CN106809370A - Flight instruments - Google Patents
Flight instruments Download PDFInfo
- Publication number
- CN106809370A CN106809370A CN201510847762.XA CN201510847762A CN106809370A CN 106809370 A CN106809370 A CN 106809370A CN 201510847762 A CN201510847762 A CN 201510847762A CN 106809370 A CN106809370 A CN 106809370A
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- China
- Prior art keywords
- rotor assemblies
- spheroid
- flight instruments
- axle
- circuit controling
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Abstract
The present invention relates to a kind of flight instruments.The flight instruments includes suspensible spheroid, circuit controling assembly, wireless signal receiver and multiple rotor assemblies.Circuit controling assembly is regularly contained in spheroid；Wireless signal receiver is regularly contained in spheroid, and wireless signal receiver is electrically connected with circuit controling assembly, and wireless signal receiver can receive control signal, and the control signal of reception can be transferred into circuit controling assembly；Multiple rotor assemblies are dispersedly fixed on the outer surface of spheroid, and multiple rotor assemblies are electrically connected with circuit controling assembly；Wherein, circuit controling assembly can control the work of rotor assemblies according to control signal.Above-mentioned flight instruments can reducing energy consumption, and structure is relatively simple.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of flight instruments.
Background technology
Current flight instruments is all to control it to rise by rotor, and in flight course and resuspension procedure
Also all it is to be realized by the work of rotor, i.e., the whole work process of flight instruments all needs to be revolved by rotor
Change a job work, energy consumption is larger.
The content of the invention
Based on this, it is necessary to provide a kind of relatively low flight instruments that consumes energy.
A kind of flight instruments, including：
Suspensible spheroid；
Circuit controling assembly, is regularly contained in the spheroid；
Wireless signal receiver, is regularly contained in the spheroid, the wireless signal receiver with it is described
Circuit controling assembly is electrically connected, and the wireless signal receiver can receive control signal, and the institute that will can be received
State control signal and be transferred to the circuit controling assembly；And
Multiple rotor assemblies, are dispersedly fixed on the outer surface of the spheroid, and multiple rotor assemblies are equal
Electrically connected with the circuit controling assembly；Wherein, the circuit controling assembly can be according to the control signal control
Make the work of the rotor assemblies.
Wherein in one embodiment, each described rotor assemblies includes pedestal, rotor and motor, institute
State pedestal to be fixed on the spheroid, the rotor is rotatably mounted on the pedestal, it is described to drive electricity
Machine is contained in the pedestal, and is electrically connected with the circuit controling assembly, and the motor can drive institute
State rotor wing rotation.
Wherein in one embodiment, each described rotor assemblies also includes being fixedly installed in the pedestal
Speed regulator, the speed regulator electrically connects the circuit controling assembly and the motor, and the speed regulator can
By controlling the motor to adjust the rotary speed of the rotor.
Wherein in one embodiment, the rotor assemblies are six, and rotor assemblies position described in two of which
On by the first axle of the ball centre, wherein rotor assemblies described in another two are located across the spheroid
On second axle at center, remaining two rotor assemblies are located across on the 3rd axle of the ball centre,
And the first axle, second axle and the 3rd axle are vertical two-by-two.
Wherein in one embodiment, the rotor assemblies are four, and rotor assemblies position described in two of which
On by the first axle of the ball centre, wherein rotor assemblies described in another two are located across the spheroid
On second axle at center, and the first axle and second axle are vertical.
Wherein in one embodiment, the spheroid includes ball and lid, is opened in the ball
Inflation inlet is provided with, the cover cap is connected on the inflation inlet with the edge seal of the inflation inlet,
Wherein, multiple rotor assemblies are both secured in the ball.
Wherein in one embodiment, the battery case being fixedly connected with the lid is provided with the inside of the lid,
The circuit controling assembly is contained in the battery in the battery case.
Wherein in one embodiment, it is provided with the inside of the lid and is electrically connected with the circuit controling assembly
Color-changing lamp.
Wherein in one embodiment, the ball is the spherical body of polyvinyl chloride.
Wherein in one embodiment, the spheroid is helium balloon.
The main body of above-mentioned flight instruments is suspensible spheroid so that the spheroid of flight instruments can inherently hang
It is floating that spheroid can rise and suspend in the case of rotor assemblies are idle, reduce energy consumption in an atmosphere,
And multiple rotor assemblies are arranged on the outer surface of spheroid and are used to control the direction of motion of spheroid, to realize spheroid
Controllable and flight instruments the function in direction, meanwhile, the main body of above-mentioned flight instruments is only a suspensible ball
Body, simplifies the structure of flight instruments.
Brief description of the drawings
Fig. 1 be the spheroid of the flight instruments of an implementation method ball and lid separate after structural representation
Figure；
Fig. 2 is circuit, the signal annexation figure of the flight instruments shown in Fig. 1；
Fig. 3 is the structural representation of the lid, color-changing lamp and battery case of the flight instruments shown in Fig. 1.
Specific embodiment
For the ease of understanding the present invention, the present invention is described more fully below with reference to relevant drawings.
Preferred embodiment of the invention is given in accompanying drawing.But, the present invention can come in many different forms
Realize, however it is not limited to embodiment described herein.On the contrary, the purpose that these embodiments are provided be make it is right
The understanding of the disclosure is more thorough comprehensive.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly another
On individual element or can also there is element placed in the middle.When an element is considered as " connection " another yuan
Part, it can be directly to another element or may be simultaneously present centering elements.It is used herein
Term " vertical ", " level ", "left", "right" and similar statement simply to illustrate that mesh
's.
Unless otherwise defined, all of technologies and scientific terms used here by the article with belong to technology of the invention
The implication that the technical staff in field is generally understood that is identical.The art for being used in the description of the invention herein
Language is intended merely to describe the purpose of specific embodiment, it is not intended that in the limitation present invention.
As shown in Figures 1 and 2, the flight instruments 100 of an implementation method can be controlled wirelessly device 200 and send
Control signal control.Wherein, wireless controller 200 is operated for operator, and operator can be by control
The flying speed of the control flight instruments 100 of wireless controller 200 and direction etc..Wherein, the flight instruments
100 include spheroid 110, circuit controling assembly 120, wireless signal receiver 130 and rotor assemblies 140.
Spheroid 110 can suspend.In the present embodiment, spheroid 110 is helium balloon.In other embodiments,
Spheroid 110 can also be the spheroid that hydrogen balloon etc. can suspend in an atmosphere.
Specifically in the illustrated embodiment, spheroid 110 includes ball 112 and lid 114.
Inflation inlet 112a is offered in ball 112.Ball 112 can be one a diameter of 2 meters
Spheroid 110.Wherein, ball 112 is the spherical body of polyvinyl chloride.
Lid 114 is covered on inflation inlet 112a, and is connected with the edge seal of inflation inlet 112a.
Circuit controling assembly 120 is regularly contained in spheroid 110.Specifically, circuit controling assembly 120
Regularly it is contained in ball 112.Circuit controling assembly 120 is used to control the electrical equipment on spheroid 110
The work of part and the treatment of signal etc..
Wireless signal receiver 130 is regularly contained in spheroid 110, wireless signal receiver 130 with electricity
Road control assembly 120 is electrically connected, and wireless signal receiver 130 can receive what wireless controller 200 sent
Control signal, and control signal can be transferred to circuit controling assembly 120.Specifically, wireless signal receiver
130 are contained in ball 112.
Rotor assemblies 140 are multiple, and multiple rotor assemblies 140 are dispersedly fixed on the outer surface of spheroid 110
On, multiple rotor assemblies 140 are electrically connected with circuit controling assembly 120.Specifically, multiple rotor assemblies
140 are fixed in ball 112.Wherein, circuit controling assembly 120 can control rotor according to control signal
The work of component 140.For example, multiple rotor assemblies 140 can be controlled not work, or control is wherein
One rotor assemblies 140 works, or control several rotor assemblies 140 to work together etc..
Further, rotor assemblies 140 are six, and two of which rotor assemblies 140 are located across spheroid
In the first axle at 110 centers, wherein another two rotor assemblies 140 are located across second axle at the center of spheroid 110
On, remaining two rotor assemblies 140 are located across on the 3rd axle at the center of spheroid 110, and first axle, the
Two axles and the 3rd axle are vertical two-by-two.
It is appreciated that the quantity of rotor assemblies 140 can not also be six, for example, in other embodiments,
Rotor assemblies 140 are four, and two of which rotor assemblies 140 are located across the first axle at the center of spheroid 110
On, wherein another two rotor assemblies 140 are located across on second axle at the center of spheroid 110, and first axle and
Second axle is vertical；Or, rotor assemblies 140 can be for eight or more.
Specifically, each described rotor assemblies 140 includes pedestal 142, rotor 144 and motor 146.
Pedestal 142 is fixed on spheroid 110.Specifically, pedestal 142 is fixed in ball 112.
Rotor 144 is rotatably mounted on pedestal 142.
Motor 146 is contained in pedestal 142, and is electrically connected with circuit controling assembly 120, drives electricity
Machine 146 can drive rotor 144 to rotate.
Further, each rotor assemblies 140 also includes the speed regulator 148 being fixedly installed in pedestal 142,
The electrical connection circuit control assembly 120 of speed regulator 148 and motor 146, speed regulator 148 can be by controlling to drive
Motor 146 is moved to adjust the rotary speed of rotor 144.Rotor 144 can be controlled by setting speed regulator 148
Rotary speed, to adjust the flying speed of flight instruments 100.Wherein, speed regulator 148 is electronic speed regulation
Device.
Also referring to Fig. 3, further, the inner side of lid 114 is provided with the electricity being fixedly connected with lid 114
Pond box 150, circuit controling assembly 120 includes the battery (not shown) being contained in battery case 150.Specifically
, battery case 150 is cuboid-type.
Further, the inner side of lid 114 is provided with the color-changing lamp 160 electrically connected with circuit controling assembly 120,
Wherein, circuit controling assembly 120 can control color-changing lamp according to the control signal of the transmitting of wireless controller 200
160 opening and closing.Setting color-changing lamp 160 can make flight instruments 100 in night flying.Specifically in figure
In the embodiment shown, color-changing lamp 150 is installed on battery case 160.
Further, color-changing lamp 160 is color laser lamp.Color laser lamp 160 can make spheroid 110 with
The change of the color of the light that color-changing lamp 160 sends and change.
Above-mentioned flight instruments 100 at least has the advantage that：
The main body of above-mentioned flight instruments 100 is suspensible spheroid 110 so that the spheroid of flight instruments 100
110 can inherently suspend in an atmosphere, spheroid 110 can be in the case of rotor assemblies 140 be idle on
Rise and suspend, reduce energy consumption, and multiple rotor assemblies 140 are arranged on the outer surface of spheroid 110 for controlling
The direction of motion of spheroid processed 110, wireless receiver 130 upon the reception of control signals, control signal is passed
Circuit controling assembly 120 is defeated by, circuit controling assembly 120 controls rotor assemblies 140 to work according to control signal,
The function of and flight instruments 100 controllable with the direction for realizing spheroid 110, meanwhile, above-mentioned flight instruments 100
Main body be only a suspensible spheroid 110, simplify the structure of flight instruments 100.
Each technical characteristic of embodiment described above can be combined arbitrarily, not right to make description succinct
The all possible combination of each technical characteristic in above-described embodiment is all described, as long as however, these skills
The combination of art feature does not exist contradiction, is all considered to be the scope of this specification record.
Embodiment described above only expresses several embodiments of the invention, and its description is more specific and detailed,
But can not therefore be construed as limiting the scope of the patent.It should be pointed out that for this area
For those of ordinary skill, without departing from the inventive concept of the premise, some deformations can also be made and changed
Enter, these belong to protection scope of the present invention.Therefore, the protection domain of patent of the present invention should be with appended power
Profit requires to be defined.
Claims (10)
1. a kind of flight instruments, it is characterised in that including：
Suspensible spheroid；
Circuit controling assembly, is regularly contained in the spheroid；
Wireless signal receiver, is regularly contained in the spheroid, the wireless signal receiver with it is described
Circuit controling assembly is electrically connected, and the wireless signal receiver can receive control signal, and can be by reception
The control signal is transferred to the circuit controling assembly；And
Multiple rotor assemblies, are dispersedly fixed on the outer surface of the spheroid, and multiple rotor assemblies are equal
Electrically connected with the circuit controling assembly；Wherein, the circuit controling assembly can be according to the control signal control
Make the work of the rotor assemblies.
2. flight instruments according to claim 1, it is characterised in that each described rotor assemblies includes
Pedestal, rotor and motor, the pedestal are fixed on the spheroid, and the rotor is rotatably mounted
In on the pedestal, the motor is contained in the pedestal, and is electrically connected with the circuit controling assembly
Connect, the motor can drive the rotor wing rotation.
3. flight instruments according to claim 2, it is characterised in that each described rotor assemblies is also wrapped
The speed regulator being fixedly installed in the pedestal is included, the speed regulator electrically connects the circuit controling assembly and institute
Motor is stated, the speed regulator can be by controlling the motor to adjust the rotary speed of the rotor.
4. flight instruments according to claim 1, it is characterised in that the rotor assemblies are six,
And rotor assemblies described in two of which are located across in the first axle of the ball centre, wherein described in another two
Rotor assemblies are located across on the second axle of the ball centre, and remaining two rotor assemblies are located across
On 3rd axle of the ball centre, and the first axle, second axle and the 3rd axle are vertical two-by-two.
5. flight instruments according to claim 1, it is characterised in that the rotor assemblies are four,
And rotor assemblies described in two of which are located across in the first axle of the ball centre, wherein described in another two
Rotor assemblies are located across on the second axle of the ball centre, and the first axle and second axle are vertical.
6. flight instruments according to claim 1, it is characterised in that the spheroid includes ball
And lid, inflation inlet is offered in the ball, the cover cap is located on the inflation inlet, and with
The edge seal connection of the inflation inlet, wherein, multiple rotor assemblies are both secured to the ball
On.
7. flight instruments according to claim 6, it is characterised in that be provided with the inside of the lid with
The battery case that the lid is fixedly connected, the circuit controling assembly includes the electricity being contained in the battery case
Pond.
8. flight instruments according to claim 6, it is characterised in that be provided with the inside of the lid
The color-changing lamp electrically connected with the circuit controling assembly.
9. flight instruments according to claim 6, it is characterised in that the ball is polychlorostyrene second
Alkene orbicule.
10. flight instruments according to claim 1, it is characterised in that the spheroid is helium balloon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510847762.XA CN106809370A (en) | 2015-11-27 | 2015-11-27 | Flight instruments |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510847762.XA CN106809370A (en) | 2015-11-27 | 2015-11-27 | Flight instruments |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106809370A true CN106809370A (en) | 2017-06-09 |
Family
ID=59102937
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510847762.XA Pending CN106809370A (en) | 2015-11-27 | 2015-11-27 | Flight instruments |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106809370A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019034713A (en) * | 2017-08-16 | 2019-03-07 | 国立大学法人高知大学 | Unmanned aircraft, method for using the same, system for supporting study lesson review and method for supporting study lesson review |
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| CN102424104A (en) * | 2011-12-31 | 2012-04-25 | 沈阳航空航天大学 | Four-rotor-wing indoor airship |
| CN102717887A (en) * | 2012-05-23 | 2012-10-10 | 北京航空航天大学 | Near space airship using inflatable wings and tiltable propellers |
| RU2546741C1 (en) * | 2014-03-12 | 2015-04-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Уфимский государственный авиационный технический университет" | Power propulsion system for airship |
| CN104590533A (en) * | 2014-12-24 | 2015-05-06 | 中国特种飞行器研究所 | Novel deformable airship |
| CN105083521A (en) * | 2015-09-18 | 2015-11-25 | 深圳市惠通环宇科技有限公司 | Airship |
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Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101316639A (en) * | 2005-09-29 | 2008-12-03 | 新创有限公司 | Method and device for free-standing support of objects in space |
| CN102424104A (en) * | 2011-12-31 | 2012-04-25 | 沈阳航空航天大学 | Four-rotor-wing indoor airship |
| CN102717887A (en) * | 2012-05-23 | 2012-10-10 | 北京航空航天大学 | Near space airship using inflatable wings and tiltable propellers |
| RU2546741C1 (en) * | 2014-03-12 | 2015-04-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Уфимский государственный авиационный технический университет" | Power propulsion system for airship |
| CN104590533A (en) * | 2014-12-24 | 2015-05-06 | 中国特种飞行器研究所 | Novel deformable airship |
| CN105083521A (en) * | 2015-09-18 | 2015-11-25 | 深圳市惠通环宇科技有限公司 | Airship |
| CN205256647U (en) * | 2015-11-27 | 2016-05-25 | 深圳市鼎创旭飞科技有限公司 | Aviation device |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019034713A (en) * | 2017-08-16 | 2019-03-07 | 国立大学法人高知大学 | Unmanned aircraft, method for using the same, system for supporting study lesson review and method for supporting study lesson review |
| JP7171015B2 (en) | 2017-08-16 | 2022-11-15 | 国立大学法人高知大学 | Unmanned aerial vehicle, usage thereof, study lesson review support system and study lesson review support method |
| JP2022173447A (en) * | 2017-08-16 | 2022-11-18 | 国立大学法人高知大学 | Method for using unmanned aircraft |
| JP7412030B2 (en) | 2017-08-16 | 2024-01-12 | 国立大学法人高知大学 | How to use unmanned aircraft |
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