CN205168869U - A unmanned aerial vehicle control system for being air travel's unmanned aerial vehicle increase is continued a journey - Google Patents
A unmanned aerial vehicle control system for being air travel's unmanned aerial vehicle increase is continued a journey Download PDFInfo
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- CN205168869U CN205168869U CN201520935388.4U CN201520935388U CN205168869U CN 205168869 U CN205168869 U CN 205168869U CN 201520935388 U CN201520935388 U CN 201520935388U CN 205168869 U CN205168869 U CN 205168869U
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- unmanned plane
- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle control system for being air travel's unmanned aerial vehicle increase is continued a journey, this unmanned aerial vehicle control system include controlgear, an unmanned aerial vehicle and the 2nd unmanned aerial vehicle, controlgear passes through radio control an unmanned aerial vehicle and the 2nd unmanned aerial vehicle, an unmanned aerial vehicle includes an unmanned aerial vehicle host computer, telescopic link and continuation of the journey battery, the telescopic link sets up in the below of an unmanned aerial vehicle host computer, the continuation of the journey battery set up in the end of telescopic link, the 2nd unmanned aerial vehicle includes the 2nd unmanned aerial vehicle host computer, controlgear is used for control an unmanned aerial vehicle flies to the 2nd unmanned aerial vehicle top preset the position to the control telescopic link is followed predetermine position extension with the battery of will continuing a journey place in in the 2nd unmanned aerial vehicle host computer. The utility model discloses can guarantee unmanned aerial vehicle perform tasks's continuity aloft for unmanned aerial vehicle increases the continuation of the journey, shorten the time that unmanned aerial vehicle finished the work, improve the efficiency that the task was carried out.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, particularly relates to a kind of unmanned aerial vehicle control system for increasing continuation of the journey for the unmanned plane of airflight.
Background technology
Unmanned plane is a kind of based on radio telecommand or the not manned aircraft by self programming control.Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc.Unmanned plane can be divided into military and civilian by application.
Further, compared with manned aircraft, it has, and volume is little, cost is low, easy to use, to the advantage such as environmental requirement is low.The application of unmanned plane and industry is the real firm need of unmanned plane.At present taking photo by plane, agricultural plant protection, the field such as mapping application, expanded the purposes of unmanned plane itself greatly.
Such as, but when executing the task, there is the situation that continuation of the journey is not enough unavoidably, in unmanned plane, during mapping, because deficiency of continuing a journey must come back to the base the supplementary energy, thus, make tasks interrupt, cut off the continuity that unmanned plane is executed the task, added the time that unmanned plane is finished the work.
Utility model content
Main purpose of the present utility model is to provide a kind of unmanned aerial vehicle control system for increasing continuation of the journey for the unmanned plane of airflight, is intended to solve the problem that existing unmanned plane cannot increase continuation of the journey aloft.
For achieving the above object, the utility model provides a kind of unmanned aerial vehicle control system for increasing continuation of the journey for the unmanned plane of airflight, described unmanned aerial vehicle control system comprises control convenience, the first unmanned plane and the second unmanned plane, described control convenience controls described first unmanned plane and the second unmanned plane by radio communication, wherein:
Described first unmanned plane comprises described first unmanned plane main frame, expansion link and continuation of the journey battery, and wherein, described expansion link is arranged at the below of described first unmanned plane main frame, and described continuation of the journey battery is arranged at the end of described expansion link;
Described second unmanned plane comprises described second unmanned plane main frame; And
Described control convenience flies to predeterminated position above described second unmanned plane for controlling described first unmanned plane, and controls described expansion link and extend to be placed by described continuation of the journey battery and to be installed in described second unmanned plane main frame from described predeterminated position.
Preferably, arrange first control device in described control convenience, described first control device connects the first antenna.
Preferably, described first control device is by the flight of the first unmanned plane described in described first day line control.
Preferably, described first unmanned plane also comprises multiple hold-down arm, multiple motor and by motor-driven screw propeller, wherein, a hold-down arm, a motor and form a rotor by this motor-driven screw propeller, one end of each hold-down arm connects described first unmanned plane main frame, the other end of this hold-down arm fixes a motor, and the top of this motor arranges a screw propeller.
Preferably, arrange second control device in described control convenience, wherein, described second control device connects the second antenna.
Preferably, described second control device is by the flight of the second unmanned plane described in described second day line control.
Preferably, the upper surface of described second unmanned plane main frame also arranges a left side and to uncap and uncap in the right side.
Preferably, described second unmanned plane also comprises multiple hold-down arm, multiple motor and by motor-driven screw propeller, wherein, a hold-down arm, a motor and form a rotor by this motor-driven screw propeller, one end of each hold-down arm connects described second unmanned plane main frame, the other end of this hold-down arm fixes a motor, and the top of this motor arranges a screw propeller.
Compared to prior art, unmanned aerial vehicle control system for increasing continuation of the journey for the unmanned plane of airflight described in the utility model is by installing continuation of the journey battery for the unmanned plane of airflight, thus be aloft that unmanned plane increases continuation of the journey in flight course, ensure that the continuity that unmanned plane is executed the task, shorten the time that unmanned plane is finished the work, improve the efficiency of tasks carrying.
Accompanying drawing explanation
Fig. 1 is that the utility model is for increasing the structural representation of the unmanned aerial vehicle control system preferred embodiment of continuation of the journey for the unmanned plane of airflight;
The schematic diagram of the preferred embodiment of Fig. 2 when to be the utility model be in using state for the unmanned aerial vehicle control system increasing continuation of the journey for the unmanned plane of airflight.
The realization of the utility model object, functional characteristics and advantage will in conjunction with the embodiments, are described further with reference to accompanying drawing.
Detailed description of the invention
For further setting forth the utility model for the technological means reaching above-mentioned purpose and take and effect, below in conjunction with accompanying drawing and preferred embodiment, describe in detail bright to detailed description of the invention of the present utility model, structure, feature and effect thereof.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.
As shown in Figure 1, Fig. 1 is that the utility model is for increasing the structural representation of the unmanned aerial vehicle control system preferred embodiment of continuation of the journey for the unmanned plane of airflight.In the present embodiment, described Unmanned Aircraft Systems (UAS) includes, but not limited to control convenience 1, first unmanned plane 2 and the second unmanned plane 3.Described control convenience 1 controls described first unmanned plane 2 and the second unmanned plane 3 by radio communication.
Specifically, arrange first control device 10 and second control device 12 in described control convenience 1, wherein, described first control device 10 connects the first antenna 100, and described second control device 12 connects the second antenna 120.Described first control device 10 is communicated with described first unmanned plane 2 by described first antenna 100, for controlling the flight of described first unmanned plane 2.Described second control device 12 is communicated with described second unmanned plane 3 by described second antenna 120, for controlling the flight of described second unmanned plane 3.
Described first unmanned plane 2 comprises, but be not limited only to, described first unmanned plane main frame 20, multiple hold-down arm 21, multiple motor 22 and the screw propeller 23 driven by motor 22, multiple foot rest 24 (such as, two foot rests), expansion link 25 and continuation of the journey battery 26.
A hold-down arm 21, motor 22 and the screw propeller 23 driven by this motor 22 form the rotor of first unmanned plane 2, one end of each hold-down arm 20 connects described first unmanned plane main frame 20, the other end of this hold-down arm 20 fixes a motor 22, and the top of this motor 22 arranges a screw propeller 24.
The rotor of described first unmanned plane 2 provides flying power for described first unmanned plane 2.
Described unmanned plane main frame 20 is also connected with foot rest 24 and expansion link 25.Specifically, described foot rest 24 and described expansion link 25 are arranged at the below of described first unmanned plane main frame 20.Described continuation of the journey battery 26 is arranged at the end of described expansion link 25.
Described foot rest 24 is for providing support for described first unmanned plane 2 rests against ground.
Described expansion link 25 can stretch the relative position (as shown in Figure 2) regulating described continuation of the journey battery 26 and described first unmanned plane 2, so that described continuation of the journey battery 26 is put into described second unmanned plane 3, thus be aloft that described second unmanned plane 3 increases continuation of the journey.
Described continuation of the journey battery 26 is chargeable batteries of a kind of Low emissivity, low-power consumption.Described continuation of the journey battery 26 is also connected with a charging port (not shown).This charging port can be the battery charging inlet of a kind of USB interface or other standard, and this charging port directly can insert on external power supply (such as computer USB interface or low pressure voltage stabilizer etc.) and charge to described continuation of the journey battery 26.When the electricity of described continuation of the journey battery 26 is finished, user charges to continuation of the journey battery 26 by described charging port.
It should be noted that, also arrange built-in battery (not shown in figure 1) in described first unmanned plane main frame 20, this built-in battery provides electric energy for described first unmanned plane 2.
Described second unmanned plane 3 include but not limited to, described second unmanned plane main frame 30, multiple hold-down arm 30, multiple motor 32 and the screw propeller 33 driven by motor 32 and multiple foot rest 34 (such as, two foot rests).
A hold-down arm 31, motor 32 and the screw propeller 33 driven by this motor 32 form the rotor of second unmanned plane 3, one end of each hold-down arm 30 connects described second unmanned plane main frame 30, the other end of this hold-down arm 30 fixes a motor 32, and the top of this motor 32 arranges described screw propeller 34.
The rotor of described second unmanned plane 3 provides flying power for described second unmanned plane 3.
Described unmanned plane main frame 30 is also connected with foot rest 34.
Described foot rest 34 is for providing support for described second unmanned plane 3 rests against ground.
Further, as shown in Figure 2, the upper surface of described second unmanned plane main frame 30 also arrange a left side uncap 301 and the right side uncap 302, open a described left side uncap 301 and the right side uncap after 302, described continuation of the journey battery 26 can be placed and is installed in described second unmanned plane main frame 30.
The first described unmanned plane 2 and the second unmanned plane 3 are a kind of small unmanned vehicles handled by radio robot or self process controller, the SUAV (small unmanned aerial vehicle) such as such as unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned parasol.
As shown in Figure 2, the schematic diagram of the preferred embodiment of Fig. 2 when to be the utility model be in using state for the unmanned aerial vehicle control system increasing continuation of the journey for the unmanned plane of airflight.
When described second unmanned plane 3 is continued a journey under power, when needing to increase continuation of the journey power, the second control device 12 of described control convenience 1 controls described second unmanned plane 3 and hovers and obtain geographic position when described second unmanned plane 3 hovers, the first control device 10 of described control convenience 1 controls described first unmanned plane 2 according to described geographic position and flies to predeterminated position above described second unmanned plane 3 and this estimated location that hovers, described first unmanned plane 2 extends described expansion link 25, the left side controlling the second unmanned plane main frame 30 by described second control device 12 uncap 301 and the right side uncap and 302 automatically to open, and the continuation of the journey battery 26 of described expansion link 25 end is put into described second unmanned plane main frame 30.Described continuation of the journey battery 26 is put into and after being arranged on described second unmanned plane main frame 30, described expansion link 25 disconnects with described continuation of the journey battery 26, and this expansion link 25 shrinks back described first unmanned plane main frame 20.
It should be noted that, when described second unmanned plane main frame 30 put into by described continuation of the journey battery 26, the electrical lead in described second unmanned plane main frame 30 is connected to described continuation of the journey battery 26, to obtain the electric energy of described continuation of the journey battery 26.
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 utilize the utility model specification sheets and accompanying drawing content to do equivalent structure or equivalent function conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (8)
1. one kind increases the unmanned aerial vehicle control system of continuing a journey for the unmanned plane for airflight, it is characterized in that, described unmanned aerial vehicle control system comprises control convenience, the first unmanned plane and the second unmanned plane, described control convenience controls described first unmanned plane and the second unmanned plane by radio communication, wherein:
Described first unmanned plane comprises described first unmanned plane main frame, expansion link and continuation of the journey battery, and wherein, described expansion link is arranged at the below of described first unmanned plane main frame, and described continuation of the journey battery is arranged at the end of described expansion link;
Described second unmanned plane comprises described second unmanned plane main frame; And
Described control convenience flies to predeterminated position above described second unmanned plane for controlling described first unmanned plane, and controls described expansion link and extend to be placed by described continuation of the journey battery and to be installed in described second unmanned plane main frame from described predeterminated position.
2., as claimed in claim 1 for increasing the unmanned aerial vehicle control system of continuation of the journey for the unmanned plane of airflight, it is characterized in that, arrange first control device in described control convenience, described first control device connects the first antenna.
3., as claimed in claim 2 for increasing the unmanned aerial vehicle control system of continuation of the journey for the unmanned plane of airflight, it is characterized in that, described first control device is by the flight of the first unmanned plane described in described first day line control.
4. as claimed in claim 1 for increasing the unmanned aerial vehicle control system of continuation of the journey for the unmanned plane of airflight, it is characterized in that, described first unmanned plane also comprises multiple hold-down arm, multiple motor and by motor-driven screw propeller, wherein, a hold-down arm, a motor and form a rotor by this motor-driven screw propeller, one end of each hold-down arm connects described first unmanned plane main frame, and the other end of this hold-down arm fixes a motor, and the top of this motor arranges a screw propeller.
5., as claimed in claim 1 for increasing the unmanned aerial vehicle control system of continuation of the journey for the unmanned plane of airflight, it is characterized in that, arrange second control device in described control convenience, wherein, described second control device connects the second antenna.
6., as claimed in claim 5 for increasing the unmanned aerial vehicle control system of continuation of the journey for the unmanned plane of airflight, it is characterized in that, described second control device is by the flight of the second unmanned plane described in described second day line control.
7. as claimed in claim 1 increase the unmanned aerial vehicle control system of continuing a journey for the unmanned plane for airflight, it is characterized in that, the upper surface of described second unmanned plane main frame also arranges a left side and to uncap and uncap in the right side.
8. the unmanned aerial vehicle control system for increasing continuation of the journey for the unmanned plane of airflight as described in claim 1 or 7, it is characterized in that, described second unmanned plane also comprises multiple hold-down arm, multiple motor and by motor-driven screw propeller, wherein, a hold-down arm, a motor and form a rotor by this motor-driven screw propeller, one end of each hold-down arm connects described second unmanned plane main frame, the other end of this hold-down arm fixes a motor, and the top of this motor arranges a screw propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520935388.4U CN205168869U (en) | 2015-11-21 | 2015-11-21 | A unmanned aerial vehicle control system for being air travel's unmanned aerial vehicle increase is continued a journey |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520935388.4U CN205168869U (en) | 2015-11-21 | 2015-11-21 | A unmanned aerial vehicle control system for being air travel's unmanned aerial vehicle increase is continued a journey |
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| Publication Number | Publication Date |
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| CN205168869U true CN205168869U (en) | 2016-04-20 |
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| CN201520935388.4U Expired - Fee Related CN205168869U (en) | 2015-11-21 | 2015-11-21 | A unmanned aerial vehicle control system for being air travel's unmanned aerial vehicle increase is continued a journey |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106596551A (en) * | 2016-12-19 | 2017-04-26 | 重庆信首科技有限公司 | Disease and insect pest monitoring device based on unmanned aerial vehicle |
| CN107323674A (en) * | 2017-06-21 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of strong unmanned plane of endurance |
| CN110683051A (en) * | 2018-07-04 | 2020-01-14 | 保时捷股份公司 | Power supply system for an aircraft and corresponding aircraft |
-
2015
- 2015-11-21 CN CN201520935388.4U patent/CN205168869U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106596551A (en) * | 2016-12-19 | 2017-04-26 | 重庆信首科技有限公司 | Disease and insect pest monitoring device based on unmanned aerial vehicle |
| CN107323674A (en) * | 2017-06-21 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of strong unmanned plane of endurance |
| CN107323674B (en) * | 2017-06-21 | 2019-10-08 | 胡方娟 | A kind of unmanned plane that cruising ability is strong |
| CN110683051A (en) * | 2018-07-04 | 2020-01-14 | 保时捷股份公司 | Power supply system for an aircraft and corresponding aircraft |
| CN110683051B (en) * | 2018-07-04 | 2023-05-09 | 保时捷股份公司 | Electric power supply system for an aircraft and corresponding aircraft |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160420 Termination date: 20201121 |