CN105438440A - Scratch resistant unmanned aerial vehicle wing - Google Patents
Scratch resistant unmanned aerial vehicle wing Download PDFInfo
- Publication number
- CN105438440A CN105438440A CN201510852902.2A CN201510852902A CN105438440A CN 105438440 A CN105438440 A CN 105438440A CN 201510852902 A CN201510852902 A CN 201510852902A CN 105438440 A CN105438440 A CN 105438440A
- Authority
- CN
- China
- Prior art keywords
- thin film
- scratch resistant
- unmanned plane
- aerial vehicle
- unmanned aerial
- 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
- 230000003678 scratch resistant effect Effects 0.000 title abstract 10
- 229920000515 polycarbonate Polymers 0.000 claims abstract description 27
- 239000004417 polycarbonate Substances 0.000 claims abstract description 27
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 11
- 239000010936 titanium Substances 0.000 claims abstract description 11
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 11
- 238000007790 scraping Methods 0.000 claims description 23
- 239000010409 thin film Substances 0.000 claims description 23
- 239000000758 substrate Substances 0.000 claims description 10
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 9
- 229910000989 Alclad Inorganic materials 0.000 claims description 3
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 3
- 239000010408 film Substances 0.000 claims description 3
- 239000002105 nanoparticle Substances 0.000 claims description 3
- 239000002245 particle Substances 0.000 claims description 3
- 238000006068 polycondensation reaction Methods 0.000 claims description 3
- 239000007790 solid phase Substances 0.000 claims description 3
- 239000013078 crystal Substances 0.000 abstract 1
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a scratch resistant unmanned aerial vehicle wing. The scratch resistant unmanned aerial vehicle wing comprises a base plate, a first polycarbonate sheet and a second polycarbonate sheet, wherein the first polycarbonate sheet and the second polycarbonate sheet are respectively arranged on the two sides of the base plate; a first scratch resistant film is arranged on the upper surface of the first polycarbonate sheet; a second scratch resistant film is arranged on the lower surface of the second polycarbonate sheet; and a titanium crystal nanometer layer is also arranged on the first scratch resistant film. Through the adoption of the mode, the invention is advantaged in that the strength and hardness of the scratch resistant unmanned aerial vehicle wing are excellent, the impact resistance of the scratch resistant unmanned aerial vehicle wing is excellent, the scratch resistant unmanned aerial vehicle wing is durable and scratch resistant, and the service life of the unmanned aerial vehicle wing is greatly prolonged.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly relate to a kind of anti-scratch formula unmanned plane wing.
Background technology
Unmanned plane is the not manned aircraft utilizing radio robot and the process controller provided for oneself to handle, at present taking photo by plane, agricultural plant protection, the field such as mapping have a wide range of applications.
The friction that existing unmanned plane wing in flight course receives various material in air resistance and environment is easy to produce wearing and tearing, can reduce the service life of unmanned plane like this.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of anti-scratch formula unmanned plane wing, has excellent intensity and hardness, has more excellent impact resistance, more wear-resisting scratch resistance, substantially increase the service life of unmanned plane wing.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: provide a kind of anti-scratch formula unmanned plane wing, comprise: substrate and be located at the first polycarbonate plate and second polycarbonate plate of substrate both sides respectively, the upper surface of described first polycarbonate plate is provided with the first anti scraping thin film, the lower surface of described second polycarbonate plate is provided with the second anti scraping thin film, described first anti scraping thin film is also provided with the brilliant nanometer layer of titanium.
In a preferred embodiment of the present invention, described substrate is Alclad plate or titanium alloy sheet.
In a preferred embodiment of the present invention, described first polycarbonate plate and the second polycarbonate plate are made by solid phase polycondensation mode.
In a preferred embodiment of the present invention, described first anti scraping thin film and the second anti scraping thin film are nano aluminium oxide film.
In a preferred embodiment of the present invention, the thickness of described first anti scraping thin film is 3 ~ 15 microns, and the thickness of described second anti scraping thin film is 5 ~ 30 microns.
In a preferred embodiment of the present invention, in the brilliant nanometer layer of described titanium, the particle diameter of the brilliant nano particle of titanium is 0.5 ~ 1.5 micron.
The invention has the beneficial effects as follows: the present invention's anti-scratch formula unmanned plane wing has excellent intensity and hardness, has more excellent impact resistance, more wear-resisting scratch resistance, substantially increases the service life of unmanned plane wing.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, below the accompanying drawing used required in describing embodiment is briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of anti-scratch formula unmanned plane wing one of the present invention preferred embodiment;
In accompanying drawing, the mark of each parts is as follows: 1, substrate, 2, one polycarbonate plate, the 3, second polycarbonate plate, the 4, first anti scraping thin film, the 5, second anti scraping thin film, and 6, the brilliant nanometer layer of titanium.
Detailed description of the invention
Be clearly and completely described to the technical scheme in the embodiment of the present invention below, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1, the embodiment of the present invention comprises:
A kind of anti-scratch formula unmanned plane wing, comprising: substrate 1 and be located at the first polycarbonate plate 2 and the second polycarbonate plate 3 of substrate 1 both sides respectively, and described substrate 1 is Alclad plate or titanium alloy sheet.
Described first polycarbonate plate 2 and the second polycarbonate plate 3 are made by solid phase polycondensation mode, ensure that the polycarbonate plate formed out has higher intensity and hardness, have more excellent impact resistance, meet the demand of aviation flight.
The upper surface of described first polycarbonate plate 2 is provided with the first anti scraping thin film 4, and the lower surface of described second polycarbonate plate 3 is provided with the second anti scraping thin film 5.
Described first anti scraping thin film 4 and the second anti scraping thin film 5 are nano aluminium oxide film, and more wear-resisting scratch resistance, substantially increases the service life of unmanned plane wing.
The thickness of described first anti scraping thin film is 3 ~ 15 microns, and the thickness of described second anti scraping thin film is 5 ~ 30 microns.
Described first anti scraping thin film 5 is also provided with the brilliant nanometer layer 6 of titanium, in the brilliant nanometer layer 6 of described titanium, the particle diameter of the brilliant nano particle of titanium is 0.5 ~ 1.5 micron, further increases intensity and the hardness of wing, more wear-resistant anti-scratch.
The beneficial effect of the present invention's anti-scratch formula unmanned plane wing is:
There is excellent intensity and hardness, there is more excellent impact resistance, more wear-resisting scratch resistance, substantially increase the service life of unmanned plane wing.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize description of the present invention to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present invention.
Claims (6)
1. an anti-scratch formula unmanned plane wing, it is characterized in that, comprise: substrate and be located at the first polycarbonate plate and second polycarbonate plate of substrate both sides respectively, the upper surface of described first polycarbonate plate is provided with the first anti scraping thin film, the lower surface of described second polycarbonate plate is provided with the second anti scraping thin film, described first anti scraping thin film is also provided with the brilliant nanometer layer of titanium.
2. anti-scratch formula unmanned plane wing according to claim 1, it is characterized in that, described substrate is Alclad plate or titanium alloy sheet.
3. anti-scratch formula unmanned plane wing according to claim 1, it is characterized in that, described first polycarbonate plate and the second polycarbonate plate are made by solid phase polycondensation mode.
4. anti-scratch formula unmanned plane wing according to claim 1, it is characterized in that, described first anti scraping thin film and the second anti scraping thin film are nano aluminium oxide film.
5. anti-scratch formula unmanned plane wing according to claim 1, is characterized in that, the thickness of described first anti scraping thin film is 3 ~ 15 microns, and the thickness of described second anti scraping thin film is 5 ~ 30 microns.
6. anti-scratch formula unmanned plane wing according to claim 1, is characterized in that, in the brilliant nanometer layer of described titanium, the particle diameter of the brilliant nano particle of titanium is 0.5 ~ 1.5 micron.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510852902.2A CN105438440A (en) | 2015-11-30 | 2015-11-30 | Scratch resistant unmanned aerial vehicle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510852902.2A CN105438440A (en) | 2015-11-30 | 2015-11-30 | Scratch resistant unmanned aerial vehicle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105438440A true CN105438440A (en) | 2016-03-30 |
Family
ID=55549186
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510852902.2A Pending CN105438440A (en) | 2015-11-30 | 2015-11-30 | Scratch resistant unmanned aerial vehicle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105438440A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106981249A (en) * | 2017-03-17 | 2017-07-25 | 苏州工业园区高泰电子有限公司 | A kind of novel local gum small dimension label material |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0056288A1 (en) * | 1981-01-09 | 1982-07-21 | Technische Universiteit Delft | Laminate of metal sheet material and threads bonded thereto, as well as processes for the manufacture thereof |
| CN101786351A (en) * | 2010-01-29 | 2010-07-28 | 湖州金泰科技股份有限公司 | Coated polycarbonate |
| CN202295282U (en) * | 2011-09-08 | 2012-07-04 | 中国航天科工集团第三研究院第八三五七研究所 | Wing point friction-preventing device of fixed-wing unmanned aerial vehicle |
| CN103140349A (en) * | 2010-10-15 | 2013-06-05 | 法国肯联铝业 | Airfoil and fiber metal laminate forming part of said airfoil |
| CN103587198A (en) * | 2013-10-26 | 2014-02-19 | 溧阳市哈大成果转化中心有限公司 | Wing shell |
| CN103770391A (en) * | 2012-07-03 | 2014-05-07 | 古德里奇公司 | Nanoreinforced films and laminates for aerospace structures |
-
2015
- 2015-11-30 CN CN201510852902.2A patent/CN105438440A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0056288A1 (en) * | 1981-01-09 | 1982-07-21 | Technische Universiteit Delft | Laminate of metal sheet material and threads bonded thereto, as well as processes for the manufacture thereof |
| CN101786351A (en) * | 2010-01-29 | 2010-07-28 | 湖州金泰科技股份有限公司 | Coated polycarbonate |
| CN103140349A (en) * | 2010-10-15 | 2013-06-05 | 法国肯联铝业 | Airfoil and fiber metal laminate forming part of said airfoil |
| CN202295282U (en) * | 2011-09-08 | 2012-07-04 | 中国航天科工集团第三研究院第八三五七研究所 | Wing point friction-preventing device of fixed-wing unmanned aerial vehicle |
| CN103770391A (en) * | 2012-07-03 | 2014-05-07 | 古德里奇公司 | Nanoreinforced films and laminates for aerospace structures |
| CN103587198A (en) * | 2013-10-26 | 2014-02-19 | 溧阳市哈大成果转化中心有限公司 | Wing shell |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106981249A (en) * | 2017-03-17 | 2017-07-25 | 苏州工业园区高泰电子有限公司 | A kind of novel local gum small dimension label material |
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| 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: 20160330 |