CN107697276A - A kind of method and device for increasing multi-rotor aerocraft flying distance - Google Patents
A kind of method and device for increasing multi-rotor aerocraft flying distance Download PDFInfo
- Publication number
- CN107697276A CN107697276A CN201710842355.9A CN201710842355A CN107697276A CN 107697276 A CN107697276 A CN 107697276A CN 201710842355 A CN201710842355 A CN 201710842355A CN 107697276 A CN107697276 A CN 107697276A
- Authority
- CN
- China
- Prior art keywords
- rotor aerocraft
- rotor
- aerocraft
- connection end
- fuselage
- 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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Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
Abstract
A kind of method and device for increasing multi-rotor aerocraft flying distance, belong to technical field of aerospace, including control terminal, the first multi-rotor aerocraft and the second multi-rotor aerocraft；The control terminal wireless controls the first multi-rotor aerocraft and the second multi-rotor aerocraft；First multi-rotor aerocraft is provided with connection end, and connection end and the fuselage of the second multi-rotor aerocraft coincide, and connection end edge is provided with 4 grooves, and 4 axles with the second multi-rotor aerocraft coincide respectively.During first multi-rotor aerocraft flies with the second multi-rotor aerocraft, the dynamical system of only the first multi-rotor aerocraft starts, the dynamical system of second multi-rotor aerocraft is in holding state, a part of electric energy is saved for the second multi-rotor aerocraft, which adds the cruising time of the second multi-rotor aerocraft and flying distance.
Description
Technical field
A kind of method and device for increasing multi-rotor aerocraft flying distance, belongs to technical field of aerospace, more particularly to one
Kind increases the method and device of multi-rotor aerocraft flying distance.
Background technology
Traditional multi-rotor aerocraft is mostly using battery as the energy, because the capacity of battery is smaller, so cruising time
It is usually no more than 40 minutes, voyage is limited by very large, and this is also the short slab of multi-rotor aerocraft.
The content of the invention
The purpose of the present invention is to overcome the above-mentioned deficiency of traditional multi-rotor aerocraft, there is provided one kind increases more rotor flyings
The method and device of device flying distance.
A kind of method and device for increasing multi-rotor aerocraft flying distance, including control terminal, rotor flying more than first
Device and the second multi-rotor aerocraft；The control terminal wireless controls the first multi-rotor aerocraft and the second multi-rotor aerocraft；
First multi-rotor aerocraft is provided with connection end, and connection end and the fuselage of the second multi-rotor aerocraft coincide, and connects end edge
4 grooves are provided with, 4 axles with the second multi-rotor aerocraft coincide respectively.
When the second multi-rotor aerocraft needs execution task, the rotation of fuselage alignment more than first of the second multi-rotor aerocraft
The connection end of rotor aircraft, 4 grooves of 4 axles alignment connection end of the second multi-rotor aerocraft, then rotor more than first
Aircraft and the second multi-rotor aerocraft are combined.By controlling the multi-rotor aerocraft of terminal control first to take off, more than first
Rotor craft flies together with the second multi-rotor aerocraft, and the direction flown to is that the second multi-rotor aerocraft performs task
Direction, after the segment distance that flies, the electricity of the first multi-rotor aerocraft can just enable the first multi-rotor aerocraft return alone
Departure location is returned, at this moment, the dynamical system of the second multi-rotor aerocraft starts, until the second multi-rotor aerocraft can independently fly
When, the first multi-rotor aerocraft is toward declining, and the fuselage and connection end that make the second multi-rotor aerocraft depart from, rotor flying more than first
Device determines origin information by built-in GPS, then returns to takeoff point alone, the second multi-rotor aerocraft is with continuing the task of flying to
Point.
The beneficial effects of the invention are as follows：The machine to be flown using the first multi-rotor aerocraft with the second multi-rotor aerocraft
System, during the first multi-rotor aerocraft flies with the second multi-rotor aerocraft, only the first multi-rotor aerocraft
Dynamical system starts, and the dynamical system of the second multi-rotor aerocraft is in holding state, is saved for the second multi-rotor aerocraft
A part of electric energy, which adds the cruising time of the second multi-rotor aerocraft and flying distance.
Brief description of the drawings
Fig. 1 is the first multi-rotor aerocraft and the second multi-rotor aerocraft docking schematic diagram, and Fig. 2 is rotor flying more than first
The structural representation of device, Fig. 3 are the overlooking the structure diagrams of the first multi-rotor aerocraft.
Label in figure：The multi-rotor aerocrafts of 1- first, the multi-rotor aerocrafts of 2- second, 3- connection ends, 31- grooves, 4-
The fuselage of two multi-rotor aerocrafts, 5- control terminals, the fuselage of the multi-rotor aerocrafts of 6- first.
Embodiment
The present invention is illustrated below in conjunction with the accompanying drawings.
A kind of method and device for increasing multi-rotor aerocraft flying distance, including control terminal 5, rotor flying more than first
The multi-rotor aerocraft 2 of device 1 and second；Control first multi-rotor aerocraft of controlled in wireless 1 of terminal 5 and rotor flying more than second
Device 2；Connection end 3 is installed, connection end 3 and the fuselage 4 of the second multi-rotor aerocraft are kissed on first multi-rotor aerocraft 1
Close, the side of connection end 3 is provided with 4 grooves 31, and 4 axles with the second multi-rotor aerocraft coincide respectively.
When the second multi-rotor aerocraft 2 needs execution task, the fuselage 4 of the second multi-rotor aerocraft is aligned more than first
The connection end 3 of rotor craft 1,4 grooves 31 of 4 axles alignment connection end 3 of the second multi-rotor aerocraft 2, then the
Together with one multi-rotor aerocraft 1 is 2-in-1 with the second multi-rotor aerocraft.By controlling terminal 5 to control the first multi-rotor aerocraft 1
Take off, the first multi-rotor aerocraft 1 flies together with the second multi-rotor aerocraft 2, and the direction flown to is that rotor flies more than second
Row device 2 performs the direction of task, and after the segment distance that flies, the electricity of the first multi-rotor aerocraft 1 can just make to revolve first more
Rotor aircraft 1 can return to departure location alone, and at this moment, the dynamical system of the second multi-rotor aerocraft 2 starts, until more than second rotations
Rotor aircraft 2 can independent flight when, the first multi-rotor aerocraft 1 makes fuselage 4 and the connection of the second multi-rotor aerocraft toward declining
3 ends depart from, and the first multi-rotor aerocraft 1 determines origin information by built-in GPS, takeoff point then returned to alone, more than second
Rotor craft 2 continues task place of flying to.
Claims (2)
- A kind of 1. device for increasing multi-rotor aerocraft flying distance, it is characterised in that：Including control terminal (5), more than first rotations Rotor aircraft (1) and the second multi-rotor aerocraft (2)；It is described control terminal (5) first multi-rotor aerocraft of controlled in wireless (1) and Second multi-rotor aerocraft (2)；Connection end (3), connection end (3) and second are installed on first multi-rotor aerocraft (1) The fuselage (4) of multi-rotor aerocraft coincide, and connection end (3) side is provided with 4 grooves (31), respectively with the second multi-rotor aerocraft 4 axles coincide.
- 2. a kind of method for increasing multi-rotor aerocraft flying distance, is realized by the device described in claim 1, its It is characterised by：When the second multi-rotor aerocraft needs execution task, the fuselage of the second multi-rotor aerocraft is directed at more than first The connection end of rotor craft, 4 grooves of 4 axles alignment connection end of the second multi-rotor aerocraft, then more than first rotations Rotor aircraft and the second multi-rotor aerocraft are combined；By controlling the multi-rotor aerocraft of terminal control first to take off, first Multi-rotor aerocraft flies together with the second multi-rotor aerocraft, and the direction flown to is that the second multi-rotor aerocraft performs task Direction, after the segment distance that flies, the electricity of the first multi-rotor aerocraft can just enable the first multi-rotor aerocraft alone Departure location is returned to, at this moment, the dynamical system of the second multi-rotor aerocraft starts, until the second multi-rotor aerocraft can independently fly During row, the first multi-rotor aerocraft is toward declining, and the fuselage and connection end that make the second multi-rotor aerocraft depart from, and rotor flies more than first Row device determines origin information by built-in GPS, then returns to takeoff point alone, and the second multi-rotor aerocraft continues the task of flying to Place.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710842355.9A CN107697276A (en) | 2017-09-18 | 2017-09-18 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710842355.9A CN107697276A (en) | 2017-09-18 | 2017-09-18 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107697276A true CN107697276A (en) | 2018-02-16 |
Family
ID=61172904
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710842355.9A Withdrawn CN107697276A (en) | 2017-09-18 | 2017-09-18 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107697276A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7083142B2 (en) * | 2004-04-21 | 2006-08-01 | Sikorsky Aircraft Corporation | Compact co-axial rotor system for a rotary wing aircraft and a control system thereof |
| CN101875399A (en) * | 2009-10-30 | 2010-11-03 | 北京航空航天大学 | Tilt rotor aircraft adopting parallel coaxial dual rotors |
| CN205060020U (en) * | 2015-08-31 | 2016-03-02 | 深圳市飞研智能科技有限公司 | Promote two unmanned aerial vehicle of duration |
| CN106716273A (en) * | 2016-07-28 | 2017-05-24 | 深圳市大疆创新科技有限公司 | A multirotor unmanned aerial vehicle and a controlling method thereof |
-
2017
- 2017-09-18 CN CN201710842355.9A patent/CN107697276A/en not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7083142B2 (en) * | 2004-04-21 | 2006-08-01 | Sikorsky Aircraft Corporation | Compact co-axial rotor system for a rotary wing aircraft and a control system thereof |
| CN101875399A (en) * | 2009-10-30 | 2010-11-03 | 北京航空航天大学 | Tilt rotor aircraft adopting parallel coaxial dual rotors |
| CN205060020U (en) * | 2015-08-31 | 2016-03-02 | 深圳市飞研智能科技有限公司 | Promote two unmanned aerial vehicle of duration |
| CN106716273A (en) * | 2016-07-28 | 2017-05-24 | 深圳市大疆创新科技有限公司 | A multirotor unmanned aerial vehicle and a controlling method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180216 |
|
| WW01 | Invention patent application withdrawn after publication |