CN109305373A - A kind of fuel oil unmanned plane and its control method - Google Patents
A kind of fuel oil unmanned plane and its control method Download PDFInfo
- Publication number
- CN109305373A CN109305373A CN201811092204.7A CN201811092204A CN109305373A CN 109305373 A CN109305373 A CN 109305373A CN 201811092204 A CN201811092204 A CN 201811092204A CN 109305373 A CN109305373 A CN 109305373A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- fuel oil
- starter motor
- oil unmanned
- petrol 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.)
- Pending
Links
- 239000000295 fuel oil Substances 0.000 title claims abstract description 65
- 238000000034 method Methods 0.000 title claims abstract description 12
- 239000007858 starting material Substances 0.000 claims abstract description 36
- 239000002828 fuel tank Substances 0.000 claims abstract description 13
- 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 abstract description 11
- 239000000446 fuel Substances 0.000 claims description 7
- 239000003502 gasoline Substances 0.000 description 2
- 230000008450 motivation Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000037396 body weight Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 235000012149 noodles Nutrition 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
Classifications
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
The present invention relates to a kind of fuel oil unmanned plane and its control methods.Including starter motor, petrol engine, gearbox, flight control system, main rotor control system, tail rotation system, fuel tank, undercarriage; continuous driving force is provided using petrol engine for unmanned plane; and utilize starter motor; restarting is carried out when unmanned plane is surprisingly ceased fire in the sky; after unmanned plane starting; starter motor is as generator; it is provided safeguard for backup power; to improve unmanned plane stability and safety, also possesses length in cruise duration compared to battery unmanned plane, saves the features such as charging time.
Description
Technical field
The present invention relates to air vehicle technique field, specially a kind of fuel oil unmanned plane and its control method.
Background technique
With the fast development of unmanned plane, unmanned plane be widely used in police, city management, agricultural, geology, meteorology,
Multiple industries such as electric power, rescue and relief work, video capture.Small drone generally uses battery unmanned plane at present, however battery fills
Power consumption is time-consuming longer, and due to the stringent limitation of unmanned aerial vehicle body weight, is not suitable for loading large-capacity battery pack, so that nothing
It is man-machine to stay aloft long time, once unmanned plane is surprisingly ceased fire in the air, it is difficult to be again started up, easily leads to nobody
Machine air crash accident.In the prior art when unmanned plane failure, the gliding ability of aircraft itself is usually relied on, selects noodles at that time
Part force-lands, but the probability of success is smaller, and safety, reliability are poor, to cause biggish economic loss.
Summary of the invention
The object of the present invention is to provide a kind of cruise duration it is longer, when unmanned plane in the sky surprisingly cease fire when can carry out
The unmanned plane lighted a fire again, to improve the stability and safety of unmanned plane.
To achieve the above object, the present invention adopts the following technical scheme:
A kind of fuel oil unmanned plane, including flight control system, main rotor control system, tail rotation system, undercarriage, starting
Machine, petrol engine, gearbox, fuel tank；
The petrol engine is connect with gearbox, and petrol engine provides continuous driving force for unmanned plane；
Fuel tank provides fuels and energy for petrol engine；
Starter motor provides secondary for starting fuel oil unmanned plane, and when the aerial involuntary stoppage of fuel oil unmanned plane for it
Starting, and after the starting of fuel oil unmanned plane, starter motor is provided safeguard as generator for fuel oil unmanned plane backup power；
Preferably, when fuel oil unmanned plane involuntary stoppage in the sky, fuel oil unmanned plane by stop sign be sent to ground without
Man-machine remote control device, user know the state of flight of fuel oil unmanned plane according to ground no-manned machine distant control device, manually perform starting
The remote control operation of starter motor.
Preferably, when fuel oil unmanned plane involuntary stoppage in the sky, flight control system is sent from starter motor described in trend
Signal, starter motor work provide restarting to fuel oil unmanned plane, and are used as power electric generators after unmanned plane starting.
The control method of above-mentioned fuel oil unmanned plane is as follows:
(1) starter motor starts fuel oil unmanned plane, and fuel tank is that petrol engine supplies fuel, the gasoline hair
Motivation provides continuous driving force for unmanned plane；
(2) fuel oil unmanned plane follow-on mission；
(3) fuel oil unmanned plane in the sky involuntary stoppage when, starter motor starts work, mentions for fuel oil unmanned plane
For restarting, and fuel oil unmanned plane starting after, starter motor be used as generator, for fuel oil nobody
Machine backup power provides safeguard.
The utility model has the advantages that fuel oil unmanned plane of the present invention includes starter motor, petrol engine, gearbox, flight control system, master
Rotor control system, tail rotation system, fuel tank, undercarriage provide continuous driving force using petrol engine for unmanned plane, and utilize
Starter motor carries out restarting when unmanned plane is surprisingly ceased fire in the sky, and after unmanned plane starting, starter motor is as power generation
Machine provides safeguard for backup power, to improve unmanned plane stability and safety, also possesses continuation of the journey compared to battery unmanned plane
Time is long, saves the features such as charging time.
Detailed description of the invention
Fig. 1 is unmanned plane structural schematic diagram of the invention.
Specific embodiment
Below in conjunction with attached drawing, the present invention is described in detail.
With reference to Fig. 1, a kind of fuel oil unmanned plane, including main rotor control system 1, flight control system 2, tail rotation system 3,
Gearbox 4, petrol engine 5, starter motor 6, undercarriage 7, fuel tank；
Comprehensive control needed for main rotor control system 1 is used to provide flight and filtering external factor generate dry
It disturbs；
Flight control system 2 is used to control the flight of unmanned plane；
Tail rotation system 3 provides power transmission for tail rotor；
The petrol engine 5 is connect with gearbox 4, changes 5 revolving speed of petrol engine by gearbox 4, it is defeated to improve torsion
Out, petrol engine 5 provides continuous driving force for unmanned plane；
Fuel tank is that petrol engine 5 provides fuels and energy；
Starter motor 6, when the aerial involuntary stoppage of fuel oil unmanned plane, provides secondary open for starting fuel oil unmanned plane for it
It is dynamic, and after the starting of fuel oil unmanned plane, starter motor 6 is used as generator, provides safeguard for fuel oil unmanned plane backup power；
Preferably, when fuel oil unmanned plane involuntary stoppage in the sky, fuel oil unmanned plane by stop sign be sent to ground without
Man-machine remote control device, user know the state of flight of fuel oil unmanned plane according to ground no-manned machine distant control device, manually perform starting
The remote control operation of starter motor；It is also possible to flight control system and sends signal from starter motor described in trend, starter motor work is right
Fuel oil unmanned plane provides restarting, and is used as power electric generators after unmanned plane starting.
The control method of above-mentioned fuel oil unmanned plane is as follows:
(1) starter motor starts fuel oil unmanned plane, and fuel tank is that petrol engine supplies fuel, the gasoline hair
Motivation provides continuous driving force for unmanned plane；
(2) fuel oil unmanned plane follow-on mission；
(3) fuel oil unmanned plane in the sky involuntary stoppage when, starter motor start work, provide secondary open for fuel oil unmanned plane
It is dynamic, and after the starting of fuel oil unmanned plane, starter motor is provided safeguard as generator for fuel oil unmanned plane backup power.
The foregoing is merely presently preferred embodiments of the present invention, is not intended to restrict the invention, it is all in spirit of the invention and
In principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (6)
1. a kind of fuel oil unmanned plane, including flight control system, main rotor control system, tail rotation system, undercarriage, feature
It is: further includes starter motor, petrol engine, gearbox, fuel tank；
The petrol engine is connect with gearbox, and petrol engine provides continuous driving force for unmanned plane；
Fuel tank provides fuels and energy for petrol engine；
Starter motor provides secondary open for starting fuel oil unmanned plane, and when the aerial involuntary stoppage of fuel oil unmanned plane for it
It is dynamic, and after the starting of fuel oil unmanned plane, starter motor is provided safeguard as generator for fuel oil unmanned plane backup power.
2. a kind of fuel oil unmanned plane as described in claim 1, it is characterised in that: when fuel oil unmanned plane involuntary stoppage in the sky
When, stop sign is sent to ground no-manned machine distant control device by fuel oil unmanned plane, and user obtains according to ground no-manned machine distant control device
The state of flight for knowing fuel oil unmanned plane manually performs the remote control operation of starting starter motor.
3. a kind of fuel oil unmanned plane as described in claim 1, it is characterised in that: when fuel oil unmanned plane involuntary stoppage in the sky
When, flight control system sends signal from starter motor described in trend, and starter motor work provides restarting to fuel oil unmanned plane,
And power electric generators are used as after unmanned plane starting.
4. a kind of control method of fuel oil unmanned plane, it is characterised in that: the fuel oil unmanned plane includes flight control system, main rotation
Wing control system, tail rotation system, undercarriage, starter motor, petrol engine, gearbox, fuel tank, the petrol engine and change
Fast case connection, fuel tank provide fuels and energy for petrol engine, and the control method is as follows:
(1) starter motor starts fuel oil unmanned plane, and fuel tank is that petrol engine supplies fuel, and the petrol engine mentions for unmanned plane
For continuous driving force；
(2) fuel oil unmanned plane follow-on mission；
(3) fuel oil unmanned plane in the sky involuntary stoppage when, starter motor start work, provide restarting for fuel oil unmanned plane, and
After the starting of fuel oil unmanned plane, starter motor is provided safeguard as generator for fuel oil unmanned plane backup power.
5. a kind of control method of fuel oil unmanned plane as claimed in claim 4, it is characterised in that: when fuel oil unmanned plane in the sky
When involuntary stoppage, stop sign is sent to ground no-manned machine distant control device by fuel oil unmanned plane, and user is distant according to ground unmanned plane
Control device knows the state of flight of fuel oil unmanned plane, manually performs the remote control operation of starting starter motor.
6. a kind of control method of fuel oil unmanned plane as claimed in claim 4, it is characterised in that: when fuel oil unmanned plane in the sky
When involuntary stoppage, flight control system sends signal from starter motor described in trend, and starter motor work provides two to fuel oil unmanned plane
Secondary starting, and power electric generators are used as after unmanned plane starting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811092204.7A CN109305373A (en) | 2018-09-19 | 2018-09-19 | A kind of fuel oil unmanned plane and its control method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811092204.7A CN109305373A (en) | 2018-09-19 | 2018-09-19 | A kind of fuel oil unmanned plane and its control method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109305373A true CN109305373A (en) | 2019-02-05 |
Family
ID=65224881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811092204.7A Pending CN109305373A (en) | 2018-09-19 | 2018-09-19 | A kind of fuel oil unmanned plane and its control method |
Country Status (1)
| Country | Link |
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| CN (1) | CN109305373A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP7448199B2 (en) | 2020-05-07 | 2024-03-12 | インダストリーネットワーク株式会社 | Unmanned aerial vehicles and fuel tanks |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2976554A1 (en) * | 2011-06-20 | 2012-12-21 | Cassidian | SYSTEM FOR INTEGRATING A DIESEL ENGINE IN A DRONE |
| CN104743103A (en) * | 2015-03-31 | 2015-07-01 | 东莞市汇天玩具模型有限公司 | Super-miniature fuel oil unmanned helicopter |
| CN205225553U (en) * | 2015-10-23 | 2016-05-11 | 四川测绘地理信息局测绘技术服务中心 | Unmanned aerial vehicle with remote start up device |
| CN106218881A (en) * | 2016-08-30 | 2016-12-14 | 辽宁壮龙无人机科技有限公司 | Vertical layout fuel power four rotor flying platform |
| CN106585974A (en) * | 2015-10-14 | 2017-04-26 | 徐建宁 | Rotorcraft adopting free piston compression |
| CN108263618A (en) * | 2017-12-22 | 2018-07-10 | 成都才智圣有科技有限责任公司 | A kind of hybrid power multiaxis rotor wing unmanned aerial vehicle |
| CN108454865A (en) * | 2018-03-23 | 2018-08-28 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle electricity generation system |
-
2018
- 2018-09-19 CN CN201811092204.7A patent/CN109305373A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2976554A1 (en) * | 2011-06-20 | 2012-12-21 | Cassidian | SYSTEM FOR INTEGRATING A DIESEL ENGINE IN A DRONE |
| CN104743103A (en) * | 2015-03-31 | 2015-07-01 | 东莞市汇天玩具模型有限公司 | Super-miniature fuel oil unmanned helicopter |
| CN106585974A (en) * | 2015-10-14 | 2017-04-26 | 徐建宁 | Rotorcraft adopting free piston compression |
| CN205225553U (en) * | 2015-10-23 | 2016-05-11 | 四川测绘地理信息局测绘技术服务中心 | Unmanned aerial vehicle with remote start up device |
| CN106218881A (en) * | 2016-08-30 | 2016-12-14 | 辽宁壮龙无人机科技有限公司 | Vertical layout fuel power four rotor flying platform |
| CN108263618A (en) * | 2017-12-22 | 2018-07-10 | 成都才智圣有科技有限责任公司 | A kind of hybrid power multiaxis rotor wing unmanned aerial vehicle |
| CN108454865A (en) * | 2018-03-23 | 2018-08-28 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle electricity generation system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP7448199B2 (en) | 2020-05-07 | 2024-03-12 | インダストリーネットワーク株式会社 | Unmanned aerial vehicles and fuel tanks |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190205 |