CN105438439A - Fluorescent unmanned aerial vehicle wing - Google Patents
Fluorescent unmanned aerial vehicle wing Download PDFInfo
- Publication number
- CN105438439A CN105438439A CN201510851059.6A CN201510851059A CN105438439A CN 105438439 A CN105438439 A CN 105438439A CN 201510851059 A CN201510851059 A CN 201510851059A CN 105438439 A CN105438439 A CN 105438439A
- Authority
- CN
- China
- Prior art keywords
- guide plate
- light guide
- fluorescent
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
Abstract
The invention discloses a fluorescent unmanned aerial vehicle wing. The fluorescent unmanned aerial vehicle wing comprises a base plate, wherein a first light guide plate and a second light guide plate are respectively arranged on two surfaces of the base plate; a circle of LED digital energy-saving lamp tubes are distributed on the surrounding of the first light guide plate and the second light guide plate; and reflective fluorescent films are also arranged on the upper surface of the first light guide plate and the lower surface of the second light guide plate. Through the adoption of the mode, the invention is advantaged in that the light guiding efficiency of the fluorescent unmanned aerial vehicle wing is excellent, the fluorescent unmanned aerial vehicle wing is energy-saving and environment friendly, can generate beautiful luster in dark places and has a dazzling warning effect, the flight safety at nights is ensured and assurance is provided to endurance of an unmanned aerial vehicle at nights.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly relate to a kind of fluorescence type 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.
Because illumination is not enough, usually can there is phenomenon of going off course when navigation at night in current unmanned plane, cause night flying more difficult on the one hand, also cannot provide warning on the other hand, there is flight safety hidden danger.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of fluorescence type unmanned plane wing, there is excellent guide-lighting efficiency, energy-conserving and environment-protective more, gorgeous brilliance can be sent in the place of dark, serve the effect of brilliant warning, ensure that the safety of night flying, for the continuation of the journey at night of unmanned plane provides guarantee.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: provide a kind of fluorescence type unmanned plane wing, comprise: substrate, two surfaces of described substrate are respectively equipped with the first light guide plate and the second light guide plate, the surrounding of described first light guide plate and the second light guide plate is distributed with a circle LED digital energy-saving fluorescent tube, and the upper surface of described first light guide plate and the lower surface of the second light guide plate are also provided with reflected fluorescent light film.
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 light guide plate and the second light guide plate are optical grade glass light guide plate.
In a preferred embodiment of the present invention, described LED digital energy-saving fluorescent tube comprises the LED lamp tube of at least two kinds of colors.
In a preferred embodiment of the present invention, described reflected fluorescent light film and between the first light guide plate and the second light guide plate for adhesion is arranged, the thickness of described reflected fluorescent light film is 1.6 ~ 8.6 microns.
The invention has the beneficial effects as follows: fluorescence type unmanned plane wing of the present invention has excellent guide-lighting efficiency, energy-conserving and environment-protective more, can send gorgeous brilliance in the place of dark, serve the effect of brilliant warning, ensure that the safety of night flying, for the continuation of the journey at night of unmanned plane provides guarantee.
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 fluorescence type unmanned plane wing one of the present invention preferred embodiment;
In accompanying drawing, the mark of each parts is as follows: 1, substrate, the 2, first light guide plate, the 3, second light guide plate, and 4, LED digital energy-saving fluorescent tube, 5, reflected fluorescent light film.
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 fluorescence type unmanned plane wing, comprising: substrate 1, two surfaces of described substrate 1 are respectively equipped with the first light guide plate 2 and the second light guide plate 3.
Wherein, described substrate 1 is Alclad plate or titanium alloy sheet, ensure that the demand of aviation flight.
Described first light guide plate 2 and the second light guide plate 3 are optical grade glass light guide plate, have excellent guide-lighting efficiency, energy-conserving and environment-protective more.
The surrounding of described first light guide plate 2 and the second light guide plate 3 is distributed with a circle LED digital energy-saving fluorescent tube 4, and described LED digital energy-saving fluorescent tube 4 comprises the LED lamp tube of at least two kinds of colors.
Serve the effect of lighting energy saving on the one hand, can also alarming effect be played on the other hand, for the continuation of the journey at night of unmanned plane provides guarantee.
The upper surface of described first light guide plate 1 and the lower surface of the second light guide plate 3 are also provided with reflected fluorescent light film 5, can send gorgeous brilliance, serve the effect of brilliant warning, ensure that the safety of night flying in the place of dark.
Described reflected fluorescent light film 5 and between the first light guide plate 2 and the second light guide plate 3 for adhesion is arranged, the thickness of described reflected fluorescent light film 5 is 1.6 ~ 8.6 microns.
The beneficial effect of fluorescence type unmanned plane wing of the present invention is:
Have excellent guide-lighting efficiency, energy-conserving and environment-protective more, can send gorgeous brilliance in the place of dark, serve the effect of brilliant warning, ensure that the safety of night flying, for the continuation of the journey at night of unmanned plane provides guarantee.
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 (5)
1. a fluorescence type unmanned plane wing, it is characterized in that, comprise: substrate, two surfaces of described substrate are respectively equipped with the first light guide plate and the second light guide plate, the surrounding of described first light guide plate and the second light guide plate is distributed with a circle LED digital energy-saving fluorescent tube, and the upper surface of described first light guide plate and the lower surface of the second light guide plate are also provided with reflected fluorescent light film.
2. fluorescence type unmanned plane wing according to claim 1, is characterized in that, described substrate is Alclad plate or titanium alloy sheet.
3. fluorescence type unmanned plane wing according to claim 1, is characterized in that, described first light guide plate and the second light guide plate are optical grade glass light guide plate.
4. fluorescence type unmanned plane wing according to claim 1, is characterized in that, described LED digital energy-saving fluorescent tube comprises the LED lamp tube of at least two kinds of colors.
5. fluorescence type unmanned plane wing according to claim 1, is characterized in that, described reflected fluorescent light film and between the first light guide plate and the second light guide plate for adhesion is arranged, the thickness of described reflected fluorescent light film is 1.6 ~ 8.6 microns.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510851059.6A CN105438439A (en) | 2015-11-30 | 2015-11-30 | Fluorescent unmanned aerial vehicle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510851059.6A CN105438439A (en) | 2015-11-30 | 2015-11-30 | Fluorescent unmanned aerial vehicle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105438439A true CN105438439A (en) | 2016-03-30 |
Family
ID=55549185
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510851059.6A Pending CN105438439A (en) | 2015-11-30 | 2015-11-30 | Fluorescent unmanned aerial vehicle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105438439A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106662313A (en) * | 2016-09-27 | 2017-05-10 | 深圳市大疆创新科技有限公司 | Navigationlamp of drone and drone |
| US10554097B2 (en) | 2017-03-29 | 2020-02-04 | SZ DJI Technology Co., Ltd. | Hollow motor apparatuses and associated systems and methods |
| US10899471B2 (en) | 2017-01-24 | 2021-01-26 | SZ DJI Technology Co., Ltd. | Flight indication apparatuses, systems and associated methods |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201129667Y (en) * | 2007-11-26 | 2008-10-08 | 上海广电光电子有限公司 | Side light type back light module unit using LED light source |
| CN201377736Y (en) * | 2009-04-08 | 2010-01-06 | 胡枝清 | LED high-power tunnel lamp with wings |
| ES1073164U (en) * | 2010-09-03 | 2010-11-02 | Fundiven, S.L. | Led adapter device for luminaires (Machine-translation by Google Translate, not legally binding) |
| CN101965242A (en) * | 2008-03-07 | 2011-02-02 | Imra美国公司 | Utilize the transparent material processing of ultra-short pulse laser |
| CN202541829U (en) * | 2011-12-16 | 2012-11-21 | 李大成 | Novel seaplane wing |
| CN103140349A (en) * | 2010-10-15 | 2013-06-05 | 法国肯联铝业 | Aircraft wing and fiber metal laminate forming part of such an aircraft wing |
-
2015
- 2015-11-30 CN CN201510851059.6A patent/CN105438439A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201129667Y (en) * | 2007-11-26 | 2008-10-08 | 上海广电光电子有限公司 | Side light type back light module unit using LED light source |
| CN101965242A (en) * | 2008-03-07 | 2011-02-02 | Imra美国公司 | Utilize the transparent material processing of ultra-short pulse laser |
| CN201377736Y (en) * | 2009-04-08 | 2010-01-06 | 胡枝清 | LED high-power tunnel lamp with wings |
| ES1073164U (en) * | 2010-09-03 | 2010-11-02 | Fundiven, S.L. | Led adapter device for luminaires (Machine-translation by Google Translate, not legally binding) |
| CN103140349A (en) * | 2010-10-15 | 2013-06-05 | 法国肯联铝业 | Aircraft wing and fiber metal laminate forming part of such an aircraft wing |
| CN202541829U (en) * | 2011-12-16 | 2012-11-21 | 李大成 | Novel seaplane wing |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106662313A (en) * | 2016-09-27 | 2017-05-10 | 深圳市大疆创新科技有限公司 | Navigationlamp of drone and drone |
| WO2018058297A1 (en) * | 2016-09-27 | 2018-04-05 | 深圳市大疆创新科技有限公司 | Navigation lamp of unmanned aerial vehicle and unmanned aerial vehicle |
| US10899471B2 (en) | 2017-01-24 | 2021-01-26 | SZ DJI Technology Co., Ltd. | Flight indication apparatuses, systems and associated methods |
| US10554097B2 (en) | 2017-03-29 | 2020-02-04 | SZ DJI Technology Co., Ltd. | Hollow motor apparatuses and associated systems and methods |
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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 |