CN208119432U - A kind of electric assembly power unmanned vehicle of distributed oil - Google Patents
A kind of electric assembly power unmanned vehicle of distributed oil Download PDFInfo
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- CN208119432U CN208119432U CN201720927649.7U CN201720927649U CN208119432U CN 208119432 U CN208119432 U CN 208119432U CN 201720927649 U CN201720927649 U CN 201720927649U CN 208119432 U CN208119432 U CN 208119432U
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Abstract
The utility model provides a kind of electric assembly power unmanned vehicle of distributed oil：Oil motor, motor, foldable propeller, propeller, empennage, wing, aileron, fuselage, nose-gear and rear undercarriage；Aircaft configuration uses the composite material based on carbon fiber, and oily power and electric power are perfectly combined, to save more fuel to extend cruise duration and voyage.
Description
Technical field
The utility model belongs to field of aerospace technology, and more particularly to a kind of distributed electric assembly power of oil, nobody flies
Row device.
Background technique
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.The people
With aspect, it is that unmanned plane has really just needed that unmanned plane, which adds industrial application,；At present take photo by plane, agricultural, plant protection, self-timer, express delivery fortune
Defeated, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture
The purposes of unmanned plane itself has greatly been expanded in the application in romance etc. field, and developed country is also in actively extension industrial application
With development unmanned air vehicle technique.
Cruise duration, the loading capacity for improving unmanned vehicle, are the emphasis in current unmanned vehicle R&D process.Generally
Unmanned vehicle only relies on oil or electric power provides power, can not obtain more power to extend cruise duration and voyage.
Summary of the invention
To achieve the above object, the technical solution adopted in the utility model is：A kind of electric assembly power of distributed oil nobody
Aircraft, aircaft configuration use the composite material based on carbon fiber, and oily power and electric power are perfectly combined, from
And more fuel are saved to extend cruise duration and voyage.
A kind of electric assembly power unmanned vehicle of distributed oil includes：Oil motor, motor, foldable propeller, spiral
Paddle, empennage, wing, aileron, fuselage, nose-gear and rear undercarriage；Wherein, propeller is mounted on oil motor, foldable spiral shell
Rotation paddle is mounted on motor, and motor is bolted on the both ends of wing, and empennage is mounted on the rear side of fuselage, oil motor
It is mounted between empennage and fuselage, aileron is mounted on the both ends of wing, and nose-gear is mounted on the front side of fuselage, rear undercarriage pair
What is claimed is mounted on close to fuselage positions below wing, and flight control system is mounted on the front of fuselage, and is connected with fuselage；
The flight control system, including revolution speed of propeller sensor, flying speed recorder, oil motor Throttle Opening Control
Device and motor controller；Flight control system connects revolution speed of propeller sensor, flying speed recorder, oil by conducting wire and moves
Machine oil door controller and motor controller；Revolution speed of propeller sensor is connect with propeller, oil motor throttle control and oil
Motivation connection, motor controller are connect with motor, and the front of fuselage is arranged in flying speed recorder, for analyzing record
The real-time speed data of aircraft, and by data back to flight control system.
The flight control system uses chip model for the ARM microcontroller of STM32F427IIH6.
The revolution speed of propeller sensor is using 4 road Hall sensors.
The flying speed recorder is using MPU-6050 module.
It is JX6221 steering engine that the oil motor throttle control, which uses,.
The motor controller is using MG996R number steering engine.
A kind of length of distributed electric assembly power unmanned vehicle of oil is 2 meters to 3 meters.
A kind of weight of distributed electric assembly power unmanned vehicle of oil is 20 kilograms to 30 kilograms.
A kind of radiation pattern of distributed electric assembly power unmanned vehicle of oil is vehicle-mounted accelerated take-off or compression
Air ejection.
A kind of way of recycling of described distributed electric assembly power unmanned vehicle of oil is that ventral downhill race or hit is netted back
It receives.
The front side of fuselage, rear undercarriage are symmetrically installed below wing close to fuselage positions.
The beneficial effects of the utility model：
In the take-off climb stage, oil motor and motor are worked at the same time, and substantially increase unmanned plane in the speed of ramp-up period
Degree.
In cruising phase, motor, and the motor-driven propeller that folds back are closed, resistance is reduced, oil motor is best
Work status to effectively save fuel oil, and reduces operating cost.
During aircraft flight, gasoline engine can charge for battery, to greatly improve battery utilization rate.
An emergency situation is encountered in flight course, can not normal work if oil supply system or other reasons cause oil motor to stop
Make, at this point, motor can full speed operation, continue to unmanned plane and fly in a short time, and safe falling.
Detailed description of the invention
Fig. 1 is a kind of main view of electric assembly power unmanned vehicle of distributed oil.
Fig. 2 is a kind of left view of electric assembly power unmanned vehicle of distributed oil.
Fig. 3 is a kind of top view of electric assembly power unmanned vehicle of distributed oil.
Fig. 4 is flight control system control flow chart.
As shown, 1 is oil motor, 2 be motor, and 3 be foldable propeller, and 4 be propeller, and 5 be empennage, and 6 be machine
The wing, 7 be aileron, and 8 be fuselage, and 9 be nose-gear, and 10 be rear undercarriage, and 11 be flight control system, and 111 be revolution speed of propeller
Sensor, 112 be flying speed recorder, and 113 be oil motor throttle control, and 114 be motor controller.
Specific embodiment
In order to further illustrate the utility model, the utility model is retouched in detail with reference to the accompanying drawings and embodiments
It states, but they cannot be interpreted as to the restriction to scope of protection of the utility model.
As shown, a kind of electric assembly power unmanned vehicle of distributed oil includes：Oil motor 1, motor 2 are foldable
Propeller 3, propeller 4, empennage 5, wing 6, aileron 7, fuselage 8, nose-gear 9 and rear undercarriage 10；Wherein, propeller 4 is pacified
On oil motor 1, foldable propeller 3 is mounted on motor 2, and motor 2 is bolted on the both ends of wing 6,
Empennage 5 is mounted on the rear side of fuselage 8, and oil motor 1 is mounted between empennage 5 and fuselage 8, and aileron 7 is mounted on the both ends of wing 6,
Nose-gear 9 is mounted on the front side of fuselage 8, and rear undercarriage 10 is symmetrically installed on 6 lower section of wing close to 8 position of fuselage, flight
Control system 11 is mounted on the front of fuselage 8, and is connected with fuselage 8；
The flight control system 11, including revolution speed of propeller sensor 111, flying speed recorder 112, oil motor
Throttle control 113 and motor controller 114；Flight control system 11 by conducting wire connect revolution speed of propeller sensor 111,
Flying speed recorder 112, oil motor throttle control 113 and motor controller 114；Revolution speed of propeller sensor 111 with
Propeller 4 connects, and oil motor throttle control 113 is connect with oil motor 1, and motor controller 114 is connect with motor 2, flies
The front of fuselage 8 is arranged in row velograph 112, returns for analyzing the real-time speed data of record aircraft, and by data
It is transmitted to flight control system 11.
The flight control system 11 uses chip model for the ARM microcontroller of STM32F427IIH6.
The revolution speed of propeller sensor 111 is using 4 road Hall sensors.
The flying speed recorder 112 is using MPU-6050 module.
It is JX6221 steering engine that the oil motor throttle control 113, which uses,.
The motor controller 114 is using MG996R number steering engine.
The chord of the wing 6 is 3 meters to 4 meters.
A kind of length of distributed electric assembly power unmanned vehicle of oil is 2 meters to 3 meters.
A kind of weight of distributed electric assembly power unmanned vehicle of oil is 20 kilograms to 30 kilograms.
A kind of radiation pattern of distributed electric assembly power unmanned vehicle of oil is vehicle-mounted accelerated take-off or compression
Air ejection.
A kind of way of recycling of described distributed electric assembly power unmanned vehicle of oil is that ventral downhill race or hit is netted back
It receives.
Working principle：When unmanned plane take-off climb, due to needing biggish thrust, the meeting basis of flight control system 11 can roll over
The setting of the rotary speed parameter of coiled coil paddle 3 and propeller 4 guarantees that oil motor 1 and motor 2 cooperate, drives foldable spiral
Paddle 3 and propeller 4 provide required thrust of taking off for aircraft；When aircraft cruise reaches certain cruising speed, flight control system
11 can close motor 2, and pack up foldable propeller 3 backward according to the cruise-speed value of setting, be by the work of oil motor 1
Aircraft provides power；Oil motor 1 is started to work, and is charged for battery, to be 2 electric energy supplement of motor.
The revolution speed of propeller sensor 111 and flying speed recorder 112 that flight control system 11 connects, flight control system
System 11 can adjust separately oil motor throttle according to the data that revolution speed of propeller sensor 111 and flying speed recorder 112 return
The parameter of controller 113 and motor controller 114, to control the working condition of oil motor 1 and motor 2.
In the take-off climb stage, when the speed that flying speed recorder 112 collects aircraft is not up to setting value, can incite somebody to action
Data back is acquired to flight control system 11, flight control system 11 will give oil motor throttle control 113 and motor control
Device 114 processed issues signal, and oil motor throttle control 113 and motor controller 114 control oil motor 1 and motor 2 simultaneously
Work,
In cruising phase, when the speed that flying speed recorder 112 collects aircraft reaches setting value, data will be acquired
Pass back to flight control system 11, flight control system 11 issues signal, motor controller 114 to motor controller 114
Control motor 2 stops working and the motor-driven propeller that folds back, and reduces resistance, and optimum state works oil motor,
To effectively save fuel oil, and reduce operating cost.
During aircraft flight, gasoline engine can charge for battery, to greatly improve battery utilization rate.
An emergency situation is encountered in flight course, can not normal work if oil supply system or other reasons cause oil motor to stop
Make, at this point, the revolving speed of propeller 4 can decline, revolution speed of propeller sensor 111 arrives collected revolution speed of propeller data back
Flight control system 11, flight control system 11 issue working signal to motor controller 114, control 2 full speed work of motor
Make, continues to unmanned plane and fly in a short time, and safe falling.
Claims (6)
1. a kind of electric assembly power unmanned vehicle of distributed oil, which is characterized in that including：Oil motor, motor, foldable spiral shell
Revolve paddle, propeller, empennage, wing, aileron, fuselage, nose-gear and rear undercarriage；Wherein, propeller is mounted on oil motor,
Foldable propeller is mounted on motor, and motor is bolted on the both ends of wing, after empennage is mounted on fuselage
Side, oil motor are mounted between empennage and fuselage, and aileron is mounted on the both ends of wing, and nose-gear is mounted on the front side of fuselage,
Undercarriage is symmetrically installed below wing close to fuselage positions afterwards, and flight control system is mounted on the front of fuselage, and with
Fuselage is connected；
The flight control system, including revolution speed of propeller sensor, flying speed recorder, oil motor throttle control and
Motor controller；Flight control system connects revolution speed of propeller sensor, flying speed recorder, oil motor oil by conducting wire
Door controller and motor controller；Revolution speed of propeller sensor is connect with propeller, oil motor throttle control and oil motor
Connection, motor controller are connect with motor, and the front of fuselage is arranged in flying speed recorder, for analyzing record flight
The real-time speed data of device, and by data back to flight control system.
2. a kind of distributed electric assembly power unmanned vehicle of oil according to claim 1, it is characterised in that：Described flies
Row control system uses chip model for the ARM microcontroller of STM32F427IIH6.
3. a kind of distributed electric assembly power unmanned vehicle of oil according to claim 1, it is characterised in that：The spiral shell
Paddle speed probe is revolved using 4 road Hall sensors.
4. a kind of distributed electric assembly power unmanned vehicle of oil according to claim 1, it is characterised in that：Described flies
Row velograph is using MPU-6050 module.
5. a kind of distributed electric assembly power unmanned vehicle of oil according to claim 1, it is characterised in that：The oil
It is JX6221 steering engine that motivation throttle control, which uses,.
6. a kind of distributed electric assembly power unmanned vehicle of oil according to claim 1, it is characterised in that：The electricity
Motivation controller is using MG996R number steering engine.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720037515 | 2017-01-13 | ||
| CN2017200375158 | 2017-01-13 |
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| CN208119432U true CN208119432U (en) | 2018-11-20 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109733620A (en) * | 2018-11-22 | 2019-05-10 | 南京航空航天大学 | A kind of hybrid power unmanned plane and its control method |
| CN109733621A (en) * | 2018-12-17 | 2019-05-10 | 南京航空航天大学 | A kind of hybrid power unmanned plane promoting mode more |
-
2017
- 2017-07-28 CN CN201720927649.7U patent/CN208119432U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109733620A (en) * | 2018-11-22 | 2019-05-10 | 南京航空航天大学 | A kind of hybrid power unmanned plane and its control method |
| CN109733621A (en) * | 2018-12-17 | 2019-05-10 | 南京航空航天大学 | A kind of hybrid power unmanned plane promoting mode more |
| CN109733621B (en) * | 2018-12-17 | 2022-01-18 | 南京航空航天大学 | Hybrid unmanned aerial vehicle of many propulsion modes |
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