CN206679263U - A kind of bionic mechanical bird - Google Patents
A kind of bionic mechanical bird Download PDFInfo
- Publication number
- CN206679263U CN206679263U CN201720314223.4U CN201720314223U CN206679263U CN 206679263 U CN206679263 U CN 206679263U CN 201720314223 U CN201720314223 U CN 201720314223U CN 206679263 U CN206679263 U CN 206679263U
- Authority
- CN
- China
- Prior art keywords
- power source
- flapping wing
- connecting rod
- bionic mechanical
- rotating shaft
- 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
A kind of bionic mechanical bird, it is characterised in that：The flapping wing mechanism is provided with the rotating shaft extended to side, and the rotating shaft is connected with the second power source that it can be driven to rotate；The front end of the fuselage is provided with the infrared inductor that can sense barrier, infrared inductor control second power source of connection.It the advantage is that sensing flight front by infrared inductor whether there is barrier, once sense barrier, send a signal to the second power source, second power source drives flapping wing mechanism integrally to rotate forward or backward by rotating shaft, realize the nutation of flapping wing mechanism or face upward, so as to realize the rapid decrease of bionic mechanical bird or rising, with this avoiding barrier, it is not only simple in structure, and realizes automatic obstacle-avoiding effect.
Description
Technical field
A kind of aircraft is the utility model is related to, more particularly to a kind of bionic mechanical bird.
Background technology
Bionic mechanical bird is a kind of aircraft for exactly liking birds, can not only be flown, and can be fluttered, mould
Intend birds action.
Generally, bionic mechanical bird includes fuselage and flapping wing mechanism, and reality is agitated by flapping wing mechanism simulation birds wing
Now fly, but during flight in the air, still can encounter many barriers, and existing bionic mechanical bird will not automatic obstacle-avoiding,
Damaged so as to cause bionic mechanical bird easily to knock barrier.
Utility model content
In order to overcome the shortcomings of background technology, the utility model provides a kind of bionic mechanical bird, can automatic obstacle-avoiding, avoid
Knock barrier.
Technical scheme used by the utility model：A kind of bionic mechanical bird, including fuselage, flapping wing mechanism, the flapping wing
Mechanism includes installing plate, is symmetricly set on the flapping wing component of installing plate both sides, the first power source for driving flapping wing component to act；Institute
State flapping wing mechanism and be provided with the rotating shaft extended to side, the rotating shaft is connected with the second power source that it can be driven to rotate；It is described
The front end of fuselage is provided with the infrared inductor that can sense barrier, infrared inductor control second power source of connection.
The flapping wing component includes revolving part, swing arm, first connecting rod, second connecting rod, connector, locating part, third connecting rod；
The revolving part can be rotatably set on installing plate；One end of the swing arm is hinged with revolving part, and its pin joint and rotation
The pivot eccentric setting of part；The first connecting rod, one end of second connecting rod are hinged with swing arm respectively, the other end then respectively with
Connector is hinged；The first connecting rod is coordinated by locating part and installing plate locating slip；One end of the third connecting rod is fixed
Connect the connector.
The revolving part is gear, and the gear of two groups of flapping wing components is meshed.
First power source includes first reducing motors, the one of rotation of the first reducing motors drive connection
Part.
Second power source is second reducing motors, the second reducing motors drive connection rotating shaft.
The output end connection first reducing motors of the rotating shaft.
The beneficial effects of the utility model are：Using above scheme, whether flight front is sensed by infrared inductor
Barrier be present, once sensing barrier, send a signal to the second power source, the second power source drives flapping-wing aircraft by rotating shaft
Structure integrally rotates forward or backward, realize the nutation of flapping wing mechanism or face upward, so as to realize the rapid decrease of bionic mechanical bird or
Rise, with this avoiding barrier, be not only simple in structure, and realize automatic obstacle-avoiding effect.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model embodiment bionic mechanical bird.
Fig. 2 is the enlarged diagram at A in Fig. 1.
Fig. 3 is the positive structure schematic of the utility model embodiment flapping-wing aircraft component.
Fig. 4 is the structure schematic diagram of the utility model embodiment flapping wing mechanism.
Fig. 5 is the structural representation of the utility model embodiment flapping wing component.
1- installing plates in figure, 2- flapping wing components, 21- revolving parts, 22- swing arms, 23- first connecting rods, 24- second connecting rods, 25-
Connector, 26- locating parts, 27- third connecting rods, the power sources of -3- first, 4- rotating shafts, the power sources of 5- second, 6- infrared inductions dress
Put.
Embodiment
The utility model embodiment is described further below in conjunction with the accompanying drawings：
As illustrated, a kind of bionic mechanical bird, including fuselage, flapping wing mechanism, the flapping wing mechanism includes installing plate 1, right
Claim the first power source 3 for being arranged on the flapping wing component 2 of the both sides of installing plate 1, driving flapping wing component 2 to act；On the flapping wing mechanism
Provided with the rotating shaft 4 extended to side, the rotating shaft 4 is connected with the second power source 5 that it can be driven to rotate；The front end of the fuselage
Provided with the infrared inductor 6 that can sense barrier, the control of infrared inductor 6 second power source 5 of connection.
Flight front is sensed by infrared inductor 6 and whether there is barrier, once sensing barrier, sends signal
To the second power source 5, the second power source 5 drives flapping wing mechanism integrally to rotate forward or backward by rotating shaft 4, realizes flapping wing mechanism
Nutation or face upward, so as to realize the rapid decrease of bionic mechanical bird or rising, with this avoiding barrier, be not only simple in structure,
And realize automatic obstacle-avoiding effect.
As illustrated, the flapping wing component 2 includes revolving part 21, swing arm 22, first connecting rod 23, second connecting rod 24, connection
Part 25, locating part 26, third connecting rod 27；The revolving part 21 can be rotatably set on installing plate 1；One end of the swing arm 22
It is be hinged with revolving part 21, and the pivot eccentric setting of its pin joint and revolving part 21；The first connecting rod 23, second connecting rod
24 one end is be hinged with swing arm 22 respectively, and the other end is then be hinged with connector 25 respectively；The first connecting rod 23 passes through locating part
26 coordinate with the locating slip of installing plate 1；One end of the third connecting rod 27 is fixedly connected with the connector 25.
First power source 3 drives revolving part 21 to rotate, and revolving part 21 drives first connecting rod 23, second connecting rod by swing arm 22
24 move back and forth and the swing of low-angle, and the swing of third connecting rod 27 is driven by connector 25, so as to perfect simulation
Go out the flapping wing action of bionic mechanical bird.
Wherein, the revolving part 21 is gear, and the gear of two groups of flapping wing components 2 is meshed, first power source 3
Including first reducing motors, the one of gear of first reducing motors drive connection, it is not only simple in structure, and synchronism
It is good so that two groups of flapping wing components 2 are kept strokes.
In addition, second power source 5 is second reducing motors, the second reducing motors drive connection rotating shaft 4 is described
The output end connection first reducing motors of rotating shaft 4, it is simple in construction, it is easy to connect.
Embodiment is not construed as the limitation to utility model, but it is any be based on spiritual improvements introduced of the present utility model,
All should be within the scope of protection of the utility model.
Claims (6)
1. a kind of bionic mechanical bird, including fuselage, flapping wing mechanism, the flapping wing mechanism includes installing plate（1）, be symmetricly set on peace
Loading board（1）The flapping wing component of both sides（2）, drive flapping wing component（2）First power source of action（3）；
It is characterized in that：The flapping wing mechanism is provided with the rotating shaft extended to side（4）, the rotating shaft（4）Being connected with to drive
Its second power source rotated（5）；The front end of the fuselage is provided with the infrared inductor that can sense barrier（6）, it is described red
Outer induction installation（6）Control the second power source of connection（5）.
2. bionic mechanical bird according to claim 1, it is characterised in that：The flapping wing component（2）Including revolving part（21）、
Swing arm（22）, first connecting rod（23）, second connecting rod（24）, connector（25）, locating part（26）, third connecting rod（27）；The rotation
Turn part（21）It can be rotatably set in installing plate（1）On；The swing arm（22）One end and revolving part（21）It is be hinged, and it is be hinged
Point and revolving part（21）Pivot eccentric setting；The first connecting rod（23）, second connecting rod（24）One end respectively with pendulum
Arm（22）It is be hinged, the other end then respectively with connector（25）It is be hinged；The first connecting rod（23）Pass through locating part（26）With installation
Plate（1）Locating slip coordinates；The third connecting rod（27）One end be fixedly connected with the connector（25）.
3. bionic mechanical bird according to claim 2, it is characterised in that：The revolving part（21）For gear, two groups of flapping wings
Component（2）Gear be meshed.
4. bionic mechanical bird according to claim 3, it is characterised in that：First power source（3）Slow down including first
Motor, the one of revolving part of first reducing motors drive connection（21）.
5. bionic mechanical bird according to claim 4, it is characterised in that：Second power source（5）Slow down for second electric
Machine, the second reducing motors drive connection rotating shaft（4）.
6. bionic mechanical bird according to claim 5, it is characterised in that：The rotating shaft（4）Output end connection first subtract
Speed motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720314223.4U CN206679263U (en) | 2017-03-29 | 2017-03-29 | A kind of bionic mechanical bird |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720314223.4U CN206679263U (en) | 2017-03-29 | 2017-03-29 | A kind of bionic mechanical bird |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206679263U true CN206679263U (en) | 2017-11-28 |
Family
ID=60391283
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720314223.4U Expired - Fee Related CN206679263U (en) | 2017-03-29 | 2017-03-29 | A kind of bionic mechanical bird |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206679263U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033006A (en) * | 2017-12-16 | 2018-05-15 | 佛山市神风航空科技有限公司 | A kind of intelligent bionic mechanical bird |
| CN108082472A (en) * | 2017-12-16 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of highly emulated tool bird |
| CN108313312A (en) * | 2018-01-25 | 2018-07-24 | 芜湖应天光电科技有限责任公司 | A kind of unmanned plane drop preventer |
-
2017
- 2017-03-29 CN CN201720314223.4U patent/CN206679263U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033006A (en) * | 2017-12-16 | 2018-05-15 | 佛山市神风航空科技有限公司 | A kind of intelligent bionic mechanical bird |
| CN108082472A (en) * | 2017-12-16 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of highly emulated tool bird |
| CN108313312A (en) * | 2018-01-25 | 2018-07-24 | 芜湖应天光电科技有限责任公司 | A kind of unmanned plane drop preventer |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171128 Termination date: 20180329 |