CN106669170A - Aero-model implementation video monitoring system - Google Patents
Aero-model implementation video monitoring system Download PDFInfo
- Publication number
- CN106669170A CN106669170A CN201510758168.3A CN201510758168A CN106669170A CN 106669170 A CN106669170 A CN 106669170A CN 201510758168 A CN201510758168 A CN 201510758168A CN 106669170 A CN106669170 A CN 106669170A
- Authority
- CN
- China
- Prior art keywords
- skeleton
- main framing
- pitman
- central controller
- monitoring system
- 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- Withdrawn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 an aero-model implementation video monitoring system which comprises a framework, a direction control device and a central controller, wherein the direction control device is mounted at the tail end of the framework, and the central controller is mounted in the framework. The aero-model implementation video monitoring system is quite simple in structure, light in weight, easy to control and freer to operate, so that the system is widely applicable to various flight sites.
Description
Technical field
The present invention relates to electronic toy field, espespecially a kind of model airplane realizes video monitoring system.
Background technology
Mould aircraft has been liked always since emerge by people, to meet consumer demand, toy manufacturer continually develops various helicopter models and carries out sustained improvement, general mould aircraft can only be with hand-thrown type or wheeled rolling start, for pad has certain selectivity, running into space with obstacle cannot be freely lifted, and greatly limit the entertainment environment of border mould Air Fan.And, general mould aircraft systems are complex, high cost, and are difficult to control.
In view of this, there is provided a kind of simple structure, it is easy to control model airplane and realize that video monitoring system is very necessary.
The content of the invention
Based on the deficiencies in the prior art, present invention is primarily targeted at providing a kind of simple structure, it is easy to control environment mould aircraft.
In order to achieve the above object, the invention provides a kind of model airplane realizes video monitoring system, including skeleton and remote control, the skeleton includes skeleton, direction control device and central controller, the direction control device is installed on skeleton end, central controller is installed in skeleton, the skeleton includes main framing, anterior skeleton and bottom skeleton, anterior skeleton is fixed on the front center of main framing, the built-in central controller of central cavity, the bottom skeleton is installed on main framing lower section, i.e., by main framing described in the skeletal support of bottom.Skeleton still further comprises horizontal skeleton, and it crosses at main framing lower section, and the bottom skeleton is installed on horizontal skeleton lower section, and main framing is fixed on the skeleton of bottom by the wood of strengthening.
The direction control device includes wing and pitman, and the wing is connected by pitman with central controller.Wing includes some pieces of flat boards and wood of weighing and considering in order to uphold justice, and flat board is installed on main framing, and wood of weighing and considering in order to uphold justice is propped by flat board, and keeps level with main framing.Pitman is included the position controller pitman coordinated with fluid rotary device and turns to pitman, flat board is connected with central controller by the position controller pitman coordinated with fluid rotary device, is connected main framing with wood of weighing and considering in order to uphold justice by turning to pitman.
The central controller includes power supply, integrated control unit, signal receiving/transmission device, motor locating device, motor, gearbox, fluid rotary device and the position controller coordinated with fluid rotary device, wherein, power supply, integrated control unit and signal receiving/transmission device are built in the cavity of anterior skeleton, integrated control unit is electrically connected with signal receiving/transmission device, motor locating device is built in gearbox, it is built-in with motor, and motor is electrically connected with the power supply, and its end is provided with motor gear.The gearbox is provided with transmission main shaft and gearbox gear, and transmission main shaft runs through gearbox gear, and the gearbox gear is meshed with motor gear.Fluid rotary device includes skull and blade, and transmission main shaft sequentially runs through the gearbox gear, the blade of fluid rotary device and skull, and blade is fixed between skull and gearbox gear.The position controller coordinated with fluid rotary device is built in the anterior skeleton, and is electrically connected with integrated control unit, and it is connected by the position controller pitman coordinated with fluid rotary device with flat board.
Compared with prior art, the model airplane of the present invention realizes video monitoring system structure very simple, it is lightweight, easily controllable and outgoing carrying, roomy main framing makes its flight more steadily, and manipulate more freely, and, flying field is less demanding, it is only necessary to more than ten square metres of clear space.
To make the present invention easier to understand, the specific embodiment that a kind of model airplane of the invention realizes video monitoring system is expanded on further below in conjunction with accompanying drawing.
Description of the drawings
Fig. 1 is the structural representation of the skeleton that model airplane of the present invention realizes video monitoring system；
Fig. 2 is the disassembly diagram of the skeleton that model airplane of the present invention realizes video monitoring system；
Fig. 3 is the schematic diagram of the anterior skeleton that model airplane of the present invention realizes video monitoring system；
Fig. 4 is the structural representation of the direction control device that model airplane of the present invention realizes video monitoring system.
Specific embodiment
Below in conjunction with the accompanying drawings, the present invention will be further described.Shown in seeing figures.1.and.2, the model airplane of the present invention realizes that video monitoring system includes main framing 100.Wherein, the main framing 100 mainly includes main framing 10, direction control device 20 and central controller 30.The direction control device 20 is installed on the end of main framing 10, and central controller 30 is installed in main framing 10.
Shown in seeing figures.1.and.2, main framing 10 includes main framing 101, anterior main framing 102, horizontal main framing 103 and two bottom main framings 104., used as the supporting mechanism of main framing 10, with roomy plane, its is light and thin, and surface is smooth for main framing 101, with impact resistance, is made using the material of corrosion resistance.Anterior main framing 102 is fixed on the front center of main framing 101, its trapezoidal cell body, the built-in central controller 30 of central cavity.Laterally main framing 103 crosses at the lower section of main framing 101, the bottom main framing 104 is installed on the lower section of horizontal main framing 103, support the main framing 101 by two bottom main framings 104, improve the height of skeleton, fluid rotary device is safely rotated, avoid fluid rotary device they strike ground and cause to damage, it is steady and safe when also ensure that skeleton rises and falls.
In one embodiment of the invention, main framing 10 also includes bottom Matrix patches 105, the bottom Matrix patches 105 are made using abrasive material, the smooth bottom surface in the bottom main framing 104 so that model airplane realizes that video monitoring system also can be slided in water.
Referring to figs. 1 to shown in Fig. 3, direction control device 20 includes wing 201 and pitman 202.Wherein, the wing 201 includes three pieces of flat board 201a and the wooden 201b that weighs and consider in order to uphold justice.Three pieces of flat board 201a are installed on the afterbody of the main framing 101, and it is perpendicular with it, wherein two pieces flat board 201a are symmetrically installed on the both sides of the main framing 101, in addition one flat plate 201a is then installed on the rear center of main framing 101, three pieces of flat board 201a are with high, its end sets up the weigh and consider in order to uphold justice wooden 201b parallel with main framing 101, keeps the smooth flight of skeleton.Pitman 202 includes the position controller pitman 202a coordinated with fluid rotary device and turns to pitman 202b, wherein, flat board 201a and main framing 101 are connected with the position controller coordinated with fluid rotary device of central controller 30 by the position controller pitman 202a that coordinates with fluid rotary device, i.e., the position controller by coordinating with fluid rotary device respectively manipulates vacillating now to the left, now to the right and flying up and down for skeleton.Main framing 101 is connected with the wooden 201b that weighs and consider in order to uphold justice by turning to pitman 202b, it is ensured that whole machine is steady in flight course.
With reference to shown in Fig. 1 and Fig. 3, central controller 30 includes that power supply 301, integrated control unit 302, signal receiving/transmission device 303, motor locating device 304, motor 305, speed regulator fix wood 306, gearbox 307, fluid rotary device 308 and three position controllers 309 coordinated with fluid rotary device.Wherein, power supply 301, integrated control unit 302 and signal receiving/transmission device 303 are built in the cavity of anterior main framing 102.Integrated control unit 302 is electrically connected with signal receiving/transmission device 303, and by signal receiving/transmission device 303 wireless signal that remote control sends is received, then carries out reception processing by integrated control unit 302, and then manipulates the flight of skeleton.Motor locating device 304 is built in gearbox 307, and it is built-in with motor 305, and the end of motor 305 is provided with motor gear 305a, and motor 305 is electrically connected with power supply 301, is provided power drive motor 305 by power supply 301 and is rotated at a high speed.Motor locating device 304 is fixed on speed regulator by screw to be fixed on wood 306 so that motor 302 being capable of steadily start.The gearbox 307 is provided with transmission main shaft 307a and gearbox gear 307b.The fluid rotary device 308 includes skull 308a and blade 308b, transmission main shaft 307a sequentially runs through the gearbox gear 307b, the blade 308b of fluid rotary device 308 and skull 308a, and blade 308b is fixed between skull 308a and gearbox gear 305a；Meanwhile, gearbox gear 305a is meshed with motor gear 305a so that motor 305 can drive the start of fluid rotary device 308.It is described to be respectively 309a, 309b and 309c with the position controller 309 that fluid rotary device coordinates, it is built in respectively in the anterior main framing 102, and be electrically connected with integrated control unit 302, this three position controllers 309 coordinated with fluid rotary device are connected by the position controller pitman 202a coordinated with fluid rotary device with flat board 201a, the position controller 309a and 309b for wherein coordinating with fluid rotary device is used to manipulate the flight up and down of skeleton, is used to manipulate the left and right flight of skeleton with the position controller 309c that fluid rotary device coordinates.
In one embodiment of the invention, the central controller 30 still further comprises some pieces of speed regulator fixed plates 300, fixes speed regulator by the speed regulator fixed plate 300 and fixes wood 306, strengthens the steady running of central controller 30.
The model airplane of the present invention realizes video monitoring system structure very simple, it is lightweight, easily controllable and outgoing carrying, roomy main framing makes its flight more steadily, and manipulate more freely, and, because it rises and falls without castor, without hand-thrown, flying field is less demanding, it is only necessary to more than ten square metres of clear space.
Claims (5)
1. a kind of model airplane realizes video monitoring system, it is characterised in that：Including skeleton, direction control device and central controller, the direction control device is installed on skeleton end, central controller is installed in skeleton, the skeleton includes main framing, anterior skeleton and bottom skeleton, anterior skeleton is fixed on the front center of main framing, the built-in central controller of central cavity, the bottom skeleton is installed on main framing lower section, pass through main framing described in the skeletal support of bottom, the skeleton still further comprises horizontal skeleton, it crosses at main framing lower section, the bottom skeleton is installed on horizontal skeleton lower section, main framing is fixed on the skeleton of bottom by the horizontal skeleton.
2. model airplane as claimed in claim 1 realizes video monitoring system, it is characterised in that：The direction control device includes wing and pitman, and the wing is connected by pitman with central controller, and the wing includes some pieces of flat boards and wood of weighing and considering in order to uphold justice, and flat board is installed on main framing, and wood of weighing and considering in order to uphold justice is propped by flat board, and keeps level with main framing.
3. model airplane as claimed in claim 1 realizes video monitoring system, it is characterised in that：The pitman includes the position controller pitman coordinated with fluid rotary device and turns to pitman, flat board is connected with central controller by the position controller pitman coordinated with fluid rotary device, is connected main framing with wood of weighing and considering in order to uphold justice by turning to pitman.
4. model airplane as claimed in claim 1 realizes video monitoring system, it is characterised in that：The central controller includes power supply, integrated control unit, signal receiving/transmission device, motor locating device, motor and gearbox, wherein, power supply, integrated control unit and signal receiving/transmission device are built in the cavity of anterior skeleton, integrated control unit is electrically connected with signal receiving/transmission device, motor locating device is built in gearbox, it is built-in with motor, motor is electrically connected with the power supply, its end is provided with motor gear, the gearbox is provided with transmission main shaft and gearbox gear, transmission main shaft runs through gearbox gear, the gearbox gear is meshed with motor gear.
5. model airplane as claimed in claim 4 realizes video monitoring system, it is characterised in that：The central controller still further comprises fluid rotary device, and it includes skull and blade, and transmission main shaft sequentially runs through the gearbox gear, the blade of fluid rotary device and skull, and blade is fixed between skull and gearbox gear；The central controller still further comprises the position controller coordinated with fluid rotary device, it is built in the anterior skeleton, and be electrically connected with integrated control unit, the position controller coordinated with fluid rotary device is connected by the position controller pitman coordinated with fluid rotary device with flat board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510758168.3A CN106669170A (en) | 2015-11-07 | 2015-11-07 | Aero-model implementation video monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510758168.3A CN106669170A (en) | 2015-11-07 | 2015-11-07 | Aero-model implementation video monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106669170A true CN106669170A (en) | 2017-05-17 |
Family
ID=58863422
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510758168.3A Withdrawn CN106669170A (en) | 2015-11-07 | 2015-11-07 | Aero-model implementation video monitoring system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106669170A (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103816670A (en) * | 2013-12-19 | 2014-05-28 | 广东立沃信息科技有限公司 | Model airplane video monitoring implementation system |
| CN204337755U (en) * | 2014-10-25 | 2015-05-20 | 马铿钧 | Accurate control type mould aircraft |
-
2015
- 2015-11-07 CN CN201510758168.3A patent/CN106669170A/en not_active Withdrawn
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103816670A (en) * | 2013-12-19 | 2014-05-28 | 广东立沃信息科技有限公司 | Model airplane video monitoring implementation system |
| CN204337755U (en) * | 2014-10-25 | 2015-05-20 | 马铿钧 | Accurate control type mould aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101965217B (en) | Acrobatic rotary-wing toy helicopter | |
| JP5497373B2 (en) | Propeller toy | |
| CN205060006U (en) | Four -rotor unmanned aerial vehicle | |
| CN204337755U (en) | Accurate control type mould aircraft | |
| CN102887224B (en) | Insect flapping wing simulating aircraft | |
| CN2882743Y (en) | Model airplane | |
| CN106669170A (en) | Aero-model implementation video monitoring system | |
| CN202569558U (en) | Remote controlled single-rotor helicopter model structure | |
| CN204219777U (en) | aerial toy | |
| CN105617679A (en) | Accurate-control model airplane | |
| CN107335232A (en) | One kind lifting and gliding mating type remote control distributor toy | |
| JP2017190091A (en) | Tray type multi-copter | |
| CN203916079U (en) | Have the fixed wing aircraft toy of helicopter function concurrently | |
| CN105797398A (en) | Remote-controlled flying toy having strong impact resistance | |
| CN2848315Y (en) | Aircraft model | |
| CN202087051U (en) | Remote control capable of being operated by one hand and toy | |
| CN203525315U (en) | Vertical take-off and landing fixed-wing model plane toy | |
| CN108066999A (en) | Blended wing-body list culvert vertical take-off and landing aircraft | |
| CN106672228A (en) | Multi-blade rotor tandem type aircraft | |
| CN203601562U (en) | Boomerang quadrotor aircraft | |
| CN203355289U (en) | Triaxial flying device | |
| CN102743880A (en) | Disc-shaped aircraft toy | |
| CN203494166U (en) | Telecontrolled aircraft with side wings and side rollers | |
| CN203075664U (en) | Flying machine | |
| CN207024636U (en) | A kind of small-sized aerial model airplane |
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: 20170517 |
|
| WW01 | Invention patent application withdrawn after publication | ||
| DD01 | Delivery of document by public notice |
Addressee: Ma Kengjie Document name: Notification of Approving Refund |
|
| DD01 | Delivery of document by public notice |