CN2021/129486 WO2022096012A1 (en) | 2020-11-09 | 2021-11-09 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011235947.2A CN114524092A (en) | 2020-11-09 | 2020-11-09 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114524092A true CN114524092A (en) | 2022-05-24 |
Family
ID=81457528
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011235947.2A Pending CN114524092A (en) | 2020-11-09 | 2020-11-09 | Unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN114524092A (en) |
| WO (1) | WO2022096012A1 (en) |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206427261U (en) * | 2017-01-16 | 2017-08-22 | 蔡波 | One kind folds aircraft |
| GB201704375D0 (en) * | 2017-03-20 | 2017-05-03 | Swarm Systems Ltd | Folding propeller |
| KR102323447B1 (en) * | 2017-06-08 | 2021-11-08 | 삼성전자주식회사 | Transformable unmanned aerial vehicle |
| CN108513563B (en) * | 2017-08-30 | 2021-12-21 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN209366441U (en) * | 2018-10-31 | 2019-09-10 | 国网宁夏电力有限公司检修公司 | A kind of wing Collapsible multifunctional unmanned plane |
| CN209553496U (en) * | 2019-02-22 | 2019-10-29 | 郑顺发 | A kind of four axis aircrafts |
-
2020
- 2020-11-09 CN CN202011235947.2A patent/CN114524092A/en active Pending
-
2021
- 2021-11-09 WO PCT/CN2021/129486 patent/WO2022096012A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2022096012A1 (en) | 2022-05-12 |
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