CN206518880U - Remote control amphibious aircraft - Google Patents
Remote control amphibious aircraft Download PDFInfo
- Publication number
- CN206518880U CN206518880U CN201720042842.2U CN201720042842U CN206518880U CN 206518880 U CN206518880 U CN 206518880U CN 201720042842 U CN201720042842 U CN 201720042842U CN 206518880 U CN206518880 U CN 206518880U
- Authority
- CN
- China
- Prior art keywords
- floating body
- wing
- support plate
- fuselage
- remote control
- 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.)
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Abstract
Remote control amphibious aircraft, including fuselage.Fuselage is sealed empty capsid, and fuselage both sides are respectively arranged with the first wing and the second wing.It is provided with below first wing below the first support plate, the first support plate and is provided with the first floating body.It is provided with below second wing below the second support plate, the second support plate and is provided with the second floating body.First floating body and the second floating body can be that ship type is empty capsid.It can easily drop on the water surface, extend the scope of application of telecontrolled aircraft.
Description
Technical field
The utility model belongs to game device field, more particularly to remote control amphibious aircraft.
Background technology
The game stations such as current model plane, Che Mo and ship model, can only all be operated on land or in the air,
It can only also fall in the anhydrous place such as land when landing, currently there are no the telecontrolled aircraft that can land on the water.
Utility model content
The purpose of this utility model is to be directed to the problem of current telecontrolled aircraft can not be dropped on the water surface, and provides remote-controlled water
The dual-purpose aircraft in land, in that context it may be convenient to drop on the water surface, extends the scope of application of telecontrolled aircraft.
The technical scheme of use is：
Remote control amphibious aircraft, including fuselage.
Technical points are：
Fuselage is sealed empty capsid, and fuselage both sides are respectively arranged with the first wing and the second wing.
It is provided with below first wing below the first support plate, the first support plate and is provided with the first floating body.
It is provided with below second wing below the second support plate, the second support plate and is provided with the second floating body.
First floating body and the second floating body can be ship type empty capsid.
It the advantage is that：
Using airframe as main floating body, wing is above floating body, and both sides use small boat type floating body（First floating body and
Second floating body）To keep balance, it is used as power with preceding pull-type propeller, power is made of battery, wing both sides have undercarriage to be easy to
Land landing.Respectively there is a steering wheel in fuselage both sides, rudder and elevator above wing can be pulled to swim on the water surface.
Storage battery power supply 12v is to electronic controller.Motor is arrived after electronic controller adjustment, electronic controller comes out a signal wire company
Receiver is connected to, the signal of set remote-controller is received, two-way is exported to steering wheel from the passage of receiver 12.Power supply and letter are provided to steering wheel
Number.
Brief description of the drawings
Fig. 1 is front view of the present utility model.
Fig. 2 is side view of the present utility model.
Fig. 3 is top view of the present utility model.
Embodiment
Remote control amphibious aircraft, including fuselage 1.
Fuselage 1 is sealed empty capsid, and as main floating body, the both sides of fuselage 1 are respectively arranged with the first wing 2 and the second wing
3。
The lower section of first wing 2 is fixedly installed the first support plate 4, and the lower section of the first support plate 4 is fixed with the first floating body 6.
The lower section of second wing 3 is fixedly installed the second support plate 5, and the lower section of the second support plate 5 is fixed with the second floating body.
First floating body 6 is ship type empty capsid, and leading section is pointed.
Second floating body is ship type empty capsid, and leading section is pointed.
The inner upper of fuselage 1 is provided with battery 7, and the electron adjuster 8 of battery 7 powers, electronic controller 8 to motor 9,
Receiver 11 is powered, and receiver 11 powers and provided signal to steering wheel 10, rudder and elevator, the control direction rudder of steering wheel 10 and
Elevator works, and this is routine techniques, therefore not repeated description.
The upper surface of fuselage 1 is provided with top cover 15, is used for placing the inner member of fuselage 1.
The middle part of fuselage 1 is provided with the dividing plate 14 of horizontal seal.
The rear portion of fuselage 1 is fixed with vertical tail 13.There is propeller on the output shaft of motor 9.The rear portion both sides of fuselage 1 are solid respectively
Surely it is provided with tailplane 12.
Claims (4)
1. remote control amphibious aircraft, including fuselage（1）；It is characterized in that：
Fuselage（1）For sealed empty capsid, fuselage（1）Both sides are respectively arranged with the first wing（2）With the second wing（3）；
First wing（2）Lower section is provided with the first support plate（4）, the first support plate（4）Lower section is provided with the first floating body（6）；
Second wing（3）Lower section is provided with the second support plate（5）, the second support plate（5）Lower section is provided with the second floating body.
2. remote control amphibious aircraft according to claim 1, it is characterised in that：First floating body（6）For empty capsid；Second
Floating body is empty capsid.
3. remote control amphibious aircraft according to claim 1, it is characterised in that：First floating body（6）Floated for ship type, second
Body is ship type.
4. remote control amphibious aircraft according to claim 1, it is characterised in that：First floating body（6）It is point for leading section
Shape；Second floating body is that leading section is pointed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720042842.2U CN206518880U (en) | 2017-01-16 | 2017-01-16 | Remote control amphibious aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720042842.2U CN206518880U (en) | 2017-01-16 | 2017-01-16 | Remote control amphibious aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206518880U true CN206518880U (en) | 2017-09-26 |
Family
ID=59890642
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720042842.2U Active CN206518880U (en) | 2017-01-16 | 2017-01-16 | Remote control amphibious aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206518880U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621379A (en) * | 2017-01-16 | 2017-05-10 | 王长民 | Telecontrolled amphibious aircraft |
-
2017
- 2017-01-16 CN CN201720042842.2U patent/CN206518880U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621379A (en) * | 2017-01-16 | 2017-05-10 | 王长民 | Telecontrolled amphibious aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |