CN106585983A - Novel flying flapping wing moving mechanism - Google Patents
Novel flying flapping wing moving mechanism Download PDFInfo
- Publication number
- CN106585983A CN106585983A CN201611257774.8A CN201611257774A CN106585983A CN 106585983 A CN106585983 A CN 106585983A CN 201611257774 A CN201611257774 A CN 201611257774A CN 106585983 A CN106585983 A CN 106585983A
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- CN
- China
- Prior art keywords
- flapping wing
- moving mechanism
- gears
- wing moving
- gear
- 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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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C33/00—Ornithopters
- B64C33/02—Wings; Actuating mechanisms therefor
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention provides a novel flying flapping wing moving mechanism. The novel flying flapping wing moving mechanism comprises a gear case which is in electric connection with a motor; two mutually-engaged gears are fixedly arranged in the gear case, the two gears are connected with a swing rod set in a transmission mode, and the swing rod set is connected with a fan blade set in a transmission mode; and each of two swing rods of the swing rod set is connected with the corresponding gear in a transmission mode, the two swing rods are connected with two fan blades of the fan blade set in a transmission through the two gears, and the two fan blades of the fan blade set are connected with the two gears in a transmission mode correspondingly. According to the novel flying flapping wing moving mechanism, the structure is reasonable, cost is low, the mechanism is durable, the flying time and the service life are long, standardized production is achieved, and applicability is high; standardization and modularization of a factory can be achieved; the novel flying flapping wing moving mechanism is subjected to flow line production and can be produced in bulk according to a plan and then made into stock, product precision is high, industrialized and scale development can be achieved, and the application range is wide; and the novel flying flapping wing moving mechanism can be widely used in necessary occasions and has high market economic benefits.
Description
Technical field
The present invention relates to a kind of flight flapping wing mechanism, more particularly to a kind of new flight flapping wing wing motion.
Background technology
A kind of new flight flapping wing wing motion in the market is broadly divided into static and dynamic two types, moves
The general of state compares the more favourable of static state.But a kind of dynamic new flight flapping wing wing motion structure is more multiple on market
It is miscellaneous, therefore material cost is higher with assembly cost.
A kind of minitype bionic space flapping wing mechanism is disclosed in prior art, which is mainly by DC micromotor, reducing gear
Wheel, deflection main shaft, fork, flexible joint, flapping wing, flapping wing mounting bracket and casing are constituted.DC micromotor passes through reducing gear
Wheel drive deflection main shaft does gyration, and deflection main shaft band driven fork does space motion, and flapping wing is arranged in flapping wing mounting bracket,
Flapping wing mounting bracket is arranged on casing by flexible joint, and the other end is connected with fork by bearing pin, when fork does space fortune
Flapping wing wing tip is driven to do space 8 font motion when dynamic.
Very not rationally, energy consumption is big, and consumption of raw materials is more, and flight effect is undesirable for the flight flapping wing structure of said structure, safeguards
Maintenance is difficult, is not suitable with the requirement of today's society.
The content of the invention
It is an object of the invention to provide a kind of simple for structure, reasonable, less energy consumption, effect it is good, so as to greatly improving flight effect
The new flight flapping wing wing motion of rate.
A kind of new flight flapping wing wing motion, it is including the gear-box electrically connected with motor, solid in the gear-box
If two engaged gears, described two gears are connected with fork group, the fork group is connected with flabellum group.
Two forks of the fork group are respectively connected with a gear drive.
Described two forks are connected with two flabellums of flabellum group respectively by two gears.
Two flabellums of the flabellum group are connected with two gear drives respectively.
The present invention can reach following beneficial effect using after above-mentioned technical proposal：
1st, it is simple for structure, reasonable.Compared with the static flight flapping wing wing motion on market, the present invention is dynamic
, so there is certain advantage.Again compared with the dynamic a kind of new flight flapping wing wing motion on market, present invention knot
Structure is fairly simple, thus saves material cost, also allows installation process to become easy, and then saves assembly cost.
2nd, practical new property is strong, long service life.Rationally, product is durable, long service life for present configuration.
3rd, standardized production.The present invention can realize factory normalization, modularity, and production line balance can be given birth to according to plan in batches
Product makes stock, and Product Precision is high, is capable of achieving industrialization, large-scale development.
4th, it is elegant in appearance, applied widely.The present invention is elegant in appearance, and moulding is unique, adapts to the aesthetic of client, extensively can use
In occasion in need.
5th, market economy is wide.Compared with prior art, rational in infrastructure, low cost, flight time are long, with wide for the present invention
Wealthy market economy benefit.
Description of the drawings
Fig. 1 is the axonometric chart of the present invention；
Fig. 2 is the front view of the present invention；
Fig. 3 is the rearview of the present invention.
Description of reference numerals
1st, motor 2, fork 1, fork 24, gear-box 5, flabellum 6, flabellum.
Specific embodiment
Below in conjunction with the accompanying drawings and specific embodiment is described in further detail to the present invention：
Referring to Fig. 1
Fig. 1 is the axonometric chart of the present invention.In FIG, a kind of new flight flapping wing wing motion, including with motor 1
The gear-box 4 of electrical connection, fixed two engaged gears in the gear-box 4, described two gears are driven with fork group
Connection, the fork group are connected with flabellum group.
Two forks 2,3 of the fork group are respectively connected with a gear drive.
Described two forks 2,3 are connected with two flabellums 5,6 of flabellum group respectively by two gears.
Two flabellums 5,6 of the flabellum group are connected with two gear drives respectively.
Referring to Fig. 2
Fig. 2 is the front view of the present invention.In Fig. 2, a kind of new flight flapping wing wing motion, including electric with motor 1
The gear-box 4 of connection, fixed two engaged gears in the gear-box 4, the gear are connected with fork group, institute
State fork group to be connected with flabellum group.
Two forks 2,3 of the fork group are respectively connected with a gear drive.
Referring to Fig. 3
Fig. 3 is the rearview of the present invention.In figure 3, a kind of two forks 2,3 of new flight flapping wing wing motion
Respectively it is connected with a gear drive, two flabellums 5,6 are connected with two gear drives respectively.
Two forks 2,3 are connected with two flabellums 5,6 respectively by two gears.Workflow：
Fork 1 is rotated in the presence of motor 1, carrys out back rotation so as to driven the certain angle of fork 23.Fork
23 are connected with a gear in gear-box 4 again, thus have driven the rotation of gear.Because there is two gears in gear-box 4,
And two gears are mutually twisted, so two gears will do the relative motion of certain angle.And two gears and two flabellums
5th, 6 are connected, therefore two flabellums 5,6 will do the relative motion of certain angle.
Other techniques of the present invention can adopt prior art.
Highly preferred embodiment of the present invention has been illustrated, and one of ordinary skill in the art is further for what the present invention made
Expansion each falls within protection scope of the present invention.
Claims (4)
1. a kind of new flight flapping wing wing motion, including the gear-box electrically connected with motor, it is characterised in that：The tooth
Fixed two engaged gears in roller box, described two gears are connected with fork group, the fork group and flabellum group
It is connected.
2. a kind of new flight flapping wing wing motion according to claim 1, it is characterised in that：The fork group
Two forks are respectively connected with a gear drive.
3. a kind of new flight flapping wing wing motion according to claim 2, it is characterised in that：Described two forks
It is connected with two flabellums of flabellum group by two gears respectively.
4. a kind of new flight flapping wing wing motion according to claim 3, it is characterised in that：The flabellum group
Two flabellums are connected with two gear drives respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611257774.8A CN106585983A (en) | 2016-12-30 | 2016-12-30 | Novel flying flapping wing moving mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611257774.8A CN106585983A (en) | 2016-12-30 | 2016-12-30 | Novel flying flapping wing moving mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106585983A true CN106585983A (en) | 2017-04-26 |
Family
ID=58581603
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611257774.8A Pending CN106585983A (en) | 2016-12-30 | 2016-12-30 | Novel flying flapping wing moving mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106585983A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11286045B2 (en) | 2017-11-29 | 2022-03-29 | Animal Dynamics Limited | Canopy control system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009090770A (en) * | 2007-10-05 | 2009-04-30 | Osaka Prefecture Univ | Flapping flying device |
| CN102211665A (en) * | 2010-04-07 | 2011-10-12 | 上海工程技术大学 | Micro dragonfly-imitating dual-flapping wing aircraft |
| CN204279946U (en) * | 2014-11-14 | 2015-04-22 | 大连海洋大学 | Bionic mechanical bird flying device transmission device |
| CN204937507U (en) * | 2015-08-10 | 2016-01-06 | 吴锜 | The flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula |
| CN205707351U (en) * | 2016-06-24 | 2016-11-23 | 巢湖学院 | Minitype bionic flapping wing robot |
-
2016
- 2016-12-30 CN CN201611257774.8A patent/CN106585983A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009090770A (en) * | 2007-10-05 | 2009-04-30 | Osaka Prefecture Univ | Flapping flying device |
| CN102211665A (en) * | 2010-04-07 | 2011-10-12 | 上海工程技术大学 | Micro dragonfly-imitating dual-flapping wing aircraft |
| CN204279946U (en) * | 2014-11-14 | 2015-04-22 | 大连海洋大学 | Bionic mechanical bird flying device transmission device |
| CN204937507U (en) * | 2015-08-10 | 2016-01-06 | 吴锜 | The flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula |
| CN205707351U (en) * | 2016-06-24 | 2016-11-23 | 巢湖学院 | Minitype bionic flapping wing robot |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11286045B2 (en) | 2017-11-29 | 2022-03-29 | Animal Dynamics Limited | Canopy control system |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170426 |