CN207712304U - A kind of airborne tandem hybrid power apparatus of oil and electricity - Google Patents
A kind of airborne tandem hybrid power apparatus of oil and electricity Download PDFInfo
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- CN207712304U CN207712304U CN201721324804.2U CN201721324804U CN207712304U CN 207712304 U CN207712304 U CN 207712304U CN 201721324804 U CN201721324804 U CN 201721324804U CN 207712304 U CN207712304 U CN 207712304U
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- sensor
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- conducting wire
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Abstract
The utility model is related to unmanned plane equipment technical fields, and in particular to a kind of airborne tandem hybrid power apparatus of oil and electricity, 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 conducting wire；Servomechanism, fuel tank, starter, igniter by conducting wire and start mechatronics respectively；The engine is electrically connected with one end of sensor one, retarder respectively by conducting wire；The other end of the retarder and power generation mechatronics；The generator is electrically connected with sensor three, sensor five respectively by conducting 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 having small, light-weight and high reliability.
Description
Technical field
The utility model is related to unmanned plane equipment technical fields, and in particular to a kind of airborne tandem oil electric mixed dynamic dress
It sets.
Background technology
There are mainly three types of the dynamical systems of existing unmanned plane, i.e. engine power, battery power, and engine battery is simultaneously
The power that links etc..Engine power is mainly used for fixed-wing unmanned plane and unmanned helicopter, is used for multi-rotor unmanned aerial vehicle less.Battery is dynamic
Power is mainly used for fixed-wing unmanned plane, unmanned helicopter, multi-rotor unmanned aerial vehicle and VTOL mixing wing unmanned plane etc..Start
Machine battery parallel power is mainly used for multi-rotor unmanned aerial vehicle and VTOL mixing wing unmanned plane.Common structure is as shown in Fig. 1；
Engine battery parallel power operation principle is：In multi-rotor unmanned aerial vehicle application, engine drives propeller as active force
Main lift is provided；Battery is used as from power, and driving motor drives propeller to provide posture power, adjusts UAV Attitude.It is hanging down
In straight landing mixing wing unmanned plane application, engine is as fixed-wing mode power, and battery is as more rotor mode power.It is above-mentioned
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
Battery power：Energy density is low.Third is engine battery parallel power：Complicated, maintenance work is heavy, and weight is too big.
Invention content
The purpose of this utility model is that it is in view of the drawbacks of the prior art and insufficient, it is mixed to provide a kind of airborne tandem oil electricity
Power plant is closed, it, which has, can provide stable voltage output and long-time high-power power exports, and system uses modularization knot
Structure ensures that later maintenance is simple and convenient, while having small, light-weight and high reliability.
A kind of airborne tandem hybrid power apparatus of oil and electricity described in the utility model, it includes ASH controllers, starts
Machine, generator, reserve battery and power converter；ASH controllers by conducting wire respectively with servomechanism, sensor one, sensor
Two, sensor three, sensor four, sensor five, sensor six, sensor seven are electrically connected；Servomechanism, fuel tank, starter, point
Firearm by conducting wire and starts mechatronics respectively；The engine passes through conducting wire one end with sensor one, retarder respectively
Electrical connection；The other end of the retarder and power generation mechatronics；The generator by conducting wire respectively with sensor three, sensing
Device five is electrically connected；The other end of the sensor three is electrically connected with power converter；The power converter passes through conducting wire and biography
Sensor seven is electrically connected, and the other end of sensor seven is electrically connected with out connector；The igniter is electrically connected with reserve battery；Institute
Reserve battery is stated to be electrically connected with starter, sensor four, sensor six respectively by conducting wire；The other end of the sensor four with
Power converter is electrically connected.
Further, the ASH controllers are connect by data conductor with radio station/autopilot.
Further, the starter is electrically connected by conducting wire with ground power supply.
With the above structure, the utility model has the beneficial effect that：A kind of airborne tandem oil described in the utility model
Electricity mixed power device, it, which has, can provide stable voltage output and long-time high-power power exports, and system uses module
Change structure, ensures that later maintenance is simple and convenient, while there is small, light-weight and high reliability.
【Description of the drawings】
Attached drawing described herein is to be used to provide a further understanding of the present invention, and constitutes one of the application
Point, but do not constitute improper limits to the present invention, in the accompanying drawings：
Fig. 1 is the hybrid architecture schematic diagram of the utility model；
Reference sign：
1, ASH controllers；2, engine；3, generator；4, reserve battery；5, power converter；6, sensor one；7, it passes
Sensor two；8, sensor three；9, sensor four；10, sensor five；11, sensor six；12, sensor seven；13, fuel tank；
14, servomechanism；15, starter；16, igniter；17, retarder；18, out connector；19, radio station/autopilot；20, ground
Power supply.
【Specific implementation mode】
Be described in detail the utility model below in conjunction with attached drawing and specific embodiment, illustrative examples therein with
And explanation is only used for explaining the utility model, but be not intended to limit the scope of the present invention.
As shown in Figure 1, a kind of airborne tandem hybrid power apparatus of oil and electricity described in present embodiment, it includes
ASH controllers 1, engine 2, generator 3, reserve battery 4 and power converter 5；ASH controllers 1 by conducting wire respectively with watch
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 conducting wire with engine 2 respectively；It is described
Engine 2 is electrically connected with one end of sensor 1, retarder 17 respectively by conducting wire；The other end and hair of the retarder 17
Motor 3 is electrically connected；The generator 3 is electrically connected with sensor 38, sensor 5 10 respectively by conducting wire；The sensor 38
The other end be electrically connected with power converter 5；The power converter 5 is electrically connected by conducting wire with sensor 7 12, sensor
7 12 other end is electrically connected with out connector 18；The igniter 16 is electrically connected with reserve battery 4；The reserve battery 4
It is electrically connected respectively with starter 15, sensor 49, sensor 6 11 by conducting wire；The other end and power of the sensor 49
Converter 5 is electrically connected.
Further, the ASH controllers 1 are connect by data conductor with radio station/autopilot 19.
Further, the starter 15 is electrically connected by conducting wire with ground power supply 20.
The function of each component composition in the utility model is as follows：
1）Engine is power electric generators.
2）Retarder is used for matching suitable rotating speed for generator.
3）Generator converts the kinetic energy into electrical energy, output to power converter.
4）Starter is used for starting engine, and 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 normal work required ignition voltage for engine.
9）Servomechanism receives the control signal of ASH controllers, and executes corresponding action.
10）ASH controllers acquire sensor one, sensor two, sensor three, sensor four, sensor five, sensor
Six, the data of sensor seven drive servomechanism to control engine, engine are made to be operated in suitable operating mode after being handled.
11）Out connector is as external electric energy delivery outlet.
The operation principle of the utility model is as follows：
When the utility model at work, sensor one acquires the operating temperature of engine, the data such as working speed, and feeds back
Give ASH controllers.Sensor two acquires the Fuel Oil Remaining of fuel tank, the data such as pressure, and feeds back to ASH controllers.Sensor
The output voltage of three acquisition generators, the data such as output current, and feed back to ASH controllers.Sensor four acquires reserve battery
Output voltage, data such as output current, and feed back to ASH controllers.Sensor five acquires the temperature of generator, the number such as rotating speed
According to, and feed back to ASH controllers.Sensor six acquires the data such as the temperature of battery, and feeds back to ASH controllers.Sensor seven
The voltage of the comprehensive output of acquisition, the data such as electric current, and feed back to ASH controllers.
Power is exported to generator by retarder 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 ASH controllers driving servomechanism increases the output of 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 is individually for equipment power supply by generator, while ASH controllers driving servomechanism reduces engine output so that power generation
Machine reduces electric energy output.
When detecting reserve battery not enough power supply by sensor four, ASH controllers drive servomechanism to increase engine
Output power so that generator exports extra electric energy, and power converter is charged using extra 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 or autopilot passback will be passed through
Alarm signal.
The above description is only a preferred embodiment of the present invention, therefore all according to described in the utility model patent application range
The equivalent change or modification done of structure, feature and principle, be included in the scope of the utility model patent application.
Claims (3)
1. a kind of airborne tandem hybrid power apparatus of oil and electricity, it is characterised in that：It includes ASH controllers, engine, power generation
Machine, reserve battery and power converter；ASH controllers by conducting wire respectively with servomechanism, sensor one, sensor two, sensing
Device three, sensor four, sensor five, sensor six, sensor seven are electrically connected；Servomechanism, fuel tank, starter, igniter point
Not by conducting wire and starting mechatronics；The engine is electrically connected with one end of sensor one, retarder respectively by conducting wire；
The other end of the retarder and power generation mechatronics；The generator is electric with sensor three, sensor five respectively by conducting wire
Connection；The other end of the sensor three is electrically connected with power converter；The power converter passes through conducting wire and sensor seven
Electrical connection, the other end of sensor seven are electrically connected with out connector；The igniter is electrically connected with reserve battery；It is described spare
Battery is electrically connected with starter, sensor four, sensor six respectively by conducting wire；The other end of the sensor four turns with power
Parallel operation is electrically connected.
2. a kind of airborne tandem hybrid power apparatus of oil and electricity according to claim 1, it is characterised in that：The ASH controls
Device processed is connect by data conductor with radio station/autopilot.
3. a kind of airborne tandem hybrid power apparatus of oil and electricity according to claim 1, it is characterised in that：The starter
It is electrically connected with ground power supply by conducting wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721324804.2U CN207712304U (en) | 2017-10-16 | 2017-10-16 | A kind of airborne tandem hybrid power apparatus of oil and electricity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721324804.2U CN207712304U (en) | 2017-10-16 | 2017-10-16 | A kind of airborne tandem hybrid power apparatus of oil and electricity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207712304U true CN207712304U (en) | 2018-08-10 |
Family
ID=63063935
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721324804.2U Expired - Fee Related CN207712304U (en) | 2017-10-16 | 2017-10-16 | A kind of airborne tandem hybrid power apparatus of oil and electricity |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207712304U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107600438A (en) * | 2017-10-16 | 2018-01-19 | 北京大白科技有限公司 | A kind of airborne tandem oil electric mixed dynamic system |
-
2017
- 2017-10-16 CN CN201721324804.2U patent/CN207712304U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107600438A (en) * | 2017-10-16 | 2018-01-19 | 北京大白科技有限公司 | A kind of airborne tandem oil electric mixed dynamic system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180810 Termination date: 20201016 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |