CN107600438A - A kind of airborne tandem oil electric mixed dynamic system - Google Patents
A kind of airborne tandem oil electric mixed dynamic system Download PDFInfo
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- CN107600438A CN107600438A CN201710957558.2A CN201710957558A CN107600438A CN 107600438 A CN107600438 A CN 107600438A CN 201710957558 A CN201710957558 A CN 201710957558A CN 107600438 A CN107600438 A CN 107600438A
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- 239000007858 starting material Substances 0.000 claims abstract description 12
- 239000002828 fuel tank Substances 0.000 claims abstract description 7
- 239000004020 conductor Substances 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 5
- 238000010276 construction Methods 0.000 abstract description 4
- 230000005611 electricity Effects 0.000 description 6
- 239000003921 oil Substances 0.000 description 6
- 230000007812 deficiency Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000875 corresponding effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
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Abstract
The present invention relates to unmanned plane equipment technical field, and in particular to a kind of airborne tandem oil electric mixed dynamic system, it includes ASH controllers, engine, generator, reserve battery and power converter；ASH controllers are electrically connected with servomechanism, sensor one, sensor two, sensor three, sensor four, sensor five, sensor six, sensor seven respectively by wire；Servomechanism, fuel tank, starter, igniter by wire and start mechatronics respectively；The engine is electrically connected by the one end of wire respectively with sensor one, decelerator；The other end of the decelerator and generating mechatronics；The generator is electrically connected with sensor three, sensor five respectively by wire；It, which has, can provide stable voltage output and long-time high-power power exports, and system uses modular construction, ensure that later maintenance is simple and convenient, while have small volume, in light weight and high reliability.
Description
Technical field
The present invention relates to unmanned plane equipment technical field, and in particular to a kind of airborne tandem oil electric mixed dynamic system.
Background technology
The dynamical system of existing unmanned plane mainly has three kinds, i.e. engine power, battery power, engine battery parallel connection
Power etc..Engine power is mainly used in fixed-wing unmanned plane and depopulated helicopter, less for multi-rotor unmanned aerial vehicle.Battery power
It is mainly used in fixed-wing unmanned plane, depopulated helicopter, multi-rotor unmanned aerial vehicle and VTOL mixing wing unmanned plane etc..Engine
Cell parallel power is mainly used in multi-rotor unmanned aerial vehicle and VTOL mixing wing unmanned plane.Common structure is as shown in Figure 1；Hair
Motor battery parallel power operation principle is：In multi-rotor unmanned aerial vehicle application, engine carries as active force, driving propeller
For main lift；Battery, which is used as from power, motor, drives propeller to provide posture power, adjusts UAV Attitude.Vertical
In the application of landing mixing wing unmanned plane, engine is as fixed-wing mode power, and battery is as more rotor mode power.Above-mentioned knot
There are the following problems for the work system of structure：First is engine power：Drive mechanism is complicated, and maintenance work is heavy.Second is electricity
Pond power：Energy density is low.3rd is engine battery parallel power：Complicated, maintenance work is heavy, and weight is too big.
The content of the invention
In view of the defects and deficiencies of the prior art, the present invention intends to provide a kind of airborne tandem oil electricity mixing is dynamic
Force system, it, which has, can provide stable voltage output and long-time high-power power exports, and system uses modular construction, protects
It is simple and convenient to demonstrate,prove later maintenance, while there is small volume, in light weight and high reliability.
A kind of airborne tandem oil electric mixed dynamic system of the present invention, it includes ASH controllers, engine, hair
Motor, reserve battery and power converter；ASH controllers by wire respectively with servomechanism, sensor one, sensor two, pass
Sensor three, sensor four, sensor five, sensor six, sensor seven electrically connect；Servomechanism, fuel tank, starter, igniter
Respectively by wire with starting mechatronics；The engine is electrically connected by the one end of wire respectively with sensor one, decelerator
Connect；The other end of the decelerator and generating mechatronics；The generator by wire respectively with sensor three, sensor five
Electrical connection；The other end of the sensor three electrically connects with power converter；The power converter passes through wire and sensor
Seven electrical connections, the other end of sensor seven electrically connect with out connector；The igniter electrically connects with reserve battery；It is described standby
Electrically connected respectively with starter, sensor four, sensor six by wire with battery；The other end and power of the sensor four
Converter electrically connects.
Further, the ASH controllers are connected by data conductor with radio station/autopilot.
Further, the starter is electrically connected by wire with ground power supply.
After said structure, the present invention has the beneficial effect that：A kind of airborne tandem oil electricity mixing of the present invention is dynamic
Force system, it, which has, can provide stable voltage output and long-time high-power power exports, and system uses modular construction, protects
It is simple and convenient to demonstrate,prove later maintenance, while there is small volume, in light weight and high reliability.
【Brief description of the drawings】
Accompanying drawing described herein is for providing a further understanding of the present invention, forming the part of the application, but not
Inappropriate limitation of the present invention is formed, in the accompanying drawings：
Fig. 1 is the hybrid architecture schematic diagram of the present invention；
Description of reference numerals：
1st, ASH controllers；2nd, engine；3rd, generator；4th, reserve battery；5th, power converter；6th, sensor one；7th, sensor
Two；8th, sensor three；9th, sensor four；10th, sensor five；11st, sensor six；12nd, sensor seven；13rd, fuel tank；14th, watch
Take device；15th, starter；16th, igniter；17th, decelerator；18th, out connector；19th, radio station/autopilot；20th, ground power supply.
【Embodiment】
The present invention is described in detail below in conjunction with accompanying drawing and specific embodiment, and illustrative examples therein and explanation are only
For explaining the present invention, but it is not as a limitation of the invention.
As shown in figure 1, a kind of airborne tandem oil electric mixed dynamic system described in present embodiment, it includes
ASH controllers 1, engine 2, generator 3, reserve battery 4 and power converter 5；ASH controllers 1 are by wire respectively with watching
Take device 14, sensor 1, sensor 27, sensor 38, sensor 49, sensor 5 10, sensor 6 11, sensor seven
12 electrical connections；Servomechanism 14, fuel tank 13, starter 15, igniter 16 are electrically connected by wire with engine 2 respectively；It is described
Engine 2 is electrically connected by the one end of wire respectively with sensor 1, decelerator 17；The other end and hair of the decelerator 17
Motor 3 electrically connects；The generator 3 is electrically connected with sensor 38, sensor 5 10 respectively by wire；The sensor 38
The other end electrically connected with power converter 5；The power converter 5 is electrically connected by wire with sensor 7 12, sensor
7 12 other end electrically connects with out connector 18；The igniter 16 electrically connects with reserve battery 4；The reserve battery 4
Electrically connected respectively with starter 15, sensor 49, sensor 6 11 by wire；The other end and power of the sensor 49
Converter 5 electrically connects.
Further, the ASH controllers 1 are connected by data conductor with radio station/autopilot 19.
Further, the starter 15 is electrically connected by wire with ground power supply 20.
The function of each part composition in the present invention is as follows：
1）Engine is power electric generators.
2）Decelerator is used for matching suitable rotating speed for generator.
3）Generator converts kinetic energy into electric energy, exports to power converter.
4）Starter is used for starting engine, and its power supply may be derived from reserve battery, also may be from ground power supply.
5）Reserve battery is all power supply for electrical equipment before an engine is started.
6）Power converter is used for distributing the power of generator and reserve battery.
7）Fuel tank provides fuel for engine.
8）Igniter provides the ignition voltage required for normal work for engine.
9）Servomechanism receives the control signal of ASH controllers, and performs corresponding action.
10）ASH controllers gather sensor one, sensor two, sensor three, sensor four, sensor five, sensor
Six, the data of sensor seven, servomechanism control engine is driven after being handled, engine is operated in suitable operating mode.
11）Out connector is as external electric energy delivery outlet.
The operation principle of the present invention is as follows：
At work, sensor one gathers the data such as operating temperature, working speed of engine to the present invention, and feeds back to ASH controls
Device processed.Sensor two gathers the data such as Fuel Oil Remaining, pressure of fuel tank, and feeds back to ASH controllers.The collection hair of sensor three
The data such as the output voltage of motor, output current, and feed back to ASH controllers.Sensor four gathers the output electricity of reserve battery
The data such as pressure, output current, and feed back to ASH controllers.Sensor five gathers the data such as temperature, rotating speed of generator, and instead
Feed ASH controllers.Sensor six gathers the data such as the temperature of battery, and feeds back to ASH controllers.The collection synthesis of sensor seven
The data such as the voltage of output, electric current, and feed back to ASH controllers.
Power is exported to generator by decelerator after engine start.
When detecting generated output power deficiency by sensor three and sensor seven, power converter will turn on standby
With battery, generator and reserve battery are powered for equipment simultaneously, while the output of ASH controllers driving servomechanism increase engine
Power so that generator exports enough electric energy.
When detecting generator power surplus by sensor three and sensor seven, power converter will be switched off standby electricity
Pond, equipment power supply is individually for by generator, while ASH controllers driving servomechanism reduces engine output so that generate electricity
Machine reduces electric energy output.
When detecting reserve battery not enough power supply by sensor four, ASH controllers driving servomechanism increase engine
Power output so that generator exports unnecessary electric energy, and power converter is charged using unnecessary electric energy for reserve battery.
When ASH controllers detect that working temperature abnormity or working speed are abnormal by sensor one, will by radio station or
Autopilot returns alarm signal.
When ASH controllers detect that low on fuel or pressure are excessive by sensor two, radio station will be passed through or autopilot is returned
Pass alarm signal.
When ASH controllers by sensor five detect generator-temperature detection exception, will pass through radio station or autopilot passback report
Alert signal.
When ASH controllers detect reserve battery operation irregularity by sensor six, radio station will be passed through or autopilot returns
Alarm signal.
Described above is only the better embodiment of the present invention, therefore all constructions according to described in present patent application scope,
The equivalent change or modification that feature and principle are done, is included in the range of present patent application.
Claims (3)
- A kind of 1. airborne tandem oil electric mixed dynamic system, it is characterised in that：It includes ASH controllers, engine, generating Machine, reserve battery and power converter；ASH controllers by wire respectively with servomechanism, sensor one, sensor two, sensing Device three, sensor four, sensor five, sensor six, sensor seven electrically connect；Servomechanism, fuel tank, starter, igniter point Not by wire and start mechatronics；The engine is electrically connected by the one end of wire respectively with sensor one, decelerator； The other end of the decelerator and generating mechatronics；The generator is electric with sensor three, sensor five respectively by wire Connection；The other end of the sensor three electrically connects with power converter；The power converter passes through wire and sensor seven Electrical connection, the other end of sensor seven electrically connect with out connector；The igniter electrically connects with reserve battery；It is described standby Battery is electrically connected with starter, sensor four, sensor six respectively by wire；The other end of the sensor four turns with power Parallel operation electrically connects.
- A kind of 2. airborne tandem oil electric mixed dynamic system according to claim 1, it is characterised in that：The ASH controls Device processed is connected by data conductor with radio station/autopilot.
- A kind of 3. airborne tandem oil electric mixed dynamic system according to claim 1, it is characterised in that：The starter Electrically connected by wire with ground power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710957558.2A CN107600438A (en) | 2017-10-16 | 2017-10-16 | A kind of airborne tandem oil electric mixed dynamic system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710957558.2A CN107600438A (en) | 2017-10-16 | 2017-10-16 | A kind of airborne tandem oil electric mixed dynamic system |
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| Publication Number | Publication Date |
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| CN107600438A true CN107600438A (en) | 2018-01-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710957558.2A Pending CN107600438A (en) | 2017-10-16 | 2017-10-16 | A kind of airborne tandem oil electric mixed dynamic system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528735A (en) * | 2018-04-16 | 2018-09-14 | 中电科芜湖通用航空产业技术研究院有限公司 | Serial mixed power aircraft and its control method |
| CN117227984A (en) * | 2023-11-10 | 2023-12-15 | 山西彗星智能科技有限责任公司 | Control system for aviation hybrid energy system and control method thereof |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5899411A (en) * | 1996-01-22 | 1999-05-04 | Sundstrand Corporation | Aircraft electrical system providing emergency power and electric starting of propulsion engines |
| CN205239905U (en) * | 2015-12-08 | 2016-05-18 | 陈蜀乔 | From many rotor crafts of electricity generation oil -electricity hybrid vehicle |
| DE102014224637A1 (en) * | 2014-12-02 | 2016-06-02 | Georgi Atanasov | Hybrid electric propulsion system for an aircraft |
| CN207712304U (en) * | 2017-10-16 | 2018-08-10 | 北京大白科技有限公司 | A kind of airborne tandem hybrid power apparatus of oil and electricity |
-
2017
- 2017-10-16 CN CN201710957558.2A patent/CN107600438A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5899411A (en) * | 1996-01-22 | 1999-05-04 | Sundstrand Corporation | Aircraft electrical system providing emergency power and electric starting of propulsion engines |
| DE102014224637A1 (en) * | 2014-12-02 | 2016-06-02 | Georgi Atanasov | Hybrid electric propulsion system for an aircraft |
| CN205239905U (en) * | 2015-12-08 | 2016-05-18 | 陈蜀乔 | From many rotor crafts of electricity generation oil -electricity hybrid vehicle |
| CN207712304U (en) * | 2017-10-16 | 2018-08-10 | 北京大白科技有限公司 | A kind of airborne tandem hybrid power apparatus of oil and electricity |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528735A (en) * | 2018-04-16 | 2018-09-14 | 中电科芜湖通用航空产业技术研究院有限公司 | Serial mixed power aircraft and its control method |
| CN108528735B (en) * | 2018-04-16 | 2021-06-29 | 中电科芜湖通用航空产业技术研究院有限公司 | Tandem type hybrid power aircraft and control method thereof |
| CN117227984A (en) * | 2023-11-10 | 2023-12-15 | 山西彗星智能科技有限责任公司 | Control system for aviation hybrid energy system and control method thereof |
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Application publication date: 20180119 |