CN105799919A - Oil-driven multi-rotor wing air vehicle - Google Patents
Oil-driven multi-rotor wing air vehicle Download PDFInfo
- Publication number
- CN105799919A CN105799919A CN201610162023.1A CN201610162023A CN105799919A CN 105799919 A CN105799919 A CN 105799919A CN 201610162023 A CN201610162023 A CN 201610162023A CN 105799919 A CN105799919 A CN 105799919A
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- CN
- China
- Prior art keywords
- dish
- underframe
- mounting seat
- engine
- bottom centre
- 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
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
An oil-driven multi-rotor wing air vehicle comprises a center disc, an even number of drive rods, an even number of paddle installing seats, a bottom center disc, a base frame and a remote control mechanism. One end of each drive rod is fixed between the top center disc and the bottom center disc through a drive rod fixing part, one paddle installing seat is installed at the other end of the drive rod, each paddle installing seat is provided with two paddle blades, installed on an engine seat and connected with a gasoline engine through a belt, each engine seat is provided with a steering engine fixing position used for installing a steering engine, the steering engines and the paddle installing seats are connected through connecting rods, and the base frame is fixed to the lower portion of the bottom center disc through a base frame fixing seat. According to the oil-driven multi-rotor wing air vehicle, the bearing capacity is enhanced, the strength is high, the weight is small, and the service life is prolonged.
Description
Technical field
The present invention relates to aeronautical product technical field, be specifically related to the dynamic multi-rotor aerocraft of a kind of oil.
Background technology
Multi-rotor aerocraft operates on it control by wireless remote control system and independent flight control system, to realize the landing of aircraft, all around flight, acceleration and deceleration and direction controlling etc..Navigability, stability, effective mission payload and cruising time are the important indicators investigating multi-rotor aerocraft, and under identical navigability and stability condition, user pursues bigger effective mission payload and long-time duration flight ability.
The rotor type of drive of multi-rotor aerocraft currently on the market is only applicable to motor and drives, other kinds of electromotor (such as petrol engine, Diesel engine, charging motor etc.) can not be carried as power source, deficiency when so causing existing multi-rotor aerocraft to navigate, is difficult to meet the requirement of long-time continuation of the journey.
Summary of the invention
The invention provides the dynamic multi-rotor aerocraft of a kind of oil, with solve that prior art exists be only applicable to motor drive cause navigating time not enough problem.
The technical solution adopted for the present invention to solve the technical problems is:
The dynamic multi-rotor aerocraft of oil, including top center dish, even number drive link and oar mounting seat, bottom centre's dish, underframe and remote control, one end of drive link is fixed between top center dish and bottom centre's dish by drive link fixture, oar mounting seat is arranged on the other end of drive link, each oar mounting seat is respectively mounted two panels blade, electric motor starting is had to be dynamically connected axle by the synchromesh gear variable velocity zone in spider between top center dish and bottom centre's dish, connect the axle other end and connect oar mounting seat, oar mounting seat belt and electromotor connect, each engine bearer there is steering wheel fixed position steering wheel is installed, steering wheel and oar mounting seat are connected by connecting rod, underframe is fixed on bottom centre's dish bottom by the fixing seat of underframe.
Above-mentioned electromotor can be petrol engine, Diesel engine or charging motor.
Above-mentioned underframe includes the bend pipe of falling U that two parallel interval arrange, for connecting the connecting tube of the bend pipe of falling U end and the reinforced pipe between two bend pipes of falling U, being provided with the fixing seat of underframe on two bend pipe of falling U tops, underframe is fixed on bottom centre's tray bottom by the fixing seat of underframe.
Above-mentioned remote control includes central processing unit, gps antenna, signal projector, data-interface, picture sensor and control station, wherein gps antenna, signal projector, data-interface, picture sensor and control station are all connected with central processing unit, and gps antenna is connected with the image information launcher signal at top center dish top by central processing unit；Central processing unit is connected with engine signal by speed regulator；Being provided with computer in control station, computer is connected with signal controller, and signal controller is connected with image monitor.
Above-mentioned top center dish and bottom centre's dish, blade material are carbon fiber, and oar mounting seat, engine bearer, connection axle, synchromesh gear material are titanium alloy material.
Compared to prior art, the present invention can carry various types of electromotor (such as petrol engine, Diesel engine, charging motor etc.) as requested as power source, fully solve problem not enough during electric-powered aircraft boat, meet the requirement of work during various long boat；Spider, connecting rod are high-strength carbon fiber, oar mounting seat, engine bearer, connection axle, synchromesh gear material are titanium alloy material, both strengths of materials are high, lightweight, be effectively reduced aircraft own wt, making its bearing capacity strengthen, intensity is high, lightweight, extend service life.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described:
Fig. 1 is the structural representation of apparatus of the present invention；
Fig. 2 is the front elevational schematic of apparatus of the present invention；
Fig. 3 is the enlarged diagram of a-quadrant in Fig. 2；
Fig. 4 is the enlarged diagram in B region in Fig. 2；
Fig. 5 is the structural representation of apparatus of the present invention underframe；
Fig. 6 is the fundamental diagram of apparatus of the present invention remote control.
Tu Zhong 1 bottom centre dish, 2 top center dishes, 3 drive link fixtures, 4 drive links, 5 blades, 6 oar mounting seats, 7 steering wheels, seat fixed by 8 electromotors, 9 electromotors, 10 batteries, 11 image information emitters, 12 synchromesh gears, 13 control chambers, 14 synchronous motors, seat fixed by 15 underframe, 16 underframe, 17 photographic head, 19 speed regulators, 20 central processing units, 21GPS antenna, 22 signal projectors, 23 data-interfaces, 24 control stations, 25 computers, 26 signal controllers, 27 picture sensors, 28 image monitors, 1601 bend pipes of falling U, 1602 reinforced pipes, 1603 connecting tubes.
Detailed description of the invention
nullSuch as Fig. 1、Fig. 2、Fig. 3、Fig. 4、Shown in Fig. 5 and Fig. 6，The dynamic multi-rotor aerocraft of a kind of oil，Including a top center dish 2、The oar mounting seat 6 of four drive links 4 and four、One bottom centre's dish 1、One underframe 16 and remote control，Top center dish 2 and bottom centre's dish 1 material are carbon fiber，One end of drive link 4 is fixed between top center dish 2 and bottom centre's dish 1 by drive link fixture 3，The other end of drive link 4 installs the fixing seat 8 of electromotor，Each oar mounting seat 6 is connected each oar mounting seat 6 with belt with electromotor 12 and is respectively mounted two panels blade 5，Blade 5 material is carbon fiber，Each drive link 4 is installed the fixing seat 8 of a steering wheel，The fixing seat 8 of each steering wheel installs a steering wheel 7，Steering wheel 7 and oar mounting seat 6 are connected by connecting rod 18，Top center dish 2 crown center is provided with image information emitter 11 and control chamber 13，Underframe 16 is fixed on bottom centre's dish 1 bottom by the fixing seat 15 of some underframe，Bottom centre's dish 1 is provided with photographic head 17，Bottom centre's dish 1 synchronous motor installed below drives drive link 4 by synchromesh gear 12，Drive link 4 drives the oar mounting seat 6 of the other end，Blade 5 in oar mounting seat 6 rotates with，Oar mounting seat 6 is by belt drive electromotor 9，And the electromotor 9 starting each rotor works.
Underframe 16 includes the bend pipe of falling U 1601 that two parallel interval arrange, for connecting the connecting tube 1603 of the bend pipe of falling U 1601 end and the reinforced pipe 1602 between two bend pipes of falling U 1601, being provided with the fixing seat 15 of underframe on two bend pipe of falling U 1601 tops, underframe 16 is fixed on bottom bottom centre's dish 1 by the fixing seat 15 of underframe.
Above-mentioned remote control includes central processing unit 20, gps antenna 21, signal projector 22, data-interface 23, picture sensor 27 and control station 24, wherein gps antenna 21, signal projector 22, data-interface 23, picture sensor 27 and control station 24 are all connected with central processing unit 20, and gps antenna 21 is connected with image information emitter 11 signal at top center dish 1 top by central processing unit 20；Central processing unit 20 is connected with electromotor 12 signal by speed regulator 19；Being provided with computer 25 in control station 24, computer 25 is connected with signal controller 26, and signal controller 26 is connected with image monitor 27.Device 26 is connected with image monitor 27.
Claims (5)
1. the dynamic multi-rotor aerocraft of oil, including top center dish, even number drive link and oar mounting seat, bottom centre's dish, underframe and remote control, it is characterized in that: one end of drive link is fixed between top center dish and bottom centre's dish by drive link fixture, oar mounting seat is arranged on the other end of drive link, each oar mounting seat is respectively mounted two panels blade, electric motor starting is had to be dynamically connected axle by the synchromesh gear variable velocity zone in spider between top center dish and bottom centre's dish, connect the axle other end and connect oar mounting seat, oar mounting seat belt and electromotor connect, each engine bearer there is steering wheel fixed position steering wheel is installed, steering wheel and oar mounting seat are connected by connecting rod, underframe is fixed on bottom centre's dish bottom by the fixing seat of underframe.
2. the dynamic multi-rotor aerocraft of oil according to claim 1, is characterized in that above-mentioned electromotor can be petrol engine, Diesel engine or charging motor.
3. the dynamic multi-rotor aerocraft of oil according to claim 1 and 2, it is characterized in that underframe include the bend pipe of falling U that two parallel interval are arranged, for connecting the connecting tube of the bend pipe of falling U end and the reinforced pipe between two bend pipes of falling U, being provided with the fixing seat of underframe on two bend pipe of falling U tops, underframe is fixed on bottom centre's tray bottom by the fixing seat of underframe.
4. the dynamic multi-rotor aerocraft of oil according to claim 1 and 2, it is characterized in that remote control includes central processing unit, gps antenna, signal projector, data-interface, picture sensor and control station, wherein gps antenna, signal projector, data-interface, picture sensor and control station are all connected with central processing unit, and gps antenna is connected with the image information launcher signal at top center dish top by central processing unit；Central processing unit is connected with engine signal by speed regulator；Being provided with computer in control station, computer is connected with signal controller, and signal controller is connected with image monitor.
5. the dynamic multi-rotor aerocraft of oil according to claim 1 or 4, is characterized in that top center dish and bottom centre's dish, blade material are carbon fiber, and oar mounting seat, engine bearer, connection axle, reduction gearing material are titanium alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610162023.1A CN105799919A (en) | 2016-03-22 | 2016-03-22 | Oil-driven multi-rotor wing air vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610162023.1A CN105799919A (en) | 2016-03-22 | 2016-03-22 | Oil-driven multi-rotor wing air vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105799919A true CN105799919A (en) | 2016-07-27 |
Family
ID=56453493
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610162023.1A Pending CN105799919A (en) | 2016-03-22 | 2016-03-22 | Oil-driven multi-rotor wing air vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN105799919A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103359284A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | Petrol-electric hybrid four-rotor unmanned aerial vehicle |
| US8774982B2 (en) * | 2010-08-26 | 2014-07-08 | Leptron Industrial Robotic Helicopters, Inc. | Helicopter with multi-rotors and wireless capability |
| CN203698658U (en) * | 2014-01-06 | 2014-07-09 | 江苏神谷无人飞行器技术有限公司 | Foldable multi-rotor unmanned aerial vehicle |
| CN203958614U (en) * | 2014-07-24 | 2014-11-26 | 山东新晨科技有限公司 | Integral type multi-rotor aerocraft |
| CN204452926U (en) * | 2015-02-10 | 2015-07-08 | 曹兵 | The dynamic many rotor wing unmanned aerial vehicles of variable pitch shaft drive of oil |
| CN205707321U (en) * | 2016-03-22 | 2016-11-23 | 山东乾通航空科技有限公司 | The dynamic multi-rotor aerocraft of oil |
-
2016
- 2016-03-22 CN CN201610162023.1A patent/CN105799919A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8774982B2 (en) * | 2010-08-26 | 2014-07-08 | Leptron Industrial Robotic Helicopters, Inc. | Helicopter with multi-rotors and wireless capability |
| CN103359284A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | Petrol-electric hybrid four-rotor unmanned aerial vehicle |
| CN203698658U (en) * | 2014-01-06 | 2014-07-09 | 江苏神谷无人飞行器技术有限公司 | Foldable multi-rotor unmanned aerial vehicle |
| CN203958614U (en) * | 2014-07-24 | 2014-11-26 | 山东新晨科技有限公司 | Integral type multi-rotor aerocraft |
| CN204452926U (en) * | 2015-02-10 | 2015-07-08 | 曹兵 | The dynamic many rotor wing unmanned aerial vehicles of variable pitch shaft drive of oil |
| CN205707321U (en) * | 2016-03-22 | 2016-11-23 | 山东乾通航空科技有限公司 | The dynamic multi-rotor aerocraft of oil |
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Application publication date: 20160727 |