CN201200812Y - Aeromodelling - Google Patents
Aeromodelling Download PDFInfo
- Publication number
- CN201200812Y CN201200812Y CNU2008200486946U CN200820048694U CN201200812Y CN 201200812 Y CN201200812 Y CN 201200812Y CN U2008200486946 U CNU2008200486946 U CN U2008200486946U CN 200820048694 U CN200820048694 U CN 200820048694U CN 201200812 Y CN201200812 Y CN 201200812Y
- Authority
- CN
- China
- Prior art keywords
- model plane
- support tube
- model
- direction control
- steering wheel
- 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.)
- Expired - Lifetime
Links
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
Images
Landscapes
- Toys (AREA)
Abstract
The utility model discloses an aeromodelling, which comprises a bracket pipe, a tripod component arranged at the lower end of the bracket pipe, a direction control component arranged in the middle part of the bracket pipe, an electronic system which can receive external signals and can control the direction control component, a battery, and two dynamic rotation sets arranged at the front end and the tail end of the bracket pipe. The aeromodelling makes use of the dynamic rotation sets arranged at the front end and the rear end of the bracket pipe to enhance the balancing airflow so as to ensure that an aeromodelling helicopter flies more smoothly and stably.
Description
Technical field
The utility model relates to a kind of electronic toy, relates in particular to a kind of model helicopter.
Background technology
General model helicopter is controlled its balance in the hope of smooth flight by main wing and empennage, but this model helicopter is not very steady when flying, and is not easy control.
Therefore, our demand is a kind of when the flying more steady and model helicopter that is easier to control.
Summary of the invention
Based on the deficiencies in the prior art, problem to be solved in the utility model adopts two oar two-shippers to make model helicopter balance and smooth flight, and each power unit of front and back strengthens its balance air-flow, and more steady being easier to controlled when making its flight.
For addressing the above problem, the model plane that the utility model provides comprise support tube, are arranged at the foot rest assembly of described support tube lower end, are arranged at the Direction Control Unit at this support tube middle part, electronic system, the battery that can receive external signal and can control described Direction Control Unit, also comprise two power rotation groups, be arranged at described support tube front-end and back-end respectively.
As the improvement of a kind of model plane of the utility model, a kind of model plane of the utility model can also comprise part or all of following technical characterictic:
Described Direction Control Unit comprise the pitch that is arranged on described two power rotation groups, by the steering wheel fixed mount be fixed in described support tube middle part steering wheel, connect the pull bar of described steering wheel and described pitch.
Described two power rotation groups are made up of one group of complete dual-rotor helicopter respectively, and described two complete dual-rotor helicopters are fixed in the front-end and back-end of described support tube respectively by main frame.
Described electronic system is made up of remote controller and receiver.Described receiver is connected with described steering wheel, and described electronic system receiver receives the instruction of remote controller, by the heading of described Direction Control Unit control model plane.Also comprise the model plane main body cover in addition.
Compared with prior art, model plane utilization of the present utility model be arranged at described support tube front-end and back-end two power rotation groups, strengthen its balance air-flow, make model helicopter more balance and more reposefully flight.
For making the utility model easier to understand, further set forth model plane of the present utility model below in conjunction with accompanying drawing.
Description of drawings
Fig. 1 is the model plane structural representation of a preferred embodiment of the utility model.
Fig. 2 is the explosive view of model plane shown in Fig. 1.
The specific embodiment
With reference now to accompanying drawing, preferred embodiment of the present utility model is described.
With reference to figure 1 and Fig. 2, model plane of the present utility model comprise support tube 48, be arranged at the foot rest assembly 4 of described support tube 48 lower ends, be arranged at this support tube middle part Direction Control Unit 3, can receive external signal and can control described Direction Control Unit electronic system, be used for also comprising two power rotation groups 1 and 2 that are arranged at described support tube front-end and back-end to model plane the power battery 56 and the model plane main body cover 40 of energy.
Described foot rest assembly 4 is fixed in the lower end of support tube 48, and during the model plane kiss the earth, this foot rest assembly 4 plays the effect of supporting and protecting the model plane body.Described battery is fixed on the middle part of support tube 48 by battery carrier.
With reference to figure 1,2, described two power rotation groups 1 and 2 that are arranged at described support tube front-end and back-end, produce aerostatic buoyancy when being used for model plane flight, so that model plane can fly up, be made up of one group of complete dual-rotor helicopter respectively, described two complete dual-rotor helicopters are fixed in the front-end and back-end of described support tube 48 respectively by main frame 29 and main frame 61.Two complete dual-rotor helicopter rotations produce lift, and each unit of front and back strengthens its balance air-flow, and more steady being easier to controlled when making its flight, finally reaches the purpose of smooth flight.
With reference to figure 2, described Direction Control Unit 3 comprises pitch, the steering wheel 53 that is arranged on described two power rotation groups 1 and 2, pull bar 51 and the pull bar 52 that is connected described steering wheel 53 and pitch, and described steering wheel 53 is fixed on the middle part of support tube 48 by steering wheel fixed mount 49.
Electronic system is made up of remote controller and receiver.Described receiver is connected with described steering wheel 53, and described electronic system receiver receives the instruction of remote controller, by the heading of described Direction Control Unit 3 control model plane.
Above disclosed only is preferred embodiment of the present utility model, can not limit the interest field of the utility model certainly with this, and therefore the equivalent variations of being done according to the utility model claim still belongs to the scope that the utility model is contained.
Claims (7)
1. model plane, it comprises support tube, is arranged at the foot rest assembly of described support tube lower end, is arranged at the Direction Control Unit at this support tube middle part, electronic system, the battery that can receive external signal and can control described Direction Control Unit, it is characterized in that: also comprise two power rotation groups, be arranged at described support tube front-end and back-end respectively.
2. model plane as claimed in claim 1 is characterized in that: described Direction Control Unit comprise the pitch that is arranged on described two power rotation groups, by the steering wheel fixed mount be fixed in described support tube middle part steering wheel, connect the pull bar of described steering wheel and described pitch.
3. model plane as claimed in claim 1 is characterized in that: described two power rotation groups are made up of one group of complete dual-rotor helicopter respectively.
4. model plane as claimed in claim 3 is characterized in that: described two complete dual-rotor helicopters are fixed in the front-end and back-end of described support tube respectively by main frame.
5. model plane as claimed in claim 1 is characterized in that: described electronic system is made up of remote controller and receiver.
6. as claim 2 or 4 described model plane, it is characterized in that: described receiver is connected with described steering wheel, and described electronic system receiver receives the instruction of remote controller, by the heading of described Direction Control Unit control model plane.
7. model plane as claimed in claim 1 is characterized in that: also comprise the model plane main body cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200486946U CN201200812Y (en) | 2008-06-03 | 2008-06-03 | Aeromodelling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200486946U CN201200812Y (en) | 2008-06-03 | 2008-06-03 | Aeromodelling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201200812Y true CN201200812Y (en) | 2009-03-04 |
Family
ID=40423123
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008200486946U Expired - Lifetime CN201200812Y (en) | 2008-06-03 | 2008-06-03 | Aeromodelling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201200812Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102743884A (en) * | 2012-07-13 | 2012-10-24 | 罗之洪 | Aeromodel helicopter |
| CN105797390A (en) * | 2014-12-31 | 2016-07-27 | 马铿钧 | Flying toy capable of achieving precise positioning control by driving wing by virtue of transmission box |
-
2008
- 2008-06-03 CN CNU2008200486946U patent/CN201200812Y/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102743884A (en) * | 2012-07-13 | 2012-10-24 | 罗之洪 | Aeromodel helicopter |
| CN102743884B (en) * | 2012-07-13 | 2015-03-25 | 罗之洪 | Aeromodel helicopter |
| CN105797390A (en) * | 2014-12-31 | 2016-07-27 | 马铿钧 | Flying toy capable of achieving precise positioning control by driving wing by virtue of transmission box |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103523221B (en) | With the bionic Aircraft that active twist controls | |
| CN106143903B (en) | A kind of wing can reverse and can realize the micro flapping wing air vehicle of more sporting flyings | |
| CN202508281U (en) | Flying device using coanda effect to generate horizontal power | |
| CN108438215A (en) | It is a kind of to have the vector four-axle aircraft for keeping organism level ability | |
| CN201200812Y (en) | Aeromodelling | |
| CN104691758B (en) | Linkage fixed-wing rotor electric vertical lifting unmanned plane | |
| CN205770116U (en) | A kind of small-sized rotor aircraft that verts | |
| CN204473119U (en) | Lightweight unmanned plane | |
| CN208963310U (en) | It is a kind of can VTOL vert the fixed-wing unmanned plane of quadrotor | |
| CN204219777U (en) | aerial toy | |
| CN202666408U (en) | Six-arm model aerial propeller | |
| CN201320405Y (en) | Helicopter aero-modeling | |
| CN202128907U (en) | Multifunctional intelligent kite | |
| CN203601562U (en) | Boomerang quadrotor aircraft | |
| CN106741932A (en) | A kind of axle unmanned plane of mixed type nine based on VTOL | |
| CN203355289U (en) | Triaxial flying device | |
| CN209051585U (en) | A kind of unmanned plane device to work under heavy load conditions | |
| CN202961882U (en) | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device | |
| CN207985188U (en) | A kind of band fixation two tilting duct quadrotor unmanned vehicle of wing | |
| CN205327402U (en) | Multi -rotor aircraft | |
| CN201147639Y (en) | Propeller type electric remote control toy aeroplane | |
| CN2564215Y (en) | Electric remote-controlled model aircraft | |
| CN203060830U (en) | Toy air boat | |
| CN204368407U (en) | A kind of portable mini frame | |
| CN203921186U (en) | Band rotating shaft function wing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: GUANGZHOU WALKERA TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: LUO ZHIHONG Effective date: 20150810 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150810 Address after: 511453 Nansha District, Guangzhou, Tung Chung Town, Tai Po Industrial Zone, Guangzhou Walkera Technology Co Ltd, Patentee after: GUANGZHOU WALKERA TECHNOLOGY CO., LTD. Address before: 511430 Guangdong city of Guangzhou province Panyu District yuwotou town Taishi Industrial Zone huakeer Technology Co. Ltd Patentee before: Luo Zhihong |
|
| CP03 | Change of name, title or address |
Address after: 511475 Nansha District, Guangdong, Tung Chung Town, Tai Po Industrial Zone Patentee after: Guangzhou city huakeer Polytron Technologies Inc Address before: 511453 Nansha District, Guangzhou, Tung Chung Town, Tai Po Industrial Zone, Guangzhou Walkera Technology Co Ltd, Patentee before: GUANGZHOU WALKERA TECHNOLOGY CO., LTD. |
|
| CP03 | Change of name, title or address | ||
| CX01 | Expiry of patent term |
Granted publication date: 20090304 |
|
| CX01 | Expiry of patent term |