CN205311906U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN205311906U CN205311906U CN201521047113.3U CN201521047113U CN205311906U CN 205311906 U CN205311906 U CN 205311906U CN 201521047113 U CN201521047113 U CN 201521047113U CN 205311906 U CN205311906 U CN 205311906U
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- unmanned plane
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- solar cells
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model discloses an unmanned aerial vehicle, including the casing, set up energy supply module in the casing, unmanned aerial vehicle is still including setting up thin -film solar cell on the casing surface energy supply module can't for the state of unmanned aerial vehicle power supply, do after the thin -film solar cell energy storage the unmanned aerial vehicle power supply. When this unmanned aerial vehicle took place to crash the accident, along with the passage of time, the original electric power deposit (being energy supply module ) on this unmanned aerial vehicle was slowly depleted, and energy supply module can't provide the electric energy for unmanned aerial vehicle promptly. The last thin -film solar cell of unmanned aerial vehicle absorbs solar energy to save solar energy conversion for the electric energy. Thin -film solar cell just can provide the electric energy for unmanned aerial vehicle like this.
Description
Technical field
This utility model relates to unmanned plane field, particularly relates to a kind of unmanned plane.
Background technology
Unmanned plane enjoyed various countries to favor in the last few years, the military field such as it can be not only used for battlefield surveillance, give warning in advance, and more had broad application prospects at civil area. It can carry high-resolution visible ray or ir imaging system, can easily enter the area that the mankind cannot arrive at and carry out aerial reconnaissance and aerophotography, it is possible to is used for carrying out mapping, disaster surveillance etc.
Unmanned plane generally will in the wild remote districts execution task, but lost efficacy (between unmanned plane and monitor terminal communication abnormality) due to the accident of Data-Link or (caused crashing as unmanned plane and other object collide) under other emergency case, causing unmanned plane loss out of control. After unmanned plane occurs crash surprisingly to cause loss, power reserve meeting exhaustion on unmanned plane, cause unmanned plane automatically to fly back or unmanned plane cannot pass its positional information back monitor terminal, therefore, people need manually to recover unmanned plane, but it is extremely difficult for finding unmanned plane in the wild, it is necessary to spend substantial amounts of manpower and materials.
Foregoing is only used for assisting understanding the technical solution of the utility model, does not represent and admits that foregoing is prior art.
Utility model content
Main purpose of the present utility model is in that to provide one unmanned plane, it is intended to solve in prior art, and unmanned plane is after occurring crash surprisingly to cause loss, when the power reserve exhaustion of unmanned plane, it is impossible to automatically recover the technological deficiency of unmanned plane.
For achieving the above object, this utility model provides a kind of unmanned plane, including housing, it is arranged on the power module in described housing, described unmanned plane also includes the thin-film solar cells being arranged in described housing outer surface, power for described unmanned plane after the state that described power module cannot be powered for described unmanned plane, described thin-film solar cells accumulation of energy.
Preferably, described thin-film solar cells covers described housing.
Preferably, described unmanned plane also include being arranged in described housing, for detecting the selftest module of the status information of described unmanned plane, described thin-film solar cells is that described selftest module is powered, and the status information of the unmanned plane that described selftest module detects is sent to monitor terminal by the communication module of described unmanned plane.
Preferably, described unmanned plane also includes accepting the alarm module that described thin-film solar cells is powered, and described alarm module is connected with described selftest module with the testing result alert according to described selftest module.
Preferably, described alarm module is light crossing-signal or voice guard.
Preferably, described thin-film solar cells is the power plant module of described unmanned plane and navigation module is powered. Preferably, described thin-film solar cells is that the communication module of described unmanned plane is powered.
Preferably, described thin-film solar cells is the communication module of described unmanned plane and positional information acquisition module is powered.
Preferably, described unmanned plane also include carry on housing, accept the video camera that described thin-film solar cells is powered, the photo that described video camera shoots is sent to monitor terminal by the communication module of described unmanned plane.
Unmanned plane disclosed in the utility model, including the functional module being arranged in housing and be arranged on the thin-film solar cells in housing outer surface, when this unmanned plane occurs to crash unexpected, as time goes by, original power reserve (i.e. power module) slowly exhaustion on this unmanned plane, namely power module cannot provide electric energy for unmanned plane. Thin-film solar cells on unmanned plane absorbs solar energy, and converts the solar into electric energy and store. Such thin-film solar cells just can provide electric energy for unmanned plane.
Accompanying drawing explanation
Fig. 1 is the schematic perspective view of this utility model unmanned plane.
The realization of this utility model purpose, functional characteristics and advantage will in conjunction with the embodiments, are described further with reference to accompanying drawing.
Detailed description of the invention
Should be appreciated that specific embodiment described herein is only in order to explain this utility model, be not used to limit this utility model.
With reference to Fig. 1, this utility model unmanned plane includes housing 10, power module, thin-film solar cells 20, controller, communication module, navigation module, positional information acquisition module (can also not want this module certainly when there being navigation module, this positional information acquisition module can be arranged as required to) and power plant module, wherein, power module, controller, communication module and positional information acquisition module are arranged in housing 10, thin-film solar cells 20 is arranged on the outer surface of housing 10, power plant module part is located at the inside of housing 10 and extends to housing 10 outside (because power plant module includes electricity tune, motor and blade, namely this place should be readily appreciated that). the annexation of power module, controller, communication module, positional information acquisition module, navigation module and power plant module each module above-mentioned with existing unmanned plane is identical, does not limit at this and repeats no more. thin-film solar cells 20 is arranged on the outer surface of housing 10 to receive solar energy and to store, and with the state cannot powered for unmanned plane at power module, powers for unmanned plane.
Common, when unmanned plane occurs to crash unexpected, it is possible to drop local at each, as dropped in the tree, grassland first-class, as long as this unmanned function is shined upon, the thin-film solar cells 20 on this unmanned plane just can absorb solar energy. When this unmanned plane occurs to crash unexpected, as time goes by, original power reserve (i.e. power module) the slowly exhaustion on this unmanned plane, namely power module cannot provide electric energy for unmanned plane. Thin-film solar cells 20 on unmanned plane absorbs solar energy, and converts the solar into electric energy and store. Such thin-film solar cells 20 just can provide electric energy for unmanned plane.
When the depleted of energy of crash accident and its supply module occurs unmanned plane, can be powered for unmanned plane by the thin-film solar cells 20 on housing 10 surface, in order to recover unmanned plane. As this thin-film solar cells 20 is powered for power plant module and navigation module, in order to this unmanned plane can homeward to or close to the position of takeoff point. For another example this thin-film solar cells 20 is communication module, positional information acquisition module powers, in order to this unmanned plane can send position information to monitor terminal, when obtaining the position of unmanned plane, conveniently recovers unmanned plane. Additionally, this thin-film solar cells 20 can be also power plant module, navigation module is powered and communication module is powered, in order to its information can be sent to monitor terminal while this unmanned plane is homeward. Wherein, monitor terminal can be earth station or smart mobile phone etc., and namely by this monitor terminal, user can view where unmanned plane crashes, and namely where unmanned plane is lost in. User, after the positional information being viewed unmanned plane by this monitor terminal, can determine it is physically go to recover unmanned plane or send instruction so that this unmanned plane flies back automatically to this unmanned plane according to practical situation.
In a preferred embodiment, thin-film solar cells 20 covers housing 10, then when this unmanned plane occurs to crash unexpected, no matter unmanned plane is the crash that faces up, or crashes upward in bottom surface, or crashes upward in side, this housing 10 there is thin-film solar cells 20 to be sunlighted, as when unmanned plane faces up crash, the thin-film solar cells 20 on the upper plate of this unmanned plane can be sunlighted, and converts solar energy into electric energy storage; When crashing upward in unmanned plane bottom surface, the thin-film solar cells 20 in the lower plate of this unmanned plane can be sunlighted, and converts solar energy into electric energy storage; When crashing upward in unmanned plane side, the thin-film solar cells 20 on the connecting plate of this unmanned plane can be sunlighted, and converts solar energy into electric energy storage.
Further, this unmanned plane also includes the selftest module being arranged in housing 10, this selftest module is for detecting the status information of unmanned plane, wherein detecting the status information of unmanned plane and include but not limited to include whether detection power plant module is normal, whether the information about power of thin-film solar cells 20, navigation module be normal, whether positional information acquisition module is normal, this thin-film solar cells 20 is powered for selftest module. As when this unmanned plane occurs to crash unexpected, can this selftest module detects this unmanned plane start flight, then passes through communication module and testing result is sent to monitor terminal. User can view the situation of unmanned plane by this monitor terminal, and to determine to adopt which kind of mode to recover this unmanned plane, if testing result is for can not start flight, then user can only physically go to crash place of this unmanned plane and fetch unmanned plane; As when testing result is for can start flight, then user can physically go to crash place of this unmanned plane and fetches or send control instruction by monitor terminal to this unmanned plane, starts flight to presetting destination controlling this unmanned plane.
Further, this unmanned plane also includes alarm module, and thin-film solar cells 20 is powered for this alarm module, and this warning message can be acoustic information and optical information, and this warning message can also be smog etc. If this voice guard is buzzer; For another example this light crossing-signal is LED, and this LED can be multiple, sends at unmanned plane and crashes unexpected, and this LED can be often bright or according to preset rules light on and off. This alarm module is connected with selftest module with according to testing result alert, and this warning message can be different according to the difference of testing result, and user, when viewing warning message, can know the position of unmanned plane easily, be quickly found out unmanned plane.
Further, this unmanned plane also includes the video camera arranged on the housing 10, the power supply of the acceptable thin-film solar cells 20 of this video camera, when this unmanned plane occurs to crash unexpected, video camera starts shooting photo, to shoot the environment residing for this unmanned plane, and by communication module, the photo that video camera shoots is sent to monitor terminal. User checks, by monitor terminal, the photo that unmanned plane sends, recognize the environment residing for this unmanned plane, can determine which kind of mode of employing fetches this unmanned plane more accurately, photo as shot by video camera as user is viewed this unmanned plane and crashes on a big tree or on steep cliff, improper artificially going is fetched, then user can send auto-returned instruction by monitor terminal to unmanned plane so that this unmanned plane is auto-returned after receiving auto-returned instruction.
These are only preferred embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every equivalent structure utilizing this utility model description and accompanying drawing content to make or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical fields, all in like manner include in scope of patent protection of the present utility model.
Claims (9)
1. a unmanned plane, including housing, it is arranged on the power module in described housing, it is characterized in that, described unmanned plane also includes the thin-film solar cells being arranged in described housing outer surface, power for described unmanned plane after the state that described power module cannot be powered for described unmanned plane, described thin-film solar cells accumulation of energy.
2. unmanned plane as claimed in claim 1, it is characterised in that described thin-film solar cells covers described housing.
3. unmanned plane as claimed in claim 1 or 2, it is characterized in that, described unmanned plane also include being arranged in described housing, for detecting the selftest module of the status information of described unmanned plane, described thin-film solar cells is that described selftest module is powered, and the status information of the unmanned plane that described selftest module detects is sent to monitor terminal by the communication module of described unmanned plane.
4. unmanned plane as claimed in claim 3, it is characterized in that, described unmanned plane also includes accepting the alarm module that described thin-film solar cells is powered, and described alarm module is connected with described selftest module with the testing result alert according to described selftest module.
5. unmanned plane as claimed in claim 4, it is characterised in that described alarm module is light crossing-signal or voice guard.
6. unmanned plane as claimed in claim 1 or 2, it is characterised in that described thin-film solar cells is the power plant module of described unmanned plane and navigation module is powered.
7. unmanned plane as claimed in claim 6, it is characterised in that the communication module that described thin-film solar cells is described unmanned plane is powered.
8. unmanned plane as claimed in claim 1 or 2, it is characterised in that described thin-film solar cells is the communication module of described unmanned plane and positional information acquisition module is powered.
9. unmanned plane as claimed in claim 1 or 2, it is characterized in that, described unmanned plane also include carry on housing, accept the video camera that described thin-film solar cells is powered, the photo that described video camera shoots is sent to monitor terminal by the communication module of described unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521047113.3U CN205311906U (en) | 2015-12-15 | 2015-12-15 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521047113.3U CN205311906U (en) | 2015-12-15 | 2015-12-15 | Unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN205311906U true CN205311906U (en) | 2016-06-15 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201521047113.3U Active CN205311906U (en) | 2015-12-15 | 2015-12-15 | Unmanned aerial vehicle |
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| CN (1) | CN205311906U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018076467A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and alarm system thereof |
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2015
- 2015-12-15 CN CN201521047113.3U patent/CN205311906U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018076467A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and alarm system thereof |
| CN109564735A (en) * | 2016-10-31 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned plane and its alarm system |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20191210 Address after: Room 812, enterprise service center, No. 17, section 3, west section of Changjiang North Road, Lingang Economic Development Zone, Yibin City, Sichuan Province Patentee after: Sichuan Yidian Aviation Technology Co., Ltd Address before: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee before: Shenzhen Yidian Aviation Technology Co., Ltd. |
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| TR01 | Transfer of patent right |