CN206492212U - A kind of model aircraft that can be run on ground - Google Patents
A kind of model aircraft that can be run on ground Download PDFInfo
- Publication number
- CN206492212U CN206492212U CN201720162185.5U CN201720162185U CN206492212U CN 206492212 U CN206492212 U CN 206492212U CN 201720162185 U CN201720162185 U CN 201720162185U CN 206492212 U CN206492212 U CN 206492212U
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- CN
- China
- Prior art keywords
- micromachine
- controller
- wheel hub
- run
- hub motor
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- 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.)
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Abstract
The utility model discloses a kind of model aircraft that can be run on ground, including fuselage and remote control, the fuselage both sides are provided with wing, the wing front side surface is provided with propeller, the propeller connects the rotor of the first micromachine, the both sides wing and fuselage afterbody are equipped with the second micromachine, the rotor connection support bar of second micromachine, the support bar connects wheel hub motor, the wheel hub motor is externally provided with tire, first micromachine, the input of two micromachines and wheel hub motor connects multiple output ends of the first controller respectively, the output end of input multiple connection power supply and the signal receivers respectively of first controller.The beneficial effects of the utility model are can both to fly, and can be run again on ground, and functional diversities can preferably adapt to the different demand of user.
Description
Technical field
The utility model is related to model aircraft field, particularly a kind of model aircraft that can be run on ground.
Background technology
Aircraft is one of most important invention of the mankind.Nowadays with the improvement of living condition, substantial amounts of model plane love is occurred in that
Good person.It is therefore desirable to design various model aircrafts for different demands.
A kind of model aircraft of utility model of Application No. 201620269167.2 and technical field phase of the present utility model
Together.A kind of this entitled utility model of model aircraft includes fuselage, and the fuselage connects into an entirety with wing, empennage；Machine
The wing, the wing is connected with fuselage；Empennage, the empennage includes tailplane and vertical tail；Back box, the back box is located at wing and tail
It is front and rear penetrating below the wing, using the Design of ventilation of optimal ratio between highness and width example 1: 4, the faster more steady of model aircraft flight can be made, and
And make model aircraft overall firmer；Take-off and landing device, the take-off and landing device is located at below head and both sides below back box, it is ensured that
Steady, and the firm shatter-resistant of model aircraft landing；The technology passes through the improvement to existing model aircraft, more ultralight heavily fortified point
Gu, so as to ensure that model aircraft is quick, stably, flexibly fly, will certainly will significantly promote the development of model plane motion.
The model aircraft generally used now only possesses airflight function, it is impossible to runs, function is single, uses on ground
Inconvenience.Although above-mentioned prior art is more ultralight firm, so that ensure that model aircraft is quick, stably, flexibly fly, certainly will
The development of model plane motion will be promoted significantly, but can not solve the above problems.
Utility model content
The purpose of this utility model is to solve the above problems, devise a kind of aircraft mould that can be run on ground
Type.
Realize that above-mentioned purpose the technical solution of the utility model is, a kind of model aircraft that can be run on ground, including
Fuselage and remote control, the fuselage both sides are provided with wing, and the wing front side surface is provided with propeller, propeller connection the
The rotor of one micromachine, the both sides wing and fuselage afterbody are equipped with the second micromachine, second micromachine
Rotor connection support bar, the support bar connects wheel hub motor, and the wheel hub motor is externally provided with tire, first micro electric
The input of machine, two micromachines and wheel hub motor connects multiple output ends of the first controller, first controller respectively
Input it is multiple respectively connection power supply and signal receivers output ends.
The remote control includes apparatus for transmitting signal, second controller, control-rod and second source, the second controller
Multiple inputs connect the output end of control-rod and second source, the output end connection signal hair of the second controller respectively
Send the input of equipment.
First micromachine is HFK180-2560-45L+ROHS type brushed DC motors, second micromachine
For HFK180-2560-45L+ROHS type brushed DC motors, first controller is SIEMENS type controllers, the signal
Receiver is F38 type signal receivers.
The wheel hub motor is good fortune horse wheel hub motor.
The apparatus for transmitting signal is SPR-RCUT-TA2 type sender units, and the second controller is SIEMENS types
Controller, the control-rod is that N64 types control rocking bar.
A kind of model aircraft that can be run on ground made using the technical solution of the utility model, can both fly
OK, it can be run again on ground, functional diversities can preferably adapt to the different demand of user.
Brief description of the drawings
Fig. 1 is a kind of structural representation of model aircraft that can be run on ground described in the utility model；
Fig. 2 is a kind of control structure schematic diagram of model aircraft that can be run on ground described in the utility model；
In figure, 1, fuselage；2nd, wing；3rd, propeller；4th, the first micromachine；5th, the second micromachine；6th, support bar；7、
Wheel hub motor；8th, tire；9th, the first controller；10th, power supply；11st, signal receiver；12nd, remote control；13rd, apparatus for transmitting signal；
14th, second controller；15th, control-rod；16th, second source.
Embodiment
The utility model is specifically described below in conjunction with the accompanying drawings, it is as shown in Figure 1-2, a kind of to be run on ground
Model aircraft, including including fuselage 1 and remote control 12, the both sides of fuselage 1 are provided with wing 2, and the front side surface of wing 2 is provided with
Propeller 3, the propeller 3 connects the rotor of the first micromachine 4, and both sides wing 2 and fuselage 1 rear portion is equipped with second
Micromachine 5, the rotor connection support bar 6 of second micromachine 5, the support bar 6 connects wheel hub motor 7, the wheel
Hub motor 7 is externally provided with tire 8, and the input of first micromachine 4, two micromachines 5 and wheel hub motor 7 connects respectively
Multiple output ends of one controller 9, input multiple connection power supply 10 and the signal receivers 11 respectively of first controller 9
Output end；The remote control 12 includes apparatus for transmitting signal 13, second controller 14, control-rod 15 and second source 16, institute
The multiple inputs for stating second controller 14 connect the output end of control-rod 15 and second source 16, the second controller respectively
14 output end connects the input of apparatus for transmitting signal 13；First micromachine 4 is HFK180-2560-45L+ROHS
Type brushed DC motor, second micromachine 5 is HFK180-2560-45L+ROHS type brushed DC motors, described first
Controller 9 is SIEMENS type controllers, and the signal receiver 11 is F38 type signal receivers；The wheel hub motor 7 is good fortune
Horse wheel hub motor；The apparatus for transmitting signal 13 is SPR-RCUT-TA2 type sender units, and the second controller 14 is
SIEMENS type controllers, the control-rod 15 is that N64 types control rocking bar.
The characteristics of the present embodiment is that both sides wing and fuselage afterbody are equipped with the second micromachine, the second micromachine
Rotor connection support bar, support bar connection wheel hub motor, wheel hub motor is externally provided with tire, when model aircraft landing on the ground
When, user can be rotated by remote control control wheel hub motor, model aircraft is run on ground, can also control
Two micromachines complete the steering of model aircraft, and the present apparatus can both fly, and can be run again on ground, and functional diversities can
Preferably to adapt to the demand that user is different.
In the present embodiment, when user operates the control-rod of remote control, sent and filled by second controller, signal
Put, signal receiving device and the first controller, make minitype motor driving propeller rotational, propeller provides dynamic for model aircraft
Power, makes model aircraft take off, and when model aircraft lands on the ground, user can pass through remote control control wheel hub motor and turn
It is dynamic, model aircraft is run on ground, the second micromachine can also be controlled to complete the steering of model aircraft.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solutions of the utility model, the technology of the art
Some variations that personnel may make to some of which part embody principle of the present utility model, belong to the utility model
Protection domain within.
Claims (5)
1. a kind of model aircraft that can be run on ground, including fuselage（1）And remote control（12）, it is characterised in that the machine
Body（1）Both sides are provided with wing（2）, the wing（2）Front side surface is provided with propeller（3）, the propeller（3）Connect first micro-
Type motor（4）Rotor, the both sides wing（2）And fuselage（1）Rear portion is equipped with the second micromachine（5）, described second is micro-
Type motor（5）Rotor connection support bar（6）, the support bar（6）Connect wheel hub motor（7）, the wheel hub motor（7）Peripheral hardware
There is tire（8）, first micromachine（4）, the second micromachine（5）And wheel hub motor（7）Input connect respectively
One controller（9）Multiple output ends, first controller（9）Input multiple connect power supply respectively（10）Connect with signal
Receive device（11）Output end.
2. a kind of model aircraft that can be run on ground according to claim 1, it is characterised in that the remote control
（12）Including apparatus for transmitting signal（13）, second controller（14）, control-rod（15）And second source（16）, second control
Device（14）Multiple inputs connect control-rod respectively（15）And second source（16）Output end, the second controller（14）
Output end connection apparatus for transmitting signal（13）Input.
3. a kind of model aircraft that can be run on ground according to claim 1, it is characterised in that described first is miniature
Motor（4）For HFK180-2560-45L+ROHS type brushed DC motors, second micromachine（5）For HFK180-2560-
45L+ROHS type brushed DC motors, first controller（9）For SIEMENS type controllers, the signal receiver（11）
For F38 type signal receivers.
4. a kind of model aircraft that can be run on ground according to claim 1, it is characterised in that the wheel hub motor
（7）For good fortune horse wheel hub motor.
5. a kind of model aircraft that can be run on ground according to claim 2, it is characterised in that the signal is sent
Equipment（13）For SPR-RCUT-TA2 type sender units, the second controller（14）For SIEMENS type controllers, the control
Bar processed（15）Rocking bar is controlled for N64 types.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720162185.5U CN206492212U (en) | 2017-02-23 | 2017-02-23 | A kind of model aircraft that can be run on ground |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720162185.5U CN206492212U (en) | 2017-02-23 | 2017-02-23 | A kind of model aircraft that can be run on ground |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206492212U true CN206492212U (en) | 2017-09-15 |
Family
ID=59806641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720162185.5U Expired - Fee Related CN206492212U (en) | 2017-02-23 | 2017-02-23 | A kind of model aircraft that can be run on ground |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206492212U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621351A (en) * | 2017-02-24 | 2017-05-10 | 武汉蛋玩科技有限公司 | Novel toy robot |
-
2017
- 2017-02-23 CN CN201720162185.5U patent/CN206492212U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621351A (en) * | 2017-02-24 | 2017-05-10 | 武汉蛋玩科技有限公司 | Novel toy robot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170915 |