CN2537441Y - Model plane with culvert channel blade tail wing - Google Patents
Model plane with culvert channel blade tail wing Download PDFInfo
- Publication number
- CN2537441Y CN2537441Y CN 02208296 CN02208296U CN2537441Y CN 2537441 Y CN2537441 Y CN 2537441Y CN 02208296 CN02208296 CN 02208296 CN 02208296 U CN02208296 U CN 02208296U CN 2537441 Y CN2537441 Y CN 2537441Y
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- CN
- China
- Prior art keywords
- aircraft
- model
- empennage
- blade
- controlled
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- Expired - Fee Related
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Abstract
The utility model relates to a radio-controlled aviation model aircraft, belonging to an aviation model aircraft technical field. The existing radio-controlled aviation model aircraft with a steering engine has the disadvantages of heavy aircraft frame, high production cost and slow response when the aircraft is controlled to turn. Aiming at the disadvantages, the utility model provides a model aircraft with a ducted blade empennage, has the advantages of light aircraft frame, low production cost and quick response when the aircraft is controlled to turn and comprises an aircraft frame, a propeller, an engine, an electronic circuit, a plurality of aircraft wings, an undercarriage, a plurality of aircraft wheels, a horizontal empennage and a vertical empennage. The utility model is characterized in that: a ducted blade empennage is arranged on the vertical empennage; wherein, the ducted blade empennage comprises a ducted hole, a blade wheel and a micro motor; when the model aircraft aviates, the flight direction of the model aircraft is controlled by the airflow of different directions generated by the different rotary directions of the blade wheel through remotely controlling and changing the rotary direction of the micro motor on the ducted blade.
Description
Technical field
The utility model belongs to model airplane aircraft technology field, particularly a kind of radio controlled model of an airplane that has duct blade empennage.
Background technology
Model airplane aircraft particularly wireless remotecontrol model airplane aircraft is an activity high in technological content, that amusement and recreation are strong, and it more and more is subjected to, and the masses are especially teen-age to be liked.In existing wireless remotecontrol model airplane aircraft, in order to control its flight attitude, steering wheel is housed all generally, reduction gearing is housed on the steering wheel.When the model airplane aircraft in when flight, handle its flight attitude by the remote control steering wheel.The existing wireless remotecontrol model airplane aircraft that steering wheel is housed exists that model of an airplane own wt is heavy, cost of manufacture is high, unresponsive weak point during the control dogled.
Summary of the invention
The utility model unresponsive weak point during at the existing existing aircraft own wt weight of wireless remotecontrol model airplane aircraft that steering wheel is housed, aircraft cost of manufacture height, control dogled provides that a kind of aircraft own wt is light, the aircraft cost of manufacture is low, the model of an airplane that has duct blade empennage of agility during the control dogled.
The technical solution adopted in the utility model is finished in the following way: the model of an airplane that has duct blade empennage comprises fuselage, screw, engine, electronic circuit, wing, nose-gear, main landing gear, wheel, tailplane and vertical tail, its main points are to be provided with the duct blade on vertical tail, wherein the duct blade comprises duct hole, paddle wheel and micromachine, open on vertical tail in the duct hole, micromachine is contained in the duct hole, and paddle wheel is contained on the output shaft of micromachine.The model of an airplane that has a duct blade empennage when the utility model is during in flight, by the direction of rotation of remote control conversion micromachine, utilizes the air-flow of the different directions that paddle wheel different rotary direction produced to control the heading of the model of an airplane.
The utility model has the model of an airplane of duct blade empennage to be compared with the existing wireless remotecontrol model airplane aircraft that steering wheel is housed, and has that the aircraft own wt is light, the aircraft cost of manufacture is low, characteristics of agility during the control dogled.The utility model is suitable as a kind of wireless remotecontrol model airplane aircraft.
Description of drawings
Fig. 1 is the structural representation that has the model of an airplane of duct blade empennage.
Fig. 2 is the structural representation of duct blade.
The specific embodiment
Contrast accompanying drawing below, the utility model is described in further detail by embodiment.
With reference to accompanying drawing 1 and accompanying drawing 2, a kind of model of an airplane that has duct blade empennage comprises fuselage (1), screw (3), engine, electronic circuit, wing (4), nose-gear (5), main landing gear (7), wheel (6), tailplane (8) and vertical tail (9).Engine and electronic circuit are contained in fuselage (1) inside, and wherein engine is contained in the head in the fuselage (1), and screw (3) is contained on the output shaft of engine, are provided with radome fairing (2) at the head of screw (3).Nose-gear (5), main landing gear (7), tailplane (8) and vertical tail (9) all are fixed on the fuselage (1), and wheel (6) is located on nose-gear (5) and the main landing gear (7).On vertical tail (9), be provided with duct blade (10), duct blade (10) comprises duct hole (11), paddle wheel (12) and micromachine (13), wherein open on vertical tail (9) duct hole (11), micromachine (13) is contained in the duct hole (11), and paddle wheel (12) is contained on the output shaft of micromachine (13).
Claims (1)
1, a kind of model of an airplane that has duct blade empennage, it comprises fuselage (1), screw (3), engine, electronic circuit, wing (4), tailplane (8) and vertical tail (9), engine and electronic circuit are contained in fuselage (1) inside, wherein engine is contained in the head in the fuselage (1), screw (3) is contained on the output shaft of engine, head at screw (3) is provided with radome fairing (2), tailplane (8) and vertical tail (9) all are fixed on the fuselage (1), it is characterized in that on vertical tail (9), being provided with duct blade (10), duct blade (10) comprises duct hole (11), paddle wheel (12) and micromachine (13), wherein open on vertical tail (9) duct hole (11), micromachine (13) is contained in the duct hole (11), and paddle wheel (12) is contained on the output shaft of micromachine (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02208296 CN2537441Y (en) | 2002-03-18 | 2002-03-18 | Model plane with culvert channel blade tail wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02208296 CN2537441Y (en) | 2002-03-18 | 2002-03-18 | Model plane with culvert channel blade tail wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2537441Y true CN2537441Y (en) | 2003-02-26 |
Family
ID=33689026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02208296 Expired - Fee Related CN2537441Y (en) | 2002-03-18 | 2002-03-18 | Model plane with culvert channel blade tail wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2537441Y (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2004078300A1 (en) * | 2003-03-03 | 2004-09-16 | Dongguan Chwenshen Technology Inc. Ltd. | Remote controlled plane |
| CN100357005C (en) * | 2006-06-05 | 2007-12-26 | 肖旭平 | Remotely-controlled plane |
| CN104129499A (en) * | 2013-05-03 | 2014-11-05 | 空客直升机 | Ducted rotor for an aircraft and a rotorcraft |
| CN107176297A (en) * | 2017-06-20 | 2017-09-19 | 北京迪鸥航空科技有限公司 | A kind of aircraft |
| CN109572945A (en) * | 2019-01-18 | 2019-04-05 | 上海交通大学 | A kind of transfer and its communicating control method for wave aerodone |
| CN109878743A (en) * | 2019-03-25 | 2019-06-14 | 北京京东尚科信息技术有限公司 | Aircraft |
-
2002
- 2002-03-18 CN CN 02208296 patent/CN2537441Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2004078300A1 (en) * | 2003-03-03 | 2004-09-16 | Dongguan Chwenshen Technology Inc. Ltd. | Remote controlled plane |
| CN100357005C (en) * | 2006-06-05 | 2007-12-26 | 肖旭平 | Remotely-controlled plane |
| CN104129499A (en) * | 2013-05-03 | 2014-11-05 | 空客直升机 | Ducted rotor for an aircraft and a rotorcraft |
| CN107176297A (en) * | 2017-06-20 | 2017-09-19 | 北京迪鸥航空科技有限公司 | A kind of aircraft |
| CN109572945A (en) * | 2019-01-18 | 2019-04-05 | 上海交通大学 | A kind of transfer and its communicating control method for wave aerodone |
| CN109878743A (en) * | 2019-03-25 | 2019-06-14 | 北京京东尚科信息技术有限公司 | Aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |