CN205837209U - A kind of integrated form power multiaxis unmanned plane - Google Patents
A kind of integrated form power multiaxis unmanned plane Download PDFInfo
- Publication number
- CN205837209U CN205837209U CN201620697287.2U CN201620697287U CN205837209U CN 205837209 U CN205837209 U CN 205837209U CN 201620697287 U CN201620697287 U CN 201620697287U CN 205837209 U CN205837209 U CN 205837209U
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- China
- Prior art keywords
- unmanned plane
- unit
- input
- outfan
- integrated form
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- 238000002485 combustion reaction Methods 0.000 claims abstract description 23
- 230000005611 electricity Effects 0.000 claims abstract description 11
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 11
- 229910052744 lithium Inorganic materials 0.000 claims description 11
- 239000002828 fuel tank Substances 0.000 claims description 6
- 230000005855 radiation Effects 0.000 claims description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 3
- 239000003921 oil Substances 0.000 abstract description 6
- 239000000295 fuel oil Substances 0.000 abstract description 3
- 238000013021 overheating Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 abstract description 2
- 238000001514 detection method Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 210000003169 central nervous system Anatomy 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
Classifications
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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
- B64U50/11—Propulsion using internal combustion piston engines
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/31—Supply or distribution of electrical power generated by photovoltaics
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Secondary Cells (AREA)
Abstract
The utility model discloses a kind of integrated form power multiaxis unmanned plane, it includes internal combustion engine, motor, charge storage unit and electrical driving unit, internal combustion engine is used to drive electrical power generators to provide energy, owing to the energy density ratio of fuel oil is high for electrical driving unit and charge storage unit；Use driven by power aircraft flight to be not required to the frame for movement of complexity, alleviate aircraft weight；The combination of the energy-provision way of oil electricity one, substantially prolongs unmanned plane voyage, and this utility model is additionally provided with radiator fan simultaneously, can be to generator heat-radiation by radiator fan, preventing generator overheating from damaging, in sum, this utility model achieves unmanned plane reliable and stable oceangoing voyage flight.This utility model, as a kind of integrated form power multiaxis unmanned plane, is widely used in unmanned air vehicle technique field.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, particularly relates to a kind of integrated form power multiaxis unmanned plane.
Background technology
In recent years, along with the popularization of unmanned plane application, application is constantly expanded, and different industries different field is to unmanned plane
Performance requirement is not quite similar, but be intended to the flight time can be the longest, be limited to current main flow unmanned plane power scheme
Various technical bottlenecks, the flight time all do not reaches the expected value of people.Existing power solution mainly has the most several: (1)
Polymer chargeable lithium cell, this is the power mode that the most most multiaxis rotor wing unmanned aerial vehicle uses, and flight controls response
Hurry up, simple in construction, light, its shortcoming is that the flight time is short, and the charging interval is long.(2) two strokes or four stroke fuel engines, use
When multiaxis unmanned plane, its shortcoming is mechanism's complexity, heaviness, easy break-down, is difficult to maintaining.(3) turbojet,
Its shortcoming is the same, the most expensive, debugging difficulty is big, service life is short.
Utility model content
In order to solve above-mentioned technical problem, the purpose of this utility model is to provide a kind of simple in construction, long boat stablizes safety
Integrated form power multiaxis unmanned plane.
This utility model be the technical scheme is that a kind of integrated form power multiaxis unmanned plane, including unmanned plane body,
Described unmanned plane this most internal be provided with generator unit, charge storage unit, fly to control unit and electrical driving unit, described in fly to control unit
Outfan is connected with the input of electrical driving unit, described in fly control unit be connected with generator unit, described generator unit and storage
Electric unit connects, and the outfan of described generator unit is connected with the input of electrical driving unit, the output of described charge storage unit
End respectively with the input of electrical driving unit and fly the input of control unit and be connected；Described electricity generation system includes internal combustion engine, oil
Case, radiator fan, electromotor and rectification module, described internal combustion engine is connected with fuel tank by oil pipe, the output of described internal combustion engine is turned round
Square is connected with electromotor input torque；Described radiator fan for electricity generation module heat radiation, its input defeated with flight control system
Go out end to connect；The outfan of described electromotor is connected with the input of electrical driving unit by rectification module.
Further, described charge storage unit includes that lithium battery and balance are filled, and the outfan of described generator unit is filled by balance
Connect with the input of lithium battery.
Further, described charge storage unit also includes that solar electrical energy generation module, described solar electrical energy generation module are layed in nothing
On man-machine body, the input that the outfan of described solar electrical energy generation module is filled with lithium battery by balance is connected.
Further, described generator unit also includes throttle steering wheel and tachoscope, and described tachoscope is interior with display for detection
Combustion engine rotating speed, described throttle steering wheel is used for controlling internal-combustion engine rotational speed, the outfan of described tachoscope and the input flying control unit
Connecting, the input of described throttle steering wheel is connected with the outfan flying to control unit.
Further, described generator unit also includes that temperature sensor, described temperature sensor are arranged at electromotor surface,
Its outfan is connected with flying control module.
Further, described electrical driving unit includes motor and propeller, the output moment of torsion of described motor and spiral
Oar connects.
The beneficial effects of the utility model are: this utility model is provided with internal combustion engine, motor, charge storage unit and electric power and drives
Moving cell, uses internal combustion engine to drive electrical power generators to provide energy, due to the energy of fuel oil for electrical driving unit and charge storage unit
Metric density ratio is high；Use driven by power aircraft flight to be not required to the frame for movement of complexity, alleviate aircraft weight；The confession of oil electricity one
The combination of energy mode, substantially prolongs unmanned plane voyage, and this utility model is additionally provided with radiator fan simultaneously, passes through radiation air
Generator heat-radiation can be prevented generator overheating from damaging by fan, and in sum, it is reliable and stable far that this utility model achieves unmanned plane
Boat flight.
Accompanying drawing explanation
Below in conjunction with the accompanying drawings detailed description of the invention of the present utility model is described further:
Fig. 1 is the structural representation of this utility model one specific embodiment.
Detailed description of the invention
It should be noted that in the case of not conflicting, the embodiment in the application and the feature in embodiment can phases
Combination mutually.
As it is shown in figure 1, a kind of integrated form power multiaxis unmanned plane, including unmanned plane body, described unmanned plane is the most internal to be set
Be equipped with generator unit, charge storage unit, fly to control unit and electrical driving unit, described in fly the outfan controlling unit and driven by power list
Unit input connect, described in fly control unit be connected with generator unit, described generator unit is connected with charge storage unit, described generating
The outfan of unit is connected with the input of electrical driving unit, the outfan of described charge storage unit respectively with electrical driving unit
Input and fly control unit input connect；Described electricity generation system include internal combustion engine, fuel tank, radiator fan, electromotor and
Rectification module, described internal combustion engine is connected with fuel tank by oil pipe, the output moment of torsion of described internal combustion engine connects with electromotor input torque
Connect；Described radiator fan is for being connected with the outfan of flight control system to electricity generation module heat radiation, its input；Described electromotor
Outfan is connected with the input of electrical driving unit by rectification module.
Its operation principle is: use internal combustion engine to drive electrical power generators to provide energy for electrical driving unit and charge storage unit
Amount, owing to the energy density ratio of fuel oil is high；Use driven by power aircraft flight to be not required to the frame for movement of complexity, alleviate aircraft weight
Amount；The combination of the energy-provision way of oil electricity one, therefore substantially prolongs unmanned plane voyage, and this utility model is additionally provided with simultaneously
Radiator fan, can prevent generator overheating from damaging generator heat-radiation by radiator fan.Said supply unit by with electric power
Driver element connection is possible not only under special circumstances as standby power source, is connected with electromotor simultaneously and is also used as
The internal combustion engine start energy.
Being further used as preferred embodiment, described charge storage unit includes that lithium battery and balance are filled, described generator unit
Outfan fill input with lithium battery by balance and connect.The use longevity that battery charging can be extended battery is filled by balance
Life.
Being further used as preferred embodiment, described charge storage unit also includes solar electrical energy generation module, the described sun
Can be layed on unmanned plane body by electricity generation module, the outfan of described solar electrical energy generation module by balance fill with lithium battery defeated
Enter end to connect, can be to lithium cell charging by solar electrical energy generation module so that unmanned plane during flying cost reduces, environmental protection and energy saving.
Being further used as preferred embodiment, described generator unit also includes throttle steering wheel and tachoscope, described rotating speed
Table is used for detecting and shows that internal-combustion engine rotational speed, described throttle steering wheel are used for controlling internal-combustion engine rotational speed, the outfan of described tachoscope
Being connected with the input flying to control unit, the input of described throttle steering wheel is connected with the outfan flying to control unit.By self
The system components such as fuel tank throttle steering wheel turn over offer motive power by internal-combustion engine.Its tachoscope can detect engine speed, so
Afterwards rotary speed information is fed back to fly to control unit, by flying control unit, control signal to throttle steering wheel, and then control internal-combustion engine
Rotating speed.
Being further used as preferred embodiment, described generator unit also includes temperature sensor, described temperature sensing
Device is arranged at electromotor surface, and its outfan is connected with flying control module, is passed by temperature sensor detection generator-temperature detection information
It is defeated by and flies to control unit, when temperature is too high, flies to control unit and can strengthen heat radiation dynamics to prevent by controlling the rotating speed of radiator fan
Electromotor damages because of overheated.
Being further used as preferred embodiment, described electrical driving unit includes electron speed regulator, motor and spiral
Oar, the output moment of torsion of described motor is connected drive propeller rotational with propeller provides lift for unmanned plane, is adjusted by electronics
Speed device, to motor speed adjusting.
Described flying controls the central nervous system that unit is whole scheme, and its effect is to collect the number that each sensing unit gathers
According to, and export various control instruction, plan and perform various aerial mission.Fly flying of the sensor unit survey aircraft in control
Row attitude also exports round-off order and makes the driving force motor of aircraft be maintained at the rotating speed of needs to electronic speed regulation itself and throttle steering wheel
On.
It is above preferable enforcement of the present utility model is illustrated, but the invention is not limited to described reality
Executing example, those of ordinary skill in the art also can make all equivalent changes on the premise of this utility model spirit
Shape or replacement, deformation or the replacement of these equivalents are all contained in the application claim limited range.
Claims (6)
1. an integrated form power multiaxis unmanned plane, including unmanned plane body, it is characterised in that: this internal setting of described unmanned plane
Have generator unit, charge storage unit, fly to control unit and electrical driving unit, described in fly to control outfan and the electrical driving unit of unit
Input connect, described in fly to control unit and be connected with generator unit, described generator unit is connected with charge storage unit, described generates electricity singly
Unit outfan be connected with the input of electrical driving unit, the outfan of described charge storage unit respectively with electrical driving unit
Input and the input flying to control unit connect；
Described electricity generation system includes that internal combustion engine, fuel tank, radiator fan, electromotor and rectification module, described internal combustion engine pass through oil pipe
Be connected with fuel tank, the output moment of torsion of described internal combustion engine is connected with electromotor input torque；Described radiator fan is for giving generating mould
Block heat radiation, its input are connected with the outfan of flight control system；The outfan of described electromotor is driven with electric power by rectification module
The input of moving cell connects.
Integrated form power multiaxis unmanned plane the most according to claim 1, it is characterised in that: described charge storage unit includes lithium electricity
Pond and balance are filled, and the outfan of described generator unit fills the input with lithium battery by balance and connects.
Integrated form power multiaxis unmanned plane the most according to claim 2, it is characterised in that: described charge storage unit also includes
Solar electrical energy generation module, described solar electrical energy generation module is layed on unmanned plane body, the output of described solar electrical energy generation module
The input filled with lithium battery by balance is held to be connected.
Integrated form power multiaxis unmanned plane the most according to claim 3, it is characterised in that: described generator unit also includes oil
Door steering wheel and tachoscope, described tachoscope is used for detecting and shows that internal-combustion engine rotational speed, described throttle steering wheel are used for controlling internal combustion engine
Rotating speed, the outfan of described tachoscope with fly control unit input is connected, the input of described throttle steering wheel with fly control unit
Outfan connect.
Integrated form power multiaxis unmanned plane the most according to claim 4, it is characterised in that: described generator unit also includes
Temperature sensor, described temperature sensor is arranged at electromotor surface, and its outfan is connected with flying control module.
Integrated form power multiaxis unmanned plane the most according to claim 5, it is characterised in that: described electrical driving unit includes
Motor and propeller, the output moment of torsion of described motor is connected with propeller.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620697287.2U CN205837209U (en) | 2016-07-04 | 2016-07-04 | A kind of integrated form power multiaxis unmanned plane |
| PCT/CN2016/090571 WO2018006439A1 (en) | 2016-07-04 | 2016-07-20 | Integrated power multi-axis unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620697287.2U CN205837209U (en) | 2016-07-04 | 2016-07-04 | A kind of integrated form power multiaxis unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205837209U true CN205837209U (en) | 2016-12-28 |
Family
ID=58150028
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620697287.2U Active CN205837209U (en) | 2016-07-04 | 2016-07-04 | A kind of integrated form power multiaxis unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN205837209U (en) |
| WO (1) | WO2018006439A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018133511A1 (en) * | 2017-01-23 | 2018-07-26 | 北京瑞深航空科技有限公司 | Hybrid-powered unmanned vehicle |
| CN109204844A (en) * | 2018-09-19 | 2019-01-15 | 沈观清 | Near space unmanned plane dynamical system and hybrid power method |
| CN111032507A (en) * | 2017-06-04 | 2020-04-17 | 阿里·图任 | Motor-assisted balance control in a drone with an engine |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455697A (en) * | 2020-12-11 | 2021-03-09 | 重庆工程职业技术学院 | Novel temperature control system of oil-electricity hybrid power water unmanned aerial vehicle |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106414238B (en) * | 2014-03-13 | 2019-12-31 | 多韧系统有限责任公司 | Drone configuration and battery augmentation for drone internal combustion engine, and related systems and methods |
| US9376208B1 (en) * | 2015-03-18 | 2016-06-28 | Amazon Technologies, Inc. | On-board redundant power system for unmanned aerial vehicles |
| CN104843181B (en) * | 2015-04-10 | 2017-10-20 | 桂林航龙科讯电子技术有限公司 | A kind of oil electric mixed dynamic fixed-wing VUAV system |
| 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 |
| CN205248881U (en) * | 2015-12-07 | 2016-05-18 | 重庆瑞升康博电气有限公司 | Unmanned aerial vehicle intelligent charging machine |
| CN105620765A (en) * | 2015-12-29 | 2016-06-01 | 苏州妙旋无人机应用有限公司 | Co-axis dual-rotor UAV (Unmanned Aerial Vehicle) hybrid power system |
-
2016
- 2016-07-04 CN CN201620697287.2U patent/CN205837209U/en active Active
- 2016-07-20 WO PCT/CN2016/090571 patent/WO2018006439A1/en active Application Filing
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018133511A1 (en) * | 2017-01-23 | 2018-07-26 | 北京瑞深航空科技有限公司 | Hybrid-powered unmanned vehicle |
| JP2019519414A (en) * | 2017-01-23 | 2019-07-11 | 北京瑞深航空科技有限公司Ｂｅｉｊｉｎｇ Ｒｉｃｈｅｎｐｏｗｅｒ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．， Ｌｔｄ． | Hybrid power source drone |
| CN111032507A (en) * | 2017-06-04 | 2020-04-17 | 阿里·图任 | Motor-assisted balance control in a drone with an engine |
| CN109204844A (en) * | 2018-09-19 | 2019-01-15 | 沈观清 | Near space unmanned plane dynamical system and hybrid power method |
| CN109204844B (en) * | 2018-09-19 | 2020-12-29 | 沈观清 | Near space unmanned aerial vehicle power system and hybrid power method |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018006439A1 (en) | 2018-01-11 |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |