CN215707006U - Unmanned aerial vehicle automatic hangar for offshore wind power plant - Google Patents

Unmanned aerial vehicle automatic hangar for offshore wind power plant Download PDF

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Publication number
CN215707006U
CN215707006U CN202122409259.XU CN202122409259U CN215707006U CN 215707006 U CN215707006 U CN 215707006U CN 202122409259 U CN202122409259 U CN 202122409259U CN 215707006 U CN215707006 U CN 215707006U
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China
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aerial vehicle
unmanned aerial
hangar
offshore wind
layer
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CN202122409259.XU
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Chinese (zh)
Inventor
童博
姚中原
牛晨晖
张宇
王有超
黄宁波
李鑫鑫
姜东�
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Huaneng Yancheng Dafeng New Energy Power Generation Co ltd
Xian Thermal Power Research Institute Co Ltd
Clean Energy Branch of Huaneng International Power Jiangsu Energy Development Co Ltd Clean Energy Branch
Huaneng International Power Jiangsu Energy Development Co Ltd
Original Assignee
Huaneng Yancheng Dafeng New Energy Power Generation Co ltd
Xian Thermal Power Research Institute Co Ltd
Clean Energy Branch of Huaneng International Power Jiangsu Energy Development Co Ltd Clean Energy Branch
Huaneng International Power Jiangsu Energy Development Co Ltd
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Priority to CN202122409259.XU priority Critical patent/CN215707006U/en
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Abstract

The utility model provides an unmanned aerial vehicle automatic hangar for an offshore wind farm, which comprises a hangar body; the hangar body is arranged at an offshore wind farm booster station; an unmanned aerial vehicle lifting platform used for lifting of an unmanned aerial vehicle is arranged in an inner cavity of the hangar body, and a charging unit used for charging the unmanned aerial vehicle is arranged on the unmanned aerial vehicle lifting platform; the unmanned aerial vehicle lifting platform and the charging unit are connected with a control system; the unmanned aerial vehicle for offshore wind power inspection can realize the functions of storage, charging, automatic taking off and landing and inspection of the unmanned aerial vehicle for offshore wind power inspection at the offshore booster station, and the unmanned aerial vehicle can be remotely controlled to realize all-weather offshore wind power inspection without depending on the operation of an operation and maintenance ship; the problem of the marine unmanned aerial vehicle that exists patrols and examines inefficiency among the background art is solved.

Description

Unmanned aerial vehicle automatic hangar for offshore wind power plant
Technical Field
The utility model belongs to the technical field of wind power generation, and particularly relates to an unmanned aerial vehicle automatic hangar for an offshore wind farm.
Background
The unmanned aerial vehicle inspection of offshore wind power generally takes off and lands from a deck platform of an operation and maintenance ship, automatic taking off and landing cannot be used due to slight stormy waves, manual taking off and landing can only be adopted, the operation difficulty is high when the stormy waves are large, the unmanned aerial vehicle takes off and lands and battery replacement is difficult, and the inspection efficiency and operation safety of the unmanned aerial vehicle are seriously influenced; in addition, because the ship is limited by the window period of going to the sea, the ship can only go to the sea at a specific time in one day due to the change of sea tide level, otherwise, the ship can only go to the sea for carrying out the inspection operation of the unmanned aerial vehicle after waiting for the next window period, and the inspection efficiency is influenced.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle automatic hangar for an offshore wind farm, which solves the defects in the prior art.
In order to achieve the purpose, the utility model adopts the technical scheme that:
the utility model provides an unmanned aerial vehicle automatic hangar for an offshore wind farm. Comprises a hangar body; the hangar body is arranged at an offshore wind farm booster station;
an unmanned aerial vehicle lifting platform used for lifting of an unmanned aerial vehicle is arranged in an inner cavity of the hangar body, and a charging unit used for charging the unmanned aerial vehicle is arranged on the unmanned aerial vehicle lifting platform;
the unmanned aerial vehicle landing platform and the charging unit are connected with a control system.
Preferably, the charging unit is a wireless charging panel; the wireless charging panel is connected with the control system.
Preferably, the unmanned aerial vehicle landing platform comprises a body, an unmanned aerial vehicle locking region for landing and taking off of the unmanned aerial vehicle is arranged at the center of the body, and an unmanned aerial vehicle charging unit is arranged right below the unmanned aerial vehicle locking region; the upper surface in unmanned aerial vehicle locking area is provided with the two-dimensional code that is used for providing hangar body positional information.
Preferably, still be provided with on the body and be used for carrying out the push-down unmanned aerial vehicle fixing device fixed a position to unmanned aerial vehicle.
Preferably, the push rod type unmanned aerial vehicle fixing device comprises an upper layer unit and a lower layer unit, wherein the upper layer unit comprises two upper layer sliding fixing rods, an upper layer push rod motor and an upper layer fixing rod slide rail, and the two upper layer sliding fixing rods are slidably mounted on the upper layer fixing rod slide rail;
the two upper-layer push rod motors are respectively in driving connection with the two upper-layer sliding fixed rods;
the lower-layer unit comprises two lower-layer sliding fixing rods, a lower-layer push rod motor and a lower-layer fixing rod slide rail, wherein the two lower-layer sliding fixing rods are slidably arranged on the lower-layer fixing rod slide rail; the lower layer push rod motor is in driving connection with the two lower layer sliding fixing rods;
the lower layer push rod motors are arranged in two numbers and are respectively in driving connection with the two lower layer sliding fixing rods.
Preferably, the two upper sliding fixing rods are arranged on two sides of a wireless charging panel arranged on the unmanned aerial vehicle landing platform as the center;
the two lower-layer sliding fixing rods are arranged on two sides of a wireless charging panel arranged on the unmanned aerial vehicle landing platform as the center;
the moving direction of the lower layer sliding fixing rod is perpendicular to the moving direction of the upper layer sliding fixing rod.
Preferably, the hangar body is of a cubic structure with the surface being corrosion-resistant and salt fog-resistant.
Preferably, two side surfaces of the hangar body, which are arranged at symmetrical positions, are provided with hangar doors which are horizontally split;
the hangar door is provided with a first driving unit for realizing automatic opening and closing of the hangar door;
the first driving unit is connected with the control system.
Compared with the prior art, the utility model has the following advantages:
the unmanned aerial vehicle automatic hangar for the offshore wind power station can realize the functions of storing and charging, automatic taking off and landing and routing inspection of the unmanned aerial vehicle for offshore wind power routing inspection in the offshore booster station, and can remotely control the unmanned aerial vehicle to realize all-weather offshore wind power routing inspection without depending on the operation and maintenance ship for going out of the sea; the problem of the marine unmanned aerial vehicle that exists patrols and examines inefficiency among the background art is solved.
Further, automatic hangar both sides set up all openable to opening the door to and the unmanned aerial vehicle that can release take off and land the platform and open the design for current top and can effectively reduce the corruption of marine wind power salt fog and steam to the inside electron device of automatic hangar when unmanned aerial vehicle takes off and land, improve the reliability of automatic hangar and reduce and maintain the number of times.
Drawings
Fig. 1 is a front view of a putter type drone fixture;
fig. 2 is a side view of a putter type drone fixture;
FIG. 3 is a front view of the automated hangar with two side hangar doors open;
wherein, 1, unmanned aerial vehicle platform 2 that rises and falls, upload push rod motor 3, lower floor's push rod motor 4, upper sliding fixed pole 5, lower floor's sliding fixed pole 6, two-dimensional code 7, unmanned aerial vehicle locking region 8, charging unit 9, upper strata dead lever slide rail 10, lower floor's dead lever slide rail 11, unmanned aerial vehicle 12, unmanned aerial vehicle undercarriage 13, second recess track 14, first recess track 15, first drive unit 16, second drive unit 17, the unit is changed to the battery.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The utility model provides a system for an unmanned aerial vehicle automatic hangar of an offshore wind farm, which comprises a hangar body for providing a take-off and landing platform for an unmanned aerial vehicle.
The hangar body is arranged on an offshore wind farm booster station.
The hangar body is of a metal cubic structure with the surface being anti-corrosion and salt fog-proof.
And the two side surfaces of the hangar body, which are arranged at the symmetrical positions, are provided with hangar doors which are horizontally split.
The first drive unit 15 on the hangar door is connected with a control system.
A first groove rail 14 is formed in the inner wall of each hangar door, and the first groove rails 14 are formed in the horizontal direction.
Be provided with unmanned aerial vehicle platform 1, second drive unit 16, charging unit 8 and battery replacement unit 17 that rises and falls in the inner chamber of hangar body, wherein, be provided with second recess track 13 in the hangar body inner chamber, second recess track 13 and first recess track 14 butt joint form the track that slides of unmanned aerial vehicle platform 1 that rises and falls.
The unmanned aerial vehicle landing platform 1 is in driving connection with the second driving unit 16 and used for driving the unmanned aerial vehicle landing platform 1 to horizontally move back and forth along the sliding track through the second driving unit.
The charging unit is connected with the unmanned aerial vehicle through a wireless device and used for charging the unmanned aerial vehicle.
The charging unit is a wireless charging panel.
The battery replacing unit comprises a multi-degree-of-freedom manipulator and an unmanned aerial vehicle standby battery, wherein the multi-degree-of-freedom manipulator is used for replacing the battery of the unmanned aerial vehicle.
The second driving unit is connected with the control system; the control system is connected with the data acquisition unit.
The data acquisition unit is used for acquiring meteorological information, current position information and distance of the unmanned aerial vehicle and landing information of the unmanned aerial vehicle.
The unmanned aerial vehicle landing platform 1 comprises a body, an unmanned aerial vehicle locking region 7 for landing and landing of an unmanned aerial vehicle is arranged at the center of the body, and an unmanned aerial vehicle charging unit is arranged right below the unmanned aerial vehicle locking region 7; the upper surface of unmanned aerial vehicle locking area 7 is provided with the two-dimensional code that is used for providing hangar body positional information.
The bottom of the body is provided with a pulley; meanwhile, the body is connected with the sliding track in a sliding mode.
Still be provided with on the body and be used for carrying out the push-down unmanned aerial vehicle fixing device who fixes to unmanned aerial vehicle.
The push rod type unmanned aerial vehicle fixing device comprises an upper layer unit and a lower layer unit, wherein the upper layer unit comprises two upper layer sliding fixing rods 4, an upper layer push rod motor and an upper layer fixing rod sliding rail 9, and the two upper layer sliding fixing rods 4 are slidably mounted on the upper layer fixing rod sliding rail 9; the upper layer push rod motors are arranged in two numbers and are respectively in driving connection with the two upper layer sliding fixing rods 4.
And the upper-layer fixed rod slide rail 9 is arranged at the side edge of the unmanned aerial vehicle landing platform.
Two upper sliding fixing rods 4 are arranged on two sides of a wireless charging panel arranged on the unmanned aerial vehicle landing platform as the center.
The lower-layer unit comprises two lower-layer sliding fixing rods 5, a lower-layer push rod motor and a lower-layer fixing rod slide rail 10, wherein the two lower-layer sliding fixing rods 5 are slidably mounted on the lower-layer fixing rod slide rail 10; the lower layer push rod motor is in driving connection with the two lower layer sliding fixing rods 5.
The lower layer push rod motors are arranged in two numbers and are respectively in driving connection with the two lower layer sliding fixing rods 5.
The dead lever slide rail 10 of lower floor installs the surplus side department at unmanned aerial vehicle platform that rises and falls.
The upper layer fixed rod slide rail 9 and the lower layer fixed rod slide rail 10 form a frame structure.
Two lower floor's slip dead lever 5 arrange the wireless panel that charges that sets up on unmanned aerial vehicle plays platform both sides as the center.
The moving direction of the lower sliding fixing rod 5 is perpendicular to the moving direction of the upper sliding fixing rod 4.
Push-down unmanned aerial vehicle fixing device's working process:
after the unmanned aerial vehicle descends on the landing platform, the unmanned aerial vehicle sends a request locking signal to the control system of the automatic hangar, the control system of the automatic hangar starts the push rod motor, and then the undercarriage of the unmanned aerial vehicle is pushed through the upper sliding fixing rod 4 and the lower sliding fixing rod 5, the unmanned aerial vehicle is accurately moved to the designated position, and the undercarriage of the unmanned aerial vehicle is fixed through the upper sliding fixing rod 4 and the lower sliding fixing rod 5.
The working process of the automatic hangar is as follows:
when the unmanned aerial vehicle needs to land and stop, the position information and the distance of the automatic hangar are obtained through a navigation system; meanwhile, the current position information and the distance of the hangar are transmitted to a data acquisition unit of the hangar body in real time through a wireless communication system;
the control system controls the start and stop of the first driving unit according to the received current position information and distance of the unmanned aerial vehicle, so that the opening and closing of the hangar door are realized;
when the garage door is opened, the control system controls the second driving unit to start and stop, and then drives the unmanned aerial vehicle landing platform to move to the outside of the automatic garage, so that the unmanned aerial vehicle can land conveniently.
When the unmanned aerial vehicle needs take-off operation, an operator of the wind power plant issues a patrol inspection instruction to the control system, the control system acquires meteorological information through the data acquisition unit, selects an automatic garage door in a leeward position according to the meteorological information, and further controls the start and stop of the first driving unit, so that the opening and closing of the garage door in the leeward position are realized;
when the garage door is opened, the control system controls the start and stop of the second driving unit, so that the unmanned aerial vehicle lifting platform is driven to move to the outer side of the automatic garage, and the unmanned aerial vehicle can take off conveniently;
after the automatic hangar senses that the unmanned aerial vehicle falls, the power supply of the wireless charging panel is switched on to the appointed position by the push rod motor, the unmanned aerial vehicle starts to be wirelessly charged, the unmanned aerial vehicle detects the residual capacity constantly in the charging process, information is sent to the automatic hangar after the unmanned aerial vehicle is full of the residual capacity, and the power supply of the charging panel is controlled to be switched off by the automatic hangar.

Claims (8)

1. An unmanned aerial vehicle automatic hangar for an offshore wind farm is characterized by comprising a hangar body; the hangar body is arranged at an offshore wind farm booster station;
an unmanned aerial vehicle lifting platform used for lifting of an unmanned aerial vehicle is arranged in an inner cavity of the hangar body, and a charging unit used for charging the unmanned aerial vehicle is arranged on the unmanned aerial vehicle lifting platform;
the unmanned aerial vehicle landing platform and the charging unit are connected with a control system.
2. The unmanned aerial vehicle automatic hangar for offshore wind farms of claim 1, wherein the charging unit is a wireless charging panel; the wireless charging panel is connected with the control system.
3. The unmanned aerial vehicle automatic hangar for offshore wind farms according to claim 1, characterized in that said unmanned aerial vehicle landing platform comprises a body, a unmanned aerial vehicle locking region (7) for unmanned aerial vehicle landing is provided at a central position of said body, and an unmanned aerial vehicle charging unit is provided right below said unmanned aerial vehicle locking region (7); the upper surface of unmanned aerial vehicle locking region (7) is provided with the two-dimensional code that is used for providing hangar body positional information.
4. The unmanned aerial vehicle automatic hangar for offshore wind farms according to claim 3, wherein the body is further provided with a push-down unmanned aerial vehicle fixing device for positioning and fixing the unmanned aerial vehicle.
5. The unmanned aerial vehicle automatic hangar for offshore wind farms according to claim 4, characterized in that the push-rod unmanned aerial vehicle fixing device comprises an upper unit and a lower unit, the upper unit comprises two upper sliding fixing rods (4), an upper push-rod motor and an upper fixing rod slide rail (9), wherein the two upper sliding fixing rods (4) are slidably mounted on the upper fixing rod slide rail (9);
the two upper-layer push rod motors are respectively in driving connection with the two upper-layer sliding fixing rods (4);
the lower-layer unit comprises two lower-layer sliding fixing rods (5), a lower-layer push rod motor and a lower-layer fixing rod sliding rail (10), wherein the two lower-layer sliding fixing rods (5) are slidably mounted on the lower-layer fixing rod sliding rail (10); the lower layer push rod motor is in driving connection with the two lower layer sliding fixing rods (5);
the lower-layer push rod motors are arranged in two numbers and are respectively in driving connection with the two lower-layer sliding fixing rods (5).
6. The unmanned aerial vehicle automatic hangar for offshore wind farms according to claim 5, characterized in that two upper sliding fixed rods (4) are arranged on both sides of a wireless charging panel arranged on the unmanned aerial vehicle landing platform as the center;
two lower-layer sliding fixing rods (5) are arranged on two sides of a wireless charging panel arranged on an unmanned aerial vehicle lifting platform as the center;
the moving direction of the lower layer sliding fixing rod (5) is vertical to the moving direction of the upper layer sliding fixing rod (4).
7. The unmanned aerial vehicle automatic hangar for an offshore wind farm according to claim 1, wherein the hangar body is of a cubic structure with anti-corrosion and anti-salt fog surfaces.
8. The unmanned aerial vehicle automatic hangar for offshore wind farms according to claim 1, wherein two side surfaces of the hangar body, which are arranged at symmetrical positions, are provided with hangar doors which are horizontally split;
the hangar door is provided with a first driving unit for realizing automatic opening and closing of the hangar door;
the first driving unit is connected with the control system.
CN202122409259.XU 2021-09-30 2021-09-30 Unmanned aerial vehicle automatic hangar for offshore wind power plant Active CN215707006U (en)

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Application Number Priority Date Filing Date Title
CN202122409259.XU CN215707006U (en) 2021-09-30 2021-09-30 Unmanned aerial vehicle automatic hangar for offshore wind power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122409259.XU CN215707006U (en) 2021-09-30 2021-09-30 Unmanned aerial vehicle automatic hangar for offshore wind power plant

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113942616A (en) * 2021-09-30 2022-01-18 华能盐城大丰新能源发电有限责任公司 Inspection mechanism and method for offshore wind farm

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113942616A (en) * 2021-09-30 2022-01-18 华能盐城大丰新能源发电有限责任公司 Inspection mechanism and method for offshore wind farm
CN113942616B (en) * 2021-09-30 2023-04-18 华能盐城大丰新能源发电有限责任公司 Inspection mechanism and method for offshore wind farm

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