CN115405144A - A full-automatic airport for open-air electric power unmanned aerial vehicle that cruises - Google Patents
A full-automatic airport for open-air electric power unmanned aerial vehicle that cruises Download PDFInfo
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- CN115405144A CN115405144A CN202211003452.6A CN202211003452A CN115405144A CN 115405144 A CN115405144 A CN 115405144A CN 202211003452 A CN202211003452 A CN 202211003452A CN 115405144 A CN115405144 A CN 115405144A
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- airport
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- aerial vehicle
- air outlet
- cover body
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- 238000009434 installation Methods 0.000 claims abstract description 10
- 238000005057 refrigeration Methods 0.000 claims abstract description 6
- 238000009423 ventilation Methods 0.000 claims description 6
- 230000000694 effects Effects 0.000 abstract description 3
- 239000000203 mixture Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- 230000017525 heat dissipation Effects 0.000 description 4
- 230000005611 electricity Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
- E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04F—FINISHING WORK ON BUILDINGS, e.g. STAIRS, FLOORS
- E04F10/00—Sunshades, e.g. Florentine blinds or jalousies; Outside screens; Awnings or baldachins
- E04F10/08—Sunshades, e.g. Florentine blinds or jalousies; Outside screens; Awnings or baldachins of a plurality of similar rigid parts, e.g. slabs, lamellae
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
- F24F5/00—Air-conditioning systems or apparatus not covered by F24F1/00 or F24F3/00, e.g. using solar heat or combined with household units such as an oven or water heater
- F24F5/0007—Air-conditioning systems or apparatus not covered by F24F1/00 or F24F3/00, e.g. using solar heat or combined with household units such as an oven or water heater cooling apparatus specially adapted for use in air-conditioning
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Traffic Control Systems (AREA)
Abstract
The utility model provides a full-automatic airport for open-air electric power unmanned aerial vehicle that cruises, it relates to a full-automatic airport. The invention aims to solve the problem that the existing airport for the unmanned aerial vehicle to stop is easy to damage the unmanned aerial vehicle due to the fact that rain and snow enter after an upper cover is opened when the unmanned aerial vehicle stops and charges the unmanned aerial vehicle. Two upper covers of the invention can be horizontally and oppositely arranged on the upper end surface of an airport body in an openable way, the lower end surface of one upper cover is provided with an installation groove, a refrigeration air outlet net is arranged in the installation groove, a refrigerator is arranged on the outer side of the airport body in the width direction, the refrigerator leads cold air into the installation groove through a pipeline and discharges the cold air from the refrigeration air outlet net to cool the inside of the airport body; the stand is installed in airport body length direction's the positive middle outside, and the telescoping cylinder is installed on the up end of stand, and the sleet cover body is installed at the flexible end of telescoping cylinder, and the sleet cover body realizes the lid dress to two upper covers intersection under the effect of telescoping cylinder. The invention is used for charging and parking of the unmanned aerial vehicle.
Description
Technical Field
The invention relates to a full-automatic airport, in particular to a full-automatic airport for a field electric cruise unmanned aerial vehicle.
Background
In 2003, the demand of a power grid in China begins to rapidly rise, the social power consumption is increased explosively, and data show that the annual compound acceleration rate of the power consumption of the whole society in China reaches 12% in 2003-2010. With the explosive growth of demand, the installed capacity of electric power in China is rapidly expanded. In 2003-2008, the generating and loading amount of China is increased from 3.91 hundred million kilowatt hours to 7.93 hundred million kilowatts, the total loading amount is doubled, and in 2020, the total loading amount of the generating electricity of China reaches 22.02 million kilowatts. However, the continuous increase of the scale of the power grid and the rapid increase of the complexity of the line in China bring great challenges to the routing inspection of the power grid in China.
Along with the continuous input of unmanned aerial vehicle electric power cruise technique, especially in remote areas, especially forest zone, during the unmanned aerial vehicle cruise process, all cruise behind one or two electricity towers usually, can produce the feed, after the feed phenomenon appears, can lead to unable continuation cruising, so need return the station and charge. The patent number is CN2020222830301, and the patent name is an unmanned aerial vehicle charging device is patrolled and examined to portable open-air electric power, and this charging device has promoted and has patrolled and examined the burden that efficiency and alleviate the operation personnel battery and carry. Subsequently, in some developed areas, the full-automatic airport of unmanned aerial vehicle has also appeared in succession, and this airport is patrolling and examining the main position that unmanned aerial vehicle stopped, but also can carry out quick charge to unmanned aerial vehicle. However, after the existing fully automatic airport is set up, the airport is usually exposed in the field, and when the airport is exposed to severe weather such as rain, snow and the like, the upper surface of the airport is corroded, or when snow exists on the upper surface of the airport, when the upper cover of the airport is opened, the snow falls onto the airport parking plane. The situation that the inspection is needed urgently in rainy days can also occur, so that the rainwater falls on the airport parking plane. These circumstances all can produce ponding (also ponding after snow melts) to airport parking plane, cause the damage of airport charging equipment even, and moreover, this ponding is difficult for discharging, and then influences the life at airport, still needs the manual work to overhaul and clear up.
To sum up, current unmanned aerial vehicle stops airport because the back is opened to the upper cover when stopping unmanned aerial vehicle and charging for unmanned aerial vehicle, the entering of sleet easily leads to the problem of unmanned aerial vehicle damage.
Disclosure of Invention
The invention aims to solve the problem that the existing unmanned aerial vehicle parking airport is easy to damage the unmanned aerial vehicle due to the fact that rain and snow enter after an upper cover is opened when the unmanned aerial vehicle is parked and the unmanned aerial vehicle is charged. And then provide a full-automatic airport that is used for open-air electric power unmanned aerial vehicle that cruises.
The technical scheme of the invention is as follows: a full-automatic airport for an outdoor electric cruise unmanned aerial vehicle comprises an airport body, wherein the airport body is a cuboid, and further comprises two upper covers, a refrigerating machine, a pipeline, a refrigerating air outlet net, a stand column, a telescopic cylinder and a rain and snow cover body, wherein the two upper covers are horizontally and oppositely arranged on the upper end surface of the airport body in an openable mode, an installation groove is formed in the lower end surface of one upper cover, the refrigerating air outlet net is arranged in the installation groove, the refrigerating machine is arranged on the outer side of the airport body in the width direction, the refrigerating machine introduces cold air into the installation groove through the pipeline, and the cold air is discharged from the refrigerating air outlet net to cool the interior of the airport body; the stand is installed in airport body length direction's the positive middle outside, and the telescoping cylinder is installed on the up end of stand, and the sleet cover body is installed at the flexible end of telescoping cylinder, and the sleet cover body realizes the lid dress to two upper covers intersection under the effect of telescoping cylinder.
Further, the cross-sectional shapes of the two upper covers are both right trapezoid.
Furthermore, a plurality of air holes are formed in the upper end surfaces of the two opposite sides of the upper covers, and the rain and snow cover body completely covers the air holes.
Further, each air hole is in an inverted cone shape.
Furthermore, a plurality of air outlet holes are formed in the refrigerating air outlet net, and openings of the air outlet holes face to the center of the interior of the airport body.
Furthermore, the sleet cover body is scalable cover body, just the cross sectional shape of the cover body is the "" shape.
Furthermore, the airport further comprises a plurality of shielding plates, wherein the shielding plates are arranged on the outer side walls of the periphery of the airport body, and the shielding plates are obliquely arranged downwards.
Furthermore, a plurality of ventilation holes are formed in the upper portion of the periphery of the outer side wall of the airport body.
Further, the shape of the vent hole is circular, triangular or rectangular.
Furthermore, the telescopic device also comprises a support, and the telescopic cylinder is arranged on the upper end surface of the upright post through the support.
Compared with the prior art, the invention has the following effects:
the invention adopts the rain and snow cover body 8, the upper end surfaces of the two opposite sides of the upper cover 2 can be covered by the rain and snow cover body 8, and the rain and snow cover body is in a "" shape, so that if the rain and snow cover body is rainy, rain can be discharged from the two sides of the airport body, can not permeate into the airport body, and the overhaul and the damage inside the airport are reduced. If it is the snowy day, snow can fall on the sleet cover body, during the use, only needs to cover the sleet cover body and withdraws, when opening the upper cover, snow can not drop inside the airport. In addition, if it is slept when the sleet weather is gone on, the operator controls unmanned aerial vehicle flight orbit, through the coordination of the control upper cover and the sleet cover body for the gap that the airport was opened only supplies unmanned aerial vehicle to take off and descend can, like this, just can reduce the possibility that sleet enters into the airport, can not cause ponding in addition yet, more can not influence the damage at airport.
Drawings
FIG. 1 is a front sectional view of the present invention; fig. 2 is a side view of the present invention.
Detailed Description
The first embodiment is as follows: the embodiment is described with reference to fig. 1 to 2, and the full-automatic airport for the field electric cruise unmanned aerial vehicle of the embodiment comprises an airport body 1, wherein the airport body 1 is a cuboid, the airport further comprises two upper covers 2, a refrigerator 3, a pipeline 4, a refrigeration air outlet net 5, a stand column 6, a telescopic cylinder 7 and a rain and snow cover body 8, the two upper covers 2 can be horizontally and oppositely installed on the upper end surface of the airport body 1 in an openable manner, an installation groove 2-1 is formed in the lower end surface of one upper cover 2, the refrigeration air outlet net 5 is installed in the installation groove 2-1, the refrigerator 3 is installed on the outer side of the airport body 1 in the width direction, and the refrigerator 3 introduces cold air into the installation groove 2-1 through the pipeline 4 and discharges the cold air outlet net 5 to the inside of the airport body 1 for cooling; the upright post 6 is arranged at the right middle outer side of the airport body 1 in the length direction, the telescopic cylinder 7 is arranged on the upper end surface of the upright post 6, the rain and snow cover body 8 is arranged at the telescopic end of the telescopic cylinder 7, and the rain and snow cover body 8 covers the junction of the two upper covers 2 under the action of the telescopic cylinder 7.
The second embodiment is as follows: the present embodiment will be described with reference to fig. 1, and both of the cross-sectional shapes of the two upper caps 2 of the present embodiment are right-angled trapezoids. So set up, two upper covers of being convenient for when closing, the upper end face forms a middle height, and the shape that both sides are low can prevent the rainwater deposit like this, and snow also can be to both sides landing, especially under the windy condition to and when the thickness of snow enough will be to both sides landing. Other components and connections are the same as in the first embodiment.
The third concrete implementation mode: referring to fig. 1, the present embodiment is described, in which a plurality of ventilation holes 2-2 are formed on the upper end surfaces of the two opposite sides of the upper cover 2, and the rain and snow cover body 8 completely covers the plurality of ventilation holes 2-2. So set up, this kind of condition is applicable to and does not have the weather of sleet and use when, and unmanned aerial vehicle charges or shuts down the in-process in the airport, can dispel the heat, prevents that unmanned aerial vehicle charging process heat is big. The rain and snow cover body is needed only when rain and snow exist. Other compositions and connections are the same as in the first or second embodiments.
The fourth concrete implementation mode: the present embodiment is described with reference to fig. 1, and each of the airing holes 2-2 of the present embodiment has an inverted cone shape. So set up, inside the outside gas of being convenient for enters into the airport fast, realize the heat dissipation. Other compositions and connection relationships are the same as in the first, second or third embodiment.
The fifth concrete implementation mode: the embodiment is described with reference to fig. 1, a plurality of air outlet holes 5-1 are provided on the refrigeration air outlet network 5 of the embodiment, and the openings of the air outlet holes 5-1 face to the central position inside the airport body 1. So set up, this kind of condition is applicable to the use when the temperature is higher in summer, has can't satisfy the actual heat dissipation demand because of conventional gas pocket heat dissipation. Other compositions and connection relationships are the same as those in the first, second, third or fourth embodiment.
The sixth specific implementation mode is as follows: the present embodiment is described with reference to fig. 1, and the rain and snow cover 8 of the present embodiment is a stretchable cover, and the cover has a cross-sectional shape of "" shape. So set up, be convenient for discharge sleet fast. Other compositions and connection relations are the same as those of the first embodiment, the second embodiment, the third embodiment, the fourth embodiment or the fifth embodiment.
The seventh concrete implementation mode: the present embodiment is described with reference to fig. 2, and the present embodiment further includes a plurality of shielding plates 9, the plurality of shielding plates 9 are mounted on the outer side walls around the airport body 1, and the shielding plates 9 are mounted to be inclined downward. So set up, prevent that the rainwater from passing through the ventilation hole and getting into in the airport. Other compositions and connection relationships are the same as in the first, second, third, fourth, fifth or sixth embodiment.
The specific implementation mode is eight: the present embodiment is described with reference to fig. 1 and 2, and a plurality of ventilation holes 1-1 are opened in an upper portion of the periphery of the outer wall of the airport body 1 of the present embodiment. So set up, be convenient for dispel the heat to airport inside when spring and autumn. Other compositions and connection relationships are the same as those of embodiment one, two, three, four, five, six or seven.
The specific implementation method nine: the present embodiment will be described with reference to fig. 1 and 2, and the shape of the vent hole 1-1 of the present embodiment is circular, triangular, or rectangular. So set up, be convenient for processing and heat dissipation. Other compositions and connection relations are the same as those of any one of the first to eighth embodiments.
The detailed implementation mode is ten: the present embodiment is described with reference to fig. 2, and the present embodiment further includes a support 10, and the telescopic cylinder 7 is mounted on the upper end surface of the column 6 through the support 10. So set up, be convenient for support the telescoping cylinder, also provide the direction for the flexible of sleet cover body. Other components and connection relationships are the same as those in any one of the first to ninth embodiments.
The principle of use of the invention is explained in connection with fig. 1 to 2:
the invention is suitable for being used all the year round in China, whether the rain and snow cover body is used or not can be selected according to the actual weather condition, the specific structure of the airport is the prior art, and the airport has the functions of positioning, weather detection, charging and the like.
The sleet cover body adopts the extending structure that can embed, and when this structure shrink, occupation space is little, and is not fragile, during the use, only need stretch out can directly cover on the upper cover. The relative position of the airport and the rain and snow cover body is calculated in advance and designed.
Although the invention has been described with respect to a preferred embodiment, it will be understood by those skilled in the art that the foregoing and other changes, omissions and deviations in the form and detail thereof may be made without departing from the scope of this invention.
Claims (10)
1. The utility model provides a full-automatic airport for open-air electric power unmanned aerial vehicle that cruises, it includes airport body (1), and airport body (1) is the cuboid, its characterized in that: the airport air outlet net type air conditioner also comprises two upper covers (2), a refrigerator (3), pipelines (4), a refrigerating air outlet net (5), a stand column (6), a telescopic cylinder (7) and a sleet cover body (8), wherein the two upper covers (2) can be horizontally and oppositely arranged on the upper end surface of the airport body (1) in an openable manner, a mounting groove (2-1) is formed in the lower end surface of one upper cover (2), the refrigerating air outlet net (5) is arranged in the mounting groove (2-1), the refrigerator (3) is arranged on the outer side of the airport body (1) in the width direction, cold air is introduced into the mounting groove (2-1) through the pipeline (4) by the refrigerator (3), and the cold air is discharged from the refrigerating air outlet net (5) to cool the interior of the airport body (1);
the upright post (6) is arranged on the outer side of the middle of the airport body (1) in the length direction, the telescopic cylinder (7) is arranged on the upper end face of the upright post (6), the rain and snow cover body (8) is arranged at the telescopic end of the telescopic cylinder (7), and the rain and snow cover body (8) covers the intersection of the two upper covers (2) under the action of the telescopic cylinder (7).
2. A fully automatic airport for field electric cruise drones according to claim 1, characterized in that: the cross sections of the two upper covers (2) are both right-angled trapezoids.
3. A fully automatic airport for field electric cruise drones according to claim 2, characterized in that: the upper end surfaces of the two opposite sides of the upper covers (2) are provided with a plurality of air holes (2-2), and the rain and snow cover body (8) completely covers the plurality of air holes (2-2).
4. A fully automatic airport for field electric cruise drones according to claim 3, characterized in that: each air hole (2-2) is in an inverted cone shape.
5. A full-automatic airport for field electric cruise unmanned aerial vehicles according to claim 4, characterized in that: a plurality of air outlet holes (5-1) are arranged on the refrigeration air outlet net (5), and the openings of the air outlet holes (5-1) face to the center position inside the airport body (1).
6. A fully automatic airport for field electric cruise drones according to claim 1 or 5, characterized in that: the rain and snow cover body (8) is a telescopic cover body, and the cross section of the cover body is in the shape of the "" shape.
7. A full-automatic airport for field electric cruise drones according to claim 6, characterized in that: it still includes a plurality of shielding plates (9), and a plurality of shielding plates (9) are installed on airport body (1) lateral wall all around, and shielding plate (9) slope installation downwards.
8. A full-automatic airport for field electric cruise unmanned aerial vehicles according to claim 7, characterized in that: a plurality of ventilation holes (1-1) are arranged on the upper part of the periphery of the outer side wall of the airport body (1).
9. A fully automatic airport for field electric cruise drones according to claim 8, characterized in that: the shape of the vent hole (1-1) is round, triangular or rectangular.
10. A fully automatic airport for field electric cruise drones according to claim 9, characterized in that: the telescopic device also comprises a support (10), and the telescopic cylinder (7) is arranged on the upper end surface of the upright post (6) through the support (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211003452.6A CN115405144A (en) | 2022-08-19 | 2022-08-19 | A full-automatic airport for open-air electric power unmanned aerial vehicle that cruises |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211003452.6A CN115405144A (en) | 2022-08-19 | 2022-08-19 | A full-automatic airport for open-air electric power unmanned aerial vehicle that cruises |
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| Publication Number | Publication Date |
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| CN115405144A true CN115405144A (en) | 2022-11-29 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202211003452.6A Pending CN115405144A (en) | 2022-08-19 | 2022-08-19 | A full-automatic airport for open-air electric power unmanned aerial vehicle that cruises |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN209111956U (en) * | 2018-09-13 | 2019-07-16 | 南昌理工学院 | Unmanned plane charging station |
| US20210031947A1 (en) * | 2018-02-05 | 2021-02-04 | H3 Dynamics Holdings Pte. Ltd. | Landing platform with improved charging for unmanned vehicles |
| WO2021082794A1 (en) * | 2019-10-28 | 2021-05-06 | 北京京东乾石科技有限公司 | Unmanned aerial vehicle airport, unmanned aerial vehicle system, patrol inspection system, method, control apparatus, device, storage medium, and unmanned aerial vehicle cruising system |
| CN114348289A (en) * | 2022-02-14 | 2022-04-15 | 唐本平 | Vertical closed type logistics unmanned aerial vehicle parking device |
| CN217151456U (en) * | 2022-04-19 | 2022-08-09 | 深圳市科比特航空技术有限公司 | Multilayer unmanned aerial vehicle hangar |
-
2022
- 2022-08-19 CN CN202211003452.6A patent/CN115405144A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210031947A1 (en) * | 2018-02-05 | 2021-02-04 | H3 Dynamics Holdings Pte. Ltd. | Landing platform with improved charging for unmanned vehicles |
| CN209111956U (en) * | 2018-09-13 | 2019-07-16 | 南昌理工学院 | Unmanned plane charging station |
| WO2021082794A1 (en) * | 2019-10-28 | 2021-05-06 | 北京京东乾石科技有限公司 | Unmanned aerial vehicle airport, unmanned aerial vehicle system, patrol inspection system, method, control apparatus, device, storage medium, and unmanned aerial vehicle cruising system |
| CN114348289A (en) * | 2022-02-14 | 2022-04-15 | 唐本平 | Vertical closed type logistics unmanned aerial vehicle parking device |
| CN217151456U (en) * | 2022-04-19 | 2022-08-09 | 深圳市科比特航空技术有限公司 | Multilayer unmanned aerial vehicle hangar |
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Application publication date: 20221129 |
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