CN106621386A - Novel model airplane avoidance system - Google Patents
Novel model airplane avoidance system Download PDFInfo
- Publication number
- CN106621386A CN106621386A CN201510728817.5A CN201510728817A CN106621386A CN 106621386 A CN106621386 A CN 106621386A CN 201510728817 A CN201510728817 A CN 201510728817A CN 106621386 A CN106621386 A CN 106621386A
- Authority
- CN
- China
- Prior art keywords
- model airplane
- engine
- flight
- avoidance system
- main shaft
- 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- Withdrawn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
Landscapes
- Toys (AREA)
Abstract
The invention discloses a novel model airplane avoidance system. The novel model airplane avoidance system comprises an airplane body, an upper cover, a landing device, a flight driving mechanism and a flight anti-collision device. The system disclosed by the invention has the advantages that a model airplane could avoid obstacles during flight in the air; continuous flight performance of the model airplane could be enhanced; practicability is high; and promotion and application are easy.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly to a kind of Novel model airplane avoidance system.
Background technology
Aircraft has been increasingly becoming the toy of people's fashion.Existing aircraft is all driven with electric motor, is so typically necessary offer battery, but existing battery electric quantity amount of storage is extremely limited.Cause the follow-on mission time of model plane shorter, and motor mechanomotive force has certain limitation, it is not powerful enough, even if where open, during without other barriers, multi rack aeromodelling airplane flies in the air simultaneously, and still suffering from collision may, a series of troubles are caused, therefore the setting of the anticollision device, collision-prevention device of aeromodelling airplane is very necessary.
The content of the invention
Based on the deficiencies in the prior art, problem to be solved by this invention is to provide a kind of Novel model airplane avoidance system strong with super remote endurance, powerful, mobility.
To solve the above problems, the Novel model airplane avoidance system that the present invention is provided includes a kind of Novel model airplane avoidance system, the Novel model airplane avoidance system includes fuselage body, the upper lid being connected in front of fuselage body, it is connected to the empennage at fuselage body rear, support the landing gear of the fuselage body, the flight drive mechanism being arranged on the fuselage body, and external signal can be received and the flight collision avoidance device of the flight drive mechanism can be controlled according to external signal, the flight drive mechanism includes engine, the engine gear being installed on the engine, the main shaft being connected with the engine gear, the forward propeller being fixed on the main shaft, the engine is miniature oil-burning machine.
Used as one embodiment, the Novel model airplane avoidance system also includes the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the engine.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.
Compared with prior art, the present invention can realize avoidance of the to barrier during aeromodelling airplane flight in the air, improve the follow-on mission performance of aeromodelling airplane, practical, easy to utilize.
To make the present invention easier to understand, the Novel model airplane avoidance system of the present invention is expanded on further below in conjunction with accompanying drawing.
Description of the drawings
Fig. 1 is the schematic diagram of the Novel model airplane avoidance system of a preferred embodiment of the present invention.
Specific embodiment
With reference now to Description of Drawings the preferred embodiments of the present invention,.
With reference to Fig. 1, the Novel model airplane avoidance system of the present embodiment includes fuselage body 1, the upper lid 2 that is connected to the front of fuselage body 1, the empennage 3 for being connected to the rear of fuselage body 1, the landing gear 4 for supporting the fuselage body 1, the flight drive mechanism 5 being arranged on the fuselage body 1, can receive external signal and the flight collision avoidance device 6 of the flight drive mechanism 5 can be controlled according to external signal.The fuselage body 1 is made by special material plate, and it passes through all component that each fixture fixes the whole model of an airplane.
The flight drive mechanism 5 includes miniature oil-burning machine, the main shaft of the engine gear being installed on the engine and the engine gear connection, the forward propeller being fixed on the main shaft.
Remote control clutch is connected with the engine gear.The remote control clutch includes the bearing of the remote control clutch lower cover being connected with engine gear and remote control clutch lower cover connection, connects the power output friction plate of the bearing, connects the remote control clutch rotating disk of the power output friction plate.It is additionally provided between the remote control clutch rotating disk and main shaft and is sequentially provided with fan, unilateral bearing, start-up rod joint and output sleeve.The fan can prevent miniature oil-burning machine from generating heat and causing temperature too high.
The Novel model airplane avoidance system also includes the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the engine.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.The fuel tank includes casing, the first briquetting, the second briquetting, flexible rubber hose and the aluminum pipe of oil bunkering.The casing is provided with an opening, and first briquetting and the second briquetting are fixedly installed on flexible rubber hose in the opening, and the flexible rubber hose is used to seal the opening, makes the fuel oil in casing occur without leakage.Through hole is designed with first briquetting, the second briquetting, flexible rubber hose, the aluminum pipe is hollow pipe, and the aluminum pipe is connected through the through hole with casing, for providing fuel oil to miniature oil-burning machine.
The empennage 3 includes the foot piece being connected with fuselage body 1 and and the tail screw that is arranged on foot piece.
The Novel model airplane avoidance system also includes balanced component, and the balanced component includes the balancing pole being installed on main shaft and the balance blade for being arranged at the balancing pole two ends.The balanced component makes the flight of Novel model airplane avoidance system more steady safe and reliable.
The Novel model airplane avoidance system also includes steering assembly 0 and drum fixed mount, the steering assembly includes the pitch being installed on main shaft, steering wheel, connect the steering wheel and pitch pull bar, turning sleeve and it is connected the connecting rod of the turning sleeve and pitch, the steering assembly efficiently controls Novel model airplane avoidance system and flexibly turns to.It also includes the battery for providing electric energy for the flight collision avoidance device, steering wheel.The drum fixed mount is used to install battery, flight collision avoidance device.
The Novel model airplane avoidance system of the present invention drives the flight of Novel model airplane avoidance system by miniature oil-burning machine, improves genemotor because of battery energy storage is less, be short of power situation.Therefore the present invention is with the strong Novel model airplane avoidance system of super remote endurance, powerful, mobility.
Above disclosed is only presently preferred embodiments of the present invention, can not limit the interest field of the present invention, therefore the equivalent variations made according to scope of the present invention patent with this certainly, still belongs to the scope that the present invention is covered.
Claims (3)
1. a kind of Novel model airplane avoidance system, it is characterised in that：It includes fuselage body, upper lid, landing gear, empennage, flight drive mechanism and flight collision avoidance device, the upper lid is placed in fuselage body top, the landing gear is placed in fuselage body bottom, the flight drive mechanism and flight collision avoidance device are arranged on inside fuselage body, the flight drive mechanism includes engine, the main shaft of the engine gear being installed on the engine and the engine gear connection, the forward propeller being fixed on the main shaft, and the engine is miniature oil-burning machine；It is connected with remote control clutch between the engine gear and main shaft, the remote control clutch includes the bearing of the remote control clutch lower cover being connected with engine gear and remote control clutch lower cover connection, connects the power output friction plate of the bearing, connects the remote control clutch rotating disk of the power output friction plate.
2. Novel model airplane avoidance system as claimed in claim 1, it is characterised in that：It also includes noise reduction device and balanced component, and the balanced component includes being installed on the balancing pole on main shaft top and being arranged at the balance blade at the balancing pole two ends.
3. Novel model airplane avoidance system as claimed in claim 1, it is characterised in that：It also includes steering assembly and the battery that provides electric energy for the flight collision avoidance device, steering wheel, and the steering assembly includes the pull bar of the pitch being installed on main shaft, steering wheel, the connection steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510728817.5A CN106621386A (en) | 2015-10-29 | 2015-10-29 | Novel model airplane avoidance system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510728817.5A CN106621386A (en) | 2015-10-29 | 2015-10-29 | Novel model airplane avoidance system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106621386A true CN106621386A (en) | 2017-05-10 |
Family
ID=58809591
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510728817.5A Withdrawn CN106621386A (en) | 2015-10-29 | 2015-10-29 | Novel model airplane avoidance system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106621386A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201445800U (en) * | 2009-06-25 | 2010-05-05 | 汕头市澄海区锦江玩具实业有限公司 | Coaxial double rotor wing remote control helicopter and obstacle avoidance system thereof |
| CN201551846U (en) * | 2009-12-01 | 2010-08-18 | 周益波 | Model airplane wing component structure and model airplane including same |
| CN202061382U (en) * | 2011-05-09 | 2011-12-07 | 蓝帽子(厦门)文化传播有限公司 | Infrared induction flying saucer |
| CN104645626A (en) * | 2014-12-01 | 2015-05-27 | 赵旭 | Infrared gesture-sensing toy structure and application thereof |
| CN106606871A (en) * | 2015-10-26 | 2017-05-03 | 马铿钧 | Aircraft having flight protection system |
-
2015
- 2015-10-29 CN CN201510728817.5A patent/CN106621386A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201445800U (en) * | 2009-06-25 | 2010-05-05 | 汕头市澄海区锦江玩具实业有限公司 | Coaxial double rotor wing remote control helicopter and obstacle avoidance system thereof |
| CN201551846U (en) * | 2009-12-01 | 2010-08-18 | 周益波 | Model airplane wing component structure and model airplane including same |
| CN202061382U (en) * | 2011-05-09 | 2011-12-07 | 蓝帽子(厦门)文化传播有限公司 | Infrared induction flying saucer |
| CN104645626A (en) * | 2014-12-01 | 2015-05-27 | 赵旭 | Infrared gesture-sensing toy structure and application thereof |
| CN106606871A (en) * | 2015-10-26 | 2017-05-03 | 马铿钧 | Aircraft having flight protection system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8096497B2 (en) | Power assembly and a coaxial twin propeller model helicopter using the same | |
| CN105752331A (en) | Single-internal combustion engine power multi-rotor wing unmanned aerial vehicle based on variable pitch control | |
| CN106492478A (en) | There are the model plane of integrated control system | |
| CN101177167A (en) | Power-driven system of aircraft | |
| CN204279919U (en) | For folding oar pull-type before motor glider | |
| CN106606871A (en) | Aircraft having flight protection system | |
| CN204337750U (en) | High sensitivity aircraft | |
| CN106492473A (en) | The strong flight system of novel operating | |
| CN106474746A (en) | Model plane with super remote endurance | |
| CN106621386A (en) | Novel model airplane avoidance system | |
| CN106466527A (en) | The new complex controll rudder face based on aerodynamic force and direct force | |
| CN205770148U (en) | A kind of can the Fixed Wing AirVehicle of VTOL | |
| CN106552428A (en) | Gear drive model plane | |
| CN106540461A (en) | Model plane with integrated chip | |
| CN106563277A (en) | Model airplane having integration control system | |
| CN106552432A (en) | The system for effectively improving flying power | |
| CN106492479A (en) | There is diesel-driven flight system | |
| CN201070541Y (en) | Model airplane | |
| CN106466529A (en) | Gyroplane break-in control device | |
| CN101003302A (en) | An aviation aircraft | |
| CN205084407U (en) | Super endurance flying device far away | |
| CN106563274A (en) | Intelligent model airplane | |
| CN106823405A (en) | Miniature oil-burning machine model plane | |
| RU2611470C1 (en) | Device for rotor prespinning of unmanned autogyro | |
| CN106606880A (en) | A model airplane with a micro-fuel oil machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170510 |
|
| WW01 | Invention patent application withdrawn after publication |