CN205203380U - Adopt gaseous unmanned vehicles who increases continuation of journey - Google Patents
Adopt gaseous unmanned vehicles who increases continuation of journey Download PDFInfo
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- CN205203380U CN205203380U CN201521004911.8U CN201521004911U CN205203380U CN 205203380 U CN205203380 U CN 205203380U CN 201521004911 U CN201521004911 U CN 201521004911U CN 205203380 U CN205203380 U CN 205203380U
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- unmanned vehicle
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Abstract
The utility model discloses an adopt gaseous unmanned vehicles who increases continuation of journey, unmanned vehicles includes unmanned vehicles host computer and rotor, the rotor with unmanned vehicles host computer horizontally connect, the rotor with unmanned vehicles host computer horizontally connect, unmanned vehicles still includes gas device, gas device set up in the upper surface of unmanned vehicles host computer, wherein: the rotor is in do under the control of unmanned vehicles host computer unmanned vehicles provides flight power, gas device is used for producing buoyancy to make unmanned vehicles suspends in aerial in order to increase unmanned vehicles continuation of the journey aloft. The utility model discloses increase duration in the time of can making unmanned vehicles aloft, guarantee unmanned vehicles perform tasks's continuity, shorten the time that unmanned vehicles finished the work, improved the efficiency that the task was carried out.
Description
Technical field
The utility model relates to unmanned vehicle field, particularly relates to a kind of unmanned vehicle adopting gas to increase continuation of the journey.
Background technology
Unmanned vehicle 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 vehicle 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 vehicle and industry is the real firm need of unmanned vehicle.At present taking photo by plane, agricultural plant protection, the field such as mapping application, expanded the purposes of unmanned vehicle itself greatly.
But, the flying power of current unmanned vehicle is generally not enough, is generally between half an hour to one hour, during to perform long airflight, the unavoidable situation occurring continuation of the journey deficiency, such as, 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 vehicle is executed the task, added the time that unmanned vehicle is finished the work.
Utility model content
Main purpose of the present utility model is to provide a kind of unmanned vehicle adopting gas to increase continuation of the journey, is intended to the product defects solving the aerial flying power deficiency of existing unmanned vehicle.
For achieving the above object, the utility model provides a kind of unmanned vehicle adopting gas to increase continuation of the journey, described unmanned vehicle comprises unmanned vehicle main frame and rotor, described rotor is connected with described unmanned vehicle host horizontal, described rotor is connected with described unmanned vehicle host horizontal, described unmanned vehicle also comprises gas device, and described gas device is arranged at the upper surface of described unmanned vehicle main frame, wherein:
Described rotor under the control of described unmanned vehicle main frame for described unmanned vehicle provides flying power;
It is aerial to increase the skyborne continuation of the journey of unmanned vehicle that described gas device makes described unmanned vehicle be suspended in for generation of buoyancy.
Preferably, described gas device comprises cylinder, the first gas courage, the second gas courage, the fine arm of the first carbon, the fine arm of the second carbon and the fine main tracheae of carbon, and described cylinder is equipped with the high pressure gas lower than density of air.
Preferably, the fine main tracheae of described carbon is arranged in described cylinder, the fine main tracheae of this carbon is arranged the fine arm of described first carbon and the fine arm of the second carbon, described first gas courage is fixed on the fine arm of described first carbon, and described second gas courage is fixed on the fine arm of described second carbon.
Preferably, described gas device comprises the first air valve and the second air valve, wherein, the fine arm of described first carbon arranges described first air valve, the fine arm of described second carbon arranges described second air valve.
Preferably, described gas device comprises the first control line, the second control line, the 3rd control line and control setup, first control line, the second control line, the 3rd control line are connected with described control setup, described cylinder is connected with described control setup, and described control setup is connected with unmanned vehicle main frame.
Preferably, the top of the fine main tracheae of described carbon arranges blow off valve, and wherein, described first control line is connected with described blow off valve, and described second control line is also connected with described first air valve, and described 3rd control line is also connected with the second air valve.
Preferably, described rotor comprises hold-down arm, motor and by motor-driven screw propeller.
Preferably, one end of described hold-down arm connects described unmanned vehicle main frame, and the other end of described hold-down arm fixes described motor, and described screw propeller is arranged on the top of described motor.
Preferably, described unmanned vehicle arranges foot rest, and described foot rest is arranged at the lower surface of described unmanned vehicle main frame.
Preferably, arrange battery in described unmanned vehicle main frame, this battery is rotor and the unmanned vehicle host supplying power of unmanned vehicle.
Compared to prior art, the unmanned vehicle that employing gas described in the utility model increases continuation of the journey makes the unmanned vehicle of airflight reduce energy resource consumption by increasing gas device, thus be aloft that unmanned vehicle increases continuation of the journey in flight course, and when the buoyancy that gas device produces equals the weight of unmanned vehicle, can be suspended in aerial for a long time, ensure that the continuity that unmanned vehicle is executed the task, shorten the time that unmanned vehicle is finished the work, improve the efficiency of tasks carrying.
Accompanying drawing explanation
Fig. 1 is that the utility model adopts gas to increase the planar structure schematic diagram of the unmanned vehicle preferred embodiment of continuation of the journey;
Fig. 2 is that the utility model adopts gas to increase the three-dimensional structure diagram of the unmanned vehicle preferred embodiment of continuation of the journey;
Fig. 3 is that the utility model adopts gas to increase the structural representation of the preferred embodiment of gas device in the unmanned vehicle of continuation of the journey.
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, detailed description of the invention of the present utility model, structure, feature and effect thereof are described in detail.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 adopts gas to increase the planar structure schematic diagram of the unmanned vehicle preferred embodiment of continuation of the journey.As shown in Figure 2, Fig. 2 is that the utility model adopts gas to increase the three-dimensional structure diagram of the unmanned vehicle preferred embodiment of continuation of the journey.
In the present embodiment, described unmanned vehicle 100 include but not limited to, unmanned vehicle main frame 20, multiple rotor 30 (such as, four rotors), gas device 40 and multiple foot rest 50 (such as, two foot rests).
Described unmanned vehicle main frame 20 is for controlling the flight of unmanned vehicle 100.
Described unmanned vehicle main frame 20 is connected with described rotor 30, gas device 40 and foot rest 50.Specifically, described rotor 30 and described unmanned vehicle main frame 20 level connection joint, described gas device 40 is arranged at the upper surface of described unmanned vehicle main frame 20.Described foot rest 50 is arranged at the lower surface of described unmanned vehicle main frame 20.
Described rotor 30 provides flying power for described unmanned vehicle 100.
Described gas device 40 makes described unmanned vehicle 100 be suspended in the air for generation of buoyancy, to reduce the power capacity of unmanned vehicle 100 because consuming needed for gravity, thus increases the skyborne flying power of described unmanned vehicle 100.Described gas device 40 comprises cylinder 4, first gas courage 5, second gas courage 8 and the fine main tracheae 12 of carbon.Described cylinder 4 is for filling pressure gas (such as, hydrogen, pressure gas that nitrogen geometric ratio density of air is light).Described cylinder 4 is also for connecting described unmanned vehicle main frame 20 and the first gas courage 5, and the fine main tracheae 12 of described carbon also connects described first gas courage 5 and described second gas courage 8, and the fine main tracheae 12 of described carbon is also through described cylinder 4 in addition.Described first gas courage 5 and the second gas courage 8 are cirque structure.
Described foot rest 50 is for providing support for described unmanned vehicle 100 rests against ground.
The screw propeller 304 that each rotor 30 comprises hold-down arm 300, motor 302 and driven by motor 302.Unmanned vehicle main frame 20 described in one end level connection joint of described hold-down arm 300, the other end of described hold-down arm 300 fixes described motor 302, and the top of described motor 302 arranges described screw propeller 304.
Described unmanned vehicle 100 is a kind of small unmanned vehicles handled by radio robot or self process controller, such as, and the small-sized unmanned aircrafts such as unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned parasol.
Described unmanned vehicle 100 also comprises battery (not shown), and described battery is connected with described unmanned vehicle main frame 20, for described unmanned vehicle main frame 20 provides electric power.In addition, described battery is also connected with described rotor 30, for described rotor 30 provides electric power.
This battery can be installed on inside or the outside of described unmanned vehicle main frame 20.In other embodiments, described battery also can be arranged at described rotor 30 is set hold-down arm 300 on.Described battery may be, but not limited to, solar cell, chargeable battery (such as, lithium ion battery) etc.Described battery is that the rotor 30 of unmanned vehicle 100 and unmanned vehicle main frame 20 are powered.
As shown in Figure 3, Fig. 3 is that the utility model adopts gas to increase the structural representation of the preferred embodiment of gas device in the unmanned vehicle of continuation of the journey.
In the present embodiment, described gas device 40 comprises the first control line 1, second control line 2, the 3rd control line 3, cylinder 4 (compression hydrogen or nitrogen are housed), fine arm 9, second air valve 10 of the first gas courage 5, first carbon fine arm 6, first air valve 7, second gas courage 8, second carbon, blow off valve 11, the fine main tracheae 12 of carbon and control setup 13.
Wherein, described cylinder 4, built with the fine main tracheae 12 of carbon, the fine main tracheae 12 of carbon is equipped with the fine arm 6 of the first carbon and the fine arm 9 of the second carbon, the fine arm 6 of described first carbon arranges the first air valve 7, the fine arm 9 of described second carbon arranges the second air valve 10.Described first gas courage 5 is fixed on the fine arm 6 of described first carbon, and the fine arm 6 of described first carbon is cross-shaped configuration, and described second gas courage 8 is fixed on the fine arm 9 of described second carbon, and the fine arm 9 of described second carbon is cross-shaped configuration.The top of the fine main tracheae 12 of described carbon arranges blow off valve 11, first control line 1 is connected with described blow off valve 11, the second control line 2 is connected with described first air valve 7, described 3rd control line 3 is connected with the second air valve 10, the other end of the first control line 1, second control line 2 and the 3rd control line 3 is connected with control setup 13, described control setup 13 is arranged at the bottom of cylinder 4, and this control setup 13 is arranged at the surface of described unmanned vehicle main frame 20.
Described unmanned vehicle principle of work is as follows: described control setup 13 opens described first air valve 7 by the second control line 2, the second air valve 10 is opened by the 3rd control line 3, described cylinder 4 mesohigh gas inputs to the first gas courage 5 and the second gas courage 8, thus makes described first gas courage 5 and the second gas courage 8 inflation.Due to the buoyancy of described first gas courage 5 and the second gas courage 8, the consumption of electricity in battery can be reduced, thus add the continuation of the journey of unmanned vehicle 100.In addition, when the buoyancy of described first gas courage 5 and the second gas courage 8 equals the weight of unmanned vehicle 100, described control setup 13 disable motor 302 makes described screw propeller 304 stop the rotation, reduce the consumption of electricity in battery, unmanned vehicle 100 is in suspended state, meets unmanned vehicle 100 and is aloft working for a long time.
When unmanned vehicle 100 will return, by described control setup 13 starter motor 302, screw propeller is rotated, open blow off valve 11 by the first control line 1 to discharge to make the gas of the first gas courage 5 and the second gas courage 8, unmanned vehicle 100 returns to user appointed place according to control command simultaneously.
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 (10)
1. the unmanned vehicle adopting gas to increase continuation of the journey, described unmanned vehicle comprises unmanned vehicle main frame and rotor, described rotor is connected with described unmanned vehicle host horizontal, described rotor is connected with described unmanned vehicle host horizontal, it is characterized in that, described unmanned vehicle also comprises gas device, and described gas device is arranged at the upper surface of described unmanned vehicle main frame, wherein:
Described rotor under the control of described unmanned vehicle main frame for described unmanned vehicle provides flying power;
It is aerial to increase the skyborne continuation of the journey of unmanned vehicle that described gas device makes described unmanned vehicle be suspended in for generation of buoyancy.
2. the unmanned vehicle adopting gas to increase continuation of the journey as claimed in claim 1, it is characterized in that, described gas device comprises cylinder, the first gas courage, the second gas courage, the fine arm of the first carbon, the fine arm of the second carbon and the fine main tracheae of carbon, and described cylinder is equipped with the high pressure gas lower than density of air.
3. the unmanned vehicle adopting gas to increase continuation of the journey as claimed in claim 2, it is characterized in that, the fine main tracheae of described carbon is arranged in described cylinder, the fine main tracheae of this carbon is arranged the fine arm of described first carbon and the fine arm of the second carbon, described first gas courage is fixed on the fine arm of described first carbon, and described second gas courage is fixed on the fine arm of described second carbon.
4. the unmanned vehicle adopting gas to increase continuation of the journey as claimed in claim 3, it is characterized in that, described gas device comprises the first air valve and the second air valve, wherein, the fine arm of described first carbon arranges described first air valve, the fine arm of described second carbon arranges described second air valve.
5. the unmanned vehicle adopting gas to increase continuation of the journey as claimed in claim 4, it is characterized in that, described gas device comprises the first control line, the second control line, the 3rd control line and control setup, first control line, the second control line, the 3rd control line are connected with described control setup, described cylinder is connected with described control setup, and described control setup is connected with unmanned vehicle main frame.
6. the unmanned vehicle adopting gas to increase continuation of the journey as claimed in claim 5, it is characterized in that, the top of the fine main tracheae of described carbon arranges blow off valve, wherein, described first control line is connected with described blow off valve, described second control line is also connected with described first air valve, and described 3rd control line is also connected with the second air valve.
7. the as claimed in claim 1 unmanned vehicle adopting gas to increase continuation of the journey, is characterized in that, described rotor comprises hold-down arm, motor and by motor-driven screw propeller.
8. the unmanned vehicle adopting gas to increase continuation of the journey as claimed in claim 7, it is characterized in that, one end of described hold-down arm connects described unmanned vehicle main frame, and the other end of described hold-down arm fixes described motor, and described screw propeller is arranged on the top of described motor.
9. the employing gas as described in any one of claim 1 to 8 increases the unmanned vehicle of continuation of the journey, and it is characterized in that, described unmanned vehicle arranges foot rest, and described foot rest is arranged at the lower surface of described unmanned vehicle main frame.
10. the employing gas as described in any one of claim 1 to 8 increases the unmanned vehicle of continuation of the journey, and it is characterized in that, arrange battery in described unmanned vehicle main frame, this battery is rotor and the unmanned vehicle host supplying power of unmanned vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521004911.8U CN205203380U (en) | 2015-12-04 | 2015-12-04 | Adopt gaseous unmanned vehicles who increases continuation of journey |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521004911.8U CN205203380U (en) | 2015-12-04 | 2015-12-04 | Adopt gaseous unmanned vehicles who increases continuation of journey |
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| Publication Number | Publication Date |
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| CN205203380U true CN205203380U (en) | 2016-05-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201521004911.8U Expired - Fee Related CN205203380U (en) | 2015-12-04 | 2015-12-04 | Adopt gaseous unmanned vehicles who increases continuation of journey |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628246A (en) * | 2017-07-26 | 2018-01-26 | 青岛万祥如光机械技术研究有限公司 | A kind of unmanned plane line walking device |
| CN107697288A (en) * | 2017-07-26 | 2018-02-16 | 青岛万祥如光机械技术研究有限公司 | A kind of energy-saving unmanned plane |
| CN108255195A (en) * | 2018-01-19 | 2018-07-06 | 启迪国信科技有限公司 | Unmanned plane and UAV system |
-
2015
- 2015-12-04 CN CN201521004911.8U patent/CN205203380U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628246A (en) * | 2017-07-26 | 2018-01-26 | 青岛万祥如光机械技术研究有限公司 | A kind of unmanned plane line walking device |
| CN107697288A (en) * | 2017-07-26 | 2018-02-16 | 青岛万祥如光机械技术研究有限公司 | A kind of energy-saving unmanned plane |
| CN108255195A (en) * | 2018-01-19 | 2018-07-06 | 启迪国信科技有限公司 | Unmanned plane and UAV system |
| CN108255195B (en) * | 2018-01-19 | 2019-03-05 | 启迪国信科技有限公司 | Unmanned plane and UAV system |
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Legal Events
| Date | Code | Title | Description |
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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: 20160504 Termination date: 20191204 |