CN107792337A - A kind of flapping flight balloon - Google Patents
A kind of flapping flight balloon Download PDFInfo
- Publication number
- CN107792337A CN107792337A CN201710760714.6A CN201710760714A CN107792337A CN 107792337 A CN107792337 A CN 107792337A CN 201710760714 A CN201710760714 A CN 201710760714A CN 107792337 A CN107792337 A CN 107792337A
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- CN
- China
- Prior art keywords
- flapping
- balloon
- wing
- controller
- flight
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/44—Balloons adapted to maintain predetermined altitude
-
- 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)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention provides a kind of flapping flight balloon, including balloon, flapping wing aerofoil, drive mechanism, controller, battery, wherein the flapping wing aerofoil is one or more, each flapping wing aerofoil is provided with independent drive mechanism, can moved alone under control of the controller.
Description
Technical field
The present invention relates to a kind of flapping flight unmanned plane, belong to low flyer field, more specifically it is related to one kind and flutterred
Wing flying balloon.
Background technology
Unmanned plane is applied to military field earliest, and during Vietnam War, U.S. army sets out 3425 frame scounting aeroplanes, and successfully
2873 framves are returned, investigate significant effect, afterwards, because unmanned plane is compact and flexible, cost is cheap, is easy to " stealth ", without personnel's wound
The advantages of dying, extensive use is obtained in military field, occurs unmanned bomber, unmanned target drone, UAV for electronic countermeasure etc. successively.
In the last few years, technical grade unmanned plane is engendered, is such as applied to agriculture (plant protection, crops data monitoring), (forest prevents for forestry
Fire, the conservation of wildlife), meteorological (air sampling, rain making), exploration resource, marine protection monitoring, petroleum conduit patrolling,
Express delivery speed fortune, power-line patrolling, inspection calamity, the disaster relief, the field such as mapping for unmanned plane, consumer level unmanned plane, as applied to take photo by plane, business
The scenes such as industry publicity, toy, game.
The unmanned plane of main flow has fixed-wing and the class of screw wing two at present, and military field is more to use fixed-wing, but fixed-wing
Unmanned plane is unable to VTOL, it is impossible to hovering, it is more difficult to applied to limited application scenarios, therefore in industry and consumer field
Mostly screw wing unmanned plane, screw wing unmanned plane has the characteristics of being vertically moved up or down, hovering, but but screw wing is adopted more at present
With pure electric-powered, in cruising time short (20-40min), fly control and require high, when in applied to the scene interacted with people compared with endanger
Danger, the mankind are easily hurt or hit by whole unmanned plane by screw wings.Therefore, whether fixed-wing or screw wing nobody
Machine, the problem of all existing be from great continuation of the journey it is short, fly control require it is high, with the interactive dangerous problem of people.
Flapping-wing aircraft is the aircraft of imitative Bird Flight, and having to carry people to fly also has unmanned flight, and it is fluttered up and down using flapping wing
Lift is produced to fly with thrust.Notification number is CN103818553A Chinese utility model patent, discloses a kind of " rotary side time
Its caused lift of being fluttered up and down by flapping wing completely of the flapping-wing aircraft of this mode of wing flapping wing mode and application " is realized with thrust to be carried
People flies, but produces flying power existing defects, due to the limitation of manufacturing technology, power liter caused by flapping wing by flapping wing completely
Power is extremely difficult to ideal effect with thrust so that flapping-wing aircraft can not be detained for a long time in the air, can not also hover, and flapping wing is flutterred up and down
It is dynamic, flapping wing fracture can also occur, potential safety hazard be present.Disclosed in Publication No. CN106945813A Chinese patent using empty
The manned method that the balloon of lift of gas is combined with flapping-wing aircraft, solves that flapping-wing aircraft can not hover and the aerial holdup time is short
The problem of, but its flapping wing area is big, and flight flexibility is not good enough.
Therefore, it is necessary to it is a kind of it is safe/can meet well interactive with people, can hover in the air, while and can long-time
The aircraft of flight.Disclose a kind of flapping wings type bionic intelligence balloon in Chinese patent CN106005351A, including balloon body,
Flapping wing dynamic structure, microcontroller and camera, have it is light, can hovering flight stability the characteristics of, can be achieved stable
Aerial photographing.But the motion details wherein not to microprocessor control air foil is illustrated, refer only to that flapping wing can be controlled
The movement velocity of aerofoil, do not refer to yet two flapping wing aerofoils whether can independent control details, and technical scheme mainly solves
Problem is balloon flight stability problem in flight shooting.
The content of the invention
In order to overcome in the prior art flapping flight unmanned plane with people's interactive scene lack security, can not be in the air
Hovering, the problem of flight time is short, flapping wing flexibility is not good enough, the invention provides a kind of flapping flight balloon, it include balloon,
Flapping wing aerofoil, drive mechanism, controller and battery.By setting drive mechanism respectively for each flapping wing aerofoil, it is set independently to transport
It is dynamic, and by increasing steering wheel quantity in drive mechanism flapping wing aerofoil can be made to realize that multiple degrees of freedom is fluttered, so as to improve balloon flight
Flexibility, by battery power, prolonged flight can be achieved.
Specifically, the invention provides a kind of flapping flight balloon, including balloon, flapping wing aerofoil, drive mechanism, control
Device, battery, it is characterised in that：The flapping wing aerofoil is one or more, and each flapping wing aerofoil is provided with independent drive mechanism,
It can be moved alone under controller control.
Preferably, the balloon is spheroid.
In the preferred embodiment of the invention, drive mechanism, controller, battery are placed in balloon interior.
Preferably, magnet is set on the controller, while set on the hinge connector of the flapping wing aerofoil tail end
Magnet is put, is interacted by magnet, controls the motion of flapping wing aerofoil.
Preferably, the controller is flexible structure.
Preferably, the flapping wing aerofoil can carry out multiple degrees of freedom and flutter.
In technical scheme of the present invention, controller can be according to plug-in or external command control balloon motion.
The method have the benefit that there is tight security in the scene interactive with people, will not cause to hurt or
Person's impact damage, flight flexibility is high, can hover in the air, and can realize flying for long time.
Brief description of the drawings
Fig. 1 is the structural representation of flapping flight balloon bird formula flying method of the present invention.
Fig. 2 is the structural representation that flapping flight balloon fish formula of the present invention swings flying method.
Description of reference numerals
1st, balloon；2nd, wing steering wheel is incited；2 ', wing steering wheel is incited；3rd, tuning steering wheel；3 ', tuning steering wheel；4th, wing；4 ', wing；
5th, controller；6th, wire
Embodiment
To enable above and other objects, features and advantages of the invention to become apparent, below in conjunction with accompanying drawing and preferably
Embodiment the structure and application method of the present invention are described further, but embodiment is not intended as to protection scope of the present invention
Restriction.
Embodiment 1
Incite and be connected between wing steering wheel 2 and 2 ', tuning steering wheel 3 and 3 ', controller 5 by wire 6, positioned at the outside of balloon 1,
The tail end of wing 4, which is provided with, incites wing steering wheel 2 and tuning steering wheel 3, and the afterbody of wing 4 ', which is provided with, incites wing steering wheel 2 ' and tuning steering wheel
3 ', in operation, two kinds of flying methods can be used：
1) flapping wing mode is flown：Start tuning steering wheel 3 and 3 ', wing is agitated up and down, there is provided downward wind-force, regulation are left
Starboard wing instigates frequency, instigates frequency to adjust the direction in aircraft occurred level direction by left and right difference；The wing is incited in startup
Steering wheel 2 and 2 ', its independent control are instigated, and swing up and down wing, reach the function of aircraft raising and lowering.
2) wing swings flight：Start tuning steering wheel 3 and 3 ', swung by wing, air is extruded backward, realize
Propulsive force；Wing steering wheel 2 and 2 ' is incited in startup, and its independent control is instigated, and swings up and down wing, reaches aircraft raising and lowering
Function.
Embodiment 2
Compared with Example 1 compared with, in addition to inciting wing steering wheel 2 and being connected with 2 ', tuning steering wheel 3 with 3 ' by flexible PCB, its
Remaining structure and mode of operation are as described in Example 1.
Embodiment 3
Compared with embodiment 1 or 2, it is connected except wing steering wheel 2 is incited with 2 ', tuning steering wheel 3 with 3 ' and controller 5 by wire
Positioned at balloon interior, or incite wing steering wheel 2 and be connected with 2 ', tuning steering wheel 3 with 3 ' by flexible PCB outside balloon interior, its
Remaining structure and mode of operation are as described in Example 1.
Embodiment 4
Compared with Example 3 compared with, positioned at inciting for balloon interior, magnet is being set respectively on wing steering wheel and tuning steering wheel, and
Magnet is arranged in correspondence with the connector of the afterbody of wing 4 and 4 ' outside balloon, it is mutual to adjust magnetic field by controller
Effect, drive wing motion.
Embodiment 5
In the technical scheme described in embodiment 1-4, loading position sensor, aircraft pass through sensor on the controller
After knowing positional information, instruction, the motion of adjust automatically aircraft are sent by the controller communicated.
These are only presently preferred embodiments of the present invention, it is impossible to protection scope of the present invention is limited with this, i.e., generally according to
The simple equivalence changes that claims of the present invention and the content of the invention are made and modification, all still fall within present patent application
Protection domain.
Claims (7)
1. a kind of flapping flight balloon, including balloon, flapping wing aerofoil, drive mechanism, controller, battery, it is characterised in that：It is described
Flapping wing aerofoil is one or more, and each flapping wing aerofoil is provided with independent drive mechanism, can moved alone under control of the controller.
2. flapping flight balloon as claimed in claim 1, it is characterised in that：The balloon is spheroid.
3. the flapping flight balloon as any one of claim 1-2, it is characterised in that：The drive mechanism, control
Device processed, battery are located at balloon interior.
4. flapping flight balloon as claimed in claim 3, it is characterised in that：Magnet is set on the controller, while
The flapping wing aerofoil tail end sets magnet, is interacted by magnet, controls the motion of flapping wing aerofoil.
5. the flapping flight balloon as any one of claim 1-4, it is characterised in that：The controller is tied to be flexible
Structure.
6. flapping flight balloon as claimed in claim 1, it is characterised in that：The flapping wing aerofoil can carry out multiple degrees of freedom and flutter
It is dynamic.
7. flapping flight balloon as claimed in claim 1, it is characterised in that：The controller can be according to plug-in or outer
Portion's instruction control balloon motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710760714.6A CN107792337A (en) | 2017-08-30 | 2017-08-30 | A kind of flapping flight balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710760714.6A CN107792337A (en) | 2017-08-30 | 2017-08-30 | A kind of flapping flight balloon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107792337A true CN107792337A (en) | 2018-03-13 |
Family
ID=61532195
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710760714.6A Pending CN107792337A (en) | 2017-08-30 | 2017-08-30 | A kind of flapping flight balloon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107792337A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019042238A1 (en) * | 2017-08-30 | 2019-03-07 | 上海未玩电子科技有限公司 | Flapping-wing flying blimp |
| US11465728B2 (en) * | 2019-05-30 | 2022-10-11 | Pliant Energy System LLC | Aerial swimmer apparatuses, methods and systems |
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| CN1453185A (en) * | 2003-03-10 | 2003-11-05 | 东南大学 | Bionic electromagnetically driven flapping wing unit for mini aircraft |
| CN201062579Y (en) * | 2007-03-27 | 2008-05-21 | 崔炳如 | Rolling rotor type refrigeration compressor |
| CN101743399A (en) * | 2006-01-26 | 2010-06-16 | 彼得·罗伯特·古道 | A flying wind energy conversion apparatus |
| CN102574391A (en) * | 2009-10-22 | 2012-07-11 | 柯尼格及包尔公开股份有限公司 | Devices in a printing couple of a printing machine |
| WO2012112939A1 (en) * | 2011-02-17 | 2012-08-23 | Georgia Tech Research Corporation | Hovering and gliding multi-wing flapping micro aerial vehicle |
| US20140345957A1 (en) * | 2011-01-05 | 2014-11-27 | Orbotix, Inc. | Magnetically coupled accessory for a self-propelled device |
| KR20150010924A (en) * | 2013-07-19 | 2015-01-29 | 이정용 | A ridable robotic bird |
| CN104443381A (en) * | 2014-12-15 | 2015-03-25 | 佛山市神风航空科技有限公司 | Small air vehicle with four oscillation wings |
| CN105586645A (en) * | 2016-03-16 | 2016-05-18 | 北京化工大学 | Multifunctional vacuum spinning device |
| CN205342705U (en) * | 2015-12-31 | 2016-06-29 | 重庆房地产职业学院 | Noiselessness dustproof wall face polisher |
| CN105797387A (en) * | 2016-04-11 | 2016-07-27 | 曹晓旭 | Shooting balloon |
| CN205524980U (en) * | 2016-03-29 | 2016-08-31 | 秦民川 | Bionical dragonfly flapping wing machine people |
| CN106828922A (en) * | 2017-02-27 | 2017-06-13 | 北京航空航天大学 | The position control mechanism that a kind of imitative insect wing is flapped |
-
2017
- 2017-08-30 CN CN201710760714.6A patent/CN107792337A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1453185A (en) * | 2003-03-10 | 2003-11-05 | 东南大学 | Bionic electromagnetically driven flapping wing unit for mini aircraft |
| CN101743399A (en) * | 2006-01-26 | 2010-06-16 | 彼得·罗伯特·古道 | A flying wind energy conversion apparatus |
| CN201062579Y (en) * | 2007-03-27 | 2008-05-21 | 崔炳如 | Rolling rotor type refrigeration compressor |
| CN102574391A (en) * | 2009-10-22 | 2012-07-11 | 柯尼格及包尔公开股份有限公司 | Devices in a printing couple of a printing machine |
| US20140345957A1 (en) * | 2011-01-05 | 2014-11-27 | Orbotix, Inc. | Magnetically coupled accessory for a self-propelled device |
| WO2012112939A1 (en) * | 2011-02-17 | 2012-08-23 | Georgia Tech Research Corporation | Hovering and gliding multi-wing flapping micro aerial vehicle |
| KR20150010924A (en) * | 2013-07-19 | 2015-01-29 | 이정용 | A ridable robotic bird |
| CN104443381A (en) * | 2014-12-15 | 2015-03-25 | 佛山市神风航空科技有限公司 | Small air vehicle with four oscillation wings |
| CN205342705U (en) * | 2015-12-31 | 2016-06-29 | 重庆房地产职业学院 | Noiselessness dustproof wall face polisher |
| CN105586645A (en) * | 2016-03-16 | 2016-05-18 | 北京化工大学 | Multifunctional vacuum spinning device |
| CN205524980U (en) * | 2016-03-29 | 2016-08-31 | 秦民川 | Bionical dragonfly flapping wing machine people |
| CN105797387A (en) * | 2016-04-11 | 2016-07-27 | 曹晓旭 | Shooting balloon |
| CN106828922A (en) * | 2017-02-27 | 2017-06-13 | 北京航空航天大学 | The position control mechanism that a kind of imitative insect wing is flapped |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019042238A1 (en) * | 2017-08-30 | 2019-03-07 | 上海未玩电子科技有限公司 | Flapping-wing flying blimp |
| US11465728B2 (en) * | 2019-05-30 | 2022-10-11 | Pliant Energy System LLC | Aerial swimmer apparatuses, methods and systems |
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Legal Events
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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 | ||
| CB02 | Change of applicant information |
Address after: 201615 Shanghai Songjiang District Jiuting town nine new highway 1005 1005 3 block 102 Applicant after: Shanghai power Fang Electronic Technology Co., Ltd. Address before: 201615 room 1006, 33 building, 518 Xinzhu Road, Songjiang District, Shanghai. Applicant before: Shanghai power Fang Electronic Technology Co., Ltd. |
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| CB02 | Change of applicant information | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180313 |
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| RJ01 | Rejection of invention patent application after publication |