CN108313305A - A kind of unmanned vehicle engine with generating function - Google Patents
A kind of unmanned vehicle engine with generating function Download PDFInfo
- Publication number
- CN108313305A CN108313305A CN201711406461.9A CN201711406461A CN108313305A CN 108313305 A CN108313305 A CN 108313305A CN 201711406461 A CN201711406461 A CN 201711406461A CN 108313305 A CN108313305 A CN 108313305A
- Authority
- CN
- China
- Prior art keywords
- power
- management system
- accumulator
- generator
- engine
- 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.)
- Withdrawn
Links
- 230000005611 electricity Effects 0.000 claims abstract description 10
- 238000001514 detection method Methods 0.000 claims abstract description 3
- 238000010248 power generation Methods 0.000 claims description 11
- 230000008878 coupling Effects 0.000 claims description 9
- 238000010168 coupling process Methods 0.000 claims description 9
- 238000005859 coupling reaction Methods 0.000 claims description 9
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000009187 flying Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
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- B64D27/026—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The present invention provides a kind of unmanned vehicle engine with generating function, including engine, generator, power-supply management system, charge controller, accumulator, the engine and the movable connection of generator, the generator is electrically connected with power-supply management system, generator exports induced field current to power-supply management system, power-supply management system converts alternating current to direct current electricity output, the direct current of the accumulator store power management system output, the charging situation of the charge controller detection accumulator, the electric current that charge controller controls accumulator input break-make situation.While the present invention will be by that will use engine to propeller output driving power, power is exported to generator, after the process converted by electric current, electric power is stored to the use of supply flight computer, the driving force service efficiency for improving engine, saves related energy consumption.
Description
【Technical field】
The present invention relates to the technical fields of the technical field of unmanned plane, especially unmanned vehicle engine.
【Background technology】
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Unmanned plane is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition：Nobody is straight
The machine of liter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol this several major class.
Current all unmanned plane during flyings are powered using the accumulator of itself institute's band to complete machine all devices substantially, electric power storage
The density in pond is very big, and dress is very uneconomical aboard.And aircraft is bigger, and the power of electronic equipment is bigger, energy consumption
It is higher, so battery is also heavier.
【Invention content】
The purpose of the present invention is exactly to solve the problems of the prior art, proposes that a kind of unmanned plane with generating function starts
While capable of making engine to propeller output driving power, power is exported to generator for machine.The process converted by electric current
Afterwards, the use that electric power is stored to supply flight computer, improves the driving force service efficiency of engine, saves the related energy
Consumption.
To achieve the above object, the present invention proposes a kind of unmanned vehicle engine with generating function, including engine,
Generator, power-supply management system, charge controller, accumulator, the engine and the movable connection of generator, the generator
It is electrically connected with power-supply management system, generator exports induced field current to power-supply management system, and power-supply management system is by alternating current
It is converted into direct current electricity output, the direct current of the accumulator store power management system output, the charge controller detection stores
The charging situation of battery, the electric current that charge controller controls accumulator input break-make situation.
Preferably, the engine is provided with driving output shaft and power generation output shaft, connection is provided on the output shaft that generates electricity
Axis device, shaft coupling are fixedly connected with power generation output shaft.
Preferably, the generator is provided with power input shaft, power input shaft passes through shaft coupling and power generation output shaft
It is connected.
Preferably, the accumulator is provided with power output end, power output end output load current.
Preferably, the power-supply management system is provided with DC output end.
Preferably, one end of the charge controller is electrically connected with accumulator, the other end and power supply of charge controller
The DC output end of management system connects.
Beneficial effects of the present invention：While the present invention will be by that will use engine to propeller output driving power, Xiang Fa
Motor output power, by electric current convert process after, by electric power store supply flight computer use, improve engine
Driving force service efficiency, save related energy consumption.
The feature and advantage of the present invention will be described in detail by embodiment combination attached drawing.
【Description of the drawings】
Fig. 1 is the structural schematic diagram of unmanned vehicle engine of the present invention with generating function.
In figure：1- engines, 2- generators, 3- power-supply management systems, 4- charge controllers, 5- accumulators, 6- electric power are defeated
Outlet, 11- drivings output shaft, 12- power generations output shaft, 13- shaft couplings, 21- power input shafts, 31- DC output ends.
【Specific implementation mode】
Refering to fig. 1, a kind of unmanned vehicle engine with generating function of the present invention, including engine 1, generator 2, power supply
Management system 3, charge controller 4, accumulator 5, the engine 1 and 2 movable connection of generator, the generator 2 and electricity
Management system 3 is electrically connected, and generator 2 exports induced field current to power-supply management system 3, and power-supply management system 3 is by alternating current
It is converted into direct current electricity output, 5 store power of the accumulator manages the direct current that system 3 exports, and the charge controller 4 detects
The charging situation of accumulator 5, the electric current that charge controller 4 controls accumulator 5 input break-make situation, and the engine 1 is provided with
Output shaft 11 and power generation output shaft 12 are driven, shaft coupling 13, shaft coupling 13 and power generation output shaft are provided on the output shaft 12 that generates electricity
12 are fixedly connected, and the generator 2 is provided with power input shaft 21, and power input shaft 21 passes through shaft coupling 13 and power generation output shaft
12 are connected, and the accumulator 5 is provided with power output end 6,6 output load current of power output end, the power management system
System 3 is provided with DC output end 31, and one end of the charge controller 4 is electrically connected with accumulator 5, charge controller 4 it is another
One end is connect with the DC output end 31 of power-supply management system 3.
The course of work of the present invention：
During the work time, the driving force input of engine 1 generates electricity unmanned vehicle engine of the present invention with generating function
Machine 2, generator 2 generate alternating current, and alternating current is converted into direct current by power-supply management system 3, and DC supply input accumulator 5 stores up
It deposits, while charge controller 4 is connect with accumulator 5, monitors the charging situation of accumulator 5.To which the electric current for controlling accumulator 5 is defeated
Enter situation, while by the way that engine 1 will be used to propeller output driving power, exports power to generator 2, pass through power supply pipe
After the process of the electric current conversion of reason system 3, electric power is stored by accumulator 5 to supply the use of flight computer, drive is improved
Power service efficiency saves related energy consumption.
Above-described embodiment is the description of the invention, is not limitation of the invention, it is any to simple transformation of the present invention after
Scheme all belong to the scope of protection of the present invention.
Claims (6)
1. a kind of unmanned vehicle engine with generating function, it is characterised in that：Including engine (1), generator (2), power supply
Management system (3), charge controller (4), accumulator (5), the engine (1) and generator (2) movable connection, the hair
Motor (2) is electrically connected with power-supply management system (3), and generator (2) exports induced field current, power supply to power-supply management system (3)
Management system (3) converts alternating current to direct current electricity output, and accumulator (5) the store power management system (3) exports straight
Galvanic electricity, the charging situation of charge controller (4) the detection accumulator (5), charge controller (4) control the electricity of accumulator (5)
Stream input break-make situation.
2. a kind of unmanned vehicle engine with generating function as described in claim 1, it is characterised in that：The engine
(1) it is provided with driving output shaft (11) and power generation output shaft (12), shaft coupling (13), shaft coupling are provided on power generation output shaft (12)
Device (13) is fixedly connected with power generation output shaft (12).
3. a kind of unmanned vehicle engine with generating function as claimed in claim 2, it is characterised in that：The generator
(2) it is provided with power input shaft (21), power input shaft (21) is connected by shaft coupling (13) with power generation output shaft (12).
4. a kind of unmanned vehicle engine with generating function as described in claim 1, it is characterised in that：The accumulator
(5) power output end (6), power output end (6) output load current are provided with.
5. a kind of unmanned vehicle engine with generating function as described in claim 1, it is characterised in that：The power management
System (3) is provided with DC output end (31).
6. a kind of unmanned vehicle engine with generating function as claimed in claim 5, it is characterised in that：The charge control
One end of device (4) is electrically connected with accumulator (5), and the direct current of the other end and power-supply management system (3) of charge controller (4) is defeated
Outlet (31) connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711406461.9A CN108313305A (en) | 2017-12-22 | 2017-12-22 | A kind of unmanned vehicle engine with generating function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711406461.9A CN108313305A (en) | 2017-12-22 | 2017-12-22 | A kind of unmanned vehicle engine with generating function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108313305A true CN108313305A (en) | 2018-07-24 |
Family
ID=62892637
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711406461.9A Withdrawn CN108313305A (en) | 2017-12-22 | 2017-12-22 | A kind of unmanned vehicle engine with generating function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108313305A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572770A (en) * | 2020-05-18 | 2020-08-25 | 河南三和航空工业有限公司 | Rescue unmanned aerial vehicle with generator and rescue mode thereof |
-
2017
- 2017-12-22 CN CN201711406461.9A patent/CN108313305A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572770A (en) * | 2020-05-18 | 2020-08-25 | 河南三和航空工业有限公司 | Rescue unmanned aerial vehicle with generator and rescue mode thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180724 |
|
| WW01 | Invention patent application withdrawn after publication |