CN203402385U - Single-axis aircraft - Google Patents
Single-axis aircraft Download PDFInfo
- Publication number
- CN203402385U CN203402385U CN201320340726.0U CN201320340726U CN203402385U CN 203402385 U CN203402385 U CN 203402385U CN 201320340726 U CN201320340726 U CN 201320340726U CN 203402385 U CN203402385 U CN 203402385U
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- hinge
- frame
- empennages
- colored ribbon
- Prior art date
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- Expired - Fee Related
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Abstract
The utility model relates to a single-axis aircraft, which comprises a frame, a propeller, a motor, a control panel, a battery, four steering engines, four connecting rod mechanisms, four empennages, four undercarriages and a colored ribbon releasing device. One ends of the four connecting rod mechanisms are respectively connected with the four undercarriages, and the other ends of the four connecting rod mechanisms are respectively connected with the four empennages. Each connecting rod mechanism comprises a crank, a connecting rod I, a connecting rod II and an angle support, wherein the crank is connected with the connecting rod I through a hinge and the connecting rod I and the connecting rod II are connected together also through a hinge. The connecting rod II and the angle support are connected together through a hinge. The upper ends of the four empennages are connected with the frame through a hinge respectively. By means of the rotation of the steering engines, the connecting rod mechanisms are driven to move, so that the empennages swing at different angles. Finally, the forwarding, the withdrawing, the left-shifting, the right-shifting, the ascending, the descending, the self-rotating and other flight attitudes of the single-axis aircraft are realized. The colored ribbon releasing device is arranged at the center of the bottom of the frame and is used for storing and releasing colored ribbons.
Description
Technical field
The utility model relates to aircraft field, specifically a kind of single shaft aircraft.
Background technology
In Festival celebration Festival, put vertically hung scroll, the phenomenons such as aerograph band are customary, mostly adopt suspension or artificial mode to carry out, lack new meaning and intention, also have at present some quadrotors, but be not also applied to this field, and four rotors exist, and cost of manufacture is high, heavy, the problem such as easy care and difficult operation not.Therefore, a kind of cost of manufacture of active demand is low, light, maintain easily, simple to operate and can realize the aircraft that discharges colored ribbon, i.e. a kind of single shaft aircraft.
Summary of the invention
In order to solve the above problems, the utility model provides a kind of single shaft aircraft.
The technical scheme in the invention for solving the above technical problem is: a kind of single shaft aircraft, comprise frame, screw propeller, motor, control desk, battery, four steering wheels, four connecting rod mechanisms, four empennages, four alighting gears and colored ribbon release gear, described frame top is provided with mount pad, middle part is provided with control board slot, middle below is provided with battery case, and surrounding is symmetrically arranged with four steering wheel grooves, described screw propeller is arranged on motor shaft, and motor is arranged on the mount pad of frame top, and screw propeller and motor provide direct flying power for the utility model, control desk is arranged in the control board slot of central rack, and control desk is used for controlling flight attitude of the present utility model, battery is arranged in the battery case of below in frame, four steering wheels respectively symmetry are arranged in four steering wheel grooves, four connecting rod mechanism one end are connected with four steering wheels respectively, the other end is connected with four empennages respectively, described connecting rod mechanism comprises crank, connecting rod I, connecting rod II and angle bearing, crank is connected by hinge with connecting rod I, connecting rod I is connected by hinge with connecting rod II, connecting rod II is connected by hinge with angle bearing, four empennage upper ends and frame are connected through the hinge respectively, by the rotation of steering wheel, drivening rod mechanism kinematic, make empennage be put into different angles, finally realize of the present utility model advancing, retreat, move to left, move to right, rise, the various flight attitudes such as landing and spin, described colored ribbon release gear is arranged on frame bottom center, and colored ribbon release gear is used for storing and discharging colored ribbon.
The beneficial effects of the utility model are: a kind of single shaft aircraft, have cost of manufacture low, light, maintain easily, simple operation and other advantages, can realize the function that discharges colored ribbon.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is perspective view of the present utility model.
1. frames in figure, 2. screw propeller, 3. motor, 4. control desk, 5. battery, 6. steering wheel, 7. connecting rod mechanism, 701. cranks, 702. connecting rod I, 703. connecting rod II, 704. jiaos of bearings, 8. empennage, 9. alighting gear, 10. colored ribbon release gear.
The specific embodiment
As shown in Figure 1, a kind of single shaft aircraft described in the utility model, comprise frame 1, screw propeller 2, motor 3, control desk 4, battery 5, four steering wheels 6, four connecting rod mechanisms 7, four empennages 8, four alighting gears 9 and colored ribbon release gears 10, described frame 1 top is provided with mount pad, middle part is provided with control board slot, middle below is provided with battery case, and surrounding is symmetrically arranged with four steering wheel grooves; Described screw propeller 2 is arranged on motor 3 axles, and motor 3 is arranged on the mount pad of frame 1 top, and screw propeller 2 and motor 3 provide direct flying power for the utility model; Control desk 4 is arranged in the control board slot at frame 1 middle part, and control desk 4 is for controlling flight attitude of the present utility model; Battery 5 is arranged in the battery case of below in frame 1; Four steering wheels 6 respectively symmetry are arranged in four steering wheel grooves, four connecting rod mechanism 7 one end are connected with four steering wheels 6 respectively, the other end is connected with four empennages 8 respectively, described connecting rod mechanism 7 comprises crank 701, connecting rod I702, connecting rod II703 and angle bearing 704, crank 701 is connected by hinge with connecting rod I702, connecting rod I702 is connected by hinge with connecting rod II703, and connecting rod II703 is connected by hinge with angle bearing 704, and four empennage 8 upper ends and frame 1 are connected through the hinge respectively; Described colored ribbon release gear 10 is arranged on frame 1 bottom center, and colored ribbon release gear 10 is for storing and discharging colored ribbon.
During work, loop is connected, screw propeller 2 rotates under the drive of motor 3, and the utility model takes off, by the rotation of steering wheel 6,7 motions of drivening rod mechanism, make empennage 8 be put into different angles, realize of the present utility modelly advance, retreat, move to left, move to right, rise, the various flight attitudes such as landing and spin, aloft appropriate location, open colored ribbon release gear 10, discharge colored ribbon.
More than show and described groundwork of the present utility model, principal character and advantage.The technical personnel of the industry should be understood; the utility model is not restricted to the described embodiments; description in above-described embodiment and specification sheets principle of the present utility model is just described; do not departing under the prerequisite of the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (2)
1. a single shaft aircraft, comprise frame, screw propeller, motor, control desk, battery, four steering wheels, four connecting rod mechanisms, four empennages, four alighting gears and colored ribbon release gear, it is characterized in that: described frame top is provided with mount pad, middle part is provided with control board slot, middle below is provided with battery case, surrounding is symmetrically arranged with four steering wheel grooves, described screw propeller is arranged on motor shaft, motor is arranged on the mount pad of frame top, control desk is arranged in the control board slot of central rack, battery is arranged in the battery case of below in frame, four steering wheels respectively symmetry are arranged in four steering wheel grooves, four connecting rod mechanism one end are connected with four steering wheels respectively, the other end is connected with four empennages respectively, four empennage upper ends and frame are connected through the hinge respectively, described colored ribbon release gear is arranged on frame bottom center.
2. a kind of single shaft aircraft according to claim 1, it is characterized in that: described connecting rod mechanism comprises crank, connecting rod I, connecting rod II and angle bearing, crank is connected by hinge with connecting rod I, and connecting rod I is connected by hinge with connecting rod II, and connecting rod II is connected by hinge with angle bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320340726.0U CN203402385U (en) | 2013-06-14 | 2013-06-14 | Single-axis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320340726.0U CN203402385U (en) | 2013-06-14 | 2013-06-14 | Single-axis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203402385U true CN203402385U (en) | 2014-01-22 |
Family
ID=49938323
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320340726.0U Expired - Fee Related CN203402385U (en) | 2013-06-14 | 2013-06-14 | Single-axis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203402385U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083537A (en) * | 2015-08-05 | 2015-11-25 | 北京韦加航通科技有限责任公司 | Control surface control device and aircraft |
| WO2017114244A1 (en) * | 2015-12-31 | 2017-07-06 | 歌尔科技有限公司 | Single-shaft aerial vehicle |
| CN108721912A (en) * | 2018-08-13 | 2018-11-02 | 江阴市翔诺电子科技有限公司 | A kind of model of an airplane |
-
2013
- 2013-06-14 CN CN201320340726.0U patent/CN203402385U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083537A (en) * | 2015-08-05 | 2015-11-25 | 北京韦加航通科技有限责任公司 | Control surface control device and aircraft |
| WO2017114244A1 (en) * | 2015-12-31 | 2017-07-06 | 歌尔科技有限公司 | Single-shaft aerial vehicle |
| US10336434B2 (en) | 2015-12-31 | 2019-07-02 | Goertek Technology Co., Ltd. | Single-shaft aerial vehicle |
| CN108721912A (en) * | 2018-08-13 | 2018-11-02 | 江阴市翔诺电子科技有限公司 | A kind of model of an airplane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140122 Termination date: 20140614 |
|
| EXPY | Termination of patent right or utility model |