CN106081106A - Wireless charging unmanned plane - Google Patents
Wireless charging unmanned plane Download PDFInfo
- Publication number
- CN106081106A CN106081106A CN201610439072.5A CN201610439072A CN106081106A CN 106081106 A CN106081106 A CN 106081106A CN 201610439072 A CN201610439072 A CN 201610439072A CN 106081106 A CN106081106 A CN 106081106A
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- China
- Prior art keywords
- unmanned plane
- wireless charging
- jib
- fuselage
- charging unmanned
- 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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- 235000001968 nicotinic acid Nutrition 0.000 claims abstract description 34
- 238000006243 chemical reaction Methods 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 210000003141 lower extremity Anatomy 0.000 claims description 2
- 239000011664 nicotinic acid Substances 0.000 claims description 2
- 230000005611 electricity Effects 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 description 6
- 238000005265 energy consumption Methods 0.000 description 3
- 238000012546 transfer Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000003592 biomimetic effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000013396 workstream Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/34—In-flight charging
- B64U50/35—In-flight charging by wireless transmission, e.g. by induction
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Power Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Toys (AREA)
Abstract
The present invention discloses a kind of wireless charging unmanned plane and includes fuselage, wing, Form of Bionics Mechanical Legs and the reception device being located on fuselage, described reception device is for receiving the energy that the energy emitting device being located at ground is launched, described Form of Bionics Mechanical Legs and fuselage bottom pivot joint.Technical scheme, by the energy emitting device receiving device tie surface being located on fuselage, makes unmanned plane possess longer cruising time, adds convenience and the experience property of user.
Description
Technical field
The present invention relates to a kind of wireless charging unmanned plane.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", utilizes radio robot and provides for oneself
The most manned aircraft that presetting apparatus is handled.At present, the range of unmanned plane has been widely used for military affairs, scientific research, the people
With three big fields, specifically in electric power, communication, meteorology, agricultural, ocean, explore, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement
The field application such as anti-smuggling, border patrol, public security anti-terrorism are the widest.More at present, there is short problem in cruising time in relevant unmanned plane,
Affect the experience property of its range of application and user.
Summary of the invention
The main object of the present invention is to provide a kind of wireless charging unmanned plane, it is intended to extends the cruising time of unmanned plane, carries
The experience property of high user.
For achieving the above object, the present invention propose wireless charging unmanned plane include fuselage, wing, Form of Bionics Mechanical Legs and
The reception device being located on fuselage, described reception device is for receiving the energy that the energy emitting device being located at ground is launched, institute
State Form of Bionics Mechanical Legs and fuselage bottom pivot joint.
Preferably, described reception device includes reception antenna and microwave rectifier, and described microwave rectifier will be for receiving
The microwave that antenna is collected is changed into HVDC electric energy.
Preferably, described microwave rectifier is cyclotron wave microwave rectifier.
Preferably, described reception antenna is arranged on Form of Bionics Mechanical Legs.
Preferably, described reception antenna is Form of Bionics Mechanical Legs.
Preferably, described Form of Bionics Mechanical Legs include the first jib with fuselage bottom pivot joint and with the first jib pivot joint
Second jib, described fuselage and the first jib junction, the first jib and the second jib junction are provided with servomotor and use
In the rotation realizing pivot points.
Preferably, the side towards wireless charging unmanned plane direction of advance of described second jib arm body is provided with wheel, institute
The motor driving vehicle wheel rotation it is provided with, described fuselage and the first jib junction, described first jib and the in stating the second jib
Two jib junctions are equipped with angle fixing device.
Preferably, Form of Bionics Mechanical Legs position faced by described fuselage bottom has a cavity formed from bottom notch,
Described cavity is used for housing described Form of Bionics Mechanical Legs.
Preferably, described chamber is taken in/released to described Form of Bionics Mechanical Legs along fuselage axis direction under the driving of servomotor
Body, it is achieved wireless charging unmanned plane is in ground run and the conversion of airflight two states.
Preferably, described fuselage, wing, Form of Bionics Mechanical Legs are carbon fiber structural.
In technical solution of the present invention, by the energy emitting device receiving device tie surface being located on fuselage, make nothing
Man-machine possessed longer cruising time, adds convenience and the experience property of user.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
In having technology to describe, the required accompanying drawing used is briefly described, it should be apparent that, the accompanying drawing in describing below is only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to
Other accompanying drawing is obtained according to the structure shown in these accompanying drawings.
Fig. 1 is the structural representation of wireless charging unmanned plane first embodiment of the present invention；
Fig. 2 is the structural representation of wireless charging unmanned plane the second embodiment of the present invention；
Fig. 3 is the schematic diagram at another visual angle of wireless charging unmanned plane in Fig. 1, and wherein Form of Bionics Mechanical Legs is not shown；
Fig. 4 is reception device and the operating diagram of ground energy emitting device of wireless charging unmanned plane of the present invention.
Drawing reference numeral illustrates:
The realization of the object of the invention, functional characteristics and advantage will in conjunction with the embodiments, are described further referring to the drawings.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.Base
Embodiment in the present invention, those of ordinary skill in the art obtained under not making creative work premise all its
His embodiment, broadly falls into the scope of protection of the invention.
It is to be appreciated that directional instruction in the embodiment of the present invention (such as up, down, left, right, before and after ...) is only used
In explaining relative position relation between each parts, motion conditions etc. under a certain particular pose (as shown in drawings), if should
When particular pose changes, then directionality instruction changes the most therewith.
It addition, in the present invention such as relating to the description of " first ", " second " etc. be only used for describe purpose, and it is not intended that
Indicate or imply its relative importance or the implicit quantity indicating indicated technical characteristic.Thus, define " first ",
The feature of " second " can express or implicitly include at least one this feature.In describing the invention, the containing of " multiple "
Justice is at least two, such as two, three etc., unless otherwise expressly limited specifically.
In the present invention, unless otherwise clearly defined and limited, term " connects ", " fixing " etc. should be interpreted broadly,
Such as, " fixing " can be fixing connection, it is also possible to be to removably connect, or integral；Can be to be mechanically connected, it is also possible to be
Electrical connection；Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, can be the connection or two of two element internals
The interaction relationship of individual element, unless otherwise clear and definite restriction.For the ordinary skill in the art, can basis
Concrete condition understands above-mentioned term concrete meaning in the present invention.
It addition, the technical scheme between each embodiment of the present invention can be combined with each other, but must be general with this area
Based on logical technical staff is capable of, when technical scheme combination occur conflicting maybe cannot realize time will be understood that this
The combination of technical scheme does not exists, the most not within the protection domain of application claims.
Refer to Fig. 1, the wireless charging unmanned plane provided in the present invention includes fuselage 10, wing 20, Form of Bionics Mechanical Legs 30
And the reception device 50 being located on fuselage 10, described reception device 50 is for receiving the energy emitting device 40 being located at ground
The energy penetrated, pivot joint bottom described Form of Bionics Mechanical Legs 30 and fuselage 10.
The wireless energy transfer system formed by the energy emitting device 40 on ground and reception device 50 is applied to the most non-
In the wireless charging scheme of permanent current row, equipment can be allowed to break away from the constraint of corded power transmission, according to the needs of applied environment from
By the orientation arranging charging equipment.Energy emitting device 40 is arranged on the ground, unmanned plane arranges reception device 50
Coordinate rechargeable battery (not shown), so that it may so that unmanned plane need not be parked in ground wiring charging, considerably increase flying of unmanned plane
The row time；The usage amount of the most disposable non-charging battery also can be greatly reduced, to economizing on resources and protecting environment to have the most very much
Profit.
Propeller or jet mode is used to advance, by arranging bionic mechanical in fuselage 10 bottom during unmanned plane airflight
Lower limb 30, makes unmanned plane at ground running, can enhance the environmental suitability of unmanned plane.
Preferably, described reception device 50 includes that reception antenna 51 and microwave rectifier 52, described microwave rectifier 52 are used
In the microwave that reception antenna 51 is collected is changed into HVDC electric energy.
The energy emitting device 40 being located at ground includes power supply 41, microwave generator 42 and launches antenna 43, described microwave
Generator 42 for being changed into microwave by the electric energy that power supply 41 transmits, then microwave transmission is gone out by launching antenna 43.
The microwave wireless energy transmission system that technical scheme uses can realize distance, powerful electric energy passes
Defeated, use microwave as the carrier of energy, due to the self-characteristic of microwave, its wavelength is comparatively short, directionality good, disperse is little, can
For realizing the remote transmission of electric energy.This described energy emitting device 40 includes power supply 41, microwave generator 42 and launches sky
Line 43, power supply 41 is the various power sources that ground can obtain, and includes but are not limited to the devices such as all kinds of battery, electromotor,
The clean energy resource converted especially from wind energy, solar energy, more agrees with the development topic of society environmental protection；Microwave occurs
Device 42, for by the electric energy from power supply 41, is changed into high-power, the microwave of high frequency, then by launching antenna 43 by microwave biography
Output is gone.
Accordingly, ground energy emitting device 40 collected by the reception antenna 51 receiving device 50 being located on fuselage 10
The microwave transmitted, then by microwave rectifier 52, the microwave collected is changed into the high straightening driven required for unmanned plane work
Stream electric energy, it is achieved that the whole work process of wireless energy transfer.
Preferably, described microwave rectifier 52 is cyclotron wave microwave rectifier.
Commutator is the Primary Component of wireless power transmission, and cyclotron wave microwave rectifier is applicable to energy high-power, high-tension
Transmission, the rectification efficiency of single tube is all close to 85%.The ultimate principle of cyclotron wave microwave rectifier is that fast circulating beam ripple is humorous
Shake resonance absorption microwave energy in chamber, and it is substantially DC source, is generally possible to quick self-protection during load overload, and
Can fast automatic recovery normally work when overload disappears.In use, input microwave frequency, resonator cavity frequency and cyclotron frequency three
Person should be as close possible to.
Preferably, described reception antenna 51 is arranged on Form of Bionics Mechanical Legs 30.
Reception antenna 51 is arranged on Form of Bionics Mechanical Legs 30 and can allow the reception antenna 50 will not be at the surface volume of fuselage 10
Overhang, it is ensured that the optimum pneumatic profile of unmanned plane, reduce air drag, reduce energy consumption.
Preferably, described reception antenna 51 is Form of Bionics Mechanical Legs 30.
As optimizing further, reception antenna 51 directly uses Form of Bionics Mechanical Legs 30, by the ground running parts of unmanned plane
Combine with wireless energy reception antenna, and Form of Bionics Mechanical Legs 30 can regulate and the angle of fuselage 10 pivot joint, allow reception sky
Line 51 reaches optimal microwave receiving effect, sets without the need for the structure optimization the most additionally arranging antenna, beneficially unmanned plane
Meter.Therefore, technical scheme by wireless energy transfer system being received device 50 and the combination of Form of Bionics Mechanical Legs 30,
Make unmanned plane possess longer cruising time, add convenience and the experience property of user.
Preferably, described Form of Bionics Mechanical Legs 30 include with fuselage 10 bottom pivot joint the first jib 31 and with the first jib
Second jib 32 of 31 pivot joints, described fuselage 10 and the first jib 31 junction, the first jib 31 and the second jib 32 junction
It is provided with servomotor (not shown) for realizing the rotation of pivot points.
The Form of Bionics Mechanical Legs 30 arranged bottom fuselage 10 is two-section jib form, can simulate the upright row of both legs of people
Walk, it is achieved that unmanned plane is in the convenience of ground running and practicality.
In a second embodiment, Fig. 2 is referred to, it is preferable that described second jib 32 arm body unmanned towards wireless charging
The side of machine direction of advance is provided with wheel 33, is provided with the motor (not shown) driving wheel 33 to rotate in described second jib 32,
Described fuselage 10 and the first jib 31 junction, described first jib 31 and the second jib 32 junction are equipped with the fixing dress of angle
Put.
Second jib 32 can rotate under the drive of servomotor, and the second jib 32 rotates to level, now car
Wheel 33 contacts with ground, and under motor drives, wheel 33 rotates and makes unmanned plane advance；And the first jib 31 also can be at servomotor
Relative fuselage 10 lower rotation under drive, to regulate the terrain clearance of unmanned plane, increases the unmanned plane obstacle when ground run
Handling capacity.The angle fixing device arranged between movable part, it is ensured that unmanned plane, at the attitude stabilization of ground run, carries
High safety.
Refer to Fig. 3, it is preferable that bottom described fuselage 10 in the face of Form of Bionics Mechanical Legs 30 position have one recessed from bottom
Falling into the cavity 60 formed, described cavity 60 is used for housing described Form of Bionics Mechanical Legs 30.
Form of Bionics Mechanical Legs 30 when unmanned plane takes off, can be housed in the cavity 60 of fuselage 10, reduces flight resistance, fall
Low energy consumption.When needs walking or reception microwave energy, Form of Bionics Mechanical Legs is put down.
Preferably, institute is taken in/released to described Form of Bionics Mechanical Legs 30 along fuselage 10 axis direction under the driving of servomotor
State cavity 60, it is achieved wireless charging unmanned plane is in ground run and the conversion of airflight two states.
Use the folding and unfolding of servomotor accurate control biomimetics pedipulator 30, make unmanned plane be accurately finished ground run and sky
The conversion of middle flight two states, improves safety and controllable property.
Preferably, described fuselage 10, wing 20 are carbon fiber structural, on the premise of ensureing structural strength, reduce weight
Amount, minimizing energy consumption.
The foregoing is only the preferred embodiments of the present invention, not thereby limit the scope of the claims of the present invention, every at this
Under the inventive concept of invention, utilize the equivalent structure transformation that description of the invention and accompanying drawing content are made, or directly/indirectly use
The technical field relevant at other is included in the scope of patent protection of the present invention.
Claims (10)
1. a wireless charging unmanned plane, it is characterised in that described wireless charging unmanned plane includes fuselage, wing, bionic mechanical
Lower limb and the reception device being located on fuselage, described reception device is for receiving the energy that the energy emitting device being located at ground is launched
Amount, described Form of Bionics Mechanical Legs and fuselage bottom pivot joint.
2. wireless charging unmanned plane as claimed in claim 1, it is characterised in that described reception device includes reception antenna and micro-
Ripple commutator, described microwave rectifier is for being changed into HVDC electric energy by the microwave that reception antenna is collected.
3. wireless charging unmanned plane as claimed in claim 2, it is characterised in that described microwave rectifier is that cyclotron wave microwave is whole
Stream device.
4. wireless charging unmanned plane as claimed in claim 2, it is characterised in that described reception antenna is arranged on Form of Bionics Mechanical Legs
On.
5. wireless charging unmanned plane as claimed in claim 2, it is characterised in that described reception antenna is Form of Bionics Mechanical Legs.
6. wireless charging unmanned plane as claimed in claim 1, it is characterised in that described Form of Bionics Mechanical Legs includes and fuselage bottom
First jib of pivot joint and the second jib with the first jib pivot joint, described fuselage and the first jib junction, the first jib
It is provided with servomotor for realizing the rotation of pivot points with the second jib junction.
7. wireless charging unmanned plane as claimed in claim 6, it is characterised in that described second jib arm body towards wireless charging
The side of electricity unmanned plane direction of advance is provided with wheel, is provided with the motor driving vehicle wheel rotation, described fuselage in described second jib
It is equipped with angle fixing device with the first jib junction, described first jib and the second jib junction.
8. wireless charging unmanned plane as claimed in claim 6, it is characterised in that Form of Bionics Mechanical Legs faced by described fuselage bottom
Position has a cavity formed from bottom notch, and described cavity is used for housing described Form of Bionics Mechanical Legs.
9. wireless charging unmanned plane as claimed in claim 8, it is characterised in that described Form of Bionics Mechanical Legs driving at servomotor
Take in/release described cavity along fuselage axis direction under Dong, it is achieved wireless charging unmanned plane is in ground run and airflight two
The conversion of the state of kind.
10. wireless charging unmanned plane as claimed in claim 1, it is characterised in that described fuselage, wing are carbon fiber knot
Structure.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610439072.5A CN106081106B (en) | 2016-06-17 | 2016-06-17 | Wireless unmanned aerial vehicle that charges |
| PCT/CN2016/107937 WO2017215200A1 (en) | 2016-06-17 | 2016-11-30 | Wirelessly-chargeable unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610439072.5A CN106081106B (en) | 2016-06-17 | 2016-06-17 | Wireless unmanned aerial vehicle that charges |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106081106A true CN106081106A (en) | 2016-11-09 |
| CN106081106B CN106081106B (en) | 2021-02-05 |
Family
ID=57237154
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610439072.5A Active CN106081106B (en) | 2016-06-17 | 2016-06-17 | Wireless unmanned aerial vehicle that charges |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106081106B (en) |
| WO (1) | WO2017215200A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017215200A1 (en) * | 2016-06-17 | 2017-12-21 | 深圳市元征科技股份有限公司 | Wirelessly-chargeable unmanned aerial vehicle |
| CN108873941A (en) * | 2018-08-29 | 2018-11-23 | 芜湖翼讯飞行智能装备有限公司 | Automatic cover control device and its application method in UAV Formation Flight |
| CN111226349A (en) * | 2017-08-21 | 2020-06-02 | 上海峰飞航空科技有限公司 | Tail tracking antenna |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102022115939B3 (en) | 2022-06-27 | 2023-09-28 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Charging system and method for air-based charging of electric aircraft |
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Also Published As
| Publication number | Publication date |
|---|---|
| WO2017215200A1 (en) | 2017-12-21 |
| CN106081106B (en) | 2021-02-05 |
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