CN106492478A - There are the model plane of integrated control system - Google Patents
There are the model plane of integrated control system Download PDFInfo
- Publication number
- CN106492478A CN106492478A CN201510560062.2A CN201510560062A CN106492478A CN 106492478 A CN106492478 A CN 106492478A CN 201510560062 A CN201510560062 A CN 201510560062A CN 106492478 A CN106492478 A CN 106492478A
- Authority
- CN
- China
- Prior art keywords
- control system
- model plane
- integrated control
- engine
- 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.)
- Pending
Links
Landscapes
- Toys (AREA)
Abstract
The invention discloses a kind of model plane with integrated control system, the model plane that should have integrated control system include main frame, upper lid, landing gear, Power Component and control board, the Power Component includes the main shaft of engine, the engine gear being installed on the engine and engine gear connection, the main screw being fixed on the main shaft, and the engine is miniature oil-burning machine.The present invention has the strong model plane with integrated control system of super remote endurance, powerful, mobility.
Description
Technical field
A kind of a kind of the present invention relates to electronic toy, more particularly to model plane with integrated control 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 with integrated control system shorter, and motor mechanomotive force has certain limitation, not powerful enough.
Therefore, a kind of flight time length of our demands, the model plane with integrated control system of powerful.
Content of the invention
The deficiencies in the prior art are based on, problem to be solved by this invention is to provide a kind of model plane with integrated control system strong with super remote endurance, powerful, mobility.
For solving the above problems, the model plane with integrated control system that the present invention is provided include a kind of model plane with integrated control system, the model plane that should have integrated control system include main frame, the upper lid being connected in front of main frame, it is connected to the empennage at main frame rear, support the landing gear of the main frame, the Power Component being arranged on the main frame, and external signal can be received and the control board of the Power Component can be controlled according to external signal, the Power Component includes engine, the engine gear being installed on the engine, the main shaft being connected with the engine gear, the main screw being fixed on the main shaft, the engine is miniature oil-burning machine.
Used as one embodiment, the model plane with integrated control system also include the fuel tank and the noise reduction device being installed on the engine for providing oil plant for miniature oil-burning machine.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.
As another embodiment, remote control clutch between the engine gear and main shaft, is connected with.The remote control clutch include the remote control clutch lower cover being connected with engine gear and the remote control clutch lower cover connection bearing, connect the power output friction plate of the bearing, connect the remote control clutch rotating disk of the power output friction plate.Fan is additionally provided between the remote control clutch rotating disk and main shaft, the fan can prevent miniature oil-burning machine heating and cause temperature too high.
Used as another embodiment, the model plane with integrated control system also include balanced component, and the balanced component includes the balancing pole for being installed on main shaft top and the balance blade for being arranged at the balancing pole two ends.It is more safe and reliable that the balanced component makes the model plane with integrated control system fly.
As further embodiment; the model plane with integrated control system also include steering assembly and H type fixed mounts; the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar for connecting the steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch, and the steering assembly efficiently controls the model plane with integrated control system and flexibly turns to.Which also includes the battery for providing electric energy for the control board, steering wheel.The H types fixed mount is used for installing battery, control board.
Compared with prior art, the model plane with integrated control system of the present invention drive aircraft flight by miniature oil-burning machine, and therefore the model plane with integrated control system of the invention have the strong model plane with integrated control system of super remote endurance, powerful, mobility.
For making the present invention easier to understand, below in conjunction with the model plane with integrated control system that accompanying drawing is expanded on further the present invention.
Description of the drawings
Schematic diagrames of the Fig. 1 for the model plane with integrated control 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 model plane with integrated control system of the present embodiment include main frame 1, the upper lid 2 being connected in front of main frame 1, the empennage 3 for being connected to 1 rear of main frame, the landing gear 4 for supporting the main frame 1, the Power Component 5 being arranged on the main frame 1, can receive external signal and can control the control board 6 of the Power Component 5 according to external signal.The main frame 1 is made by special material plate, and which passes through all component that the whole model of an airplane fixed by each fixture.
The Power Component 5 includes the main shaft of miniature oil-burning machine, the engine gear being installed on the engine and engine gear connection, the main screw being fixed on the main shaft.
Remote control clutch is connected with the engine gear.The remote control clutch include the remote control clutch lower cover being connected with engine gear and the remote control clutch lower cover connection bearing, connect the power output friction plate of the bearing, connect 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 heating and cause temperature too high.
The model plane with integrated control system also include the fuel tank and the noise reduction device being installed on the engine for providing oil plant for miniature oil-burning machine.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.The fuel tank includes the casing of oil bunkering, the first briquetting, the second briquetting, flexible rubber hose and aluminum pipe.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 for sealing the opening, makes the fuel oil in casing occur without leakage.Through hole is designed with first briquetting, the second briquetting, flexible rubber hose, and the aluminum pipe is hollow pipe, and the aluminum pipe is connected through the through hole with casing, for fuel oil being provided to miniature oil-burning machine.
The empennage 3 includes the foot piece being connected with main frame 1 and and the tail screw that is arranged on foot piece.
The model plane with integrated control system also include balanced component, and the balanced component includes the balancing pole being installed on main shaft and is arranged at the balance blade at the balancing pole two ends.It is more steadily safe and reliable that the balanced component makes the model plane with integrated control system fly.
The model plane with integrated control system also include steering assembly 0 and H type fixed mounts; the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar for connecting the steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch, and the steering assembly efficiently controls the model plane with integrated control system and flexibly turns to.Which also includes the battery for providing electric energy for the control board, steering wheel.The H types fixed mount is used for installing battery, control board.
The model plane with integrated control system of the present invention drive the model plane with integrated control system to fly by miniature oil-burning machine, improve genemotor because of battery energy storage is less, be short of power situation.Therefore the present invention has the strong model plane with integrated control system of super remote endurance, powerful, mobility.
Above disclosed is only presently preferred embodiments of the present invention, can not limit certainly the interest field of the present invention with this, and the equivalent variations that is therefore made according to scope of the present invention patent still belong to the scope covered by the present invention.
Claims (9)
1. a kind of model plane with integrated control system, it is characterised in that：Which includes main frame, upper lid, landing gear, Power Component and control board, the upper lid is placed in main frame top, the landing gear is placed in main frame bottom, the Power Component and control board are inside main frame, the Power Component includes the main shaft of engine, the engine gear being installed on the engine and engine gear connection, the main screw being fixed on the main shaft, and the engine is miniature oil-burning machine.
2. there are the model plane of integrated control system as claimed in claim 1, it is characterised in that：Remote control clutch is connected between the engine gear and main shaft.
3. there are the model plane of integrated control system as claimed in claim 2, it is characterised in that：The remote control clutch include the remote control clutch lower cover being connected with engine gear and the remote control clutch lower cover connection bearing, connect the power output friction plate of the bearing, connect the remote control clutch rotating disk of the power output friction plate.
4. there are the model plane of integrated control system as claimed in claim 3, it is characterised in that：Fan is additionally provided between the remote control clutch rotating disk and main shaft.
5. there are the model plane of integrated control system as claimed in claim 1, it is characterised in that：Which also includes the noise reduction device being installed on the engine.
6. there are the model plane of integrated control system as claimed in claim 1, it is characterised in that：Which also includes balanced component, and the balanced component includes the balancing pole for being installed on main shaft top and the balance blade for being arranged at the balancing pole two ends.
7. there are the model plane of integrated control system as claimed in claim 1, it is characterised in that：Which also includes steering assembly, and the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar for connecting the steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch.
8. there are the model plane of integrated control system as claimed in claim 7, it is characterised in that：Which also includes the battery for providing electric energy for the control board, steering wheel.
9. there are the model plane of integrated control system as claimed in claim 8, it is characterised in that：Which also includes that the H type fixed mounts being arranged on main frame, the battery, control board are installed on the H type fixed mounts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510560062.2A CN106492478A (en) | 2015-09-03 | 2015-09-03 | There are the model plane of integrated control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510560062.2A CN106492478A (en) | 2015-09-03 | 2015-09-03 | There are the model plane of integrated control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106492478A true CN106492478A (en) | 2017-03-15 |
Family
ID=58286486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510560062.2A Pending CN106492478A (en) | 2015-09-03 | 2015-09-03 | There are the model plane of integrated control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106492478A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106540461A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Model plane with integrated chip |
| CN106563274A (en) * | 2015-10-10 | 2017-04-19 | 马铿钧 | Intelligent model airplane |
| CN106563277A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | Model airplane having integration control system |
| CN106606880A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A model airplane with a micro-fuel oil machine |
-
2015
- 2015-09-03 CN CN201510560062.2A patent/CN106492478A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106540461A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Model plane with integrated chip |
| CN106563277A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | Model airplane having integration control system |
| CN106563274A (en) * | 2015-10-10 | 2017-04-19 | 马铿钧 | Intelligent model airplane |
| CN106606880A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A model airplane with a micro-fuel oil machine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106492478A (en) | There are the model plane of integrated control system | |
| US8096497B2 (en) | Power assembly and a coaxial twin propeller model helicopter using the same | |
| CN106474746A (en) | Model plane with super remote endurance | |
| CN106492473A (en) | The strong flight system of novel operating | |
| CN204337750U (en) | High sensitivity aircraft | |
| CN106492479A (en) | There is diesel-driven flight system | |
| CN106552428A (en) | Gear drive model plane | |
| CN106540461A (en) | Model plane with integrated chip | |
| CN106466529A (en) | Gyroplane break-in control device | |
| CN106466527A (en) | The new complex controll rudder face based on aerodynamic force and direct force | |
| CN106563277A (en) | Model airplane having integration control system | |
| CN106606871A (en) | Aircraft having flight protection system | |
| CN205084407U (en) | Super endurance flying device far away | |
| CN201070541Y (en) | Model airplane | |
| CN106823405A (en) | Miniature oil-burning machine model plane | |
| CN208070047U (en) | A kind of fixed structure of aircraft accessory casing | |
| CN106552432A (en) | The system for effectively improving flying power | |
| CN106552429A (en) | High transmission efficiency flight instruments | |
| CN106563274A (en) | Intelligent model airplane | |
| CN106606880A (en) | A model airplane with a micro-fuel oil machine | |
| CN106606874A (en) | Novel aircraft power system | |
| CN101003302A (en) | An aviation aircraft | |
| CN106563272A (en) | Novel flight system with high operability | |
| CN106823400A (en) | Novel aircrafts dynamical system | |
| CN109464814A (en) | Model plane azimuth control system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170315 |
|
| WD01 | Invention patent application deemed withdrawn after publication |