CN201394365Y - Interesting plane - Google Patents
Interesting plane Download PDFInfo
- Publication number
- CN201394365Y CN201394365Y CN2009203034540U CN200920303454U CN201394365Y CN 201394365 Y CN201394365 Y CN 201394365Y CN 2009203034540 U CN2009203034540 U CN 2009203034540U CN 200920303454 U CN200920303454 U CN 200920303454U CN 201394365 Y CN201394365 Y CN 201394365Y
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- CN
- China
- Prior art keywords
- plane
- bearing
- aircraft
- metal shell
- lead
- 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 - Fee Related
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Abstract
The utility model relates to toys and particularly relates to an interesting plane which can rotate in flight for a long time. The utility model comprises a fixed rod and a plane, wherein the top partof the fixed rod is provided with a rotating device and conducting wires on the rotating device guide the plane to rotate around the fixed rod at 360 degrees. The rotating device also comprises a fixed shaft which is connected with the fixed rod, a bearing arranged outside the fixed shaft, an insulation layer and a metal shell, wherein the metal shell is provided with a carbon brush. The interesting plane has strong interest and appreciation performance. Furthermore, the bearing is not connected with the plane directly so as to ensure that pull wires do not knotted. 220V to 8V voltage can beused and the plane can fly in a rotating manner for a long time after the plane is turned on. Moreover, the speed of the plane can drive the bearing to rotate.
Description
Technical field
The utility model relates to toy, refers in particular to the entertaining aircraft of the long-time spiraling of a kind of energy.
Background technology
The toy airplane of child's object for appreciation at present can only rely on battery to slide on ground mostly, and some rotation aircrafts also are directly to fixedly connected with bearing with a rope, after rotating a fixing turn, bearing will produce the phenomenon of knotting when aircraft, finally cause the aircraft can't normal flight, and rope also can produce wear phenomenon, directly influences its interest.
Summary of the invention
The purpose of this utility model is improved, is innovated at shortcoming that exists in the background technology and problem, and the trouble-free entertaining aircraft that can fly for a long time is provided.
The technical solution of the utility model is a kind of toy of being made up of fixed bar and aircraft of structure, wherein:
The top of fixed bar is provided with whirligig, and the lead towing aircraft on the whirligig rotates around fixed bar 360 degree, and whirligig also comprises:
A fixed axis that is connected with fixed bar;
Be arranged on fixed axis outer bearing, insulating barrier and metal shell, wherein metal shell is provided with carbon brush.
The beneficial effects of the utility model:
The utility model interest, sight are strong, and bearing directly do not link to each other with aircraft, make draught line not tie a knot, and can use 220-8 volt voltage, the spiraling for a long time of energising back aircraft, and air speed can drive bearing and rotates.
Description of drawings
Fig. 1 is the utility model structural representation
Fig. 2 is rotary device structure figure
Fig. 3 is Fig. 2 decomposing schematic representation
The specific embodiment
By Fig. 1 to 3 as can be known, the utility model is made up of fixed bar 1 and aircraft 2, wherein:
The top of fixed bar 1 is provided with whirligig, and lead 8,9 towing aircrafts 2 on the whirligig rotate around fixed bar 1360 degree, and whirligig also comprises:
A fixed axis 3 that is connected with fixed bar 1;
Be arranged on bearing 4, insulating barrier 5 and metal shell 6 outside the fixed axis 3, wherein metal shell 6 is provided with carbon brush 7.
Bearing 4 described in the utility model is enclosed within outside the fixed axis 3, and lead 9 is arranged on the bearing 4 and connects power supply, and welding lead 9 towing aircrafts 2 in addition on the bearing 4.Described insulating barrier 5 is enclosed within outside the bearing 4, along with bearing 4 rotations.Described metal shell 6 is arranged on the outermost layer of whirligig, is enclosed within on the insulating barrier 5, and lead 8 is fixedly installed on the top of metal shell 6 one sides, and carbon brush 7 is arranged on the middle part of metal shell 6, and carbon brush 7 bottoms connect lead 8.Described aircraft 2 is provided with terminals, and aircraft 2 front ends are provided with propeller, are provided with motor in the body.All hidden being arranged in the fixed bar 1 of described fixed axis 3 and lead 8,9 lower ends.
Embodiment described in the utility model only is the description that preferred implementation of the present utility model is carried out; be not that the utility model design and scope are limited; under the prerequisite that does not break away from the utility model design philosophy; engineers and technicians make the technical solution of the utility model in this area various modification and improvement; all should fall into protection domain of the present utility model; the technology contents that the utility model is asked for protection all is documented in claims.
Claims (6)
1. an entertaining aircraft is made up of fixed bar (1) and aircraft (2), it is characterized in that:
The top of fixed bar (1) is provided with whirligig, and (8, the 9) towing aircrafts of the lead on the whirligig (2) rotate around fixed bar (1) 360 degree, and whirligig also comprises:
A fixed axis (3) that is connected with fixed bar (1);
Be arranged on fixed axis (3) outer bearing (4), insulating barrier (5) and metal shell (6), wherein metal shell (6) is provided with carbon brush (7).
2. entertaining aircraft according to claim 1 is characterized in that described bearing (4) is enclosed within outside the fixed axis (3), and lead (9) is arranged on bearing (4) and goes up the connection power supply, and bearing (4) is gone up other welding lead (9) towing aircraft (2).
3. entertaining aircraft according to claim 1 is characterized in that described insulating barrier (5) is enclosed within outside the bearing (4), along with bearing (4) rotation.
4. entertaining aircraft according to claim 1, it is characterized in that described metal shell (6) is arranged on the outermost layer of whirligig, be enclosed within on the insulating barrier (5), lead (8) is fixedly installed on the top of metal shell (6) one sides, carbon brush (7) is arranged on the middle part of metal shell (6), and carbon brush (7) bottom connects lead (8).
5. entertaining aircraft according to claim 1 is characterized in that described aircraft (2) is provided with terminals, and aircraft (2) front end is provided with propeller, is provided with motor in the body.
6. entertaining aircraft according to claim 1 is characterized in that all hidden being arranged in the fixed bar (1) in described fixed axis (3) and lead (8,9) lower end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009203034540U CN201394365Y (en) | 2009-05-22 | 2009-05-22 | Interesting plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009203034540U CN201394365Y (en) | 2009-05-22 | 2009-05-22 | Interesting plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201394365Y true CN201394365Y (en) | 2010-02-03 |
Family
ID=41616853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009203034540U Expired - Fee Related CN201394365Y (en) | 2009-05-22 | 2009-05-22 | Interesting plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201394365Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110313763A (en) * | 2019-06-27 | 2019-10-11 | 恒昌工業有限公司 | The model aircraft bracket and model aircraft of multi-angle rotary fight maneuver device |
-
2009
- 2009-05-22 CN CN2009203034540U patent/CN201394365Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110313763A (en) * | 2019-06-27 | 2019-10-11 | 恒昌工業有限公司 | The model aircraft bracket and model aircraft of multi-angle rotary fight maneuver device |
| CN110313763B (en) * | 2019-06-27 | 2020-11-13 | 恒昌工業有限公司 | Multi-angle rotating's aircraft model support and aircraft model fight exercise device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100203 Termination date: 20120522 |