CN107323664A - A kind of aircraft for being stuck in the water surface - Google Patents
A kind of aircraft for being stuck in the water surface Download PDFInfo
- Publication number
- CN107323664A CN107323664A CN201710360129.7A CN201710360129A CN107323664A CN 107323664 A CN107323664 A CN 107323664A CN 201710360129 A CN201710360129 A CN 201710360129A CN 107323664 A CN107323664 A CN 107323664A
- Authority
- CN
- China
- Prior art keywords
- air pocket
- pocket rings
- mounting rod
- rings
- aircraft
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of aircraft for being stuck in the water surface, including the first air pocket rings, the second air pocket rings, the 3rd air pocket rings, controlling organization, the first mounting rod, the second mounting rod, propeller；The aircraft is provided with to be mutually permanently connected and the first vertical air pocket rings, the second air pocket rings, the 3rd air pocket rings two-by-two, and controlling organization and propeller are wrapped in the ring of air pocket rings, prevent from dropping when aircraft landing or propeller hurts human body by the setting.Aircraft provided by the present invention have the advantages that to be stuck in the water surface, anticollision, balance quality it is good.
Description
Technical field
The present invention relates to aircraft field；Specifically related to a kind of aircraft for being stuck in the water surface.
Background technology
Unmanned vehicle is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.From
Technical standpoint definition can be divided into：Unmanned fixed-wing aircraft, unmanned VTOL machine, unmanned airship, depopulated helicopter, rotation more than nobody
Rotor aircraft, unmanned parasol etc..In terms of civilian unmanned plane, unmanned plane+sector application is that unmanned plane has really just been needed；Mesh
It is preceding taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
The application in road, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane in itself
On the way, developed country is also in actively extension sector application and development unmanned air vehicle technique.But now unmanned plane be generally rotary wings nobody
Easily broken when machine, typically no protective gear, landing or failure, or even hurt human body.And existing flight
In device, aerial photographing is typically only used for, can not typically rest on the water surface and be shot.Therefore for needing to shoot lake surface
Many limitations are suffered from during scene, or even directly result in aircraft water inlet and cause short circuit.
The content of the invention
In order to overcome the deficiencies in the prior art, the invention aims to provide a kind of flight for being stuck in the water surface
Device, the aircraft is provided with the first air pocket rings being mutually permanently connected, the second air pocket rings, the 3rd air pocket rings, there is provided control machine
Structure is arranged on the point of intersection of the lower end of the first air pocket rings and the 3rd air pocket rings, coordinates the setting of air pocket rings, aircraft is arranged
Stop falling on the water surface when shooting lake surface scene, and taken off again from the water surface.
The purpose of the present invention is realized using following technical scheme：
A kind of aircraft for being stuck in the water surface, including the first air pocket rings, the second air pocket rings, the 3rd air pocket rings, controlling organization,
One mounting rod, the second mounting rod, propeller, camera device；First air pocket rings, the second air pocket rings, the 3rd air pocket rings are
Toroidal；The two ends of first mounting rod are fixedly connected with the second air pocket rings；The two ends and second of second mounting rod
Air pocket rings are fixedly connected；First mounting rod and the second mounting rod intersect to form X-shape；First mounting rod, the second peace
The propeller for being connected with motor is installed on dress bar；Plane, the 3rd air bag where plane, the second air pocket rings where first air pocket rings
Any two plane is mutually perpendicular in the planes for ring institute；Any two in first air pocket rings, the second air pocket rings, the 3rd air pocket rings
Air pocket rings are fixedly connected；The center of circle of first air pocket rings, the center of circle of the second air pocket rings, the center of circle of the 3rd air pocket rings are overlapped in a bit；
The controlling organization includes shell, controller and battery, and the controller and battery are located at the closed appearance of shell formation
Receive intracavitary；The controller is used to control propeller and camera device；The controlling organization respectively with camera device and propeller
Motor electrical connection；The controlling organization is arranged on the point of intersection of the lower end of the first air pocket rings and the 3rd air pocket rings；Camera device
Point of intersection installed in the first air pocket rings and the upper end of the 3rd air pocket rings.
Preferably, the upper end of the controlling organization is removably connected with balancing weight.
Preferably, the crosspoint of first mounting rod and the second mounting rod is on the center of circle where the second air pocket rings, and
One mounting rod is perpendicular to the second mounting rod；The angle of plane is 45 ° where straight line where first mounting rod and the first air pocket rings.
Compared with prior art, the beneficial effects of the present invention are：
1st, the present invention provides a kind of aircraft for being stuck in the water surface, and the aircraft is provided with the first air bag being mutually permanently connected
Ring, the second air pocket rings, the 3rd air pocket rings, there is provided controlling organization is arranged on the friendship of the lower end of the first air pocket rings and the 3rd air pocket rings
At point, coordinate the setting of air pocket rings, enable aircraft to stop falling on the water surface when arranging shooting lake surface scene, and from the water surface again
Take off.
2nd, the present invention be also provided with orthogonal first mounting rod, the second mounting rod and be provided with the first mounting rod with
The angle of plane is 45 ° where first air pocket rings, and the setting can reduce the windage produced when air pocket rings rotate to propeller, and
And the setting can accommodate longer propeller.
Brief description of the drawings
Fig. 1 is the structural representation of the aircraft of the embodiment of the present invention.
Wherein, the 1, first air pocket rings；2nd, the second air pocket rings；3rd, the 3rd air pocket rings；4th, the first mounting rod；5th, second install
Bar；6th, controlling organization；7th, propeller；8th, camera device；9th, balancing weight.
Embodiment
Below, with reference to accompanying drawing and embodiment, the present invention is described further：
As shown in figure 1, a kind of aircraft for being stuck in the water surface, including the first air pocket rings 1, the second air pocket rings 2, the 3rd air pocket rings
3rd, controlling organization 6, the first mounting rod 4, the second mounting rod 5, propeller 7, camera device 8；First air pocket rings 1, the second gas
Capsule ring 2, the 3rd air pocket rings 3 are toroidal；The two ends of first mounting rod 4 are fixedly connected with the second air pocket rings 2；It is described
The two ends of second mounting rod 5 are fixedly connected with the second air pocket rings 2；The mounting rod 5 of first mounting rod 4 and second intersects to form X
Shape；The propeller 7 for being connected with motor is installed on first mounting rod 4, the second mounting rod 5；It is flat where first air pocket rings 1
Any two plane is mutually perpendicular in the planes for face, the place plane of the second air pocket rings 2, the institute of the 3rd air pocket rings 3；First air pocket rings 1,
Any two air pocket rings in second air pocket rings 2, the 3rd air pocket rings 3 are fixedly connected；The center of circle of first air pocket rings 1, the second air bag
The center of circle of ring 2, the center of circle of the 3rd air pocket rings 3 are overlapped in a bit；The controlling organization 6 includes shell, controller and battery, institute
State controller and battery is located in the closed accommodating chamber of shell formation；The controller is used to control propeller 7 and shooting
Device 8；Motor of the controlling organization 6 respectively with camera device 8 and propeller 7 is electrically connected；The controlling organization 6 is arranged on the
The point of intersection of the lower end of one air pocket rings 1 and the 3rd air pocket rings 3；Camera device 8 is arranged on the first air pocket rings 1 and the 3rd air pocket rings 3
Upper end point of intersection.The upper end of the controlling organization 6 is removably connected with balancing weight 9.First mounting rod 4 and second is pacified
The crosspoint of bar 5 is filled on the center of circle where the second air pocket rings 2, the first mounting rod 4 is perpendicular to the second mounting rod 5；First installs
The place straight line of bar 4 and the angle of the place plane of the first air pocket rings 1 are 45 °.
In use, starting aircraft, allow above aircraft flight to the water surface, the water surface is slowly dropped to, due to being provided with gas
Capsule ring and the big controlling organization 6 of weight lower end is arranged on, the submerged of controlling organization 6, air pocket rings then provide buoyancy, make spiral shell
Rotation oar 7 and camera device 8 are exposed independent from the water surface, are shot.There is provided orthogonal first mounting rod 4, the and of the second mounting rod 5
There is provided the first mounting rod 4 and the angle of the place plane of the first air pocket rings 1 are 45 °；Due to needing to provide enough buoyancy, air bag
The ring body radius of ring is larger, if the first mounting rod 4 or the second mounting rod 5 are overlapping with the first air pocket rings 1 and the 3rd air pocket rings 3,
It is easily caused windage excessive, is unfavorable for taking off and load-carrying；The setting can reduce the wind produced when air pocket rings revolve 7 turns to propeller
Hinder, and the setting can accommodate longer propeller 7 and be more favorable to the balance of aircraft, so as to be conducive to aircraft flight
When imaged；Balancing weight 9 is also provided with, is beneficial to the stabilization and the overweight camera device 8 of balance of stabilizer surface stop, prevents
Only aircraft is overturn in the water surface.
It will be apparent to those skilled in the art that technical scheme that can be as described above and design, make other various
It is corresponding to change and deformation, and all these change and deformation should all belong to the protection domain of the claims in the present invention
Within.
Claims (3)
1. a kind of aircraft for being stuck in the water surface, it is characterised in that including the first air pocket rings, the second air pocket rings, the 3rd air bag
Ring, controlling organization, the first mounting rod, the second mounting rod, propeller, camera device；First air pocket rings, the second air pocket rings,
3rd air pocket rings are toroidal；The two ends of first mounting rod are fixedly connected with the second air pocket rings；Described second installs
The two ends of bar are fixedly connected with the second air pocket rings；First mounting rod and the second mounting rod intersect to form X-shape；Described first
The propeller for being connected with motor is installed on mounting rod, the second mounting rod；Where plane, the second air pocket rings where first air pocket rings
Any two plane is mutually perpendicular in the planes for plane, the 3rd air pocket rings institute；First air pocket rings, the second air pocket rings, the 3rd air bag
Any two air pocket rings in ring are fixedly connected；The center of circle of first air pocket rings, the center of circle of the second air pocket rings, the circle of the 3rd air pocket rings
The heart is overlapped in a bit；The controlling organization includes shell, controller and battery, and the controller and battery are located at outer hull shape
Into closed accommodating chamber in；The controller is used to control propeller and camera device；The controlling organization respectively with shooting
The motor electrical connection of device and propeller；The controlling organization is arranged on the intersection point of the lower end of the first air pocket rings and the 3rd air pocket rings
Place；Camera device is arranged on the point of intersection of the upper end of the first air pocket rings and the 3rd air pocket rings.
2. a kind of aircraft for being stuck in the water surface according to claim 1, it is characterised in that：The controlling organization it is upper
End is removably connected with balancing weight.
3. a kind of aircraft for being stuck in the water surface according to claim 1, it is characterised in that：First mounting rod and
The crosspoint of second mounting rod is on the center of circle where the second air pocket rings, and the first mounting rod is perpendicular to the second mounting rod；First peace
The angle of plane is 45 ° where straight line where filling bar and the first air pocket rings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710360129.7A CN107323664A (en) | 2017-05-20 | 2017-05-20 | A kind of aircraft for being stuck in the water surface |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710360129.7A CN107323664A (en) | 2017-05-20 | 2017-05-20 | A kind of aircraft for being stuck in the water surface |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107323664A true CN107323664A (en) | 2017-11-07 |
Family
ID=60193252
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710360129.7A Pending CN107323664A (en) | 2017-05-20 | 2017-05-20 | A kind of aircraft for being stuck in the water surface |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107323664A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108974342A (en) * | 2018-07-01 | 2018-12-11 | 庄明忠 | A kind of bridge machinery unmanned plane based on bridge security performance |
| CN108974343A (en) * | 2018-07-01 | 2018-12-11 | 朱承启 | A kind of unmanned aerial vehicle (UAV) control device |
| CN109305346A (en) * | 2018-11-27 | 2019-02-05 | 歌尔股份有限公司 | A kind of unmanned plane during flying device |
| CN111977003A (en) * | 2020-07-17 | 2020-11-24 | 苏州大晋影视传媒有限公司 | Intelligent falling protection method and system based on unmanned aerial vehicle airbag group |
-
2017
- 2017-05-20 CN CN201710360129.7A patent/CN107323664A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108974342A (en) * | 2018-07-01 | 2018-12-11 | 庄明忠 | A kind of bridge machinery unmanned plane based on bridge security performance |
| CN108974343A (en) * | 2018-07-01 | 2018-12-11 | 朱承启 | A kind of unmanned aerial vehicle (UAV) control device |
| CN109305346A (en) * | 2018-11-27 | 2019-02-05 | 歌尔股份有限公司 | A kind of unmanned plane during flying device |
| CN111977003A (en) * | 2020-07-17 | 2020-11-24 | 苏州大晋影视传媒有限公司 | Intelligent falling protection method and system based on unmanned aerial vehicle airbag group |
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Legal Events
| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171107 |