CN202070155U - Electric remotely-controlled fixed-wing airplane model - Google Patents
Electric remotely-controlled fixed-wing airplane model Download PDFInfo
- Publication number
- CN202070155U CN202070155U CN2011201077267U CN201120107726U CN202070155U CN 202070155 U CN202070155 U CN 202070155U CN 2011201077267 U CN2011201077267 U CN 2011201077267U CN 201120107726 U CN201120107726 U CN 201120107726U CN 202070155 U CN202070155 U CN 202070155U
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- aircraft
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Abstract
The utility model discloses an electric remotely-controlled fixed-wing airplane model, and aims at providing an electric remotely-controlled fixed-wing airplane model with good manoeuvrability. The electric remotely-controlled fixed-wing airplane model comprises an airplane main body, two aircraft wings arranged on the airplane main body, ailerons arranged on the wings, and an elevator arranged on the airplane main body; the electric remotely-controlled fixed-wing airplane model also comprises an aileron servo and an aileron handling steel wire arranged on the airplane main body, a lifting servo and a lifting handling steel wire arranged on the airplane main body; furthermore, the aileron servo, the aileron handling steel wire and the ailerons are sequentially connected with one another; the lifting servo, the lifting handling steel wire and the elevator are sequentially connected with one another sequentially. The electric remotely-controlled fixed-wing airplane model can be used for various electric remotely-controlled fixed-wing airplane models, especially for the minitype electric remotely-controlled fixed-wing airplane models.
Description
Technical field
The utility model relates to model aircraft, especially relates to the good electric remote control fixed wing aircraft model of a kind of maneuverability.
Background technology
At present, electric remote control fixed wing aircraft model is at the large aircraft model mostly, very rare small-sized electric remote control fixed wing aircraft model.Existing electric remote control fixed wing aircraft model mechanism is comparatively out-of-date, complex structure, servo consumption is too much, the machine that falls causes servomechanism and body easily life-span weak point, troublesome maintenance, flight maneuver and poor stability, the maneuverability of especially existing electric remote control fixed wing aircraft model is bad, has certain defective.
The utility model content
The utility model provides a kind of electric remote control fixed wing aircraft model in order to solve the bad technical problem of maneuverability of prior art electric remote control fixed wing aircraft model.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is a kind of electric remote control fixed wing aircraft model of design, comprise an aircraft main body, be arranged on wing on the aircraft main body, be arranged on the aileron on the wing and be arranged on elevator on the aircraft main body, described electric remote control fixed wing aircraft model also comprises:
Be arranged on aileron servomechanism and aileron control steel wire on the aircraft main body, and described aileron servomechanism, aileron control steel wire are connected successively with aileron;
Be arranged on lifting servomechanism and lifting manipulating wire on the aircraft main body, and described lifting servomechanism, lifting manipulating wire are connected successively with elevator.
Described lifting manipulating wire and elevator are hinged.
Described electric remote control fixed wing aircraft model comprises that also one is arranged on the showing stand of the regulated 360o of aircraft lower body part.
The utility model is by being provided with the aileron servomechanism and the aileron control steel wire drives aileron, the lifting servomechanism is set and the lifting manipulating wire drives elevator.The internal structure layout is simple and easy, tightly beat, in light weight, speed fast, easy care and assembling, servomechanism maneuverability pattern novelty, maneuverability is good, it is good to have characteristic, wind resistance and crash resistance that mobility and stability takes into account.
Description of drawings
Below in conjunction with embodiment and accompanying drawing the utility model is elaborated, wherein:
Fig. 1 is the utility model electric remote control fixed wing aircraft structure of models figure;
Fig. 2 is another visual angle structure chart of the utility model electric remote control fixed wing aircraft model;
Fig. 3 is the structure chart after the utility model electric remote control fixed wing aircraft model takes down upper casing.
The specific embodiment
See also Fig. 1, Fig. 2 and Fig. 3, the utility model electric remote control fixed wing aircraft model comprises aircraft main body 1, wing 2, the horizontal tail wing 3, aileron servomechanism 4, aileron control steel wire 5, lifting servomechanism 6, lifting manipulating wire 7 and vertical tail 8.Wherein:
Aircraft main body 1 is provided with driving cabin 11, be used to provide the battery 12 of flight energy, be used to receive the remote controller remote signal receiver 13, be provided be the aircraft lower body part regulated 360o showing stand 14 and to be arranged on aircraft top be upper casing 15.Showing stand has been used for supporting the displaying effect.
Aileron servomechanism 4 and aileron control steel wire 5 all are arranged on the aircraft main body, and aileron servomechanism, aileron control steel wire are connected successively with aileron.Thereby aileron servomechanism 4 is mainly used in and drives 5 actions of aileron control steel wire and drive ailerons and move and control aileron, thereby control flight attitude.
The operation principle of electric remote control fixed wing aircraft model of the present utility model is as follows: to be electric remote control fixed wing aircraft models produce the device of lift to wing 2 when flight, and the horizontal side can keep the model of an airplane flight time is stable.Aileron control on the wing is to drive the 5 drive aileron actions of aileron control steel wire by the aileron servomechanism 4 that is arranged on the wing, flies thereby change the aspect left and right sides.Elevator 31 on the horizontal tail wing is to drive elevator control steel wires 7 by lifting servomechanism 6 to drive the elevators action, thereby keep lifting with stable when making aircraft flight.Direction when vertical tail 8 is used to keep aircraft flight is stable, and the rudder on the vertical tail can be controlled the heading of model aircraft.
Compared with prior art, the utility model electric remote control fixed wing aircraft model layout adopts the wing structure that places an order, the good windup-degree of while wing, fuselage, radome fairing adopt highdensity EPS material, wing, horizontal tail adopt pearl plate heat pressing process, adopt directly drive change that no motor, canopy adopt the PVC material, are furnished with that showing stand, the internal structure layout that can regulate 360o are simple and easyly tightly beaten outward, in light weight, speed soon, easy care and assembling.It is good with stable characteristic, servomechanism maneuverability pattern novelty, wind resistance and the crash resistance of taking into account to have mobility.Possess the somersault of beating and inverted flight, roll, hedgehopping stunt action, possess external form and resemble flight attitude true, true to nature.
Compare with existing structure, the utility model electric remote control fixed wing aircraft model has and is easier to debug aircraft, be adapted at indoor flight, only need little space just can fly, exquisite appearance can be showed again, mechanical part simply also makes aeroplane performance stability improve greatly simultaneously, to be applicable to different crowds.The utility model is specially adapted to small-sized electric remote control fixed wing aircraft model.
The above only is preferred embodiment of the present utility model; not in order to restriction the utility model; all any modifications of within spirit of the present utility model and principle, being done, be equal to and replace and improvement etc., all should be included within the protection domain of the present utility model.
Claims (3)
1. electric remote control fixed wing aircraft model, comprise an aircraft main body, be arranged on wing on the aircraft main body, be arranged on the aileron on the wing and be arranged on elevator on the aircraft main body, it is characterized in that: described electric remote control fixed wing aircraft model also comprises:
Be arranged on aileron servomechanism and aileron control steel wire on the aircraft main body, and described aileron servomechanism, aileron control steel wire are connected successively with aileron;
Be arranged on lifting servomechanism and lifting manipulating wire on the aircraft main body, and described lifting servomechanism, lifting manipulating wire are connected successively with elevator.
2. electric remote control fixed wing aircraft model according to claim 1 is characterized in that: described lifting manipulating wire and elevator are hinged.
3. electric remote control fixed wing aircraft model according to claim 1 is characterized in that: described electric remote control fixed wing aircraft model comprises that also one is arranged on the showing stand of the regulated 360o of aircraft lower body part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201077267U CN202070155U (en) | 2011-04-13 | 2011-04-13 | Electric remotely-controlled fixed-wing airplane model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201077267U CN202070155U (en) | 2011-04-13 | 2011-04-13 | Electric remotely-controlled fixed-wing airplane model |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202070155U true CN202070155U (en) | 2011-12-14 |
Family
ID=45108271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011201077267U Expired - Fee Related CN202070155U (en) | 2011-04-13 | 2011-04-13 | Electric remotely-controlled fixed-wing airplane model |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202070155U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106139608A (en) * | 2015-04-08 | 2016-11-23 | 叶灵 | Fixed wing airplane model |
| CN108355362A (en) * | 2018-04-27 | 2018-08-03 | 深圳市阳日电子有限公司 | The intelligent control model of an airplane and its control method |
-
2011
- 2011-04-13 CN CN2011201077267U patent/CN202070155U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106139608A (en) * | 2015-04-08 | 2016-11-23 | 叶灵 | Fixed wing airplane model |
| CN108355362A (en) * | 2018-04-27 | 2018-08-03 | 深圳市阳日电子有限公司 | The intelligent control model of an airplane and its control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: SHENZHEN ART AVIATION TECHNOLOGY CO., LTD. Free format text: FORMER NAME: SHENZHEN ART-TECH R/C HOBBY CO., LTD. |
|
| CP03 | Change of name, title or address |
Address after: 518000 No. 1, building D4, Liyuan Industrial Park, Shiyan community, Shiyan street, Shiyan City, Guangdong, Shenzhen, two, Baoan District Patentee after: Shenzhen Art Aviation Technology Co., Ltd. Address before: 518000 Guangdong city of Shenzhen province Baoan District Shiyan town Tangtou Village million Liyuan Industrial Zone Industrial Park 1 Building 3 floor uplift Patentee before: Shenzhen Art-Tech R/C Hobby Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111214 Termination date: 20170413 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |