CN104176252A - Flapping wing utilizing wind energy or water flow energy to charge for continuous voyage - Google Patents
Flapping wing utilizing wind energy or water flow energy to charge for continuous voyage Download PDFInfo
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- CN104176252A CN104176252A CN201410450498.1A CN201410450498A CN104176252A CN 104176252 A CN104176252 A CN 104176252A CN 201410450498 A CN201410450498 A CN 201410450498A CN 104176252 A CN104176252 A CN 104176252A
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Abstract
The invention relates to a flapping wing utilizing wind energy or water flow energy to charge for continuous voyage. The flapping wing comprises fins, wing levers, joints, small arms, small arm joints, large arms, a motor and driving mechanism, a battery and control chip, and a main shaft, wherein the motor and driving mechanism is connected with the large arms and the small arm joints on two sides in a transmission manner; each large arm is movably connected with one fin capable of flapping up and down through the joint and the wing lever in the fin; each small arm joint is movably connected with one fin capable of rotating around the main shaft through each small arm; the motor and driving mechanism is connected with the battery and control chip. The movement of the fins is compound movement, and the compound movement consists of twisting movement of the joints and rotational movement around the main shaft within the range of a certain angle. A large arm driving mechanism is composed of an electric generator (electromotor) and the battery and control chip. When an air vehicle or an underwater vehicle is in a voyage mode, electric energy of batteries is utilized, and the motor drives the large arms to swing around the main shaft so as to drive the wing to flap up and down and control the small arm to rotate, so that the wing rotates.
Description
Technical field
The present invention relates to the engine installation of a kind of aircraft or underwater sailing body, particularly a kind of wind energy or the aircraft of water flow energy charging continuation of the journey or flapping wing of underwater sailing body of utilizing.
Background technology
Flapping wing has very high flight efficiency, and its 1ift-drag ratio is that conventional fixed-wing cannot be reached.
For flapping wing aircraft, because its capacity of cell is limited, be difficult to long journey, if can allow flapping wing aircraft there is charge function in flight course, will greatly improve the value of this class aircraft.
Summary of the invention
The present invention will provide a kind of flapping wing that utilizes wind energy or water flow energy charging continuation of the journey.
For realizing the technical scheme that object of the present invention adopts, be: a kind of flapping wing that utilizes wind energy or water flow energy charging continuation of the journey, comprise fin, wing bar, joint, forearm, little shoulder joint, large arm, motor and driver train, battery and control chip, main shaft, be characterized in: motor and driver train connect large arm and the little shoulder joint of both sides by spindle, each large arm is flexibly connected one by the joint in fin and wing bar and can goes up, under the fin of fluttering, each little shoulder joint is flexibly connected the fin that can rotate around main shaft by forearm, motor and driver train are connected with battery and control chip.
In fin, be provided with the skeleton for supporting.During navigation, the rotational angle range of fin is-46 ° ~ 46 °; During charging, rotational angle range-75 of fin ° ~ 75 °.
The invention has the beneficial effects as follows: flapping wing of the present invention, the motion of its fin is a kind of compound motion.This compound motion is respectively by twisting motion joint with rotatablely move and form in certain angle around main shaft.Large arm driver train and the mechanical, electrical pond of generating (electronic) and control chip form, when aircraft or underwater sailing body are during in sail mode, utilize the electric energy in battery, motor drives large arm around spindle swing, drives the wing to flutter up and down, and controls forearm and rotate, the wing is rotated, slewing area is-46 ° ~ 46 °, this compound, will produce lift and thrust; When aircraft or underwater sailing body berth, control chip is controlled forearm and is rotated, angular range-75 of its rotation ° ~ 75 °, and under the effect of wind or current, flapping wing is fluttered, and large arm drives electrical generator to generate electricity, and charges to battery.This aircraft or underwater sailing body have long-range or very long range navigation ability.
Accompanying drawing explanation
Fig. 1 is structural upright schematic diagram of the present invention.
The specific embodiment
Below in conjunction with accompanying drawing and embodiment, the invention will be further described.
As shown in Figure 1, a kind of flapping wing that utilizes wind energy or water flow energy charging continuation of the journey, comprises fin 1, skeleton 2, wing bar 3, joint 4, forearm 5, forearm joint 6, large arm 7, motor and driver train 8, battery and control chip 9, main shaft 10.
Motor and driver train 8 connects main shafts 10, main shaft 10 be in transmission connection large arm 7 and the forearm joint 6 of both sides, and the joint 4 that each large arm 7 connects in fins 1, joint 4 connects wing bars 3, and wing bar 3 is placed in fin 1, is provided with the skeleton 2 for supporting in fin 1.Each forearm joint 6 connects a forearm 5, and forearm 5 connects fin 1.Motor and driver train (8) are connected with battery and control chip 9.
When aircraft or underwater sailing body are during in sail mode, utilize the electric energy in battery, motor and driver train 8 drive large arm 7 to swing around main shaft 10, drive that fin 1 is upper and lower flutters, and control forearm 5 and rotate, and make fin 1 occur to rotate around main shaft 10.
The motion of flapping wing is a kind of compound motion.This compound motion rotatablely moves and forms in certain angle by forearm joint 6 with around main shaft 10 respectively.The angular dimension of rotation is to guarantee that the amplitude of flapping wing up-and-down movement is roughly that one times of chord length of fin is advisable.
The angle of fin 1 twisting motion is: the programming control forearm joint 6 in control chip, and when when navigation, the rotational angle range of fin be-46 ° ~ 46 °, when charging, rotational angle range-75 of fin ° ~ 75 °.
Claims (3)
1. a flapping wing that utilizes wind energy or water flow energy charging continuation of the journey, comprise fin (1), wing bar (3), joint (4), forearm (5), little shoulder joint (6), large arm (7), , motor and driver train (8), battery and control chip (9), main shaft (10), it is characterized in that: described motor and driver train (8) are by main shaft (10) be in transmission connection large arm (7) and the little shoulder joint (6) of both sides, each large arm (7) is flexibly connected one by the joint (4) in fin (1) and wing bar (3) and can goes up, under the fin (1) of fluttering, each little shoulder joint (6) is flexibly connected the fin (1) that can rotate around main shaft (10) by forearm (5), motor and driver train (8) are connected with battery and control chip (9).
2. the flapping wing that utilizes wind energy or water flow energy charging continuation of the journey according to claim 1, is characterized in that: in described fin (1), be provided with the skeleton (2) for supporting.
3. the flapping wing that utilizes wind energy or water flow energy charging continuation of the journey according to claim 1, is characterized in that: during navigation, the rotational angle range of described fin (1) is-46 ° ~ 46 °; During charging, rotational angle range-75 of described fin (1) ° ~ 75 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410450498.1A CN104176252B (en) | 2014-09-05 | 2014-09-05 | Utilize wind energy or the flapping wing of water flow energy charging continuation of the journey |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410450498.1A CN104176252B (en) | 2014-09-05 | 2014-09-05 | Utilize wind energy or the flapping wing of water flow energy charging continuation of the journey |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104176252A true CN104176252A (en) | 2014-12-03 |
| CN104176252B CN104176252B (en) | 2016-06-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410450498.1A Expired - Fee Related CN104176252B (en) | 2014-09-05 | 2014-09-05 | Utilize wind energy or the flapping wing of water flow energy charging continuation of the journey |
Country Status (1)
| Country | Link |
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| CN (1) | CN104176252B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105000181A (en) * | 2015-08-10 | 2015-10-28 | 吴锜 | Wing device of flapping machine |
| CN107444634A (en) * | 2017-06-13 | 2017-12-08 | 大连理工大学 | Double freedom flapping wing mechanism |
| CN110304222A (en) * | 2019-06-26 | 2019-10-08 | 河海大学常州校区 | A kind of bionical devil ray of self generation type based on IPMC driving |
| CN111188738A (en) * | 2020-01-13 | 2020-05-22 | 武汉科技大学 | Pneumatic transmission flapping wing type power generation device |
| CN111268125A (en) * | 2020-01-22 | 2020-06-12 | 北京理工大学 | Multi-mode miniature aircraft |
| CN113060262A (en) * | 2021-04-25 | 2021-07-02 | 上海交通大学 | Flapping wing power generation and driving integrated marine robot and working method |
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| JP2008081094A (en) * | 2006-09-26 | 2008-04-10 | Bunri Gakuen | Ornithopter |
| CN201678041U (en) * | 2010-03-12 | 2010-12-22 | 章静 | Circulating flapping-wing flying vehicle |
| CN201825236U (en) * | 2010-10-18 | 2011-05-11 | 南京航空航天大学 | Driving mechanism for steel-wire hinged minisize flapping-wing aircraft |
| CN102287314A (en) * | 2011-05-27 | 2011-12-21 | 河海大学 | Seagull-imitated wave power generation driving method and device |
| CN102712365A (en) * | 2009-12-18 | 2012-10-03 | 迈普伯德有限公司 | Resonance engine |
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2014
- 2014-09-05 CN CN201410450498.1A patent/CN104176252B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008081094A (en) * | 2006-09-26 | 2008-04-10 | Bunri Gakuen | Ornithopter |
| CN102712365A (en) * | 2009-12-18 | 2012-10-03 | 迈普伯德有限公司 | Resonance engine |
| CN201678041U (en) * | 2010-03-12 | 2010-12-22 | 章静 | Circulating flapping-wing flying vehicle |
| CN201825236U (en) * | 2010-10-18 | 2011-05-11 | 南京航空航天大学 | Driving mechanism for steel-wire hinged minisize flapping-wing aircraft |
| CN102287314A (en) * | 2011-05-27 | 2011-12-21 | 河海大学 | Seagull-imitated wave power generation driving method and device |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105000181A (en) * | 2015-08-10 | 2015-10-28 | 吴锜 | Wing device of flapping machine |
| CN107444634A (en) * | 2017-06-13 | 2017-12-08 | 大连理工大学 | Double freedom flapping wing mechanism |
| CN107444634B (en) * | 2017-06-13 | 2019-11-26 | 大连理工大学 | Double freedom flapping wing mechanism |
| CN110304222A (en) * | 2019-06-26 | 2019-10-08 | 河海大学常州校区 | A kind of bionical devil ray of self generation type based on IPMC driving |
| CN111188738A (en) * | 2020-01-13 | 2020-05-22 | 武汉科技大学 | Pneumatic transmission flapping wing type power generation device |
| CN111268125A (en) * | 2020-01-22 | 2020-06-12 | 北京理工大学 | Multi-mode miniature aircraft |
| CN113060262A (en) * | 2021-04-25 | 2021-07-02 | 上海交通大学 | Flapping wing power generation and driving integrated marine robot and working method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104176252B (en) | 2016-06-08 |
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Granted publication date: 20160608 Termination date: 20190905 |