CN204383758U - One is applicable to boisterous unmanned plane - Google Patents
One is applicable to boisterous unmanned plane Download PDFInfo
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- CN204383758U CN204383758U CN201420747986.4U CN201420747986U CN204383758U CN 204383758 U CN204383758 U CN 204383758U CN 201420747986 U CN201420747986 U CN 201420747986U CN 204383758 U CN204383758 U CN 204383758U
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- unmanned plane
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- led lamp
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- 239000003973 paint Substances 0.000 claims abstract description 6
- 239000003086 colorant Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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Abstract
The utility model relates to one and is applicable to boisterous unmanned plane, comprise unmanned plane body and control panel, described unmanned plane body comprises head and tail, 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 waterproof lampshade, described head is also provided with screw propeller, screw propeller scribbles fluorescent paint layer.The unmanned plane of the utility model design can use under the mal-condition such as rainy day, greasy weather, and operating personal can distinguish the service direction of unmanned plane clearly, has and widely uses value.
Description
Technical field
The utility model relates to flight equipment technical field, is specifically related to one and is 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.
Utility model content
Technical problem to be solved in the utility model 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 utility model provides following technical scheme: one is applicable to boisterous unmanned plane, comprises unmanned plane body and control panel, and 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 utility model 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 utility model is novel in design, and structure rationally, operates simple and easy, has market outlook widely.
Accompanying drawing explanation
Fig. 1 is the utility model integral structure schematic diagram;
Fig. 2 is the structural representation of the utility model mixing LED group.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
In description of the present utility model, it will be appreciated that, term " longitudinal direction ", " transverse direction ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end ", " interior ", orientation or the position relationship of the instruction such as " outward " are based on orientation shown in the drawings or position relationship, it is only the utility model 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 restriction of the present utility model.
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 utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
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 |
|---|---|---|---|
| CN201420747986.4U CN204383758U (en) | 2014-12-03 | 2014-12-03 | One is applicable to boisterous unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420747986.4U CN204383758U (en) | 2014-12-03 | 2014-12-03 | One is applicable to boisterous unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204383758U true CN204383758U (en) | 2015-06-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420747986.4U Active CN204383758U (en) | 2014-12-03 | 2014-12-03 | One is applicable to boisterous unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204383758U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354872A (en) * | 2014-12-03 | 2015-02-18 | 成都群侠科技有限公司 | Unmanned airplane suitable for severe weather |
| CN105551280A (en) * | 2016-03-09 | 2016-05-04 | 武汉博感空间科技有限公司 | Unmanned aerial vehicle traffic signal indicating system |
| WO2017166716A1 (en) * | 2016-03-30 | 2017-10-05 | 乐视控股（北京）有限公司 | Aircraft |
-
2014
- 2014-12-03 CN CN201420747986.4U patent/CN204383758U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354872A (en) * | 2014-12-03 | 2015-02-18 | 成都群侠科技有限公司 | Unmanned airplane suitable for severe weather |
| CN105551280A (en) * | 2016-03-09 | 2016-05-04 | 武汉博感空间科技有限公司 | Unmanned aerial vehicle traffic signal indicating system |
| WO2017166716A1 (en) * | 2016-03-30 | 2017-10-05 | 乐视控股（北京）有限公司 | Aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: SHANXI DEVELOP TECHNOLOGY LTD. Free format text: FORMER OWNER: CHENGDU QUNXIA TECHNOLOGY CO., LTD. Effective date: 20150603 |
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| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 610041 CHENGDU, SICHUAN PROVINCE TO: 030006 TAIYUAN, SHAANXI PROVINCE |
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| TR01 | Transfer of patent right |
Effective date of registration: 20150603 Address after: 313, room 249, 030006 Changzhi Road, Taiyuan hi tech Zone, Shanxi, China Patentee after: SHANXI DOP TECHNOLOGY CO.,LTD. Address before: The middle Tianfu Avenue in Chengdu city Sichuan province 610041 No. 1388 1 4 storey building No. 417 Patentee before: CHENGDU QUNXIA TECHNOLOGY Co.,Ltd. |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Unmanned airplane suitable for severe weather Effective date of registration: 20200102 Granted publication date: 20150610 Pledgee: Shanxi Financing Reinsurance Group Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY CO.,LTD. Registration number: Y2019980001434 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210601 Granted publication date: 20150610 Pledgee: Shanxi Financing Reinsurance Group Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY Co.,Ltd. Registration number: Y2019980001434 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A UAV suitable for bad weather Effective date of registration: 20210830 Granted publication date: 20150610 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY Co.,Ltd. Registration number: Y2021140000031 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20220905 Granted publication date: 20150610 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY CO.,LTD. Registration number: Y2021140000031 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A drone suitable for severe weather Effective date of registration: 20220908 Granted publication date: 20150610 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY CO.,LTD. Registration number: Y2022140000049 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230913 Granted publication date: 20150610 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: SHANXI DOP TECHNOLOGY CO.,LTD. Registration number: Y2022140000049 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right |