CN107380474B - Unmanned aerial vehicle auxiliary device that takes off - Google Patents
Unmanned aerial vehicle auxiliary device that takes off Download PDFInfo
- Publication number
- CN107380474B CN107380474B CN201710801018.5A CN201710801018A CN107380474B CN 107380474 B CN107380474 B CN 107380474B CN 201710801018 A CN201710801018 A CN 201710801018A CN 107380474 B CN107380474 B CN 107380474B
- Authority
- CN
- China
- Prior art keywords
- slide rail
- aerial vehicle
- unmanned aerial
- frame body
- frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H21/00—Use of propulsion power plant or units on vessels
- B63H21/12—Use of propulsion power plant or units on vessels the vessels being motor-driven
- B63H21/17—Use of propulsion power plant or units on vessels the vessels being motor-driven by electric motor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H21/00—Use of propulsion power plant or units on vessels
- B63H21/12—Use of propulsion power plant or units on vessels the vessels being motor-driven
- B63H21/17—Use of propulsion power plant or units on vessels the vessels being motor-driven by electric motor
- B63H2021/171—Use of propulsion power plant or units on vessels the vessels being motor-driven by electric motor making use of photovoltaic energy conversion, e.g. using solar panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Photovoltaic Devices (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to an auxiliary device, in particular to a take-off auxiliary device of an unmanned aerial vehicle. The invention aims to solve the technical problem of providing an unmanned aerial vehicle take-off auxiliary device which can place an unmanned aerial vehicle in a balanced manner, so that the unmanned aerial vehicle can take off well, and can block wind, so that the take-off effect is better. In order to solve the technical problem, the invention provides a takeoff auxiliary device of an unmanned aerial vehicle, which comprises a frame body and the like; the montant is installed to the symmetrical formula of bottom left and right sides outside the framework, and the wheel is installed to the montant bottom, is equipped with elevating gear in the middle of the bottom in the framework, is connected with the diaphragm on elevating gear's the lifting unit, and the diaphragm top is equipped with adjusting device, has placed unmanned aerial vehicle on the adjusting device. According to the unmanned aerial vehicle launching device, the unmanned aerial vehicle can take off on the water surface through the pushing device, so that the unmanned aerial vehicle can be placed in a balanced mode, the unmanned aerial vehicle can take off well, and meanwhile wind can be blocked, and the effect of better taking off effect is achieved.
Description
Technical Field
The invention relates to an auxiliary device, in particular to a take-off auxiliary device of an unmanned aerial vehicle.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Present people all can use unmanned aerial vehicle to shoot in order to shoot better scenery, and unmanned aerial vehicle is when taking off, the ground unevenness leads to unmanned aerial vehicle unbalanced, and then make unmanned aerial vehicle can not fine take off, still easily blown by wind, and the effect of taking off is influenced, therefore need urgently to research and develop one kind and can carry out the balance with unmanned aerial vehicle and place, and make the fine take off of unmanned aerial vehicle, can also block wind simultaneously, and make the unmanned aerial vehicle that the effect of taking off is better take off auxiliary device.
Disclosure of Invention
(1) Technical problem to be solved
The invention aims to overcome the defects that when an unmanned aerial vehicle takes off, the ground is uneven, so that the unmanned aerial vehicle is unbalanced, and further the unmanned aerial vehicle cannot take off well and is easy to blow by wind, so that the take-off effect is influenced.
(2) Technical scheme
In order to solve the technical problem, the invention provides a take-off auxiliary device of an unmanned aerial vehicle, which comprises a frame body, vertical rods, wheels, a lifting device, a transverse plate, an adjusting device and the unmanned aerial vehicle, wherein the vertical rods are symmetrically arranged on the left side and the right side of the outer bottom of the frame body, the wheels are arranged at the bottom ends of the vertical rods, the lifting device is arranged in the middle of the inner bottom of the frame body, the transverse plate is connected onto a lifting part of the lifting device, the adjusting device is arranged at the top of the transverse plate.
Preferably, the lifting device comprises a first slide rail, an electric reel, a first slide block, a pull wire, a lifting frame, a second slide rail and a second slide block, the first slide rail and the second slide rail are arranged in the frame body and are horizontally arranged, the first slide rail and the second slide rail are symmetrically arranged, the bottom of the first slide rail is connected with the middle of the bottom in the frame body, the first slide rail is provided with two first slide blocks matched with the first slide rail, the first slide block is in sliding fit with the first slide rail, the middle of the top of the first slide rail is provided with the electric reel, the electric reel is wound with two pull wires, the tail end of one pull wire is connected with the lower part of the right side surface of the left first slide block, the tail end of the other pull wire is connected with the lower part of the left side surface of the right first slide block, the top of the second slide rail is connected with the bottom of the transverse plate, the second slide rail is provided with two, a lifting frame is connected between the two second sliding blocks and the two first sliding blocks.
Preferably, adjusting device is including the sleeve, the screw rod, the nut, place the board, the scale, the fixed block, movable rod and pointer, the sleeve is installed to diaphragm top left and right sides symmetry formula, be equipped with the screw rod in the sleeve, screw rod and sleeve fit in, install the nut on the screw rod, install between the left and right sides screw rod top and place the board, place in the middle of the board top and unmanned aerial vehicle contact, it has the scale to place in the middle of the board leading flank, place and install the fixed block in the middle of the board bottom, install the movable rod through pin joint's mode in the middle of the fixed block leading flank, install the pointer in the middle of the movable rod top.
Preferably, still including complementary unit, complementary unit is including L type pole, a spring, the inserted bar, third slide rail and third slider, open at the right flank middle part outside the framework has the draw-in groove, L type pole is installed through the mode of pin joint to the right flank lower part outside the framework, be connected with the spring between the outer bottom right side of L type pole and the outer right flank lower part of framework, the inserted bar is installed through the mode of pin joint at the outer left flank middle part of L type pole, the inserted bar tail end is located the slot, the third slide rail is installed on the outer right flank upper portion of framework, the third slide rail is vertical setting, be equipped with on the third slide rail rather than complex third slider, third slider and third slide rail sliding fit, open at the third slider middle part has the through-hole.
Preferably, still including thrust unit, thrust unit is including the kicking block, the fixed plate, first propeller, net frame and second propeller, the kicking block is installed to the outer lower part of framework, the fixed plate is installed to the symmetrical formula of kicking block bottom left and right sides, the first propeller in left side fixed plate bottom left side, the second propeller is installed on right side fixed plate bottom right side, first propeller and second propeller are the symmetry setting, the net frame is installed to the symmetrical formula of kicking block bottom left and right sides, first propeller is located the net frame in left side, the second propeller is located the net frame in right side.
Preferably, still including placer, placer is including placing frame and apron, and the frame is placed to the outer left surface lower part of framework and is installed and place the frame, and it is equipped with the apron to place the frame top, and the apron right-hand member passes through pin joint with placing frame right side top.
Preferably, the solar power generation device further comprises a power storage device, the power storage device comprises a solar panel and a storage battery, the solar panel is mounted on the upper portion of the outer left side face of the frame body, the storage battery is mounted on the lower portion of the inner left side face of the frame body, and the storage battery, the solar panel, the first propeller and the second propeller are connected through the storage battery.
Preferably, the device also comprises a heavy object block, and the middle of the outer bottom of the frame body is provided with the heavy object block.
Preferably, the device also comprises a filter screen, and the filter screen is embedded at the lower part of the right side of the frame body.
The working principle is as follows: at first operating personnel moves this device to spacious place through the wheel, restarts elevating gear, elevating gear's lift part drives diaphragm rebound, and diaphragm rebound drives unmanned aerial vehicle rebound through adjusting device, and when unmanned aerial vehicle was located the frame body outside, closing elevating gear, see whether balanced through seeing adjusting device unmanned aerial vehicle, if unbalanced, can modulate unmanned aerial vehicle into balanced state through adjusting device, otherwise, then need not to adjust. Can start elevating gear's lift part downstream drives unmanned aerial vehicle downstream, when unmanned aerial vehicle downstream resumes to the normal position, closes elevating gear, can make unmanned aerial vehicle take off, and then the framework blocks the safe taking off of messenger unmanned aerial vehicle with external wind.
Because the lifting device comprises a first slide rail, an electric reel, a first slide block, a pull wire, a lifting frame, a second slide rail and a second slide block, the first slide rail and the second slide rail are arranged in the frame body and are horizontally arranged, the first slide rail and the second slide rail are symmetrically arranged, the bottom of the first slide rail is connected with the middle of the bottom in the frame body, the first slide rail is provided with two first slide blocks matched with the first slide rail, the first slide block is in sliding fit with the first slide rail, the middle of the top of the first slide rail is provided with the electric reel, the electric reel is wound with two pull wires, the tail end of one pull wire is connected with the lower part of the right side surface of the left first slide block, the tail end of the other pull wire is connected with the lower part of the left side surface of the right first slide block, the top of the second slide rail is connected with the bottom of a transverse plate, the second slide rail is provided with, be connected with the crane between two second sliders and two first sliders, when this device is located spacious position, operating personnel can start electronic reel reversal, and then the first slider of the pulling wire pulling left and right sides inwards moves, the first slider of the left and right sides inwards removes and drives the crane extension, the crane extension drives diaphragm rebound through the second slider, and then drives unmanned aerial vehicle rebound, when unmanned aerial vehicle is located the frame body outside, close electronic reel, can adjust unmanned aerial vehicle's balance. When unmanned aerial vehicle was in balanced state, can start electronic reel corotation, act as go-between and be relaxed, because of the influence of gravity, the crane moves down and drives unmanned aerial vehicle downstream and resume to the normal position, close electronic reel.
Because the adjusting device comprises a sleeve, a screw rod, a nut, a placing plate, scales, a fixed block, a movable rod and a pointer, the left side and the right side of the top of the transverse plate are symmetrically provided with the sleeve, the screw rod is arranged in the sleeve and is matched with the sleeve, the nut is arranged on the screw rod, the placing plate is arranged between the top ends of the screw rods at the left side and the right side, the middle of the top of the placing plate is contacted with the unmanned aerial vehicle, the scales are carved in the middle of the front side surface of the placing plate, the fixed block is arranged in the middle of the bottom of the placing plate, the movable rod is arranged in the middle of the front side surface of the fixed block in a manner of pin connection, the pointer is arranged in the middle of the top end of the movable rod and is positioned at the front side of the scales, when the unmanned aerial vehicle, the left and right sides nut reciprocates and drives the left and right sides screw rod and reciprocate, and the left and right sides screw rod reciprocates and drives and places the board and reciprocate, and when the directional middle scale of pointer, can the stall left and right sides nut, and then unmanned aerial vehicle is adjusted to being in balanced state.
Because still including complementary unit, complementary unit is including L type pole, a spring, the inserted bar, third slide rail and third slider, open at the right flank middle part outside the framework has the draw-in groove, L type pole is installed through the mode of pin joint to the right flank lower part outside the framework, be connected with the spring between the outer bottom right side of L type pole and the right flank lower part outside the framework, the inserted bar is installed through the mode of pin joint in the middle part of the outer left flank of L type pole, the inserted bar tail end is located the slot, third slide rail is installed on the right flank upper portion outside the framework, the third slide rail is vertical setting, be equipped with on the third slide rail rather than complex third slider, third slider and third slide rail sliding fit, open at the third slider middle part has the through-hole, when needs remove this device to spacious position with this device, operating personnel can hold L type pole upper end and remove this device to assigned position through the wheel again. When the device does not need to be pushed, an operator can pull the upper part of the L-shaped rod to move downwards, the spring is compressed, the upper part of the L-shaped rod moves downwards to drive the inserted rod to move downwards, then the inserted rod moves downwards to be separated from the clamping groove, the third sliding block is pulled to move upwards, the L-shaped rod can be loosened, the L-shaped rod moves upwards to restore to the original position under the action of the spring, the operator presses the upper part of the L-shaped rod to move leftwards to the position below the through hole again to loosen the third sliding block, and the third sliding block moves downwards to enable the L-shaped rod to be located in the through hole and fixed. Therefore, the device can be moved more conveniently by operators, and time and labor are saved.
Because the device also comprises a pushing device, the pushing device comprises a floating block, a fixed plate, a first propeller, a net frame and a second propeller, the floating block is arranged at the lower part outside the frame body, the fixed plate is symmetrically arranged at the left side and the right side of the bottom of the floating block, the left side first propeller is arranged at the bottom of the left side fixed plate, the right side second propeller is arranged at the bottom of the right side fixed plate, the first propeller and the second propeller are symmetrically arranged, the net frame is symmetrically arranged at the left side and the right side of the bottom of the floating block, the first propeller is arranged in the left side net frame, the second propeller is arranged in the right side net frame, when the unmanned aerial vehicle needs to be carried out on the water surface, the device can be moved to the water surface, the floating block drives the frame body to float on the water surface under the action of the floating block, the first propeller can be started, and then the first propeller drives the frame body to, when unmanned aerial vehicle removed to the assigned position, closed first propeller, can make unmanned aerial vehicle take off. After unmanned aerial vehicle has flown, and when being located the framework, can start the second propeller, and then the second propeller drives the framework and removes to the normal position, closes the second propeller, can take up this device from the surface of water. Therefore, the unmanned plane can take off on the water surface.
Because still including placer, placer installs including placing frame and apron in the outer left surface lower part of framework and places the frame, places the frame top and is equipped with the apron, laps the right-hand member and passes through pin joint with placing frame right side top, and at first operating personnel opens the apron, can put into the unmanned aerial vehicle part and place the frame in, closes the apron. So, deposit the unmanned aerial vehicle part, more make things convenient for operating personnel to maintain unmanned aerial vehicle.
Because still including power storage device, power storage device is including solar panel and battery, solar panel is installed on the outside left surface upper portion of framework, the battery is installed to the left surface lower part in the framework, the battery has circuit connection with solar panel and first propeller and second propeller, when sunlight shines on solar panel, solar panel absorbs the sunlight and converts the electric energy storage into in the battery, and then when first propeller and second propeller start, the battery is switched on first propeller and second propeller. Thus, the electric resource can be saved.
Because still including the heavy object piece, install the heavy object piece in the middle of the outer bottom of framework, when this device was located the surface of water, the heavy object piece made this device more firm float on the surface of water, did not influence unmanned aerial vehicle and take off.
Because still including the filter screen, the embedded filter screen that installs in framework right side lower part, the filter screen enables the ventilation in the framework, and then when making the long-time operation of electronic reel, reduces the heat and plays the radiating effect.
(3) Advantageous effects
According to the unmanned aerial vehicle take-off device, wind can be blocked through the frame body, so that the unmanned aerial vehicle is not influenced by the wind when taking off, the pushing device can enable the unmanned aerial vehicle to take off on the water surface, the unmanned aerial vehicle can be placed in a balanced mode, the unmanned aerial vehicle can take off well, meanwhile, the wind can be blocked, and the take-off effect is better.
Drawings
Fig. 1 is a schematic front view of the present invention.
Fig. 2 is a schematic front view of the lifting device of the present invention.
Fig. 3 is a schematic front view of the adjusting device of the present invention.
Fig. 4 is a schematic front view of the auxiliary mechanism of the present invention.
Fig. 5 is a schematic front view of the pushing device of the present invention.
Fig. 6 is a schematic front view of the placement device of the present invention.
FIG. 7 is a schematic front view showing a power storage device according to the present invention.
Fig. 8 is a first partial front view structure diagram of the present invention.
Fig. 9 is a second partial schematic front view structure of the present invention.
The labels in the figures are: 1-frame body, 2-vertical rod, 3-wheel, 4-lifting device, 401-first slide rail, 402-electric reel, 403-first slide block, 404-pull wire, 405-lifting frame, 406-second slide rail, 407-second slide block, 5-transverse plate, 6-adjusting device, 601-sleeve, 602-screw rod, 603-nut, 604-placing plate, 605-scale, 606-fixed block, 607-movable rod, 608-pointer, 7-unmanned aerial vehicle, 8-auxiliary mechanism, 801-L-shaped rod, 802-spring, 803-clamping groove, 804-inserted rod, 805-third slide rail, 806-through hole, 807-third slide block, 9-pushing device, 901-floating block, 902-fixing plate, 903-a first propeller, 904-a screen frame, 905-a second propeller, 10-a placing device, 1001-a placing frame, 1002-a cover plate, 11-an electric storage device, 1101-a solar panel, 1102-a storage battery, 12-a heavy object block and 13-a filter screen.
Detailed Description
The invention is further described below with reference to the figures and examples.
Example 1
The utility model provides an unmanned aerial vehicle auxiliary device that takes off, as shown in fig. 1-9, including framework 1, montant 2, wheel 3, elevating gear 4, diaphragm 5, adjusting device 6 and unmanned aerial vehicle 7, the installation of 1 outer bottom left and right sides symmetry formula of framework has montant 2, wheel 3 is installed to 2 bottoms of montant, be equipped with elevating gear 4 in the middle of the bottom in framework 1, be connected with diaphragm 5 on elevating gear 4's the lifting unit, diaphragm 5 tops are equipped with adjusting device 6, unmanned aerial vehicle 7 has been placed on adjusting device 6.
Example 2
The utility model provides an unmanned aerial vehicle auxiliary device that takes off, as shown in fig. 1-9, including framework 1, montant 2, wheel 3, elevating gear 4, diaphragm 5, adjusting device 6 and unmanned aerial vehicle 7, the installation of 1 outer bottom left and right sides symmetry formula of framework has montant 2, wheel 3 is installed to 2 bottoms of montant, be equipped with elevating gear 4 in the middle of the bottom in framework 1, be connected with diaphragm 5 on elevating gear 4's the lifting unit, diaphragm 5 tops are equipped with adjusting device 6, unmanned aerial vehicle 7 has been placed on adjusting device 6.
The lifting device 4 comprises a first slide rail 401, an electric reel 402, a first slide block 403, a pull wire 404, a lifting frame 405, a second slide rail 406 and a second slide block 407, the frame body 1 is internally provided with the first slide rail 401 and the second slide rail 406 which are horizontally arranged, the first slide rail 401 and the second slide rail 406 are symmetrically arranged, the bottom of the first slide rail 401 is connected with the middle of the bottom in the frame body 1, the first slide rail 401 is provided with two first slide blocks 403 matched with the first slide rail 401, the first slide blocks 403 are in sliding fit with the first slide rail 401, the middle of the top of the first slide rail 401 is provided with the electric reel 402, the electric reel 402 is wound with two pull wires 404, the tail end of one pull wire 404 is connected with the lower part of the right side surface of the first slide block 403 on the left side, the tail end of the other pull wire 404 is connected with the lower part of the left side surface of the first slide block 403 on the right side, the top of the second slide rail 406 is, the second sliding blocks 407 are in sliding fit with the second sliding rails 406, and lifting frames 405 are connected between the two second sliding blocks 407 and the two first sliding blocks 403.
Example 3
The utility model provides an unmanned aerial vehicle auxiliary device that takes off, as shown in fig. 1-9, including framework 1, montant 2, wheel 3, elevating gear 4, diaphragm 5, adjusting device 6 and unmanned aerial vehicle 7, the installation of 1 outer bottom left and right sides symmetry formula of framework has montant 2, wheel 3 is installed to 2 bottoms of montant, be equipped with elevating gear 4 in the middle of the bottom in framework 1, be connected with diaphragm 5 on elevating gear 4's the lifting unit, diaphragm 5 tops are equipped with adjusting device 6, unmanned aerial vehicle 7 has been placed on adjusting device 6.
The lifting device 4 comprises a first slide rail 401, an electric reel 402, a first slide block 403, a pull wire 404, a lifting frame 405, a second slide rail 406 and a second slide block 407, the frame body 1 is internally provided with the first slide rail 401 and the second slide rail 406 which are horizontally arranged, the first slide rail 401 and the second slide rail 406 are symmetrically arranged, the bottom of the first slide rail 401 is connected with the middle of the bottom in the frame body 1, the first slide rail 401 is provided with two first slide blocks 403 matched with the first slide rail 401, the first slide blocks 403 are in sliding fit with the first slide rail 401, the middle of the top of the first slide rail 401 is provided with the electric reel 402, the electric reel 402 is wound with two pull wires 404, the tail end of one pull wire 404 is connected with the lower part of the right side surface of the first slide block 403 on the left side, the tail end of the other pull wire 404 is connected with the lower part of the left side surface of the first slide block 403 on the right side, the top of the second slide rail 406 is, the second sliding blocks 407 are in sliding fit with the second sliding rails 406, and lifting frames 405 are connected between the two second sliding blocks 407 and the two first sliding blocks 403.
Adjusting device 6 is including sleeve 601, screw rod 602, nut 603, place board 604, scale 605, fixed block 606, movable rod 607 and pointer 608, the symmetrical formula of 5 top left and right sides of diaphragm installs sleeve 601, be equipped with screw rod 602 in the sleeve 601, screw rod 602 and sleeve 601 fit in, install nut 603 on the screw rod 602, it places board 604 to install between the screw rod 602 top of the left and right sides, place the middle contact with unmanned aerial vehicle 7 in the middle of the board 604 top of placing, it has scale 605 to place to be carved with in the middle of the board 604 leading flank, place and install fixed block 606 in the middle of the board 604 bottom, install movable rod 607 through pin connection's mode in the middle of the fixed block 606 leading flank, install pointer 608 in the middle of movable rod 607 top, pointer 608 is.
Example 4
The utility model provides an unmanned aerial vehicle auxiliary device that takes off, as shown in fig. 1-9, including framework 1, montant 2, wheel 3, elevating gear 4, diaphragm 5, adjusting device 6 and unmanned aerial vehicle 7, the installation of 1 outer bottom left and right sides symmetry formula of framework has montant 2, wheel 3 is installed to 2 bottoms of montant, be equipped with elevating gear 4 in the middle of the bottom in framework 1, be connected with diaphragm 5 on elevating gear 4's the lifting unit, diaphragm 5 tops are equipped with adjusting device 6, unmanned aerial vehicle 7 has been placed on adjusting device 6.
The lifting device 4 comprises a first slide rail 401, an electric reel 402, a first slide block 403, a pull wire 404, a lifting frame 405, a second slide rail 406 and a second slide block 407, the frame body 1 is internally provided with the first slide rail 401 and the second slide rail 406 which are horizontally arranged, the first slide rail 401 and the second slide rail 406 are symmetrically arranged, the bottom of the first slide rail 401 is connected with the middle of the bottom in the frame body 1, the first slide rail 401 is provided with two first slide blocks 403 matched with the first slide rail 401, the first slide blocks 403 are in sliding fit with the first slide rail 401, the middle of the top of the first slide rail 401 is provided with the electric reel 402, the electric reel 402 is wound with two pull wires 404, the tail end of one pull wire 404 is connected with the lower part of the right side surface of the first slide block 403 on the left side, the tail end of the other pull wire 404 is connected with the lower part of the left side surface of the first slide block 403 on the right side, the top of the second slide rail 406 is, the second sliding blocks 407 are in sliding fit with the second sliding rails 406, and lifting frames 405 are connected between the two second sliding blocks 407 and the two first sliding blocks 403.
Adjusting device 6 is including sleeve 601, screw rod 602, nut 603, place board 604, scale 605, fixed block 606, movable rod 607 and pointer 608, the symmetrical formula of 5 top left and right sides of diaphragm installs sleeve 601, be equipped with screw rod 602 in the sleeve 601, screw rod 602 and sleeve 601 fit in, install nut 603 on the screw rod 602, it places board 604 to install between the screw rod 602 top of the left and right sides, place the middle contact with unmanned aerial vehicle 7 in the middle of the board 604 top of placing, it has scale 605 to place to be carved with in the middle of the board 604 leading flank, place and install fixed block 606 in the middle of the board 604 bottom, install movable rod 607 through pin connection's mode in the middle of the fixed block 606 leading flank, install pointer 608 in the middle of movable rod 607 top, pointer 608 is.
Still including auxiliary mechanism 8, auxiliary mechanism 8 is including L type pole 801, spring 802, inserted bar 804, third slide rail 805 and third slider 807, open at the outer right flank middle part of framework 1 has draw-in groove 803, L type pole 801 is installed through pin connection's mode to the outer right flank lower part of framework 1, be connected with spring 802 between the outer bottom right side of L type pole 801 and the outer right flank lower part of framework 1, inserted bar 804 is installed through pin connection's mode in the outer left flank middle part of L type pole 801, the inserted bar 804 tail end is located the slot, third slide rail 805 is installed on the outer right flank upper portion of framework 1, third slide rail 805 is vertical setting, be equipped with on the third slide rail 805 rather than the complex third slider 807, third slider 807 and third slide rail sliding fit, open at the middle part of third slider 807 has through-hole 806.
Still including thrust unit 9, thrust unit 9 is including floating block 901, fixed plate 902, first propeller 903, net frame 904 and second propeller 905, floating block 901 is installed to the outer lower part of framework 1, the fixed plate 902 is installed to the symmetry formula of floating block 901 bottom left and right sides, the first propeller 903 in left side fixed plate 902 bottom left side, second propeller 905 is installed on right side fixed plate 902 bottom right side, first propeller 903 sets up for the symmetry with second propeller 905, the net frame 904 is installed to the symmetry formula of floating block 901 bottom left and right sides, first propeller 903 is located left side net frame 904, second propeller 905 is located right side net frame 904.
Still including placer 10, placer 10 is including placing frame 1001 and apron 1002, and the frame 1001 is installed to the outer left surface lower part of framework 1, and it is equipped with apron 1002 to place the frame 1001 top, and apron 1002 right-hand member passes through pin joint with the top of placing frame 1001 right side.
The solar energy power storage device comprises a power storage device 11, wherein the power storage device 11 comprises a solar panel 1101 and a storage battery 1102, the solar panel 1101 is mounted on the upper portion of the outer left side surface of a frame 1, the storage battery 1102 is mounted on the lower portion of the inner left side surface of the frame 1, and the storage battery 1102, the solar panel 1101, a first propeller 903 and a second propeller 905 are mounted on the storage battery 1102 and the solar panel.
The frame also comprises a heavy object block 12, and the middle of the outer bottom of the frame body 1 is provided with the heavy object block 12.
The device also comprises a filter screen 13, and the filter screen 13 is embedded at the lower part of the right side of the frame body 1.
The working principle is as follows: at first, operating personnel moves this device to spacious place through wheel 3, restart elevating gear 4, elevating gear 4's lift part drives diaphragm 5 rebound, diaphragm 5 rebound passes through adjusting device 6 and drives unmanned aerial vehicle 7 rebound, when unmanned aerial vehicle 7 is located framework 1 outer time, close elevating gear 4, see whether balanced unmanned aerial vehicle 7 is balanced through seeing adjusting device 6, if unbalanced, can modulate unmanned aerial vehicle 7 into balanced state through adjusting device 6, otherwise, then need not to adjust. The lift part that can start elevating gear 4 moves down and drives unmanned aerial vehicle 7 downstream, when unmanned aerial vehicle 7 downstream resumes to the normal position, closes elevating gear 4, can make unmanned aerial vehicle 7 take off, and then framework 1 blocks the safe taking off of messenger unmanned aerial vehicle 7 with external wind.
Because the lifting device 4 comprises a first slide rail 401, an electric reel 402, a first slide block 403, a pull wire 404, a lifting frame 405, a second slide rail 406 and a second slide block 407, the frame 1 is internally provided with the first slide rail 401 and the second slide rail 406 which are horizontally arranged, the first slide rail 401 and the second slide rail 406 are symmetrically arranged, the bottom of the first slide rail 401 is connected with the middle of the bottom in the frame 1, the first slide rail 401 is provided with two first slide blocks 403 matched with the first slide rail 401, the first slide blocks 403 are in sliding fit with the first slide rail 401, the middle of the top of the first slide rail 401 is provided with the electric reel 402, the electric reel 402 is wound with the two pull wires 404, the tail end of one pull wire 404 is connected with the lower part of the right side surface of the left first slide block 403, the tail end of the other pull wire 404 is connected with the lower part of the left side surface of the right first slide block 403, and, be equipped with on the second slide rail 406 rather than two second sliders 407 of complex, second slider 407 and second slide rail 406 sliding fit, be connected with crane 405 between two second sliders 407 and two first sliders 403, when this device is located spacious position, operating personnel can start electronic reel 402 reversal, and then the first slider 403 inward movement of the 404 left and right sides that act as go-between pulls, the first slider 403 inward movement of the left and right sides drives crane 405 extension, crane 405 extension drives diaphragm 5 upward movement through second slider 407, and then drive unmanned aerial vehicle 7 rebound, when unmanned aerial vehicle 7 is located outside the framework 1, close electronic reel 402, can adjust unmanned aerial vehicle 7's balance. When unmanned aerial vehicle 7 is in balanced state, can start electronic reel 402 corotation, act as go-between 404 and be loosened, because of the influence of gravity, the crane 405 moves down and drives unmanned aerial vehicle 7 downstream and resume to the normal position, closes electronic reel 402.
Because the adjusting device 6 comprises a sleeve 601, a screw 602, a nut 603, a placing plate 604, scales 605, a fixed block 606, a movable rod 607 and a pointer 608, the left side and the right side of the top of the transverse plate 5 are symmetrically provided with the sleeve 601, the screw 602 is arranged in the sleeve 601, the screw 602 is internally matched with the sleeve 601, the nut 603 is arranged on the screw 602, the placing plate 604 is arranged between the top ends of the left side screw 602 and the right side of the top of the placing plate 604 and is contacted with the unmanned aerial vehicle 7, the scales 605 are carved in the middle of the front side surface of the placing plate 604, the fixed block 606 is arranged in the middle of the bottom of the placing plate 604, the movable rod 607 is arranged in the middle of the front side surface of the fixed block 606 in a pin connection mode, the pointer 608 is arranged in the middle of the top end of the movable rod 607, the pointer 608 is positioned in front of the scales, pointer 608 can point to scale 605 of the left and right sides, and operating personnel can twist left and right sides nut 603 and reciprocate, and left and right sides nut 603 reciprocates and drives left and right sides screw 602 and reciprocate, and left and right sides screw 602 reciprocates and drives and place board 604 and reciprocate, and when pointer 608 points to middle scale 605, can stall left and right sides nut 603, and then unmanned aerial vehicle 7 is adjusted to being in balanced state.
Because the auxiliary mechanism 8 is also included, the auxiliary mechanism 8 includes an L-shaped rod 801, a spring 802, an insertion rod 804, a third slide rail 805 and a third slide block 807, the middle part of the outer right side surface of the frame body 1 is provided with a clamping groove 803, the lower part of the outer right side surface of the frame body 1 is provided with the L-shaped rod 801 in a pin connection mode, the spring 802 is connected between the right side of the outer bottom of the L-shaped rod 801 and the lower part of the outer right side surface of the frame body 1, the insertion rod 804 is arranged in the middle part of the outer left side surface of the L-shaped rod 801 in a pin connection mode, the tail end of the insertion rod 804 is positioned in the slot, the upper part of the outer right side surface of the frame body 1 is provided with the third slide rail 805, the third slide rail 805 is vertically arranged, the third slide block 805 matched with the third slide rail, when the device needs to be moved to an open position, an operator can hold the upper end of the L-shaped rod 801 and move the device to a specified position through the wheels 3. When the device does not need to be pushed, an operator can pull the upper part of the L-shaped rod 801 to move downwards, the spring 802 is compressed, the upper part of the L-shaped rod 801 moves downwards to drive the inserting rod 804 to move downwards, then the inserting rod 804 moves downwards to be separated from the clamping groove 803, then the third sliding block 807 is pulled to move upwards, the L-shaped rod 801 can be loosened, the L-shaped rod 801 moves upwards to be restored to the original position under the action of the spring 802, the operator presses the upper part of the L-shaped rod 801 to move leftwards to the position below the through hole 806, the third sliding block 807 is loosened, and the third sliding block 807 moves downwards to enable the L-shaped rod 801 to be located in the through hole 806 and fixed. Therefore, the device can be moved more conveniently by operators, and time and labor are saved.
Because the unmanned aerial vehicle further comprises a pushing device 9, the pushing device 9 comprises a floating block 901, a fixing plate 902, a first propeller 903, a net frame 904 and a second propeller 905, the floating block 901 is arranged at the outer lower part of the frame body 1, the fixing plate 902 is symmetrically arranged at the left side and the right side of the bottom of the floating block 901, the first propeller 903 at the left side of the bottom of the left side fixing plate 902 is arranged, the second propeller 905 is arranged at the right side of the bottom of the right side fixing plate 902, the first propeller 903 and the second propeller 905 are symmetrically arranged, the net frame 904 is symmetrically arranged at the left side and the right side of the bottom of the floating block 901, the first propeller 903 is arranged in the left side net frame 904, the second propeller 905 is arranged in the right side net frame 904, when the unmanned aerial vehicle 7 takes off on the water surface, the unmanned aerial vehicle can be moved to the water surface, due to the action of the floating block 901, the floating block 901 drives the frame body 1 to float on, and the screen frame 904 can prevent that debris in the water from disturbing first propeller 903, when unmanned aerial vehicle 7 moves to the assigned position, closes first propeller 903, can make unmanned aerial vehicle 7 take off. After 7 flies to finish when unmanned aerial vehicle, and be located framework 1, can start second propeller 905, and then second propeller 905 drives framework 1 and removes to the normal position, closes second propeller 905, can take up this device from the surface of water. So, can make unmanned aerial vehicle 7 can take off on the surface of water.
Because still including placer 10, placer 10 is including placing frame 1001 and apron 1002, and the frame 1001 is placed to the outer left surface lower part of framework 1 and installs, places frame 1001 top and is equipped with apron 1002, and apron 1002 right-hand member passes through pin joint with the right side top of placing frame 1001, and at first operating personnel opens apron 1002, can put into unmanned aerial vehicle 7 part and place in the frame 1001, closes apron 1002. So, deposit 7 parts of unmanned aerial vehicle, more make things convenient for operating personnel to maintain unmanned aerial vehicle 7.
Because the solar energy power storage device further comprises the power storage device 11, the power storage device 11 comprises a solar panel 1101 and a storage battery 1102, the solar panel 1101 is mounted on the upper portion of the outer left side surface of the frame 1, the storage battery 1102 is mounted on the lower portion of the inner left side surface of the frame 1, the storage battery 1102 and the solar panel 1101 are in circuit connection with the first propeller 903 and the second propeller 905, when sunlight irradiates on the solar panel 1101, the solar panel 1101 absorbs and converts sunlight into electric energy to be stored in the storage battery 1102, and further when the first propeller 903 and the second propeller 905 are started, the storage battery 1102 energizes the first propeller 903 and the second propeller 905. Thus, the electric resource can be saved.
Because still including heavy object piece 12, install heavy object piece 12 in the middle of the outer bottom of framework 1, when this device was located the surface of water, heavy object piece 12 made this device more firm float on the surface of water, did not influence unmanned aerial vehicle 7 and take off.
Because the electric reel further comprises the filter screen 13, the filter screen 13 is embedded in the lower portion of the right side of the frame body 1, and the filter screen 13 can ventilate the frame body 1, so that heat is reduced and a heat dissipation effect is achieved when the electric reel 402 operates for a long time.
The above examples are merely representative of preferred embodiments of the present invention, and the description thereof is more specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, various changes, modifications and substitutions can be made without departing from the spirit of the present invention, and these are all within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (1)
1. The takeoff auxiliary device of the unmanned aerial vehicle is characterized by comprising a frame body (1), vertical rods (2), wheels (3), a lifting device (4), transverse plates (5), an adjusting device (6) and the unmanned aerial vehicle (7), wherein the vertical rods (2) are symmetrically arranged on the left side and the right side of the outer bottom of the frame body (1), the wheels (3) are arranged at the bottom ends of the vertical rods (2), the lifting device (4) is arranged in the middle of the inner bottom of the frame body (1), the transverse plates (5) are connected onto lifting parts of the lifting device (4), the adjusting device (6) is arranged at the top of each transverse plate (5), and the unmanned aerial vehicle (7) is placed on the;
the lifting device (4) comprises a first slide rail (401), an electric reel (402), a first slider (403), a pull wire (404), a lifting frame (405), a second slide rail (406) and a second slider (407), wherein the frame body (1) is internally provided with the first slide rail (401) and the second slide rail (406), the first slide rail (401) and the second slide rail (406) are horizontally arranged, the first slide rail (401) and the second slide rail (406) are symmetrically arranged, the bottom of the first slide rail (401) is connected with the middle of the bottom in the frame body (1), the first slide rail (401) is provided with two first sliders (403) matched with the first slide rail (401), the first slider (403) is matched with the first slide rail (401) in a sliding manner, the electric reel (402) is installed in the middle of the top of the first slide rail (401), the electric reel (402) is wound with two pull wires (404), the tail end of one pull wire (404) is connected with the lower part of the right side surface of the first slider, the tail end of the other pull wire (404) is connected with the lower part of the left side face of the first slide block (403) on the right side, the top of the second slide rail (406) is connected with the bottom of the transverse plate (5), two second slide blocks (407) matched with the second slide rail (406) are arranged on the second slide rail (406), the second slide blocks (407) are matched with the second slide rail (406) in a sliding manner, and a lifting frame (405) is connected between the two second slide blocks (407) and the two first slide blocks (403);
the adjusting device (6) comprises a sleeve (601), a screw rod (602), a nut (603), a placing plate (604), scales (605), a fixed block (606), a movable rod (607) and a pointer (608), wherein the sleeve (601) is symmetrically arranged on the left side and the right side of the top of the transverse plate (5), the screw rod (602) is arranged in the sleeve (601), the screw rod (602) is matched with the sleeve (601) in the inner part, the nut (603) is arranged on the screw rod (602), the placing plate (604) is arranged between the top ends of the screw rods (602) on the left side and the right side, the middle of the top of the placing plate (604) is contacted with the unmanned aerial vehicle (7), the scales (605) are carved in the middle of the front side surface of the placing plate (604), the fixed block (606) is arranged in the middle of the bottom of the placing plate (604), the movable rod (607), the pointer (608) is positioned at the front side of the scale (605);
the sliding type frame further comprises an auxiliary mechanism (8), the auxiliary mechanism (8) comprises an L-shaped rod (801), a spring (802), an inserted rod (804), a third sliding rail (805) and a third sliding block (807), a clamping groove (803) is formed in the middle of the outer right side face of the frame body (1), the L-shaped rod (801) is installed on the lower portion of the outer right side face of the frame body (1) in a pin connection mode, the spring (802) is connected between the right side of the outer bottom of the L-shaped rod (801) and the lower portion of the outer right side face of the frame body (1), the inserted rod (804) is installed in the middle of the outer left side face of the L-shaped rod (801) in a pin connection mode, the tail end of the inserted rod (804) is located in the clamping groove, the third sliding rail (805) is installed on the upper portion of the outer right side face of the frame body (1), the third sliding rail (805) is vertically arranged, the third, a through hole (806) is formed in the middle of the third sliding block (807);
the device is characterized by further comprising a pushing device (9), wherein the pushing device (9) comprises a floating block (901), a fixing plate (902), a first propeller (903), a net frame (904) and a second propeller (905), the floating block (901) is installed at the lower portion of the outer portion of the frame body (1), the fixing plate (902) is installed at the left side and the right side of the bottom of the floating block (901) in a symmetrical mode, the first propeller (903) is arranged at the left side of the bottom of the left fixing plate (902), the second propeller (905) is installed at the right side of the bottom of the right fixing plate (902), the first propeller (903) and the second propeller (905) are symmetrically arranged, the net frame (904) is installed at the left side and the right side of the bottom of the floating block (901) in a symmetrical mode, the first propeller (903) is located in the left side net frame (904;
the device is characterized by further comprising a placing device (10), wherein the placing device (10) comprises a placing frame (1001) and a cover plate (1002), the placing frame (1001) is installed on the lower portion of the outer left side face of the frame body (1), the cover plate (1002) is arranged on the top of the placing frame (1001), and the right end of the cover plate (1002) is connected with the top of the right side of the placing frame (1001) through a pin;
the solar energy power generation system is characterized by further comprising a power storage device (11), wherein the power storage device (11) comprises a solar panel (1101) and a storage battery (1102), the solar panel (1101) is mounted on the upper portion of the outer left side face of the frame body (1), the storage battery (1102) is mounted on the lower portion of the inner left side face of the frame body (1), the storage battery (1102) is in circuit connection with the solar panel (1101), the solar panel (1101) absorbs sunlight and converts the sunlight into electric energy to be stored in the storage battery (1102), and the storage battery (1102) supplies power to the first propeller (903) and the;
the frame also comprises a heavy object block (12), wherein the middle of the outer bottom of the frame body (1) is provided with the heavy object block (12); the frame body (1) is characterized by further comprising a filter screen (13), and the filter screen (13) is embedded in the lower portion of the right side of the frame body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710801018.5A CN107380474B (en) | 2017-09-07 | 2017-09-07 | Unmanned aerial vehicle auxiliary device that takes off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710801018.5A CN107380474B (en) | 2017-09-07 | 2017-09-07 | Unmanned aerial vehicle auxiliary device that takes off |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107380474A CN107380474A (en) | 2017-11-24 |
| CN107380474B true CN107380474B (en) | 2019-12-24 |
Family
ID=60351960
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710801018.5A Active CN107380474B (en) | 2017-09-07 | 2017-09-07 | Unmanned aerial vehicle auxiliary device that takes off |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107380474B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058840B (en) * | 2017-11-27 | 2019-11-05 | 浙江大雄模业有限公司 | A kind of unmanned plane parking device being mounted on roof |
| CN108502200B (en) * | 2018-04-09 | 2020-04-14 | 杭州杭睿科技有限公司 | Unmanned aerial vehicle platform that rises and falls with buffer structure and add medicine function |
| CN109353536B (en) * | 2018-12-06 | 2023-09-15 | 广东电网有限责任公司 | Unmanned aerial vehicle take-off and landing device and car |
| CN111392053A (en) * | 2020-03-19 | 2020-07-10 | 吉林工程技术师范学院 | Unmanned aerial vehicle auxiliary device that takes off |
| CN112937905B (en) * | 2021-03-22 | 2022-08-19 | 泰山学院 | Seeding formula unmanned aerial vehicle auxiliary device that takes off based on thing networked control |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1179073A (en) * | 1997-09-08 | 1999-03-23 | Daimosha:Kk | Movable surface heliport |
| CN204737030U (en) * | 2015-05-27 | 2015-11-04 | 成都宇翔科技有限公司 | Unmanned aerial vehicle shelters from auxiliary device |
| CN204979267U (en) * | 2015-05-27 | 2016-01-20 | 成都宇翔科技有限公司 | Unmanned aerial vehicle auxiliary device that takes off |
| CN106114884B (en) * | 2016-06-28 | 2018-07-10 | 谢爱珠 | A kind of unmanned plane based on Stewart parallel institutions stops charging station |
| CN205931297U (en) * | 2016-08-19 | 2017-02-08 | 南京奇蛙智能科技有限公司 | Lifting device for in unmanned aerial vehicle basic station |
-
2017
- 2017-09-07 CN CN201710801018.5A patent/CN107380474B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN107380474A (en) | 2017-11-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107380474B (en) | Unmanned aerial vehicle auxiliary device that takes off | |
| CN209225414U (en) | A kind of unmanned plane automation airport | |
| CN207430736U (en) | A kind of camera shooting head cleaning apparatus | |
| CN204750588U (en) | Unmanned aerial vehicle takes photo by plane | |
| CN202249693U (en) | Screen window structure | |
| CN204244163U (en) | Intelligence extendible snow protection device | |
| CN220391545U (en) | Police identification unmanned aerial vehicle | |
| CN104972873A (en) | Slidable sun shade for automobile skylight | |
| CN107458616A (en) | A kind of unmanned plane with high-definition camera defencive function | |
| CN215794502U (en) | A cloud platform elevating system for surveying and mapping unmanned aerial vehicle | |
| CN206864334U (en) | A kind of air switch box of easy access | |
| CN210829005U (en) | Middle shutter control device | |
| CN110930709B (en) | Monitoring equipment for intelligent transportation | |
| CN112572797A (en) | Automatic bird-involved foreign matter removing method and system for high-voltage power tower of unmanned aerial vehicle | |
| CN105552782A (en) | Method for installing bird repeller on power transmission tower by utilizing auxiliary device with the help of unmanned aerial vehicle | |
| CN107719674B (en) | Intelligent unmanned aerial vehicle for student who possesses vertical take-off and landing function | |
| CN105552785A (en) | Device for installing bird repeller on cross arm of high-altitude power transmission tower, suitable for unmanned aerial vehicle | |
| CN216186117U (en) | Remote sensing unmanned aerial vehicle for cotton field environment monitoring and cotton verticillium wilt prediction | |
| CN206031212U (en) | Electronic string bag of vapour car trunk | |
| CN207485328U (en) | It is a kind of that there is the automatic window for receiving certificate screen window function | |
| CN214296482U (en) | Unmanned aerial vehicle with novel motor fixing frame | |
| CN212220555U (en) | Vertical take-off and landing unmanned aerial vehicle safety protection structure | |
| CN207915476U (en) | A kind of land sky security robot | |
| CN213691652U (en) | PT return circuit ground connection on-line monitoring device's dustproof protection device | |
| CN210591865U (en) | Make things convenient for circulation of air's shield door |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20191016 Address after: 518110 1014 (D11), No. 5, golf Avenue, Guangpei community, Guanlan street, Shenzhen City, Guangdong Province Applicant after: Owl Security Technology Co., Ltd. Address before: Hongshan Road 410000 in Hunan province Changsha Kaifu District No. 98 Applicant before: Yan Jie Hao |
|
| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211224 Address after: 710000 a914, Xijing international electric center, dianzi 3rd road, Yanta District, Xi'an City, Shaanxi Province Patentee after: SHAANXI JIANFENG SHENGDA AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 518110 1014 (D11), No. 5, golf Avenue, Guangpei community, Guanlan street, Shenzhen, Guangdong Patentee before: Owl Security Technology Co.,Ltd. |
|
| TR01 | Transfer of patent right |