CN107054667A - A kind of multi-rotor unmanned aerial vehicle - Google Patents
A kind of multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN107054667A CN107054667A CN201710382837.0A CN201710382837A CN107054667A CN 107054667 A CN107054667 A CN 107054667A CN 201710382837 A CN201710382837 A CN 201710382837A CN 107054667 A CN107054667 A CN 107054667A
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- fuel
- rotor unmanned
- module
- 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
- 239000000446 fuel Substances 0.000 claims abstract description 24
- 238000004891 communication Methods 0.000 claims abstract description 12
- 239000002828 fuel tank Substances 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000010146 3D printing Methods 0.000 claims description 3
- 229920013657 polymer matrix composite Polymers 0.000 claims description 3
- 239000011160 polymer matrix composite Substances 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 description 2
- 208000019901 Anxiety disease Diseases 0.000 description 1
- 238000003457 Shi epoxidation reaction Methods 0.000 description 1
- 230000036506 anxiety Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
-
- 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
-
- 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; 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
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/11—Propulsion using internal combustion piston engines
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
The invention provides a kind of multi-rotor unmanned aerial vehicle, the unmanned plane is rotated come drive shaft by fuel engines and drives many rotor wing rotations to allow unmanned plane during flying to increase nobody cruising time while can also increase the load-carrying of the unmanned plane, the energy that electrical power generators are driven furthermore with fuel engines also to save controlling communication module to power.
Description
Technical field
The present invention relates to unmanned plane field, more particularly, to a kind of multi-rotor unmanned aerial vehicle.
Background technology
Simultaneously there are multiple positive incidence rotors to produce liter on multi-rotor aerocraft abbreviation unmanned plane, exactly one aircraft
Power, and overcome according to different directions rotation the aircraft of anti-twisted power, because multiple rotors are rotated to different directions, such torque
It is exactly zero, it might even be possible to which realization is let go hovering, manual control, which is got up, also to be operated freely, while pilot training time is shortened, is pacified
It is qualitative to also improve, if installing additional and flying control, then complicated gesture stability program can just be neglected, or even will can be arrived
The fixed-wing that place can be bought flies control program dislocation and come.
But current multi-rotor aerocraft is there is also shortcoming, and first, the cruising time of multi-rotor unmanned aerial vehicle extremely makes us
Cause anxiety, this has seriously constrained the development of unmanned air vehicle technique.The either current big boundary unmanned plane of occupation rate highest in the world, also
It is the unmanned plane of some sector applications, general civilian UAS endurance is more than 20 minutes, the unmanned plane system of sector application
Endurance of uniting also only has 1-2 hours.Moreover, it is very long not continue a journey completely on the market at present, or the technology infinitely continued a journey.Big boundary
Unmanned plane during flying at most maintains half an hour, and three or four pieces of batteries must be carried by generally going out, and Foreign Media issue article claims, nobody
The commercial promise of machine is limited to of short duration battery durable and lost contact risk；In addition, the mission payload of multi-rotor aerocraft is non-at present
Normal is small, and several hectograms just have arrived at the limit, if heavy burden index to be lifted, and what the size of its aircraft will greatly shies
People.
The content of the invention
The present invention provides a kind of raising endurance, wind loading rating and the multi-rotor unmanned aerial vehicle of load-carrying.
In order to solve the above technical problems, technical scheme is as follows：
A kind of multi-rotor unmanned aerial vehicle, including be from top to bottom sequentially connected control communication module, power plant module, fuel module
And head；The power plant module includes the generator and fairing, engine and multiple rotors that are electrically connected to each other, generator and
Engine is connected by power transmission shaft, and multiple rotors are fixed on power transmission shaft；Control communication module is electrically connected with fairing, fuel
Module is connected by fuel channel with engine.
Further, the control communication module includes control panel, GPS module and battery pack；Fairing and battery pack
Connection charges to battery, and battery pack is connected to charge to it with control panel, GPS module respectively；When fuel is used in fuel module
When to the greatest extent, battery pack also drives multiple rotor wing rotations to generator powered drive power transmission shaft.
Further, the fuel module is fuel tank, and the fuel tank is connected by oil pipe with engine.
Further, the engine is 5 cylinders, 7 cylinders or 9 cylinder radial engines.
Further, the number of the rotor is 4,6 or 8.
Further, the fuel tank is polymer matrix composites fuel tank.
Further, the generator is the microgenerator using 3D printing structure.
Relative to prior art, the beneficial effects of the invention are as follows：
The present invention is rotated come drive shaft by fuel engines and drives many rotor wing rotations to allow unmanned plane during flying can
To increase nobody cruising time while the load-carrying of the unmanned plane can also be increased, generating is driven furthermore with fuel engines
Machine generates electricity come the energy also saved controlling communication module to power.
Brief description of the drawings
Fig. 1 is structure chart of the present invention.
Embodiment
Accompanying drawing being given for example only property explanation, it is impossible to be interpreted as the limitation to this patent；
In order to more preferably illustrate the present embodiment, some parts of accompanying drawing have omission, zoomed in or out, and do not represent actual product
Size；
To those skilled in the art, it is to be appreciated that some known features and its explanation, which may be omitted, in accompanying drawing
's.
Technical scheme is described further with reference to the accompanying drawings and examples.
As shown in figure 1, a kind of multi-rotor unmanned aerial vehicle, including be from top to bottom sequentially connected control communication module 1, power mould
Block 2, fuel module 3 and head 4；The generator 2-1 and fairing that power plant module 2 includes being electrically connected to each other (do not show in figure
Go out), engine 2-2 and multiple rotor 2-4, generator 2-1 and engine 2-2 connected by power transmission shaft 2-3, multiple rotor 2-4
It is fixed on power transmission shaft 2-3；Control communication module 1 is electrically connected with fairing, and fuel module 3 is by fuel channel 5 with starting
Machine 2-2 connections.
Communication module 1 is controlled to include control panel, GPS module 1-1 and battery pack 1-2；Fairing is connected with battery pack 1-2
To charge to battery, battery pack 1-2 is connected to charge to it with control panel, GPS module 1-1 respectively；When fuel in fuel module 3
When using up, battery pack 1-2 also powers to generator 2-1 drives power transmission shaft 2-3 to drive multiple rotor wing rotations.
Fuel module 3 is fuel tank, and fuel tank is connected by oil pipe 5 with engine 2-2.
Engine 2-2 is 5 cylinders, 7 cylinders or 9 cylinder radial engines.
Rotor 2-4 number is 4,6 or 8.
Fuel tank 5 is polymer matrix composites fuel tank.
Generator 2-1 is the microgenerator using 3D printing structure.
The present invention is rotated come drive shaft 2-3 by fuel engines 2-2 and drives many rotor 2-4 rotations to allow nobody
Machine flight can increase nobody cruising time while can also increase the load-carrying of the unmanned plane, come furthermore with fuel engines
The energy that driving electrical power generators are also saved to be powered to control communication module.
The same or analogous part of same or analogous label correspondence；
Term the being given for example only property explanation of position relationship described in accompanying drawing, it is impossible to be interpreted as the limitation to this patent；
Obviously, the above embodiment of the present invention is only intended to clearly illustrate example of the present invention, and is not pair
The restriction of embodiments of the present invention.For those of ordinary skill in the field, may be used also on the basis of the above description
To make other changes in different forms.There is no necessity and possibility to exhaust all the enbodiments.It is all this
Any modifications, equivalent substitutions and improvements made within the spirit and principle of invention etc., should be included in the claims in the present invention
Protection domain within.
Claims (7)
1. a kind of multi-rotor unmanned aerial vehicle, it is characterised in that including be from top to bottom sequentially connected control communication module, power mould
Block, fuel module and head；The power plant module includes generator and fairing, engine and the multiple rotations being electrically connected to each other
The wing, generator and engine are connected by power transmission shaft, and multiple rotors are fixed on power transmission shaft；Control communication module and fairing
Electrical connection, fuel module is connected by fuel channel with engine.
2. multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that the control communication module include control panel,
GPS module and battery pack；Fairing is connected with battery pack to charge to battery, and battery pack connects with control panel, GPS module respectively
Fetch and it is powered；When fuel is used up in fuel module, battery pack also drives multiple rotations to generator powered drive power transmission shaft
The wing rotates.
3. multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that the fuel module is fuel tank, the fuel tank
It is connected by oil pipe with engine.
4. multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that the engine is 5 cylinders, 7 cylinders or 9 cylinder stars
Engine.
5. multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that the number of the rotor is 4,6 or 8
It is individual.
6. multi-rotor unmanned aerial vehicle according to claim 3, it is characterised in that the fuel tank is polymer matrix composites oil
Case.
7. multi-rotor unmanned aerial vehicle according to claim 3, it is characterised in that the generator is to use 3D printing knot
The microgenerator of structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710382837.0A CN107054667A (en) | 2017-05-26 | 2017-05-26 | A kind of multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710382837.0A CN107054667A (en) | 2017-05-26 | 2017-05-26 | A kind of multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107054667A true CN107054667A (en) | 2017-08-18 |
Family
ID=59610735
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710382837.0A Pending CN107054667A (en) | 2017-05-26 | 2017-05-26 | A kind of multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107054667A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107745514A (en) * | 2017-09-18 | 2018-03-02 | 北海勇士三维科技有限公司 | The unmanned plane manufacture method of 3D printing integrated molding |
| CN108128438A (en) * | 2018-01-16 | 2018-06-08 | 沈阳朗峰科技有限公司 | A kind of dynamic trapezoidal VTOL equipment of circle of oil |
| CN109229396A (en) * | 2018-08-29 | 2019-01-18 | 易瓦特科技股份公司 | Aircraft with novel power source |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080184906A1 (en) * | 2007-02-07 | 2008-08-07 | Kejha Joseph B | Long range hybrid electric airplane |
| CN204979256U (en) * | 2015-07-15 | 2016-01-20 | 北京虹湾威鹏信息技术有限公司 | Hybrid multiaxis rotor unmanned aerial vehicle |
| CN205168923U (en) * | 2015-11-11 | 2016-04-20 | 杭州深空实业股份有限公司 | Many rotor unmanned aerial vehicle hybrid power system |
| US20160137304A1 (en) * | 2014-11-14 | 2016-05-19 | Top Flight Technologies, Inc. | Micro hybrid generator system drone |
| CN205602114U (en) * | 2016-04-15 | 2016-09-28 | 深圳市卓尔思科技有限公司 | Unmanned aerial vehicle with multiple rotor wings |
| CN207141404U (en) * | 2017-05-26 | 2018-03-27 | 广东电网有限责任公司清远供电局 | A kind of multi-rotor unmanned aerial vehicle |
-
2017
- 2017-05-26 CN CN201710382837.0A patent/CN107054667A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080184906A1 (en) * | 2007-02-07 | 2008-08-07 | Kejha Joseph B | Long range hybrid electric airplane |
| US20160137304A1 (en) * | 2014-11-14 | 2016-05-19 | Top Flight Technologies, Inc. | Micro hybrid generator system drone |
| CN204979256U (en) * | 2015-07-15 | 2016-01-20 | 北京虹湾威鹏信息技术有限公司 | Hybrid multiaxis rotor unmanned aerial vehicle |
| CN205168923U (en) * | 2015-11-11 | 2016-04-20 | 杭州深空实业股份有限公司 | Many rotor unmanned aerial vehicle hybrid power system |
| CN205602114U (en) * | 2016-04-15 | 2016-09-28 | 深圳市卓尔思科技有限公司 | Unmanned aerial vehicle with multiple rotor wings |
| CN207141404U (en) * | 2017-05-26 | 2018-03-27 | 广东电网有限责任公司清远供电局 | A kind of multi-rotor unmanned aerial vehicle |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107745514A (en) * | 2017-09-18 | 2018-03-02 | 北海勇士三维科技有限公司 | The unmanned plane manufacture method of 3D printing integrated molding |
| CN108128438A (en) * | 2018-01-16 | 2018-06-08 | 沈阳朗峰科技有限公司 | A kind of dynamic trapezoidal VTOL equipment of circle of oil |
| CN109229396A (en) * | 2018-08-29 | 2019-01-18 | 易瓦特科技股份公司 | Aircraft with novel power source |
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| 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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170818 |