CN204433050U - The hardware platform of dynamic four rotor unmanned aircrafts of oil - Google Patents
The hardware platform of dynamic four rotor unmanned aircrafts of oil Download PDFInfo
- Publication number
- CN204433050U CN204433050U CN201420806154.5U CN201420806154U CN204433050U CN 204433050 U CN204433050 U CN 204433050U CN 201420806154 U CN201420806154 U CN 201420806154U CN 204433050 U CN204433050 U CN 204433050U
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- Prior art keywords
- rotor
- aero
- gear box
- power
- hardware platform
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- 230000005540 biological transmission Effects 0.000 claims abstract description 11
- 238000006073 displacement reaction Methods 0.000 claims abstract description 6
- 239000002002 slurry Substances 0.000 claims abstract description 6
- 229920002472 Starch Polymers 0.000 claims abstract description 5
- 235000019698 starch Nutrition 0.000 claims abstract description 5
- 239000003245 coal Substances 0.000 abstract description 2
- 210000003746 feather Anatomy 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
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Abstract
The utility model discloses the hardware platform that a kind of oil moves four rotor unmanned aircrafts, include four rotors and aero-engine, each rotor comprises the fin of two panels, the fin of every sheet is connected with corresponding slurry hub respectively, transmission of power is given the change speed gear box of four groups by four transmission shafts in cross arrangement by drop-gear box by power by aero-engine, then starches hub by change speed gear box by Servo-controller and displacement Systematical control and two panels rotor is connected two and realize corresponding motion.Oil of the present utility model moves the hardware platform of four rotor unmanned aircrafts, and by adopting gasoline/boat coal to be fuel, employing small aero is power, and lift system adopts lifting airscrew form, and maneuverability pattern adopts determines rotating speed feather mode.There is cruise duration long, the features such as load capacity is large, maneuvering performance good, and wind loading rating is strong.The job task demand of most of client can be met.
Description
Technical field
The utility model relates to one
dynamic four rotor unmanned aircrafts of oil, particularly a kind of
the hardware platform of dynamic four rotor unmanned aircrafts of oil.
Background technology
The dynamic quadrotor of oil to be a kind of with small aero be power, can vertical takeoff and landing, many rotary wind types automated spacecraft.It belongs to non-co-shaft type butterfly aircraft in total arrangement in form, and compared with conventional rotary aircraft, its structure is more compact, can produce larger lift, and the anti-twisted moment and 4 rotors can be cancelled out each other, does not need special anti-twisted oar.
Four rotors in the market and multi-rotor aerocraft varied, all adopt using lithium cell as power source, brushless motor is power, lift system adopts propeller form, maneuverability pattern adopts the operating pattern of fixed pitch variable speed, many rotors of such pattern are that the lift size relying on self gravitation and motor variable speed to change screw propeller carries out balance control, shortcoming is that maneuvering performance is poor, and wind loading rating is weak.Restrict by battery power to weight ratio at present in addition, all belong to little miniature aircraft, cruise duration is short, and load capacity is little.The job task demand of most of client cannot be met.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art part, and provides a kind of cruise duration long, the aircraft of the features such as load capacity is large, maneuvering performance good, and wind loading rating is strong, can meet the job task demand of most of client
the hardware platform of dynamic four rotor unmanned aircrafts of oil.
A kind of
the hardware platform of dynamic four rotor unmanned aircrafts of oilinclude rotor and the aero-engine of four, each rotor comprises the fin of two panels, the fin of every sheet is connected with corresponding slurry hub respectively, transmission of power is given the change speed gear box of four groups by four transmission shafts in cross arrangement by drop-gear box by power by aero-engine, then starches hub by change speed gear box by Servo-controller and displacement Systematical control and two panels rotor is connected two and realize corresponding motion.
The utility model
the hardware platform of dynamic four rotor unmanned aircrafts of oil, owing to adopting aero-engine as power, and add the rotor of four groups, the control of each group rotor is realized by Servo-controller and displacement system, thus change in the past unmanned vehicle lift by propeller, operate the maneuvering performance brought apart from variable speed pattern by fixed slurry poor, the shortcoming that wind loading rating is weak, and the utility model changes the lifting airscrew pattern of employing into, maneuverability pattern determines rotating speed change slurry apart from mode for adopting, there is wind loading rating strongthe advantage that load capacity is large, maneuvering performance is good.
In sum, the utility model following advantage compared to existing technology:
Of the present utility model
the hardware platform of dynamic four rotor unmanned aircrafts of oil, passes throughadopt gasoline/boat coal to be fuel, employing small aero is power, and lift system adopts lifting airscrew form, and maneuverability pattern adopts determines rotating speed feather mode.There is cruise duration long, the features such as load capacity is large, maneuvering performance good, and wind loading rating is strong.The job task demand of most of client can be met.
The machine carry camera cradle head, can realize ratio+increasing and surely handle flight+autonomous program control flight, controls the running of camera cradle head in real time, the telemetry informations such as real-time Transmission image and aircraft flight path, speed, course, height; Use flight posture monitoring software to carry out the display of state of flight, use trajectory planning and monitoring software to carry out trajectory planning, use battlefield video monitor software carry out the display of image and record preservation.
Accompanying drawing explanation
Fig. 1 is of the present utility model
the hardware platform of dynamic four rotor unmanned aircrafts of oilmajor part connection diagram.
Fig. 2 is the connection diagram of transmission shaft to rotor.
Label declaration 1 rotor 11 fin 12 starches hub 2 aero-engine 3 transmission shaft 4 change speed gear box 5 Servo-controller 6 displacement system 7 drop-gear box.
Detailed description of the invention
Below in conjunction with embodiment, the utility model is described in more detail.
Embodiment 1
A kind of
the hardware platform of dynamic four rotor unmanned aircrafts of oilinclude rotor 1 and the aero-engine 2 of four, each rotor comprises the fin 11 of two panels, the fin of every sheet is connected with corresponding slurry hub 12 respectively, transmission of power is given the change speed gear box 4 of four groups by four transmission shafts 3 in cross arrangement by drop-gear box 7 by power by aero-engine, then controls to starch hub to two panels rotor is connected two by change speed gear box by Servo-controller 5 and displacement system 6 and realize corresponding motion.
It is same as the prior art that the present embodiment does not state part.
Claims (1)
1. an oil moves the hardware platform of four rotor unmanned aircrafts, it is characterized in that: include four rotors and aero-engine, each rotor comprises two panels fin, every sheet fin is connected with corresponding slurry hub respectively, transmission of power is given four groups of change speed gear boxs by four transmission shafts in cross arrangement by drop-gear box by power by aero-engine, then starches hub by change speed gear box by Servo-controller and displacement Systematical control and two panels rotor is connected two and realize corresponding motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420806154.5U CN204433050U (en) | 2014-12-18 | 2014-12-18 | The hardware platform of dynamic four rotor unmanned aircrafts of oil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420806154.5U CN204433050U (en) | 2014-12-18 | 2014-12-18 | The hardware platform of dynamic four rotor unmanned aircrafts of oil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204433050U true CN204433050U (en) | 2015-07-01 |
Family
ID=53600952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420806154.5U Expired - Fee Related CN204433050U (en) | 2014-12-18 | 2014-12-18 | The hardware platform of dynamic four rotor unmanned aircrafts of oil |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204433050U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035313A (en) * | 2015-06-30 | 2015-11-11 | 北京航空航天大学 | Rotated quadrotor |
| CN105270618A (en) * | 2015-11-04 | 2016-01-27 | 中航维拓（北京）科技有限责任公司 | Variable-pitch coaxial oil-driven six-rotor helicopter |
| CN105398570A (en) * | 2015-11-26 | 2016-03-16 | 北京浩恒征途航空科技有限公司 | Oil-operated multi- rotor aerocraft |
| CN106628124A (en) * | 2016-11-08 | 2017-05-10 | 瀚伦贝尔通用航空器有限公司 | Automatic balance adjusting mechanism for left and right rotors of twin-rotor air vehicle |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
-
2014
- 2014-12-18 CN CN201420806154.5U patent/CN204433050U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035313A (en) * | 2015-06-30 | 2015-11-11 | 北京航空航天大学 | Rotated quadrotor |
| CN105035313B (en) * | 2015-06-30 | 2017-03-08 | 北京航空航天大学 | One kind is verted quadrotor |
| CN105270618A (en) * | 2015-11-04 | 2016-01-27 | 中航维拓（北京）科技有限责任公司 | Variable-pitch coaxial oil-driven six-rotor helicopter |
| CN105270618B (en) * | 2015-11-04 | 2017-07-25 | 中航维拓（北京）科技有限责任公司 | A kind of coaxial six heligyro of dynamic displacement of oil |
| CN105398570A (en) * | 2015-11-26 | 2016-03-16 | 北京浩恒征途航空科技有限公司 | Oil-operated multi- rotor aerocraft |
| CN106628124A (en) * | 2016-11-08 | 2017-05-10 | 瀚伦贝尔通用航空器有限公司 | Automatic balance adjusting mechanism for left and right rotors of twin-rotor air vehicle |
| CN106628124B (en) * | 2016-11-08 | 2023-06-06 | 瀚伦贝尔通用航空器有限公司 | Automatic adjusting and balancing mechanism for left rotor wing and right rotor wing of double-rotor aircraft |
| US11368002B2 (en) | 2016-11-22 | 2022-06-21 | Hydro-Quebec | Unmanned aerial vehicle for monitoring an electrical line |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150701 Termination date: 20211218 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |