CN205045005U - A portable simple and easy air park for rotor unmanned aerial vehicle - Google Patents
A portable simple and easy air park for rotor unmanned aerial vehicle Download PDFInfo
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- CN205045005U CN205045005U CN201520618518.1U CN201520618518U CN205045005U CN 205045005 U CN205045005 U CN 205045005U CN 201520618518 U CN201520618518 U CN 201520618518U CN 205045005 U CN205045005 U CN 205045005U
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- hardstand
- inductor
- magnetic sheet
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- aerial vehicle
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Abstract
The utility model discloses a portable simple and easy air park for rotor unmanned aerial vehicle, including solar energy rete, electrostatic precipitator layer, circuit layer and basic material layer, wherein, there are S level magnetic sheet A, S level magnetic sheet B, N level magnetic sheet A, N level magnetic sheet B, H mark, edge line, lamp area, remote control receiver, battery and backup battery on the solar energy rete, battery and backup battery are used for providing the air park upper -part required power consumption, the inductor that wherein takes off on the circuit layer, CPU, descending inductor, controller A, electrostatic precipitator device, controller B and H mark, lamp area. When taking off, trigger the inductor that takes off, CPU is given to signal of the inductor that takes off transmission, CPU control controller A, and controller A triggers the electrostatic precipitator device and removes dust, when the aircraft descends, trigger the descending inductor, CPU is given to signal of descending inductor transmission, CPU control controller B, and controller B triggers electrostatic precipitator device, H mark and lamp area simultaneously. A portable simple and easy air park for rotor unmanned aerial vehicle conveniently carries, and it has the dust problem effectively to solve camera lens and aircraft, and be energy -concerving and environment -protective, more intelligent.
Description
Technical field
The utility model relates to aerial survey unmanned plane of taking photo by plane, and particularly relates to many rotors and to take photo by plane aerial survey unmanned plane.
Background technology
In recent years, the increasing market of unmanned plane is large, and professional unmanned plane and player's level unmanned plane, all relate to spaceflight in the wild, and during flight, the dust on ground can blow afloat by wing, causes the pollution of unmanned plane; Particularly take photo by plane with unmanned plane, before taking off, camera lens cover must be opened, the dust that screw propeller downwash flow causes makes dust is infected with by camera lens, the scuffing of cause taking photo by plane aerial survey poor effect and camera lens.Tradition unmanned plane, does not have hardstand mostly, is trouble on the one hand, is do not promote this product on the other hand, and large people from department does not go to use.For above problem, research and development one can dedusting, and the portable simple and easy hardstand that unmanned plane is accurately landed.The design of this utility model meets International Civil Aviation Organization (ICAO) annex 14-airport, the specification of International Civil Aviation Organization (ICAO) airport design manual-Part IV.
Utility model content
Technical solutions of the utility model are:
A kind ofly be applied to a kind of portable simple and easy hardstand for rotor wing unmanned aerial vehicle; comprise solar power rete, electrostatic precipitation layer, circuit layer and basic material layer; wherein; solar power rete there are S level magnetic sheet A, S level magnetic sheet B, N level magnetic sheet A, N level magnetic sheet B, H mark, edge line, light bar, remote control receiver, battery and emergency battery; battery and emergency battery are used to provide electricity consumption needed for hardstand upper-part, the inductor that wherein circuit layer takes off, CPU, landing inductor, controller A, electrostatic dust collector, controller B and H mark, light bar.
When taking off, trigger the inductor that takes off, the inductor that takes off transmits a signal and controls controller A to CPU, CPU, and controller A triggering electrostatic dust collector carries out dedusting; During aircraft landing, trigger landing inductor, landing inductor transmits a signal and controls controller B to CPU, CPU, and controller B is triggering electrostatic dust collector, H mark and light bar simultaneously.
Adopt S level magnetic sheet A, N level magnetic sheet A, N level magnetic sheet B, S level magnetic sheet B to be placed in corner, hardstand, the adhesive of S, N pole, after whole folding device, be reduced into 1/4 area.
H mark adopts electromagnet, produces magnetic after energising, more accurate when rotor is declined.
Light bar adopts LED, green front and back, left red right side white, energy-conserving and environment-protective.
The hardstand the superiors adopt solar power rete, solar power are transformed energy electrical power storage in the battery, supply the electricity consumption of whole hardstand.
Hardstand has emergency battery, when battery electric quantity is not enough, jointly powers for whole hardstand with battery.
Hardstand is equipped with remote control receiver, and far-end controls the contactor on hardstand.
Basic material layer adopts TPE environment-friendly materials, recyclable degraded.
The utility model tool has the following advantages:
1: facilitate portable.The utility model adopts corner folding device to adopt alternate S, N pole magnetic sheet, and when needs are folding, the adhesive of S, N pole, is reduced into 1/4 area after whole folding device.
2: effectively solution camera lens and aircraft have dirt problems.The utility model has added electrostatic precipitation layer, processes dust when taking off and land, and to decrease on aircraft and dust on camera lens.
3: energy-conserving and environment-protective.Light bar of the present utility model adopts LED, energy-conserving and environment-protective; Base Material layer adopts TPE material environmental-protecting material, recyclable degraded.
4: more intelligent.Built-in control system, can respond to and take off and descent, and unlatching dust collector and electromagnet H are marked with and light bar automatically, ensures landing accurately simultaneously, more convenient and smart.
Accompanying drawing explanation
Fig. 1 is integral structure schematic diagram of the present utility model.
Fig. 2 is level distribution schematic diagram of the present utility model.
Fig. 3 is the utility model control system diagram of circuit.
Detailed description of the invention
In order to better the utility model is described, be described further below in conjunction with accompanying drawing.
As shown in Fig. 1 Fig. 2 Fig. 3, a kind ofly be applied to a kind of portable simple and easy hardstand for rotor wing unmanned aerial vehicle, comprise solar power rete 1, electrostatic precipitation layer 2, circuit layer 3 and basic material layer 4, wherein, solar power rete 1 there is S level magnetic sheet A101, N level magnetic sheet A102, N level magnetic sheet B103, S level magnetic sheet B104, H mark 107, edge line 106, light bar 105, remote control receiver 108, battery 109 and emergency battery 110, battery 109 and emergency battery 110 are used to provide electricity consumption needed for hardstand upper-part, wherein circuit layer 3 takes off inductor 301, CPU302, landing inductor 303, controller A304, electrostatic dust collector 5, controller B306 and H marks 107, light bar 105.
When taking off, trigger the inductor 301 that takes off, the inductor 301 that takes off transmits a signal and controls controller A304 to CPU302, CPU302, and controller A triggering electrostatic dust collector 305 carries out dedusting; During aircraft landing, trigger landing inductor 303, landing inductor transmits a signal and controls controller B306 to CPU302, CPU, and controller B306 is triggering electrostatic dust collector 305, H mark 107 and light bar 105 simultaneously.
Principle of work of the present utility model is: before taking off, and by remote controller, opens switch, takes off, and triggers the inductor that takes off, dust collector is started, carries out dedusting; During landing, trigger landing inductor, trigger H marker tape and be magnetic, more accurately land, meanwhile, light bar lights, and reminds operating personal depression area, and dust collector starts simultaneously, processes, complete the whole descent that takes off to dust.
Obviously, above-described embodiment is only for the utility model example is clearly described, and is not the restriction to embodiment of the present utility model.For those of ordinary skill in the field, other multi-form change or variations can also be made on the basis of the above description.Here exhaustive without the need to also giving all embodiments.And these belong to spirit of the present utility model the apparent change of extending out or variation throw away and be among protection domain of the present utility model.
Claims (9)
1. the portable simple and easy hardstand for rotor wing unmanned aerial vehicle, it is characterized in that: comprise solar power rete (1), electrostatic precipitation layer (2), circuit layer (3) and basic material layer (4), wherein, solar power rete (1) there is S level magnetic sheet A (101), N level magnetic sheet A (102), N level magnetic sheet B (103), S level magnetic sheet B (104), H marks (107), edge line (106), light bar (105), remote control receiver (108), battery (109) and emergency battery (110), battery (109) and emergency battery (110) are used to provide electricity consumption needed for hardstand upper-part, wherein circuit layer (3) takes off inductor (301), CPU (302), landing inductor (303), controller A (304), electrostatic dust collector (5), controller B (306) and H mark (107), light bar (105).
2. as claimed in claim 1 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle, it is characterized in that: when taking off, triggering is taken off inductor (301), the inductor (301) that takes off transmits a signal to CPU (302), CPU (302) controls controller A (304), and controller A (304) triggering electrostatic dust collector (305) carries out dedusting; During aircraft landing, trigger landing inductor (303), landing inductor transmits a signal to CPU (302), CPU controls controller B (306), and controller B (306) simultaneously triggering electrostatic dust collector (305), H marks (107) and light bar (105).
3. as claimed in claim 1 or 2 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle; it is characterized in that: adopt S level magnetic sheet A (101), N level magnetic sheet A (102), N level magnetic sheet B (103), S level magnetic sheet B (104) to be placed in corner, hardstand; the adhesive of S, N pole, is reduced into 1/4 area after whole folding device.
4. as claimed in claim 3 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle, it is characterized in that: H mark (107) adopts electromagnet, produces magnetic after energising, more accurate when rotor is declined.
5. as claimed in claim 4 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle, it is characterized in that: light bar (105) adopts LED, green front and back, left red right side white, energy-conserving and environment-protective.
6. as claimed in claim 5 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle; it is characterized in that: the hardstand the superiors adopt solar power rete (1); solar power is transformed energy electrical power storage in battery (109), supply the electricity consumption of whole hardstand.
7. as claimed in claim 6 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle; it is characterized in that: hardstand has emergency battery (110); when battery (109) electricity is not enough, jointly power for whole hardstand with battery (109).
8. as claimed in claim 7 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle, it is characterized in that: hardstand is equipped with remote control receiver (108), far-end controls the contactor on hardstand.
9. as claimed in claim 6 for the portable simple and easy hardstand of rotor wing unmanned aerial vehicle, it is characterized in that: basic material layer (4) adopts TPE environment-friendly materials, recyclable degraded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520618518.1U CN205045005U (en) | 2015-08-17 | 2015-08-17 | A portable simple and easy air park for rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520618518.1U CN205045005U (en) | 2015-08-17 | 2015-08-17 | A portable simple and easy air park for rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205045005U true CN205045005U (en) | 2016-02-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520618518.1U Withdrawn - After Issue CN205045005U (en) | 2015-08-17 | 2015-08-17 | A portable simple and easy air park for rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN205045005U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081952A (en) * | 2016-08-18 | 2016-11-09 | 无锡石油化工起重机有限公司 | Possesses the tower crane that beacon guides unmanned plane to stop |
| CN106144913A (en) * | 2016-08-18 | 2016-11-23 | 无锡石油化工起重机有限公司 | The tower crane of unmanned plane airplane parking area is installed |
| CN106477059A (en) * | 2015-08-17 | 2017-03-08 | 武汉好奥航空技术有限公司 | A kind of portable simple airplane parking area for rotor wing unmanned aerial vehicle |
| CN107161343A (en) * | 2017-04-26 | 2017-09-15 | 海南大学 | A kind of rotor wing unmanned aerial vehicle and its replacing battery system |
| CN107284667A (en) * | 2017-07-19 | 2017-10-24 | 北京军秀咨询有限公司 | A kind of new and effective unmanned plane |
| CN110626515A (en) * | 2018-06-21 | 2019-12-31 | 上汽通用汽车有限公司 | Parking apron device of vehicle-mounted rotor unmanned aerial vehicle, automobile and control method of parking apron device |
-
2015
- 2015-08-17 CN CN201520618518.1U patent/CN205045005U/en not_active Withdrawn - After Issue
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106477059A (en) * | 2015-08-17 | 2017-03-08 | 武汉好奥航空技术有限公司 | A kind of portable simple airplane parking area for rotor wing unmanned aerial vehicle |
| CN106477059B (en) * | 2015-08-17 | 2019-11-05 | 湖北电鹰科技有限公司 | A kind of portable simple airplane parking area for rotor wing unmanned aerial vehicle |
| CN106081952A (en) * | 2016-08-18 | 2016-11-09 | 无锡石油化工起重机有限公司 | Possesses the tower crane that beacon guides unmanned plane to stop |
| CN106144913A (en) * | 2016-08-18 | 2016-11-23 | 无锡石油化工起重机有限公司 | The tower crane of unmanned plane airplane parking area is installed |
| CN107161343A (en) * | 2017-04-26 | 2017-09-15 | 海南大学 | A kind of rotor wing unmanned aerial vehicle and its replacing battery system |
| CN107161343B (en) * | 2017-04-26 | 2020-08-21 | 海南大学 | Rotor unmanned aerial vehicle and change battery system thereof |
| CN107284667A (en) * | 2017-07-19 | 2017-10-24 | 北京军秀咨询有限公司 | A kind of new and effective unmanned plane |
| CN110626515A (en) * | 2018-06-21 | 2019-12-31 | 上汽通用汽车有限公司 | Parking apron device of vehicle-mounted rotor unmanned aerial vehicle, automobile and control method of parking apron device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 430073 Hubei city of Wuhan Province, East Lake New Technology Development Zone, Road No. 1 Software Industrial Park 4-1 A3 building 15 floor of No. 01 Patentee after: Hubei electric Eagle Technology Co., Ltd. Address before: 430073 Hubei city of Wuhan Province, East Lake New Technology Development Zone, Road No. 1 Software Industry Park 4.1 A3 15 storey building No. 01 Patentee before: WUHAN HAOAO AVIATION TECHNOLOGY CO., LTD. |
|
| CP03 | Change of name, title or address | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160224 Effective date of abandoning: 20191105 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20160224 Effective date of abandoning: 20191105 |
|
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |