CN105000181A - Wing device of flapping machine - Google Patents
Wing device of flapping machine Download PDFInfo
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- CN105000181A CN105000181A CN201510486483.5A CN201510486483A CN105000181A CN 105000181 A CN105000181 A CN 105000181A CN 201510486483 A CN201510486483 A CN 201510486483A CN 105000181 A CN105000181 A CN 105000181A
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- wing
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- swatting
- adapter shaft
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Abstract
The invention belongs to the technical field of flatting machine preparing, and particularly relates to a wing device of a flapping machine. A main structure comprises a connecting shaft, a left support, a right support, main frameworks, ribs, films, a left wing and a right wing. The left support and the right support are fixedly arranged on the connecting shaft. The connecting shaft is fixedly connected with a power machine of the flapping machine through the left support and the right support. The left support and the right support support the rotation of the connecting shaft. Each of the left wing and the right wing is formed by connecting and combining the main frameworks, the ribs and the films in a matched manner. The main framework of the left wing and the main framework of the right wing are in mechanical transmission connection with the connecting shaft. The components are matched to form a wing structure of the flapping machine. Climbing force and advancing force are provided for flight through power generated by left-and-right swinging when a fish tail moves, and a flight mechanism of the flight state of the flapping machine is achieved. The wing device is simple in structure, scientific in principle, low in manufacturing cost, easy to regulate, good in flight effect and wide in application prospect.
Description
Technical field:
The invention belongs to and swat machine preparing technical field, be specifically related to one and swat machine wing device, utilize the principle design of fish tail to swat machine wing structure, realize Bird Flight condition regulation effect.
Background technology:
For a long time, people's dream realize birds like that on high in the technical scheme of circling in the air, a lot of people imitates the wing having made birds, attempts to fly up, and does not all have successfully; People, by having carried out long analytical investigation to the parade principle of fish, have grasped the principle of some parades, find that the tail of fish swings as the power provided forward of parading; Because the plane swung can produce air-flow to the vertical direction swung, and these air-flows can produce antagonistic force in the opposite direction, just as our Fan fan in daily life, the cool breeze that Fan fan brings, not on the direction in fan face, but in the vertical direction of fan swing; Also have the wooden boat in rivers,lakes and seas, swinging back and forth by the wooden oar on stern exactly provides front action edge, and this is the example imitating the swing of fish tail; At present, many person skilled swing at researching fish tail and provide the fluid mechanics principle of power, but the tail not yet proposing fish in numerous documents and report swings and provides machine of the swatting wing device of rising and front action edge for swatting machine.Therefore, research and develop a kind of machine of swatting wing device swinging principle based on fish tail, have very much science and using value, also there is good society and application prospect.
Summary of the invention:
The object of the invention is to the shortcoming overcoming prior art existence, seek design one and swat machine wing device, thering is provided raising force and the principle of power of moving ahead by means of the fish tail power formed that swings when parading for flight, realizing the structure design that freely circles in the air of machine of swatting.
To achieve these goals, the agent structure of machine of the swatting wing device that the present invention relates to comprises adapter shaft, left socle, right support, main framing, muscles and bones, film, left wing and right wing; With swat interval type on adapter shaft that mechanomotive force machine mechanical type is connected and be fixedly installed left socle and right support, adapter shaft is divided into three parts of equal length by left socle and right support, adapter shaft is fixedly connected with the engine swatting machine with right support respectively by left socle, the rotation of left socle and right support adapter shaft; Left wing and right wing are made up of the combination that is connected of main framing, muscles and bones and film respectively, all in 15-30 degree angle inclined downward between the left wing of symmetrical structure and right wing and the plane of swatting residing for machine body lateral cross section; The right part of the main framing of left wing is connected with the left part mechanical transmission of adapter shaft; The left end of the main framing of right wing is connected with the right part mechanical transmission of adapter shaft; Each part fits forms the wing structure of machine of swatting, and realizes the fly mechanics swatting machine state of flight.
The structure of the muscles and bones that the present invention relates to is the fine strip shape of elastic material, and muscles and bones and diaphragm seal connect and compose plumage structure, and muscles and bones is that film provides support power; Film is the light structures of airtight draining material.
When machine of the swatting wing device that the present invention relates to uses, the power that swatting power plants provides drives left wing and right wing synchronously oliquely downward to swing up and down by the main framing of adapter shaft, left wing and the main framing of right wing, produce the antagonistic force of oblique top, according to physics principle, antagonistic force provides application force forward and upwards, promotes to swat machine forward and upward movement; The power size making it provide by the setting of swatting power plants is controlled, realize the regulation and control of the speed of swatting up and down of left wing and right wing, and make the speed of flutterring slow, under to flutter speed fast, speed is swung up and down for left wing and right wing provide different, produce different power forward and upwards, realize the lifting of machine of swatting, fly, turn to and speed governing effect, complete the fly mechanics voluntarily of the birds state of the machine of swatting.
Compared with prior art, provide raising force and the principle of power of moving ahead based on swing when the parading power that formed of fish tail for flight, research and development make one and swat machine wing structure in the present invention; Its structure is simple, scientific in principle, and cost of manufacture is low, and be easy to regulation and control, flight effect is good, has a extensive future.
Accompanying drawing illustrates:
Fig. 1 is agent structure principle schematic of the present invention.
Detailed description of the invention:
Also by reference to the accompanying drawings the present invention is described further below by embodiment.
Embodiment:
The agent structure of what the present embodiment related to swat machine wing device comprises adapter shaft 1, left socle 2, right support 3, main framing 4, muscles and bones 5, film 6, left wing 7 and right wing 8; With swat interval type on adapter shaft 1 that mechanomotive force machine mechanical type is connected and be fixedly installed left socle 2 and right support 3, adapter shaft 1 is divided into three parts of equal length by left socle 2 and right support 3, adapter shaft 1 is fixedly connected with the engine swatting machine with right support 3 respectively by left socle 2, the rotation of left socle 2 and right support 3 support and connection axle 1; Left wing 7 and right wing 8 are made up of the combination that is connected of main framing 4, muscles and bones 5 and film 6 respectively, all in 15-30 degree angle inclined downward between the left wing 7 of symmetrical structure and right wing 8 and the plane of swatting residing for machine body lateral cross section; The right part of the main framing 4 of left wing 7 is connected with the left part mechanical transmission of adapter shaft 1; The left end of the main framing 4 of right wing 8 is connected with the right part mechanical transmission of adapter shaft 1; Each part fits forms the wing structure of machine of swatting, and realizes the fly mechanics swatting machine state of flight.
The structure of the muscles and bones 5 that the present embodiment relates to is the fine strip shape of elastic material, and muscles and bones 5 and film 6 are tightly connected and form plumage structure, and muscles and bones 5 provides support power for film 6; Film 6 is the light structures of airtight draining material.
When the present embodiment uses, the power that swatting power plants provides drives left wing 7 and right wing 8 synchronously oliquely downward to swing up and down by the main framing 4 of adapter shaft 1, left wing 7 and the main framing 4 of right wing 8, produce the antagonistic force of oblique top, according to physics principle, antagonistic force provides application force forward and upwards, promotes to swat machine forward and upward movement; The power size making it provide by the setting of swatting power plants is controlled, thus realize the regulation and control of the speed of swatting up and down of left wing 7 and right wing 8, and make the speed of flutterring slow, under to flutter speed fast, speed is swung up and down for left wing 7 and right wing 8 provide different, produce different power forward and upwards, realize the lifting of machine of swatting, fly, turn to and speed governing effect, complete the fly mechanics voluntarily of the birds state of the machine of swatting.
Claims (3)
1. swat a machine wing device, it is characterized in that agent structure comprises adapter shaft, left socle, right support, main framing, muscles and bones, film, left wing and right wing; With swat interval type on adapter shaft that mechanomotive force machine mechanical type is connected and be fixedly installed left socle and right support, adapter shaft is divided into three parts of equal length by left socle and right support, adapter shaft is fixedly connected with the engine swatting machine with right support respectively by left socle, the rotation of left socle and right support adapter shaft; Left wing and right wing are made up of the combination that is connected of main framing, muscles and bones and film respectively, all in 15-30 degree angle inclined downward between the left wing of symmetrical structure and right wing and the plane of swatting residing for machine body lateral cross section; The right part of the main framing of left wing is connected with the left part mechanical transmission of adapter shaft; The left end of the main framing of right wing is connected with the right part mechanical transmission of adapter shaft; Each part fits forms the wing structure of machine of swatting, and realizes the fly mechanics swatting machine state of flight.
2. according to claim 1ly swat machine wing device, it is characterized in that the structure of described muscles and bones is the fine strip shape of elastic material, muscles and bones and diaphragm seal connect and compose plumage structure, and muscles and bones is that film provides support power; Described film is the light structures of airtight draining material.
3. according to claim 1 and 2ly swat machine wing device, when it is characterized in that using, the power that swatting power plants provides drives left wing and right wing synchronously oliquely downward to swing up and down by the main framing of adapter shaft, left wing and the main framing of right wing, produce the antagonistic force of oblique top, according to physics principle, antagonistic force provides application force forward and upwards, promotes to swat machine forward and upward movement; The power size making it provide by the setting of swatting power plants is controlled, realize the regulation and control of the speed of swatting up and down of left wing and right wing, and make the speed of flutterring slow, under to flutter speed fast, speed is swung up and down for left wing and right wing provide different, produce different power forward and upwards, realize the lifting of machine of swatting, fly, turn to and speed governing effect, complete the fly mechanics voluntarily of the birds state of the machine of swatting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510486483.5A CN105000181A (en) | 2015-08-10 | 2015-08-10 | Wing device of flapping machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510486483.5A CN105000181A (en) | 2015-08-10 | 2015-08-10 | Wing device of flapping machine |
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| Publication Number | Publication Date |
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| CN105000181A true CN105000181A (en) | 2015-10-28 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510486483.5A Pending CN105000181A (en) | 2015-08-10 | 2015-08-10 | Wing device of flapping machine |
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| CN (1) | CN105000181A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018028569A1 (en) * | 2016-08-11 | 2018-02-15 | 谭佑军 | Ornithopter |
| CN109383794A (en) * | 2018-09-28 | 2019-02-26 | 合肥联合飞机科技有限公司 | A kind of all-wing aircraft dynamic structure |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6659397B1 (en) * | 2002-10-18 | 2003-12-09 | Richard Charron | Control system for ornithopter |
| CN101049858A (en) * | 2006-04-06 | 2007-10-10 | 西北工业大学 | Driving mechanism for wings of minitype ornithopter |
| KR20110057414A (en) * | 2009-11-24 | 2011-06-01 | 우병화 | Ornithopter |
| CN104176252A (en) * | 2014-09-05 | 2014-12-03 | 上海理工大学 | Flapping wing utilizing wind energy or water flow energy to charge for continuous voyage |
| CN204937504U (en) * | 2015-08-10 | 2016-01-06 | 吴锜 | One swats machine wing device |
-
2015
- 2015-08-10 CN CN201510486483.5A patent/CN105000181A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6659397B1 (en) * | 2002-10-18 | 2003-12-09 | Richard Charron | Control system for ornithopter |
| CN101049858A (en) * | 2006-04-06 | 2007-10-10 | 西北工业大学 | Driving mechanism for wings of minitype ornithopter |
| KR20110057414A (en) * | 2009-11-24 | 2011-06-01 | 우병화 | Ornithopter |
| CN104176252A (en) * | 2014-09-05 | 2014-12-03 | 上海理工大学 | Flapping wing utilizing wind energy or water flow energy to charge for continuous voyage |
| CN204937504U (en) * | 2015-08-10 | 2016-01-06 | 吴锜 | One swats machine wing device |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018028569A1 (en) * | 2016-08-11 | 2018-02-15 | 谭佑军 | Ornithopter |
| CN109383794A (en) * | 2018-09-28 | 2019-02-26 | 合肥联合飞机科技有限公司 | A kind of all-wing aircraft dynamic structure |
| CN109383794B (en) * | 2018-09-28 | 2021-09-21 | 合肥联合飞机科技有限公司 | Flying wing power structure |
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Application publication date: 20151028 |