CN105416579A - Energy-saving unmanned aerial vehicle - Google Patents
Energy-saving unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105416579A CN105416579A CN201510934185.8A CN201510934185A CN105416579A CN 105416579 A CN105416579 A CN 105416579A CN 201510934185 A CN201510934185 A CN 201510934185A CN 105416579 A CN105416579 A CN 105416579A
- Authority
- CN
- China
- Prior art keywords
- energy
- flying wing
- conservation
- unmanned vehicle
- aerial vehicle
- 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
- 238000010168 coupling process Methods 0.000 claims description 27
- 238000005859 coupling reaction Methods 0.000 claims description 27
- 238000004134 energy conservation Methods 0.000 claims description 27
- 230000008878 coupling Effects 0.000 claims description 26
- 210000002683 foot Anatomy 0.000 claims description 6
- 238000000034 method Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 238000001514 detection method Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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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
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses an energy-saving unmanned aerial vehicle which comprises a circular truncated cone-shaped aerial vehicle main body (1), at least three flying wings (2) and a connecting ring (3), wherein one end of each flying wing (2) is fixedly connected on the outside wall of the aerial vehicle main body (1), and the other end of each flying wing (2) extends outwards along the radial direction of the aerial vehicle main body (1); the at least three flying wings (2) are uniformly arranged at intervals along the circumferential direction of the aerial vehicle main body (1); a flying propeller (4) is installed at the upper end part of the other end of each flying wing (2), and the connecting ring (3) is arranged below the aerial vehicle main body (1) and is sequentially connected with the bottom ends of the flying wings (2) along the circumferential direction to form a closed ring; and a layer of solar cell panel (6) is laid on the outer wall of the aerial vehicle main body (1), and the solar cell panel (6) is electrically connected with a switching circuit of the energy-saving unmanned aerial vehicle. The aerial vehicle is good in stability, strong in cruising ability and capable of using solar power supply as a power source for flying so as to save energy sources.
Description
Technical field
The present invention relates to unmanned vehicle field, particularly, relate to a kind of energy-conservation unmanned vehicle.
Background technology
Unmanned plane is the not manned aircraft utilizing radio telecommand or the process controller provided for oneself to handle, along with the continuous progress of science and technology, the development of unmanned air vehicle technique is more and more ripe, use more and more extensive, not only can be used for battle reconnaissance and supervision, positioning school are penetrated, injured the military missions such as assessment, electronic warfare, but also oneself is as target drone, also can be used for civilian, as border patrol, nuclear radiation detection, aerial photography, mineral exploration aviation, the condition of a disaster supervision, traffic patrolling, security monitoring etc.
And existing unmanned vehicle uses storage battery to carry out power supply supply, flying power is poor, and flight electric power supply is not enough for a long time, and flying distance is brief.
Therefore, the energy-conservation unmanned vehicle that a kind of good stability, flying power will be provided strong is badly in need of.
Summary of the invention
The object of this invention is to provide a kind of energy-conservation unmanned vehicle, this energy-conservation unmanned vehicle good stability, flying power are strong, can use solar powered as power supply flight, economize energy.
To achieve these goals, the invention provides a kind of energy-conservation unmanned vehicle, this energy-conservation unmanned vehicle comprises round table-like aircraft body, flying wing and coupling link; One end of flying wing is fixed on the lateral wall of aircraft body, and the other end stretches out along the radial direction of aircraft body; The quantity of flying wing is at least three and flying wing is arranged along the circumferential direction uniform intervals of aircraft body; The upper end of the other end of flying wing is provided with flight oar, coupling link be placed in aircraft body below and circumferentially direction be connected to form closed ring with the bottom of flying wing successively; Wherein, the outer wall of aircraft body is laid with one deck solar panel, solar panel is electrically connected with the switch circuit of energy-conservation unmanned vehicle.
Preferably, flying wing is flexible flying wing and can stretches along the radial direction of aircraft body.
Preferably, the connection between coupling link and flying wing is detachable connection.
Preferably, detachable connection, for being threaded, coupling link and flying wing bottom face being equipped with internal thread hole, coupling link can being solidly connected on flying wing by screw bolt passes internal thread hole.
Preferably, coupling link is rubber ring.
Preferably, the oar that flies is double bladed paddle or three leaf oars.
Preferably, this energy-conservation unmanned vehicle also comprises at least three feets, and feet circumferentially direction is disposed in an evenly spaced relation on the bottom face of aircraft body.
According to technique scheme, one end of flying wing is fixed on the lateral wall of aircraft body by the present invention, coupling link is utilized to be linked together by the other end of multiple flying wing, the position that multiple flying wing can be made to remain original by the power that involves of coupling link like this, maintain original angle each other, make whole aircraft can remain balance in flight course, stabilized flight.Meanwhile, the outer wall of aircraft body establishes solar panel, solar panel is electrically connected with the switch circuit of energy-conservation unmanned vehicle.Like this, when aircraft storage battery has enough batteries, storage battery is to aircraft supply regular power; When accumulator electric-quantity exhausts, the electric power stored by solar panel continues to power to aircraft, just greatly can extend the cruise duration of aircraft, makes its longer distance of can flying.
Other features and advantages of the present invention are described in detail in detailed description of the invention part subsequently.
Accompanying drawing explanation
Accompanying drawing is used to provide a further understanding of the present invention, and forms a part for specification sheets, is used from explanation the present invention, but is not construed as limiting the invention with detailed description of the invention one below.In the accompanying drawings:
Fig. 1 is the structural representation according to the energy-conservation unmanned vehicle in a kind of embodiment provided by the invention.
Description of reference numerals
1-aircraft body 2-flying wing
3-coupling link 4-flies oar
5-feet 6-solar panel
Detailed description of the invention
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is described in detail.Should be understood that, detailed description of the invention described herein, only for instruction and explanation of the present invention, is not limited to the present invention.
In the present invention, when not doing contrary explanation, the nouns of locality be included in term such as " top, bottoms " only represents the orientation of this term under normal service condition, or being commonly called as those skilled in the art's understanding, and should not be considered as the restriction to this term.
See Fig. 1, the invention provides a kind of energy-conservation unmanned vehicle, this energy-conservation unmanned vehicle comprises round table-like aircraft body 1, flying wing 2 and coupling link 3; One end of flying wing 2 is fixed on the lateral wall of aircraft body 1, and the other end stretches out along the radial direction of aircraft body 1; The quantity of flying wing 2 is at least three and flying wing 2 is arranged along the circumferential direction uniform intervals of aircraft body 1; The upper end of the other end of flying wing 2 is provided with flight oar 4, coupling link 3 be placed in aircraft body 1 below and circumferentially direction be connected to form closed ring with the bottom of flying wing 2 successively; Wherein, the outer wall of aircraft body 1 is laid with one deck solar panel 6, solar panel 6 is electrically connected with the switch circuit of energy-conservation unmanned vehicle.
Pass through technique scheme, one end of flying wing 2 is fixed on the lateral wall of aircraft body 1, coupling link 3 is utilized to be linked together by the other end of multiple flying wing 2, multiple flying wing 2 can be made to remain original position by the power that involves of coupling link 3 like this, maintain original angle each other, make whole aircraft can remain balance in flight course, stabilized flight.Meanwhile, the outer wall of aircraft body 1 is established solar panel 6, solar panel 6 is electrically connected with the switch circuit of energy-conservation unmanned vehicle.Like this, when aircraft storage battery has enough batteries, storage battery is to aircraft supply regular power; When accumulator electric-quantity exhausts, the electric power stored by solar panel 6 continues to power to aircraft, just greatly can extend the cruise duration of aircraft, makes its longer distance of can flying.
In present embodiment, in order to the flight that can adjust unmanned vehicle easily according to flight space size takes up room, make it can free flight in different spaces, preferably, flying wing 2 be flexible flying wing and can stretches along the radial direction of aircraft body 1.
In addition, for the ease of dismounting coupling link 3 to keep in repair aircraft body 1, preferably, the connection between coupling link 3 and flying wing 2 is detachable connection.
Above-mentioned detouchable connection mode can be any one connection mode fast and easily common in this area, but from controlling cost of product and alleviating the angle consideration of aircraft overall weight, preferably detachable connection is for being threaded, coupling link 3 and flying wing 2 bottom face are equipped with internal thread hole, coupling link 3 can be solidly connected on flying wing 2 by screw bolt passes internal thread hole.
When energy-conservation unmanned vehicle landing, once landing unstable flight device lack of equilibrium or ground relief easily make crooked coupling link 3 and the earth surface of causing of aircraft occur to abrade and even break, substantially reduce the service life of coupling link 3, in order to avoid the generation of above-mentioned situation, preferred coupling link 3 is rubber ring.
In addition, in order to obtain pulsation-free up current when flying oar 4 High Rotation Speed, keep the stability of aircraft, preferably, flight oar 4 is double bladed paddle or three leaf oars.
When aircraft drop to rugged jump area, in order to avoid colliding with in aircraft body 1, flying wing 2 or coupling link 3 and ground, extend the service life of aircraft, preferably, energy-conservation unmanned vehicle also comprises at least three feets 5, and feet 5 circumferentially direction is disposed in an evenly spaced relation on the bottom face of aircraft body 1.
Below the preferred embodiment of the present invention is described in detail by reference to the accompanying drawings; but; the present invention is not limited to the detail in above-mentioned embodiment; within the scope of technical conceive of the present invention; can carry out multiple simple variant to technical scheme of the present invention, these simple variant all belong to protection scope of the present invention.
It should be noted that in addition, each concrete technical characteristic described in above-mentioned detailed description of the invention, in reconcilable situation, can be combined by any suitable mode, in order to avoid unnecessary repetition, the present invention illustrates no longer separately to various possible array mode.
In addition, also can carry out combination in any between various different embodiment of the present invention, as long as it is without prejudice to thought of the present invention, it should be considered as content disclosed in this invention equally.
Claims (7)
1. an energy-conservation unmanned vehicle, is characterized in that, described energy-conservation unmanned vehicle comprises round table-like aircraft body (1), flying wing (2) and coupling link (3); One end of described flying wing (2) is fixed on the lateral wall of described aircraft body (1), and the other end stretches out along the radial direction of described aircraft body (1); The quantity of described flying wing (2) is at least three and described flying wing (2) is arranged along the circumferential direction uniform intervals of described aircraft body (1); The upper end of the other end of described flying wing (2) is provided with flight oar (4), described coupling link (3) be placed in described aircraft body (1) below and circumferentially direction be connected to form closed ring with the bottom of described flying wing (2) successively; Wherein, the outer wall of described aircraft body (1) is laid with one deck solar panel (6), described solar panel (6) is electrically connected with the switch circuit of described energy-conservation unmanned vehicle.
2. energy-conservation unmanned vehicle according to claim 1, is characterized in that, described flying wing (2) is flexible flying wing and can stretches along the radial direction of described aircraft body (1).
3. energy-conservation unmanned vehicle according to claim 1, is characterized in that, the connection between described coupling link (3) and flying wing (2) is detachable connection.
4. energy-conservation unmanned vehicle according to claim 3, it is characterized in that, described detachable connection is for being threaded, described coupling link (3) and flying wing (2) bottom face are equipped with internal thread hole, described coupling link (3) can be solidly connected on described flying wing (2) by internal thread hole described in screw bolt passes.
5. energy-conservation unmanned vehicle according to claim 1, is characterized in that, described coupling link (3) is rubber ring.
6. energy-conservation unmanned vehicle according to claim 1, is characterized in that, described flight oar (4) is double bladed paddle or three leaf oars.
7. energy-conservation unmanned vehicle according to claim 1, it is characterized in that, described energy-conservation unmanned vehicle also comprises at least three feets (5), and described feet (5) circumferentially direction is disposed in an evenly spaced relation on the bottom face of described aircraft body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510934185.8A CN105416579A (en) | 2015-12-14 | 2015-12-14 | Energy-saving unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510934185.8A CN105416579A (en) | 2015-12-14 | 2015-12-14 | Energy-saving unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105416579A true CN105416579A (en) | 2016-03-23 |
Family
ID=55495219
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510934185.8A Pending CN105416579A (en) | 2015-12-14 | 2015-12-14 | Energy-saving unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105416579A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892099A (en) * | 2017-03-15 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of strong energy-saving unmanned plane of endurance |
| CN107416196A (en) * | 2017-07-05 | 2017-12-01 | 南宁学院 | A kind of aileron short distance logistics unmanned plane of a main wing four |
| CN107458588A (en) * | 2017-07-05 | 2017-12-12 | 南宁学院 | A kind of aileron short distance logistics unmanned plane of a main wing six |
| CN109310056A (en) * | 2016-01-29 | 2019-02-05 | Jg创业企业有限责任公司 | The aircraft and system changed for weather |
| CN109459355A (en) * | 2018-12-11 | 2019-03-12 | 江西众安职业危害评价检测有限公司 | Long-range dust test device |
-
2015
- 2015-12-14 CN CN201510934185.8A patent/CN105416579A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109310056A (en) * | 2016-01-29 | 2019-02-05 | Jg创业企业有限责任公司 | The aircraft and system changed for weather |
| CN106892099A (en) * | 2017-03-15 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of strong energy-saving unmanned plane of endurance |
| CN106892099B (en) * | 2017-03-15 | 2019-01-29 | 广东创意双星科技股份有限公司 | A kind of energy-saving unmanned plane that cruising ability is strong |
| CN107416196A (en) * | 2017-07-05 | 2017-12-01 | 南宁学院 | A kind of aileron short distance logistics unmanned plane of a main wing four |
| CN107458588A (en) * | 2017-07-05 | 2017-12-12 | 南宁学院 | A kind of aileron short distance logistics unmanned plane of a main wing six |
| CN109459355A (en) * | 2018-12-11 | 2019-03-12 | 江西众安职业危害评价检测有限公司 | Long-range dust test device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160323 |