CN206520748U - A kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle - Google Patents
A kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN206520748U CN206520748U CN201720069823.9U CN201720069823U CN206520748U CN 206520748 U CN206520748 U CN 206520748U CN 201720069823 U CN201720069823 U CN 201720069823U CN 206520748 U CN206520748 U CN 206520748U
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Abstract
The utility model is applied to unmanned plane field, and there is provided a kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle, including unmanned machine host（5）, at least four rotors and propeller（7）, one end of the rotor is fixed on unmanned machine host（5）On, the other end is provided with motor（6）, the propeller（7）It is connected to motor（6）On, the unmanned machine host（5）On be fixed with oil electric mixed dynamic generator and ECU chips（3）, the oil electric mixed dynamic generator include fuel engines（1）, with the fuel engines（1）The generator of output end connection（2）, the generator（2）An output end connection motor（6）, another output end connection stand-by power supply（4）, the ECU chips（3）It is connected by throttle signal with the oil electric mixed dynamic engine.The utility model uses such scheme, solves unmanned plane when generator output electric energy is not enough, battery can be supplemented unmanned plane electric energy, and is returned safely.
Description
Technical field
The utility model is related to unmanned plane field, and in particular to multi-rotor unmanned aerial vehicle hybrid power system.
Background technology
The development in unmanned plane market in recent years, multi-rotor unmanned aerial vehicle is with excellent handling, easy care simple in construction and can
The advantages of convenience of VTOL, obtains rapidly the accreditation in market.Current multi-rotor unmanned aerial vehicle is main based on electronic, right lithium
The shortcomings of low energy densities and short service life of battery, seriously constrains it and is cruised in electric power, logistics transportation, public security fire-fighting, agriculture
Industry plant protection, mapping etc. field development.The utility model provides a kind of oil electric mixed dynamic scheme, merges the high-energy of fuel oil
Density, it is electrically driven (operated) to be precisely controlled, bring the cruising time of extremely low use cost and overlength.
Utility model content
The utility model purpose is to provide a kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle, it is intended to solve current nothing
The low energy densities and the short shortcoming of service life of man-machine simple use lithium battery power supply, are also solved and are supplied using fuel electric generator
The problem of unmanned plane energy supply of energy is not enough, the shortcoming of above-mentioned prior art seriously constrains it and cruised in electric power, and logistics transportation is public
Pacify fire-fighting, agricultural plant protection, mapping etc. field development.
The utility model is achieved in that including unmanned machine host, at least four rotors and propeller, the rotor
One end is fixed on unmanned machine host, and the other end is provided with motor, and the propeller is connected on motor, it is characterised in that：Institute
State and oil electric mixed dynamic generator and ECU chips are fixed with unmanned machine host, the oil electric mixed dynamic generator includes combustion
Oil turbine, the generator being connected with the fuel engines output end, the output end connection motor of the generating is another
Individual output end connects stand-by power supply, and the ECU chips are connected by throttle signal with engine.
The further scheme of the utility model is：Control loop, the ECU chips connection are installed on the unmanned machine host
Control loop.
The further scheme of the utility model is：The stand-by power supply is battery.
The utility model obtain beneficial effect be：Unmanned plane gives ECU cores by automated driving system feedback command first
Piece, coordinated allocation oil electric mixed dynamic engine output, reaches energy-saving effect, and secondly the oil electricity mixing of UAV flight is dynamic
Force engine, electrical power generators are driven by fuel engines, and electric energy is used for for stand-by power supply charging, prominent when needing to run into
It is its electric energy supplement by stand-by power supply during heat condition, two kinds of power save modes are combined, and have preferably reached the effect of energy-conservation, increase
Unmanned plane cruising time.
Brief description of the drawings
Fig. 1 is unmanned plane schematic diagram；
Fig. 2 is unmanned plane top view；
Fig. 3 is unmanned side view one；
Fig. 4 is unmanned side view two；
Fig. 5 is unmanned plane bottom view.
Embodiment
Reference：In diagram 1 be fuel engines, it is illustrated that in 2 be generator, it is illustrated that in 3 be ECU chips, it is illustrated that in 4
For stand-by power supply, it is illustrated that in 5 be unmanned machine host, it is illustrated that in 6 be motor, it is illustrated that in 7 be propeller.
The specific embodiment of the summary brief description of the drawings present invention.
As shown in Figures 1 and 5, the operation of fuel engines 1 drives generator 2 to generate electricity, and this electric energy is divided into two-way, all the way directly
Powered to unmanned plane, rotate motor 6, so as to drive propeller 7 to rotate, the power risen is provided for unmanned plane and changes appearance
State, carries out real time charging to stand-by power supply 4 all the way in addition.Stand-by power supply 4 can independently drive generator 2 to generate electricity and energize, and work as generating
When the electric energy of machine 2 meets flight and required, stand-by power supply 4 is not involved in work, is required when the electric energy of generator 2 can not meet flight
When, stand-by power supply 4 participates in electric energy supplement, and when fuel engines 1, which breaks down, to stop working in the air, stand-by power supply 4 can provide nothing
Required whole electric energy of man-machine flight, it is ensured that unmanned plane can be returned safely, stand-by power supply 4 can also be carried out when not flight
It is manual powered.
As shown in Figures 3 and 4, unmanned plane includes control loop, and control loop according to current flight attitude and will fly
Throttle commands are sent to ECU chips 3 by row task, while generator 2, which is motor 6, provides electric power, it is driven 7 turns of propeller
It is dynamic, lift is produced, the signal fed back according to ECU chips 3 is adjusted to the rotating speed of propeller 7, realizes stabilized flight, and
And save unnecessary power consumption.
As shown in Figures 1 and 2, the electric hybrid engine of oil is connected by throttle signal line with ECU chips 3, ECU chips 3
, can be according to the output of the extraneous factor coordinated allocation generators 2 such as the wind-force at scene and stand-by power supply 4 according to the instruction of automatic pilot
Power, reaches the purpose for saving electric power.
As shown in Fig. 1 and Fig. 4, the need for the oil electric mixed dynamic engine of unmanned plane can be according to varying environment, install
In the either above or below of unmanned plane.
Above content is to combine specific preferred embodiment further description made for the present invention, it is impossible to assert
The specific implementation of the present invention is confined to these explanations.For general technical staff of the technical field of the invention,
On the premise of not departing from present inventive concept, some simple deduction or replace can also be made, should all be considered as belonging to the present invention's
Protection domain.
Claims (5)
1. a kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle, including unmanned machine host（5）, at least four rotors and propeller（7）,
One end of the rotor is fixed on unmanned machine host（5）On, the other end is provided with motor（6）, the propeller（7）It is connected to electricity
Machine（6）On, the unmanned machine host（5）On be fixed with oil electric mixed dynamic generator and ECU chips（3）, the oil electricity mixing
Power electric generator includes fuel engines（1）, with the fuel engines（1）The generator of output end connection（2）, it is described to generate electricity
Machine（2）An output end connection motor（6）, another output end connection stand-by power supply（4）, the ECU chips（3）Pass through oil
Gate signal is connected with the oil electric mixed dynamic engine.
2. oil electric mixed dynamic multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The unmanned machine host
（5）On control loop, the ECU chips are installed（3）Connect control loop.
3. oil electric mixed dynamic multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The oil electric mixed dynamic
Engine is fixed on unmanned machine host（5）Top.
4. oil electric mixed dynamic multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The oil electric mixed dynamic
Engine is fixed on unmanned machine host（5）Lower section.
5. oil electric mixed dynamic multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The stand-by power supply（4）
For battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720069823.9U CN206520748U (en) | 2017-01-20 | 2017-01-20 | A kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201720069823.9U CN206520748U (en) | 2017-01-20 | 2017-01-20 | A kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle |
Publications (1)
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| CN206520748U true CN206520748U (en) | 2017-09-26 |
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| CN201720069823.9U Active CN206520748U (en) | 2017-01-20 | 2017-01-20 | A kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622398A (en) * | 2018-06-04 | 2018-10-09 | 广州市华科尔科技股份有限公司 | A kind of oil electricity is mixed to move multi-rotor unmanned aerial vehicle control system and control method |
| CN109319145A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with closed type fuselage |
| CN109319142A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned vehicle with closed type fuselage |
| CN109319144A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Aircraft with closed type fuselage |
| CN109319143A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with closed type fuselage |
| CN109319146A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Novel flight equipment |
| CN109319141A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Oily cutting with closed type fuselage changes aircraft |
| CN110697058A (en) * | 2019-11-26 | 2020-01-17 | 复旦大学 | Hybrid unmanned aerial vehicle |
| WO2020052106A1 (en) * | 2018-09-14 | 2020-03-19 | 广州市华科尔科技股份有限公司 | Compact long-endurance crop protecting unmanned aerial vehicle |
-
2017
- 2017-01-20 CN CN201720069823.9U patent/CN206520748U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622398A (en) * | 2018-06-04 | 2018-10-09 | 广州市华科尔科技股份有限公司 | A kind of oil electricity is mixed to move multi-rotor unmanned aerial vehicle control system and control method |
| CN109319145A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with closed type fuselage |
| CN109319142A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned vehicle with closed type fuselage |
| CN109319144A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Aircraft with closed type fuselage |
| CN109319143A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with closed type fuselage |
| CN109319146A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Novel flight equipment |
| CN109319141A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Oily cutting with closed type fuselage changes aircraft |
| WO2020052106A1 (en) * | 2018-09-14 | 2020-03-19 | 广州市华科尔科技股份有限公司 | Compact long-endurance crop protecting unmanned aerial vehicle |
| CN110697058A (en) * | 2019-11-26 | 2020-01-17 | 复旦大学 | Hybrid unmanned aerial vehicle |
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