CN106218880A - A kind of aircraft containing macromolecule conducting material - Google Patents
A kind of aircraft containing macromolecule conducting material Download PDFInfo
- Publication number
- CN106218880A CN106218880A CN201610751431.0A CN201610751431A CN106218880A CN 106218880 A CN106218880 A CN 106218880A CN 201610751431 A CN201610751431 A CN 201610751431A CN 106218880 A CN106218880 A CN 106218880A
- Authority
- CN
- China
- Prior art keywords
- frame
- conducting material
- conductive layer
- macromolecule conducting
- 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
Links
- 239000004020 conductor Substances 0.000 title claims abstract description 25
- 229920002521 macromolecule Polymers 0.000 title claims abstract description 21
- 230000001681 protective effect Effects 0.000 claims abstract description 10
- 239000007769 metal material Substances 0.000 claims description 3
- 230000007423 decrease Effects 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 4
- 230000004888 barrier function Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Transforming Light Signals Into Electric Signals (AREA)
Abstract
The invention discloses a kind of aircraft containing macromolecule conducting material, the propeller that is connected with frame including frame, the rotary shaft of support helix oar, high-definition camera is installed in frame, high-definition camera is coated with hollow out protective cover, being additionally provided with Mobile phone clip in frame, described Mobile phone clip is between adjoining spiral oar；Described machine frame inside is provided with conductive layer, and conductive layer is provided with at least two binding post；Described conductive layer is the internal layer of frame, and described conductive layer connects components and parts.The present invention can take pictures simultaneously and record a video, and it is few to connect wires in frame, present invention employs conductive material and decreases the access of electric wire as internal layer, does not results in short circuit phenomenon after aircraft is dropped.
Description
Technical field
The present invention relates to a kind of four-axle aircraft, be specifically related to a kind of aircraft containing macromolecule conducting material.
Background technology
At present unmanned plane taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring biography
There is extensive application in fields such as catching an illness, survey and draw, news report, electric inspection process, the disaster relief, movies-making, manufacture are romantic.
But, unmanned plane is generally used for video capture, it is impossible to enough use camera to take pictures, and most people now
Like the auto heterodyne of different angles, preserve photo；And in use easily drop from the air due to various factors unmanned plane,
Falling on the ground, the electric wire of interface unit may be made because of insulating barrier short circuit, burn out device, the most on fire, aircraft drops from the air
Battery explosion after rear line short.
Summary of the invention
Present invention aim at providing a kind of aircraft containing macromolecule conducting material, in solving how to ensure unmanned plane
Portion's electric wire is few, it is to avoid after unmanned plane falling from high altitude occur line short and utilize unmanned plane realize the most simultaneously high-altitude take pictures and
The problem of videograph.
The present invention is achieved through the following technical solutions:
A kind of aircraft containing macromolecule conducting material, the propeller being connected with frame including frame, the rotation of support helix oar
Rotating shaft, frame is provided with high-definition camera, and high-definition camera is coated with hollow out protective cover, and frame is additionally provided with mobile phone
Folder, described Mobile phone clip is between adjoining spiral oar；
Described machine frame inside is provided with conductive layer, and conductive layer is provided with at least two binding post；Described conductive layer is frame
Internal layer, described conductive layer connects and has components and parts.
The operation principle of the present invention is: the present invention combines high-definition camera and mobile phone on the basis of existing unmanned plane
Function, it is possible to realize taking pictures simultaneously and carrying out videograph, different-effect can be taken by the flying height adjusting unmanned plane
Photo；It is outside equipped with hollow out protective cover at high-definition camera and does not interferes with video recording effect, it is thus also avoided that when unmanned plane occurs
Collision rift damages high-definition camera；The blade of each propeller is provided with two panels, is distributed in the both sides of rotary shaft, but sheet blade
Vary in size；The frame internal layer of the present invention is conductive layer, and conductive layer is it is avoided that use a lot of electric wires, the most according to actual needs
Suitable connection line；Without a large amount of electric wires, when four-axle aircraft drops from the air, pound on the ground just without because of insulating barrier
Damage the danger causing line short.Even if falling very serious is also that frame was broken (the most not considering that components and parts are broken),
Also will not short circuit.
Described conductive layer is provided with pad lamp.According to actual needs, pad lamp is reserved in the place needed.
Described conductive layer uses macromolecule conducting material.Macromolecule conducting material have density processing little, easy, corrosion-resistant,
Large area film forming and electrical conductivity the feature such as can be adjusted in the range of more than ten orders of magnitude, can be used as multiple gold
Belong to material and the succedaneum of inorganic conductive material, and become many advanced industrial departments and sophisticated technology field is indispensable
A class material.
Described propeller is set to four.
It is positioned at high-definition camera side in described frame and is provided with infrared sensor.Infrared sensor is used for coordinating high definition to take the photograph
As head carries out image record.
Described Mobile phone clip is internally provided with rubber blanket.On the one hand rubber blanket is set so that mobile phone and mobile phone in Mobile phone clip
Folder combines tightr, on the other hand avoids mobile phone to receive abrasion.
Described hollow out protective cover uses lightweight metal material.If protective cover uses other metals, quality will increase the most greatly
Add the flight difficulty of aircraft.
The present invention compared with prior art, has such advantages as and beneficial effect:
1, a kind of aircraft containing macromolecule conducting material of the present invention can be taken pictures simultaneously and record a video, and aircraft is installed
There are Mobile phone clip and high-definition camera；
2, connect wires in a kind of aircraft containing macromolecule conducting material of the present invention less, present invention employs conductive material conduct
Internal layer decreases the access of electric wire, does not results in short circuit phenomenon after aircraft is dropped.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing being further appreciated by the embodiment of the present invention, constitutes of the application
Point, it is not intended that the restriction to the embodiment of the present invention.In the accompanying drawings:
Fig. 1 is present configuration schematic diagram；
Fig. 2 is the internal structure schematic diagram of frame of the present invention.
The parts title of labelling and correspondence in accompanying drawing:
1-frame, 2-propeller, 3-rotary shaft, the clear photographic head of 4-, 5-hollow out protective cover, 6-Mobile phone clip, 7-conductive layer, 8-wiring
Post.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with embodiment and accompanying drawing, to this
Invention is described in further detail, and the exemplary embodiment of the present invention and explanation thereof are only used for explaining the present invention, do not make
For limitation of the invention.
Embodiment 1
As shown in Figure 1 and Figure 2, a kind of aircraft containing macromolecule conducting material of the present invention, it is connected with frame 1 including frame 1
Propeller 2, the rotary shaft 3 of support helix oar 2, frame 1 is provided with high-definition camera 4, high-definition camera 4 is coated with to be engraved
Air defence guard shield 5, frame 1 is additionally provided with Mobile phone clip 6, and described Mobile phone clip 6 is between adjoining spiral oar 2；
Described frame 1 is internally provided with conductive layer 7, and conductive layer 7 is provided with at least two binding post 8；Described conductive layer 7 is machine
The internal layer of frame 1, described conductive layer 7 connects and has components and parts.
The present invention combines the function of high-definition camera and mobile phone on the basis of existing unmanned plane, it is possible to realize clapping simultaneously
According to and carry out videograph, the photo of different-effect can be taken by the flying height adjusting unmanned plane；At high-definition camera
It is outside equipped with hollow out protective cover and does not interferes with video recording effect, it is thus also avoided that after unmanned plane collides, damaging high-definition camera
Head；The blade of each propeller is provided with two panels, is distributed in the both sides of rotary shaft, but the varying in size of sheet blade；The present invention's
Frame internal layer is conductive layer, and conductive layer, it is avoided that use a lot of electric wires, is the most suitable connection line；Not yet
There is a large amount of electric wire, when four-axle aircraft drops from the air, pounded and the most just cause line short without because insulating barrier damages
Danger.Even if falling very serious is also that frame was broken (the most not considering that components and parts are broken), also will not short circuit.
Embodiment 2
Based on embodiment 1, described conductive layer 7 is provided with pad lamp.According to actual needs, pad lamp is reserved in the place needed.
Embodiment 3
Based on above-described embodiment, described conductive layer 7 uses macromolecule conducting material.It is little, easy that macromolecule conducting material has density
Processing, corrosion-resistant, large area film forming and electrical conductivity the feature such as can be adjusted in the range of more than ten orders of magnitude, not only
As various metals material and the succedaneum of inorganic conductive material, and many advanced industrial departments and sophisticated technology can be become
The indispensable class material in field.
Embodiment 4
Based on above-described embodiment, described propeller 2 is set to four.Propeller is set to four, and counterbalance effect is more preferable.
Embodiment 5
Based on above-described embodiment, described frame 1 is positioned at high-definition camera 4 side and is provided with infrared sensor.Infrared sensor
For coordinating high-definition camera to carry out image record.Machine frame inside can also be provided with temperature sensor, be used for monitoring frame
Internal temperature.
Embodiment 6
Based on above-described embodiment, described Mobile phone clip 6 is internally provided with rubber blanket.Arrange rubber blanket in Mobile phone clip on the one hand can make
Obtain mobile phone and be combined tightr with Mobile phone clip, on the other hand avoid mobile phone to receive abrasion.
Embodiment 7
Described hollow out protective cover 5 uses lightweight metal material.If protective cover uses other metals, quality will increase the most greatly and fly
The flight difficulty of row device.
Above-described detailed description of the invention, has been carried out the purpose of the present invention, technical scheme and beneficial effect further
Describe in detail, be it should be understood that the detailed description of the invention that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, all within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, all should wrap
Within being contained in protection scope of the present invention.
Claims (7)
1. containing the aircraft of macromolecule conducting material, the propeller (2) that is connected with frame (1) including frame (1),
The rotary shaft (3) of support propeller (2), it is characterised in that be provided with high-definition camera (4), high-definition camera (4) in frame (1)
Being coated with hollow out protective cover (5), frame (1) is additionally provided with Mobile phone clip (6), described Mobile phone clip (6) is positioned at adjoining spiral oar
(2) between；
Described frame (1) is internally provided with conductive layer (7), and conductive layer (7) is provided with at least two binding post (8)；Described lead
Electric layer (7) is the internal layer of frame (1), and the upper connection of described conductive layer (7) has components and parts.
A kind of aircraft containing macromolecule conducting material the most according to claim 1, it is characterised in that described conductive layer
(7) pad lamp it is provided with.
A kind of aircraft containing macromolecule conducting material the most according to claim 1 and 2, it is characterised in that described in lead
Electric layer (7) uses macromolecule conducting material.
A kind of aircraft containing macromolecule conducting material the most according to claim 1 and 2, it is characterised in that described spiral shell
Rotation oar (2) is set to four.
A kind of aircraft containing macromolecule conducting material the most according to claim 1 and 2, it is characterised in that described machine
It is positioned at high-definition camera (4) side on frame (1) and is provided with infrared sensor.
A kind of aircraft containing macromolecule conducting material the most according to claim 1 and 2, it is characterised in that described hands
Machine folder (6) is internally provided with rubber blanket.
A kind of aircraft containing macromolecule conducting material the most according to claim 1, it is characterised in that described hollow out is prevented
Guard shield (5) uses lightweight metal material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610751431.0A CN106218880A (en) | 2016-08-30 | 2016-08-30 | A kind of aircraft containing macromolecule conducting material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610751431.0A CN106218880A (en) | 2016-08-30 | 2016-08-30 | A kind of aircraft containing macromolecule conducting material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106218880A true CN106218880A (en) | 2016-12-14 |
Family
ID=57556026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610751431.0A Pending CN106218880A (en) | 2016-08-30 | 2016-08-30 | A kind of aircraft containing macromolecule conducting material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106218880A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2121745A (en) * | 1982-06-17 | 1984-01-04 | Westland Plc | Aircraft de-icing apparatus |
| CN103523241A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Brushless tripod head of unmanned aerial vehicle |
| CN103662083A (en) * | 2012-09-04 | 2014-03-26 | 空中客车运作有限责任公司 | Method for producing an aircraft structure component having an outer skin provided with electric conductor elements |
| CN104347154A (en) * | 2013-07-31 | 2015-02-11 | 南昌欧菲光科技有限公司 | Transparent conducting film |
| CN205327401U (en) * | 2016-01-12 | 2016-06-22 | 童欣 | Flying device is assisted to cell -phone |
| CN206012956U (en) * | 2016-08-30 | 2017-03-15 | 成都创客空间科技有限公司 | A kind of 3D printing four-axle aircraft of embedded conductive material |
-
2016
- 2016-08-30 CN CN201610751431.0A patent/CN106218880A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2121745A (en) * | 1982-06-17 | 1984-01-04 | Westland Plc | Aircraft de-icing apparatus |
| CN103662083A (en) * | 2012-09-04 | 2014-03-26 | 空中客车运作有限责任公司 | Method for producing an aircraft structure component having an outer skin provided with electric conductor elements |
| CN104347154A (en) * | 2013-07-31 | 2015-02-11 | 南昌欧菲光科技有限公司 | Transparent conducting film |
| CN103523241A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Brushless tripod head of unmanned aerial vehicle |
| CN205327401U (en) * | 2016-01-12 | 2016-06-22 | 童欣 | Flying device is assisted to cell -phone |
| CN206012956U (en) * | 2016-08-30 | 2017-03-15 | 成都创客空间科技有限公司 | A kind of 3D printing four-axle aircraft of embedded conductive material |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161214 |