CN105797402A - Toy aircraft remote-control intelligent control system - Google Patents
Toy aircraft remote-control intelligent control system Download PDFInfo
- Publication number
- CN105797402A CN105797402A CN201410855395.3A CN201410855395A CN105797402A CN 105797402 A CN105797402 A CN 105797402A CN 201410855395 A CN201410855395 A CN 201410855395A CN 105797402 A CN105797402 A CN 105797402A
- Authority
- CN
- China
- Prior art keywords
- control system
- toy aircraft
- aircraft remote
- remote intelligence
- tail vane
- 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 provides a toy aircraft remote-control intelligent control system, which is composed of a main body and an integrated control chip, wherein a function display signal lamp and a plurality of control buttons are arranged on the panel; the control buttons include a mode change-over switch, a positive and negative direction control button, a delay regulator and a maximal stroke regulator; and the various control buttons electrically communicate with the integrated control chip. According to the toy aircraft remote-control intelligent control system, a sensor and a controller are integrally combined; and the modes of steering engines can be switched and selected by virtue of the mode change-over switch, so that the intelligent control system is not only applicable to a digital steering engine but also suitable for an analog steering engine.
Description
Technical field
The present invention relates to a kind of model plane product, in particular relate to the toy aircraft Remote intelligence control system on a kind of model of an airplane.
Background technology
When mould aircraft is aloft in and stops hanging state, it is subject to blowing of crosswind sometimes, now the tail vane of helicopter can produce the phenomenon of horizontal direction skew, for correcting this shift phenomenon, it is installed on the toy aircraft Remote intelligence control system meeting sending control signal of helicopter tail vane to tail vane steering wheel, resists the skew of tail vane in a reverse direction.When tail vane stops skew, the control signal of toy aircraft Remote intelligence control system also disappears therewith.If crosswind blows helicopter constantly, tail vane can be caused constantly to offset, now toy aircraft Remote intelligence control system can resist the skew of tail vane always, until tail vane moves to leeward, here it is weathercock effect, thus causing that tail vane produces shift phenomenon, and original position cannot be kept；Secondly, traditional toy aircraft Remote intelligence control system is only when the tail vane of helicopter moves, just can sending control signal to tail vane steering wheel, when tail vane stops mobile, control signal also makes zero therewith, thus causing that toy aircraft Remote intelligence control system cannot control tail vane steering wheel in time；It addition, traditional toy aircraft Remote intelligence control system volume is relatively big, heavier-weight, energy during aircraft flight can be consumed, thus decreasing the flight time of aircraft.
Therefore, in order to overcome the many disadvantages of traditional toy aircraft Remote intelligence control system, it would be highly desirable to offer one manipulation is flexible, mobility is good, and build toy aircraft Remote intelligence control system modest, lightweight.
Summary of the invention
It is an object of the invention to provide a kind of manipulation flexibly, mobility good, and the toy aircraft Remote intelligence control system that build is modest, lightweight, flight resistance is little.
The invention provides a toy aircraft Remote intelligence control system, it is by a body with control surface and is built in integrating control chip therein and forms, panel is provided with function displaing lamp and several control knobs, control knob includes mode conversion switch, forward and reverse control knob, delays actuator, range actuator, and each control knob and integrating control chip are electrically connected.
The model of an airplane is further provided with the reception device of tail vane steering wheel, motor and reception remote controller control signal, this toy aircraft Remote intelligence control system still further comprises the error transfer factor device and tail vane adjustor drawn by integrating control chip, error transfer factor device and the sensitivity channel receiving device are electrically connected, and tail vane adjustor and tail vane steering wheel are electrically connected.
Compared with prior art, the toy aircraft Remote intelligence control system of the present invention has the following advantages:
(1) build slight of stature, lighter in weight, consequently facilitating be installed on aircraft, and can effectively reducing flight resistance, thus reducing flight energy consumption, increasing the cruising time of mould aircraft；
(2) induction apparatus and controller are combined as a whole, and by the pattern of the changeable selection steering wheel of mode conversion switch so that it is be applicable not only to digital signal steering wheel, are also suitable analogue signal steering wheel；
(3) the running speed of tail vane control signal can be adjusted by controlling delay adjustment knob, it is adaptable to during slow steering wheel, can pass through to increase the mode of time delay, eliminate and turn over phenomenon.
For making the present invention easier to understand, the specific embodiment of the present invention a kind of toy aircraft Remote intelligence control system is expanded on further below in conjunction with accompanying drawing.
Accompanying drawing explanation
Fig. 1 is the operating surface structural representation of toy aircraft Remote intelligence control system of the present invention；
Fig. 2 is the structural representation that toy aircraft Remote intelligence control system of the present invention is connected with tail vane steering wheel and reception device.
Detailed description of the invention
Illustrated toy aircraft Remote intelligence control system, aim at designed by model helicopter, induction apparatus and controller are combined, owing to the effect of toy aircraft Remote intelligence control system is in that to adjust steering wheel, the mainly skew of tail vane steering wheel, hold concurrently and adjust turning to of model helicopter so that it is flight control is more accurate.
As depicted in figs. 1 and 2, toy aircraft Remote intelligence control system is by a body with control surface 100 and is built in integrating control chip therein and forms, control knob on control surface 100 is electrically connected with the corresponding functional module on integrating control chip respectively, integrating control chip is electrically connected tail vane steering wheel and receives device, wherein, receive device to send the signal of telecommunication of remote controller to toy aircraft Remote intelligence control system, toy aircraft Remote intelligence control system sends and controls signal to tail vane steering wheel, adjust the skew of tail vane steering wheel.
The control surface 100 of toy aircraft Remote intelligence control system is provided with function displaing lamp 10 and several control knobs, wherein, control knob includes mode conversion switch 11, forward and reverse control knob 12, delays actuator 13, range actuator 14, is built in the integrating control chip in body and connects error transfer factor device 15 and tail vane adjustor 16 also by cable.Function displaing lamp 10 is located at the top in the middle part of control surface 100, mode conversion switch 11 is positioned at the lower section of function displaing lamp 10, forward and reverse control knob 12 is positioned at the lower section of mode conversion switch 11, the middle upper position of control surface 100 is provided with delays actuator 13, and the upper right corner of control surface 100 is additionally provided with range actuator 14.The functional module that each control knob is corresponding with on integrating control chip is electrically connected, by each control knob on control surface 100, it is achieved the various function point analysis of toy aircraft Remote intelligence control system.
Function displaing lamp 10 is generally LED, for showing the duty of this toy aircraft Remote intelligence control system.When its fast blink, after representing power-on, toy aircraft Remote intelligence control system is carrying out the initialized program of data；When its permanent bright time, represent toy aircraft Remote intelligence control system initialize be complete, be positioned at locking (AVCS) pattern；When it glimmers at a slow speed, representing that toy aircraft Remote intelligence control system is not received by the tail vane control signal sent by remote controller, now tail vane steering wheel cannot operate；Glimmer twice expression when locking mode, and the tail vane control signal received at present is different from the neutrality point signal being stored in toy aircraft Remote intelligence control system, all there will be this lamp in situations below and glimmers twice: a) is stirring tail vane rocking bar；B) central point of tail vane offsets, it is necessary to reset central point.
Mode conversion switch 11, i.e. digital rudder controller mode switch, when the steering wheel used is digital rudder controller, it is necessary to mode conversion switch switches to the position of ON；And when the steering wheel used is general steering wheel, then mode conversion switch is switched to the position of OFF, at this moment, if switching to the position of ON, if being easy for when steering gear power is relatively low causing that steering wheel burns.Correspondingly, integrating control chip also on be configured with the circuit being respectively applied to general steering wheel and digital rudder controller, support the selection of mode conversion function.Mode conversion switch set up so that toy aircraft Remote intelligence control system can not only with general steering wheel with the use of, it is also possible to digital rudder controller with the use of, versatility is greatly enhanced.
Forward and reverse control knob 12 is for switching the control direction of toy aircraft Remote intelligence control system, and user can do correct switching according to the direction of the main rotor direction of rotation of model helicopter and tail vane connecting rod.
Delay actuator 13 for adjusting the running speed of tail vane control signal, if the steering wheel that operating speed is slower, it has been found that when the tail vane of model helicopter produces to follow the trail of phenomenon, knob can be rotated clockwise, increase the time postponed, tracking phenomenon can be eliminated；If tail vane uses high speed steering wheel, for instance digital rudder controller, user needs to adjust knob the position to 0, adjusts the running speed of tail vane control signal according to the steering wheel used.
Steering wheel range adjusts knob 14 for setting the range amount of tail vane steering wheel, tail vane rocking bar is made rudder to from left to right, adjust knob and make the path increment full range of movement without departing from tail pitch sliding sleeve of tail vane steering wheel, rotate clockwise knob for increasing path increment.
Error transfer factor device 15, drawn by the integrating control chip of toy aircraft Remote intelligence control system, and the model of an airplane receive device sensitivity channel electrically connect, can being used simultaneously as sensitivity and the pattern of switching toy aircraft Remote intelligence control system, the pattern of selection is locking mode or general modfel.
Tail vane adjustor 16, is drawn by the integrating control chip of toy aircraft Remote intelligence control system, and electrically connects with the tail vane steering wheel of the model of an airplane, for controlling direction and the fine setting of tail vane.
Toy aircraft Remote intelligence control system can be pasted or weld or be installed on the model of an airplane by the mode of screw riveted, and the bottom of this toy aircraft Remote intelligence control system must be vertical with the main shaft of helicopter, otherwise can affect left and right and sidewinder and the direction of somersault；When this toy aircraft Remote intelligence control system being installed on electric model airplane, the spacing between this toy aircraft Remote intelligence control system and motor of the model of an airplane is necessarily equal to or more than 10cm, to avoid producing interference with motor.
When the tail vane of the model of an airplane be subject to crosswind blow and produce skew phenomenon time, toy aircraft Remote intelligence control system can resist the skew of tail vane, toy aircraft Remote intelligence control system can calculate the angle of skew simultaneously, and continue sending control signal to resist crosswind, therefore even if crosswind ceaselessly blows helicopter, tail vane still will not produce skew.In other words, toy aircraft Remote intelligence control system can offset by the tail vane caused by automatic modifying factor crosswind.It addition, this toy aircraft Remote intelligence control system build slight of stature, lighter in weight, it is simple to be installed on helicopter, and can effectively reduce flight energy consumption, extend the flight time.By being gradually increased the sensitivity of toy aircraft Remote intelligence control system, and then increase the time postponed, tracking phenomenon can be eliminated.
The above disclosed preferred embodiment being only a kind of toy aircraft Remote intelligence control system of the present invention, certainly the interest field of the present invention can not be limited with this, therefore the equivalent variations made according to the present patent application the scope of the claims, still belongs to the scope that the present invention contains.
Claims (5)
1. a toy aircraft Remote intelligence control system, it is by a body with control surface and is built in integrating control chip therein and forms, it is characterized in that: panel is provided with function displaing lamp and several control knobs, control knob includes mode conversion switch, forward and reverse control knob, delays actuator, range actuator, and each control knob and integrating control chip are electrically connected.
2. toy aircraft Remote intelligence control system according to claim 1, it is characterised in that: this toy aircraft Remote intelligence control system still further comprises the error transfer factor device and tail vane adjustor drawn by integrating control chip.
3. toy aircraft Remote intelligence control system according to claim 2, it is characterised in that: farther including to be provided with the reception device receiving remote controller control signal, described error transfer factor device and the sensitivity channel receiving device are electrically connected.
4. toy aircraft Remote intelligence control system according to claim 2, it is characterised in that: being further provided with tail vane steering wheel on the model of an airplane, described tail vane adjustor and tail vane steering wheel are electrically connected.
5. toy aircraft Remote intelligence control system according to claim 1, it is characterised in that: this toy aircraft Remote intelligence control system is applicable to digital rudder controller and simulation steering wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410855395.3A CN105797402A (en) | 2014-12-31 | 2014-12-31 | Toy aircraft remote-control intelligent control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410855395.3A CN105797402A (en) | 2014-12-31 | 2014-12-31 | Toy aircraft remote-control intelligent control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105797402A true CN105797402A (en) | 2016-07-27 |
Family
ID=56464966
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410855395.3A Pending CN105797402A (en) | 2014-12-31 | 2014-12-31 | Toy aircraft remote-control intelligent control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105797402A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03268780A (en) * | 1990-03-20 | 1991-11-29 | Takara Co Ltd | Floating body |
| JP2000167261A (en) * | 1998-12-02 | 2000-06-20 | Marusho:Kk | Rotation transmission airplane toy for multiple jet fan |
| CN204050974U (en) * | 2014-06-26 | 2014-12-31 | 许美兰 | There is the remote control distributor toy of multiple power set |
| CN204355275U (en) * | 2014-08-29 | 2015-05-27 | 深圳市艾特航空科技股份有限公司 | There is the aircraft of safe propulsion system |
| CN105771275A (en) * | 2014-12-25 | 2016-07-20 | 许美兰 | Toy aircraft remote control intelligent control system |
-
2014
- 2014-12-31 CN CN201410855395.3A patent/CN105797402A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03268780A (en) * | 1990-03-20 | 1991-11-29 | Takara Co Ltd | Floating body |
| JP2000167261A (en) * | 1998-12-02 | 2000-06-20 | Marusho:Kk | Rotation transmission airplane toy for multiple jet fan |
| CN204050974U (en) * | 2014-06-26 | 2014-12-31 | 许美兰 | There is the remote control distributor toy of multiple power set |
| CN204355275U (en) * | 2014-08-29 | 2015-05-27 | 深圳市艾特航空科技股份有限公司 | There is the aircraft of safe propulsion system |
| CN105771275A (en) * | 2014-12-25 | 2016-07-20 | 许美兰 | Toy aircraft remote control intelligent control system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105966617B (en) | The water surface, it is underwater, aerial three dwell unmanned vehicle | |
| CN104020777A (en) | Motion-sensing follow-type flight control system and method | |
| US20030197092A1 (en) | Speed regulated model airplane with double motor | |
| CN201894848U (en) | Multipurpose model airplane and electronic toy controller | |
| CN204219776U (en) | Aviation aircraft position controller | |
| CN105771275A (en) | Toy aircraft remote control intelligent control system | |
| CN102380216A (en) | Method for remotely controlling toy plane and swing remote controller | |
| CN204380266U (en) | Aviation aircraft position controller | |
| CN105771272A (en) | Long-distance remote control system for high-altitude flying toy | |
| CN105561598A (en) | Novel direction control system flexible to manipulate | |
| JP5774952B2 (en) | MOTOR CONTROL CIRCUIT AND SERVO DEVICE MOUNTING THE CIRCUIT | |
| CN105797402A (en) | Toy aircraft remote-control intelligent control system | |
| CN105498250A (en) | Azimuth controller applicable to aircraft | |
| JP6114862B1 (en) | Multicopter control method | |
| CN106693400A (en) | Remote control system of flying tool | |
| CN106621395A (en) | High-altitude flight toy long distance remote control system | |
| CN107335235A (en) | Combined flying toy | |
| CN109464815A (en) | High-altitude flight toy long-distance remote control control system | |
| CN106669198A (en) | Long-distance remote control system for high-altitude flying toy | |
| CN109107191A (en) | High-altitude flight toy long-distance remote control control system | |
| CN106669165A (en) | Steering gear simulation operation debugger | |
| CN108568121A (en) | High-altitude flight toy long-distance remote control control system | |
| CN203793587U (en) | Power steering device of remote-control airship | |
| CN108261782A (en) | Steering structure for toy airplane and infrared four-channel remote control electric toy airplane | |
| CN107149776A (en) | Steering engine simulation running debugger |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160727 |