CN104354872A - Unmanned airplane suitable for severe weather - Google Patents
Unmanned airplane suitable for severe weather Download PDFInfo
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- CN104354872A CN104354872A CN201410723486.1A CN201410723486A CN104354872A CN 104354872 A CN104354872 A CN 104354872A CN 201410723486 A CN201410723486 A CN 201410723486A CN 104354872 A CN104354872 A CN 104354872A
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- led lamp
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Abstract
The invention relates to an unmanned airplane suitable for severe weather. The unmanned airplane comprises an unmanned airplane body and a control panel, wherein the unmanned airplane body comprises a nose and an empennage, an LED (Light Emitting Diode) signal lamp is installed on the nose, another LED signal lamp is installed on the empennage, the LED signal lamp on the empennage emits red light, the LED signal lamp on the nose emits green light, mixed LED lamp groups are arranged at the bottom of the nose, the mixed LED lamp groups include a white light LED lamp group and a yellow light LED lamp group which is arranged on the periphery of the white light LED lamp group, two mutually independent electrical systems are used for the yellow light LED lamp group and the white light LED lamp group, switch buttons of the yellow light LED lamp group and the white light LED lamp group are arranged on the control panel, a waterproof lampshade is arranged on the outer part of the mixed LED lamp groups, a propeller is further arranged on the nose, and the propeller is coated with a fluorescent coating. The unmanned airplane designed by the invention can be used in severe conditions such as rainy days and foggy days, operating personnel can clearly distinguish the moving direction of the unmanned airplane, and the unmanned airplane has a wide use value.
Description
Technical field
The present invention relates to flight equipment technical field, be specifically related to one and be applicable to boisterous unmanned plane.
Background technology
Unmanned plane is used in the middle of the modern life widely, be mainly used to carry out some operations cannot carried out on the ground, unmanned plane still will lean on ground people to manipulate normally could carry out work, due to the polytropy of work-hours, unmanned plane is also being worked at night sometimes, because the flying height of unmanned plane is higher, ground people are difficult to the operation conditions observing unmanned plane, this brings certain restriction working at night also to unmanned plane, especially, in the weather of rainy day or dense fog, unmanned plane all can not work.
Summary of the invention
Technical matters to be solved by this invention is to provide a kind of novel in design, and rationally, flexible operation is simple and easy, the novel unmanned plane that normally can work under the mal-condition such as rainy day, greasy weather for structure.
For solving the problems of the technologies described above, the invention provides following technical scheme: one is applicable to boisterous unmanned plane, comprising unmanned plane body and control panel, described unmanned plane body comprises head and tail, it is characterized in that, described head is equipped with LED signal lamp, described tail is also provided with LED signal lamp, LED signal lamp on described tail sends ruddiness, LED signal lamp on described head sends green glow, the bottom of described head is provided with mixing LED group, described mixing LED group comprises white LED lamp group and yellow light LED lamp group, described yellow light LED lamp group is arranged on the periphery of white LED lamp group, yellow light LED lamp group and white LED lamp group are two separate Circuits System, the shift knob of yellow light LED lamp group and white LED lamp group is all arranged on control panel, the outside of described mixing LED group is provided with lampshade, described head is also provided with screw propeller, screw propeller scribbles fluorescent paint layer.
The beneficial effect that the present invention compared with prior art has is: on unmanned plane body, be provided with screw propeller, screw propeller scribbles fluorescent paint layer, the particular location of such convenient operation personal observations unmanned plane; The head and tail of unmanned plane body are provided with the signal lamp of different colours, handled easily personnel can determine the service direction of unmanned plane; Mixing LED group is also provided with in the bottom of unmanned plane body, under the control of operating personal, mix LED group can send gold-tinted and white light, LED group Yellow light-emitting low temperature can be made at dense fog or rainy night, gold-tinted has good penetrating capacity, can guarantee that unmanned plane can normally work like this, at fine night, LED group is emitted white light, also can guarantee that unmanned plane normally works.The present invention is novel in design, and structure rationally, operates simple and easy, has market outlook widely.
Accompanying drawing explanation
Fig. 1 is integral structure schematic diagram of the present invention;
Fig. 2 is the structural representation that the present invention mixes LED group.
Detailed description of the invention
In order to make object of the present invention, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the present invention, be not intended to limit the present invention.
In describing the invention, it will be appreciated that, term " longitudinal direction ", " transverse direction ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ", " interior ", the orientation of the instruction such as " outward " or position relationship be based on orientation shown in the drawings or position relationship, only the present invention for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as limitation of the present invention.
See figures.1.and.2 known, one is applicable to boisterous unmanned plane, comprise unmanned plane body and control panel 8, described unmanned plane body comprises head 1 and tail 2, described head 1 is equipped with LED signal lamp 4, described tail 2 is also provided with LED signal lamp 4, LED signal lamp 4 on described tail 2 sends ruddiness, LED signal lamp 4 on described head 1 sends green glow, the bottom of described head 1 is provided with mixing LED group, described mixing LED group comprises white LED lamp group 6 and yellow light LED lamp group 5, described yellow light LED lamp group 5 is arranged on the periphery of white LED lamp group 6, yellow light LED lamp group 5 and white LED lamp group 6 are two separate Circuits System, the shift knob of yellow light LED lamp group 5 and white LED lamp group 6 is all arranged on control panel 8, the outside of described mixing LED group is provided with rainproof lampshade 7, described head 1 is also provided with screw propeller 3, screw propeller 3 scribbles fluorescent paint layer, sonic generator is provided with in described unmanned plane body, described control panel 8 is provided with radar, radar is provided with acoustic signals read-out, the sound wave that in unmanned plane body, sonic generator sends is received by the radar on control panel 8, signal shows on a display screen, and operating personal can according to the information determination unmanned plane particular location of display, described rainproof lampshade 7 is threaded on head 1.
Unmanned plane body is provided with screw propeller 3, screw propeller 3 scribbles fluorescent paint layer, the particular location of such convenient operation personal observations unmanned plane; The head 1 and tail 2 of unmanned plane body are provided with the LED signal lamp 4 of different colours, handled easily personnel can determine the service direction of unmanned plane; Mixing LED group is also provided with in the bottom of unmanned plane body, under the control of operating personal, mix LED group can send gold-tinted and white light, LED group Yellow light-emitting low temperature can be made at dense fog or rainy night, gold-tinted has good penetrating capacity, can guarantee that unmanned plane can normally work like this, at fine night, LED group is emitted white light, also can guarantee that unmanned plane normally works.
The foregoing is only preferred embodiment of the present invention, not in order to limit the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.
Claims (3)
1. be applicable to a boisterous unmanned plane, comprise unmanned plane body and control panel, described unmanned plane body comprises head and tail, it is characterized in that, described head is equipped with LED signal lamp, described tail is also provided with LED signal lamp, LED signal lamp on described tail sends ruddiness, LED signal lamp on described head sends green glow, the bottom of described head is provided with mixing LED group, described mixing LED group comprises white LED lamp group and yellow light LED lamp group, described yellow light LED lamp group is arranged on the periphery of white LED lamp group, yellow light LED lamp group and white LED lamp group are two separate Circuits System, the shift knob of yellow light LED lamp group and white LED lamp group is all arranged on control panel, the outside of described mixing LED group is provided with rainproof lampshade, described head is also provided with screw propeller, screw propeller scribbles fluorescent paint layer.
2. one according to claim 1 is applicable to boisterous unmanned plane, it is characterized in that: be provided with sonic generator in described unmanned plane body, described control panel is provided with radar, and radar is provided with acoustic signals read-out.
3. one according to claim 1 is applicable to boisterous unmanned plane, it is characterized in that: described rainproof lampshade is threaded on head.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410723486.1A CN104354872A (en) | 2014-12-03 | 2014-12-03 | Unmanned airplane suitable for severe weather |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410723486.1A CN104354872A (en) | 2014-12-03 | 2014-12-03 | Unmanned airplane suitable for severe weather |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104354872A true CN104354872A (en) | 2015-02-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410723486.1A Pending CN104354872A (en) | 2014-12-03 | 2014-12-03 | Unmanned airplane suitable for severe weather |
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| CN (1) | CN104354872A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104843193A (en) * | 2015-05-13 | 2015-08-19 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle lamplight warning system |
| CN105217050A (en) * | 2015-10-27 | 2016-01-06 | 杨珊珊 | A kind of unmanned vehicle being convenient to observe |
| CN109367803A (en) * | 2018-09-29 | 2019-02-22 | 国网浙江省电力有限公司 | Suitable for boisterous multi-functional unmanned plane |
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| US6456205B1 (en) * | 1998-05-21 | 2002-09-24 | Thales Optronics (Taunton) Ltd | Anti-collision warning lights and method of use |
| DE10329078A1 (en) * | 2003-06-27 | 2005-01-20 | Osram Opto Semiconductors Gmbh | Illumination module especially for air-traffic signaling or warning lamp, has LED encapsulated in housing with light-emission window |
| CN2839817Y (en) * | 2005-11-07 | 2006-11-22 | 程继金 | Flight vehicle LED indicating lamp |
| CN201729275U (en) * | 2010-07-14 | 2011-02-02 | 安徽华东光电技术研究所 | Dual-mode aviation landing lamp |
| CN102639927A (en) * | 2009-12-02 | 2012-08-15 | 欧司朗股份有限公司 | Lighting apparatus for a beacon system |
| CN202419414U (en) * | 2011-12-16 | 2012-09-05 | 安徽华东光电技术研究所 | Combined dual-mode airplane search lamp |
| CN203845017U (en) * | 2014-03-19 | 2014-09-24 | 北京中飞艾维航空科技有限公司 | Unmanned aerial vehicle provided with night navigation lamp |
| CN204383758U (en) * | 2014-12-03 | 2015-06-10 | 成都群侠科技有限公司 | One is applicable to boisterous unmanned plane |
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2014
- 2014-12-03 CN CN201410723486.1A patent/CN104354872A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6456205B1 (en) * | 1998-05-21 | 2002-09-24 | Thales Optronics (Taunton) Ltd | Anti-collision warning lights and method of use |
| DE10329078A1 (en) * | 2003-06-27 | 2005-01-20 | Osram Opto Semiconductors Gmbh | Illumination module especially for air-traffic signaling or warning lamp, has LED encapsulated in housing with light-emission window |
| CN2839817Y (en) * | 2005-11-07 | 2006-11-22 | 程继金 | Flight vehicle LED indicating lamp |
| CN102639927A (en) * | 2009-12-02 | 2012-08-15 | 欧司朗股份有限公司 | Lighting apparatus for a beacon system |
| CN201729275U (en) * | 2010-07-14 | 2011-02-02 | 安徽华东光电技术研究所 | Dual-mode aviation landing lamp |
| CN202419414U (en) * | 2011-12-16 | 2012-09-05 | 安徽华东光电技术研究所 | Combined dual-mode airplane search lamp |
| CN203845017U (en) * | 2014-03-19 | 2014-09-24 | 北京中飞艾维航空科技有限公司 | Unmanned aerial vehicle provided with night navigation lamp |
| CN204383758U (en) * | 2014-12-03 | 2015-06-10 | 成都群侠科技有限公司 | One is applicable to boisterous unmanned plane |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104843193A (en) * | 2015-05-13 | 2015-08-19 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle lamplight warning system |
| CN105217050A (en) * | 2015-10-27 | 2016-01-06 | 杨珊珊 | A kind of unmanned vehicle being convenient to observe |
| CN109367803A (en) * | 2018-09-29 | 2019-02-22 | 国网浙江省电力有限公司 | Suitable for boisterous multi-functional unmanned plane |
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Application publication date: 20150218 |