CN115057396B - Cable landing device for hoisting energy storage container - Google Patents
Cable landing device for hoisting energy storage container Download PDFInfo
- Publication number
- CN115057396B CN115057396B CN202210827864.5A CN202210827864A CN115057396B CN 115057396 B CN115057396 B CN 115057396B CN 202210827864 A CN202210827864 A CN 202210827864A CN 115057396 B CN115057396 B CN 115057396B
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- Prior art keywords
- worm
- energy storage
- cable
- square cylinder
- storage container
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- 238000004146 energy storage Methods 0.000 title claims abstract description 48
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 46
- 239000010959 steel Substances 0.000 claims abstract description 46
- 239000011159 matrix material Substances 0.000 claims abstract description 33
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 9
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 4
- 235000017491 Bambusa tulda Nutrition 0.000 description 4
- 241001330002 Bambuseae Species 0.000 description 4
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 4
- 239000011425 bamboo Substances 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 238000010248 power generation Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F19/00—Hoisting, lifting, hauling or pushing, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F17/00—Safety devices, e.g. for limiting or indicating lifting force
Abstract
The invention discloses a cable landing device for hoisting an energy storage container, which comprises a matrix square cylinder, wherein the lower side of a side channel steel is hinged with extension arms, one sides of the two extension arms close to the matrix square cylinder are respectively embedded with an upper worm and a lower worm in a threaded manner, the end parts of the upper worm and the lower worm in the matrix square cylinder are respectively embedded with an upper embedded rod and a lower embedded rod, the upper worm and the lower worm are respectively meshed with the upper side and the lower side of a worm wheel, and the worm wheel is driven by a servo motor. The invention is assembled on the mounting cable of the helicopter hoisting energy storage box, the overall maximum dimension direction is the same as the vertical extension direction of the mounting cable, the upper end of the mounting cable is lifted and pulled by two unmanned planes through the stretched stretching arms after the helicopter hoisting the energy storage box on the ground, the impact on the energy storage box in the landing process of the mounting cable is effectively avoided, and the safety of the energy storage box and surrounding constructors is protected.
Description
Technical Field
The invention relates to the technical field of energy storage container hoisting, in particular to a cable landing device for hoisting an energy storage container.
Background
In view of the wide application of the energy storage container products on the power generation side, the power transmission side and the user side, along with the continuous deep implementation of the national 'double carbon' strategy, the energy storage container products become an indispensable ring in the source network charge storage of a novel power system. Because the internal electronic components of the energy storage container are more, the lithium battery is filled in the energy storage container, the external impact is extremely easy to cause faults, the energy storage container is limited to be used in places such as a windrow mountain area which are not easy to construct roads for transportation, photovoltaic power generation is generally adopted in the areas, if the energy storage container is matched, the power utilization environment of the areas is greatly improved, so that the helicopter is adopted to hoist the energy storage container, the vibration impact or impact in the helicopter hoisting process is also the difficulty which is faced by the necessity, the related solving technology is relatively short, the company is taken as a unit for developing and producing energy storage products in the national power grid under-flag profession, the research and development force is especially used for carrying out technical attack on the situation, various technical schemes are produced to cope with the difficulty, and particularly, the problem that the vertical cables and the branch cables are easy to randomly collide with the energy storage container after the helicopter is hoisted is solved, and the cable landing device for hoisting the energy storage container is especially developed.
Disclosure of Invention
According to the cable landing device for hoisting the energy storage container, the cable landing device is assembled on the mounting cable for hoisting the energy storage box by the helicopter, the upper end of the mounting cable is lifted by the two unmanned aerial vehicles through the stretched stretching arms after the energy storage box is hoisted on the ground by the helicopter, so that the impact on the energy storage box in the process of landing the mounting cable is effectively avoided, and the safety of the energy storage box and surrounding constructors is protected.
The technical scheme of the invention is as follows:
the invention provides a cable landing device for hoisting an energy storage container, which comprises an unmanned aerial vehicle mounting ring, a cable locking plate, side channel steel, a matrix square cylinder, a locking structure, an extension arm, a servo motor, a worm wheel, an upper worm, an upper embedded rod, a lower worm and a lower embedded rod, wherein the matrix square cylinder is vertically arranged, the cable locking plate for locking on the mounting cable is detachably arranged at the rear side of the matrix square cylinder, the servo motor is arranged in the center of the front side of the matrix square cylinder, the worm wheel is arranged in the center of the inside of the matrix square cylinder, a rotating shaft is arranged in the center of the worm wheel, the rear end of the rotating shaft backwards penetrates out of the matrix square cylinder and is connected with the servo motor, the upper worm and the lower worm are respectively meshed with the upper worm and the lower worm, the upper worm and the lower worm are symmetrical about the center of the axis of the worm wheel, the upper worm and the lower worm extend from the meshing part of the worm wheel in opposite directions and horizontally penetrate out of the matrix square cylinder, the upper worm and the lower worm are in hollow tubular structures near the end parts meshed with the worm wheel and are respectively embedded with an upper embedded rod and a lower embedded rod which extend horizontally, the end parts of the upper embedded rod far away from the upper worm and the end parts of the lower embedded rod far away from the lower worm are respectively fixedly arranged on the square base cylinder, the end parts of the upper worm and the lower worm penetrating out of the square base cylinder are respectively in threaded nesting with an extending arm, the extending arms vertically extend, the upper ends of the extending arms are provided with annular unmanned aerial vehicle mounting rings, the two extending arms are respectively positioned at the left side and the right side of the square base cylinder, side channel steel is arranged between the extending arms and the square base cylinder, the upper parts of the side channel steel are fixedly arranged at one side of the square base cylinder and the lower ends of the side channel steel vertically extend, the end parts of the side channel steel far away from the square base cylinder are provided with openings which are provided with openings, the corresponding extending arms are embedded in the openings, the lower extreme of extension arm corresponds the articulated lower extreme at the side channel steel for the extension arm can overturn to the horizontality from the erect state, the lower extreme of side channel steel is equipped with the hasp structure that is used for the hasp to change the extension arm of horizontality.
Further, two the stretching arms are respectively provided with a lower thread opening and an upper thread opening corresponding to the upper worm and the lower worm, the lower thread opening and the upper thread opening are respectively in a threaded hole shape, the end part of the upper worm far away from the worm wheel is in a threaded shape and is in threaded embedding in the upper thread opening on the corresponding stretching arm, and the end part of the lower worm far away from the worm wheel is in a threaded shape and is in threaded embedding in the lower thread opening on the corresponding stretching arm.
Further, a controller and a battery box are arranged between the two side groove steels and are positioned below the matrix square tube, the controller is respectively and electrically connected with the servo motor and the battery box, and the controller controls the servo motor to be started or stopped by receiving wireless remote control signals and is powered by the battery box.
Further, the lower extreme of extension arm is fixed and is provided with the hinge piece, the lower extreme of hinge piece is equipped with the hasp hole, the hasp structure is embedded in the hasp hole under the condition that the extension arm changed the horizontality from vertical state for the extension arm keeps the horizontality.
Further, the hinge block is in a right-angle structure far away from the lower side of the locking structure and is in a circular arc structure close to the lower side of the locking structure, so that the hinge block is pressed against the side wall of the side channel steel far away from the lower side of the locking structure under the condition that the extending arm is converted from a vertical state to a horizontal state.
Further, the hasp structure includes hasp lid, hasp quarter butt, fixed section of thick bamboo and spring, two fixed section of thick bamboo that is provided with the level extension on the side that the side channel steel is relative respectively, the screw thread nestification has the hasp lid on the tip that the side channel steel that corresponds was kept away from to fixed section of thick bamboo, be equipped with spring and hasp quarter butt in the fixed section of thick bamboo, be equipped with the spring between hasp quarter butt and the hasp lid that corresponds, the tip that the hasp quarter butt is kept away from the hasp lid that corresponds runs through the side channel steel that corresponds and supports and lean on the hinge piece, the hasp quarter butt can be pushed the embedding by the spring in the hasp downthehole that corresponds under the extension arm is in the horizontality.
Further, still include middle link board, undercarriage, cloud platform camera, unmanned aerial vehicle base member and mount crotch, the part that is in cloud platform camera below on the undercarriage of unmanned aerial vehicle base member is equipped with middle link board, the middle center of linking the board is equipped with the mount crotch that is used for hooking unmanned aerial vehicle mount ring.
Further, a mounting straight rod which horizontally penetrates through the unmanned aerial vehicle mounting ring is arranged at the end part of the mounting hook far away from the middle connecting plate.
Further, the cable locking plate is pressed against the rear side surface of the base square cylinder and is locked on the base square cylinder through a plurality of locking bolts, the upper end of the mounting cable is bent to form a helicopter mounting ring, and two ends of the helicopter mounting ring are respectively locked between the cable locking plate and the base square cylinder.
Further, the central lines of the helicopter mounting ring and the unmanned aerial vehicle mounting ring extend front and back respectively, and the two unmanned aerial vehicle mounting rings are positioned on the left side and the right side of the helicopter mounting ring respectively.
The invention adopts the technology, so that compared with the prior art, the invention has the following specific positive and beneficial effects:
the invention is assembled on the mounting cable of the helicopter hoisting energy storage box, the overall maximum dimension direction is the same as the vertical extension direction of the mounting cable, the wind resistance of the mounting cable in the process of hoisting the energy storage box by the helicopter can be effectively avoided, the upper end of the mounting cable is lifted by two unmanned planes through the stretched stretching arms after the energy storage box is hoisted on the ground by the helicopter, the impact on the energy storage box in the process of directly dropping the mounting cable is effectively avoided, and the safety of the energy storage box and surrounding constructors is protected.
Drawings
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is an enlarged schematic view of a portion of FIG. 1 at A;
FIG. 3 is a front view of the structure shown in FIG. 1;
FIG. 4 is a schematic view of the self-expanding mounting structure of the present invention;
FIG. 5 is a top view of the structure shown in FIG. 4;
FIG. 6 is a cross-sectional view at B-B in FIG. 5;
fig. 7 is a schematic structural view of the present invention after mounting of the unmanned aerial vehicle;
fig. 8 is a schematic structural view of the unmanned aerial vehicle structure according to the present invention.
In the figure: the helicopter comprises a 1-helicopter mounting ring, a 2-unmanned aerial vehicle mounting ring, a 3-cable lock plate, a 4-first side channel steel, a 5-controller, a 6-battery box, a 7-hinge bolt, an 8-lock buckle cover, a 9-mounting cable, a 10-branch cable, an 11-connecting frame, a 12-energy storage container, a 13-hinge block, a 14-stretching arm, a 15-second side channel steel, a 16-base square tube, a 17-locking bolt, a 18-servo motor, a 19-worm wheel, a 20-upper worm, a 21-upper embedded rod, a 22-lower worm, a 23-lower embedded rod, a 24-lower threaded opening, a 25-upper threaded opening, a 26-rotating shaft, a 27-lock buckle hole, a 28-lock buckle short rod, a 29-fixing tube, a 30-spring, a 31-mounting straight rod, a 32-intermediate connecting plate, a 33-landing gear, a 34-cradle head camera, a 35-unmanned aerial vehicle base and a 36-mounting hook.
Detailed Description
In the process of lifting the energy storage container by the helicopter, a connecting frame 11 with a lifting appliance is generally arranged on the energy storage container, four end corners of the connecting frame 11 are respectively connected with a branch cable 10, the four branch cables 10 are connected with a mounting cable 9 right above the center of the energy storage container 12, the mounting cable 9 extends vertically upwards, and the upper end of the mounting cable 9 forms a helicopter mounting ring 1 to be hooked with a lifting appliance of the helicopter.
Embodiment one:
as shown in fig. 1 to 7, the invention provides a cable landing device for hoisting an energy storage container, comprising an unmanned aerial vehicle mounting ring 2, a cable locking plate 3, a first side channel steel 4, a controller 5, a battery box 6, a base square barrel 16, a locking structure, an extension arm 14, a second side channel steel 15, a servo motor 18, a worm wheel 19, an upper worm 20, an upper embedded rod 21, a lower worm 22 and a lower embedded rod 23, wherein the base square barrel 16 is vertically arranged at the rear side and is detachably provided with the cable locking plate 3 for locking on a mounting cable 9, the servo motor 18 is arranged at the center of the front side of the base square barrel 16, the worm wheel 19 is arranged at the center of the inside of the base square barrel 16, a rotating shaft 26 is arranged at the center of the worm wheel 19, the rear end of the rotating shaft 26 penetrates out of the base square barrel 16 backwards and is connected with the servo motor 18, the upper worm 20 and the lower worm 22 are respectively meshed at the upper side and the lower side of the worm wheel 19, the upper worm 20 and the lower worm 22 are symmetrical about the axis center of the worm wheel 19, the upper worm 20 and the lower worm 22 respectively extend from the meshing position with the worm wheel 19 in opposite directions and horizontally penetrate out of the matrix square tube 16, the upper worm 20 and the lower worm 22 are close to the end part meshed with the worm wheel 19 and are respectively embedded with an upper embedded rod 21 and a lower embedded rod 23 which extend horizontally, the end part of the upper embedded rod 21 far away from the upper worm 20 and the end part of the lower embedded rod 23 far away from the lower worm 22 are respectively fixedly arranged on the matrix square tube 16, the end parts of the upper worm 20 and the lower worm 22 penetrating out of the matrix square tube 16 are respectively nested with an extending arm 14 in a threaded manner, the extending arms 14 vertically extend and are provided with annular unmanned aerial vehicle mounting rings 2 at the upper ends, the two extending arms 14 are respectively positioned at the left side and the right side of the matrix square tube 16 and the gravity center of the unmanned aerial vehicle mounting rings are respectively positioned on the side walls far away from the matrix square tube 16, the two extending arms 14 are respectively provided with a lower thread opening 24 and an upper thread opening 25 corresponding to the upper worm 20 and the lower worm 22, the lower thread opening 24 and the upper thread opening 25 are respectively in a threaded hole shape, the end part of the upper worm 20 far away from the worm wheel 19 is in a threaded shape and is in threaded embedding in the upper thread opening 25 on the corresponding extending arm 14, the end part of the lower worm 22 far away from the worm wheel 19 is in a threaded shape and is in threaded embedding in the lower thread opening 24 on the corresponding extending arm 14, a first side channel steel 4 and a second side channel steel 15 are respectively arranged between the two extending arms 14 and the matrix square tube 16, the upper parts of the first side channel steel 4 and the second side channel steel 15 are respectively fixedly arranged on the left side and the right side of the matrix square tube 16 and the lower end of the matrix square tube extends vertically, be equipped with controller 5 and battery box 6 that are in base member square tube 16 below between first side channel-section steel 4 and the second side channel-section steel 15, controller 5 and servo motor 18 and battery box 6 electric connection respectively, controller 5 is through receiving wireless remote control signal control servo motor 18's start and stop and by battery box 6 power supply, the tip that base member square tube 16 was kept away from to first side channel-section steel 4 and second side channel-section steel 15 is equipped with the opening that is the opening of opening form respectively and the expansion arm 14 embedding that corresponds in the opening, the lower extreme of two expansion arms 14 corresponds the lower extreme of articulating at first side channel-section steel 4 and second side channel-section steel 15 respectively, make expansion arm 14 can overturn into the horizontality by the erect state, the lower extreme of first side channel-section steel 4 and second side channel-section steel 15 is equipped with the hasp structure that is used for hasp to change into expansion arm 14 of horizontality.
In order to enable the extension arm 14 to be connected with the locking structure better, a hinging block 13 is fixedly arranged at the lower end of the extension arm 14, a locking hole 27 is formed in the lower end of the hinging block 13, and the locking structure is embedded in the locking hole 27 when the extension arm 14 is converted into a horizontal state from a vertical state, so that the extension arm 14 is kept in the horizontal state. Specifically, the hinge blocks 13 are in a right-angle structure away from the lower side of the locking structure and are in a circular arc structure close to the lower side of the locking structure, so that in the case that the two extending arms 14 are synchronously converted from the vertical state to the horizontal state, the lower sides of the two hinge blocks 13 away from the corresponding locking structure are respectively pressed against the side walls of the first side channel steel 4 and the second side channel steel 15.
The locking structure comprises locking covers 8, locking short rods 28, fixing cylinders 29 and springs 30, wherein the fixing cylinders 29 which extend horizontally are respectively fixedly arranged on opposite sides of the first side channel steel 4 and the second side channel steel 15, the locking covers 8 are nested on opposite ends of the two fixing cylinders 29 in a threaded mode, the springs 30 and the locking short rods 28 are arranged in the fixing cylinders 29, the springs 30 are arranged between the locking short rods 28 and the corresponding locking covers 8, the ends, away from the corresponding locking covers 8, of the two locking short rods 28 penetrate through the corresponding first side channel steel 4 and the corresponding second side channel steel 15 and abut against corresponding hinge blocks 13, and the locking short rods 28 can be pushed to be embedded in corresponding locking holes 27 by the springs 30 when the extending arms 14 are in a horizontal state.
In order to facilitate hooking of the helicopter hoisting tool and the mounting cable 9, the cable locking plate 3 is pressed against the rear side surface of the base square cylinder 16 and is locked on the base square cylinder 16 through a plurality of locking bolts 17, the upper end of the mounting cable 9 is bent to form a helicopter mounting ring 1, and two ends of the helicopter mounting ring 1 are respectively locked between the cable locking plate 3 and the base square cylinder 16.
In order to enable the unmanned aerial vehicle to hook the unmanned aerial vehicle mounting ring 2 from the two sides of the matrix square cylinder 16, accidental collision between the unmanned aerial vehicle and a helicopter hoisting appliance is avoided, the central lines of the helicopter mounting ring 1 and the unmanned aerial vehicle mounting ring 2 are respectively extended back and forth, and the two unmanned aerial vehicle mounting rings 2 are respectively positioned on the left side and the right side of the helicopter mounting ring 1.
As shown in fig. 8, the used unmanned aerial vehicle structure that involves mainly includes middle link plate 32, undercarriage 33, cloud platform camera 34, unmanned aerial vehicle base member 35 and mount crotch 36, be equipped with middle link plate 32 in the portion that is in cloud platform camera 34 below on the undercarriage 33 of unmanned aerial vehicle base member 35, the central authorities of middle link plate 32 are equipped with the mount crotch 36 that is used for hooking unmanned aerial vehicle mount crotch 2, mount crotch 36 is arc hook structure, the tip that link plate 32 was kept away from to mount crotch 36 is equipped with the mount straight bar 31 that is used for the level to pass unmanned aerial vehicle mount crotch 2 for the ground remote control personnel observe unmanned aerial vehicle mount crotch 2's of unmanned aerial vehicle through the cloud platform camera 34 that unmanned aerial vehicle carried on the unmanned aerial vehicle process on unmanned aerial vehicle, mount straight bar 31 can conveniently pass unmanned aerial vehicle mount crotch 2, and then make unmanned aerial vehicle mount crotch 2 and mount crotch 36 hook together smoothly. Of course, it should be noted that the landing stage of the unmanned aerial vehicle needs to be specially designed, that is, a hole allowing the mounting hook 36 to pass through needs to be provided in the center of the landing stage, and the landing gear 33 of the unmanned aerial vehicle is pressed against the landing stage and two sides of the hole.
The use mechanism is as follows: in the process of lifting the energy storage box 12 by the helicopter, the state of the whole device is shown in fig. 1, and after the energy storage box 12 is lifted and put in the ground by the helicopter, and before the lifting appliance of the helicopter is separated from the helicopter mounting ring 1, the ground constructor remotely controls the large unmanned aerial vehicle to take off in two frames, and in the flying process, the operation personnel on the helicopter observe through the cradle head camera 34 on the unmanned aerial vehicle matrix 35, the operation personnel on the helicopter are connected with the wireless signal of the controller 5 through the remote controller, the starting signal of the servo motor 18 is transmitted to the controller 5, the servo motor 18 drives the worm wheel 19 to rotate through the rotating shaft 26, the worm wheel 19 synchronously drives the upper worm 20 and the lower worm 22 to rotate, the upper worm 20 and the lower worm 22 are respectively in a spiral way to exit from the threaded opening 25 and the lower threaded opening 24, the upper ends of the two stretching arms 14 are respectively turned down until the locking structures lock the two stretching arms 14, the two stretching arms 14 are in a horizontal state, the two stretching arms 2 are respectively in the position of the hanging ring 2, the energy storage ring 9 is correspondingly hung on the ground, the unmanned aerial vehicle is directly hung on the ground, the hanging ring 9 is directly, the hanging ring 9 is hung on the unmanned aerial vehicle is directly, the plane is directly hung on the ground, and the plane is directly on the ground, and the plane is directly on the plane 9, and the plane is directly on the plane, and the plane is directly on the plane, and is the plane, and the plane.
Claims (10)
1. A hawser landing gear for energy storage container hoist and mount, its characterized in that: comprises an unmanned aerial vehicle mounting ring, a cable lock plate, a side channel steel, a matrix square cylinder, a locking structure, an extension arm, a servo motor, a worm wheel, an upper worm, an upper embedded rod, a lower worm and a lower embedded rod, wherein the matrix square cylinder is vertically and detachably provided with the cable lock plate for locking on a mounting cable, the servo motor is arranged in the center of the front side surface of the matrix square cylinder, the worm wheel is arranged in the center of the inside of the matrix square cylinder, the center of the worm wheel is provided with a rotating shaft, the rear end of the rotating shaft backwards penetrates out of the matrix square cylinder and is connected with the servo motor, the upper and lower sides of the worm wheel are respectively meshed with the upper worm and the lower worm, the upper worm and the lower worm are symmetrical about the axis center of the worm wheel, the upper worm and the lower worm extend oppositely from the meshing part of the worm wheel and horizontally penetrate out of the matrix square cylinder, the upper worm and the lower worm are close to the hollow tubular structure which is meshed with the worm wheel and are respectively embedded with the upper embedded rod and the lower embedded rod which extend horizontally, the end part of the upper embedded rod far away from the upper worm and the end part of the lower embedded rod far away from the lower worm are respectively fixedly arranged on the matrix square cylinder, the end parts of the upper worm and the lower worm penetrating out of the matrix square cylinder are respectively nested with an extension arm in a threaded manner, the extension arms vertically extend and are provided with annular unmanned aerial vehicle mounting rings at the upper ends, the two extension arms are respectively positioned at the left side and the right side of the matrix square cylinder, a side channel steel is arranged between the extension arms and the matrix square cylinder, the upper part of the side channel steel is fixedly arranged at one side of the matrix square cylinder and the lower end of the side channel steel vertically extends, the end part of the side channel steel far away from the matrix square cylinder is provided with an opening in a notch shape and a corresponding extension arm is embedded in the opening, the lower ends of the extension arms are correspondingly hinged at the lower ends of the side channel steel, so that the extension arms can be overturned from an upright state to a horizontal state, the lower end of the side groove steel is provided with a locking structure for locking the extension arm converted into a horizontal state.
2. A cable landing device for hoisting an energy storage container as claimed in claim 1, wherein: the two stretching arms are respectively provided with a lower thread opening and an upper thread opening which correspond to the upper worm and the lower worm, the lower thread opening and the upper thread opening are respectively in threaded hole shapes, the end part of the upper worm, which is far away from the worm wheel, is in threaded shape and is in threaded embedding in the upper thread opening on the corresponding stretching arm, and the end part of the lower worm, which is far away from the worm wheel, is in threaded shape and is in threaded embedding in the lower thread opening on the corresponding stretching arm.
3. A cable landing device for hoisting an energy storage container as claimed in claim 2, wherein: the controller is electrically connected with the servo motor and the battery box respectively, and the controller controls the servo motor to be started and stopped by receiving wireless remote control signals and is powered by the battery box.
4. A cable landing device for hoisting an energy storage container as claimed in claim 3, wherein: the lower extreme of extension arm is fixed and is provided with the hinge piece, the lower extreme of hinge piece is equipped with the hasp hole, the hasp structure is embedded in the hasp hole under the condition that the extension arm changed the horizontality from vertical state for the extension arm keeps the horizontality.
5. A cable landing gear for hoisting an energy storage container as claimed in claim 4 wherein: the hinge block is far away from the downside of locking structure and is in a right angle structure and is close to the downside of locking structure and is in a circular arc structure, so that the hinge block is far away from the downside of locking structure and leans against the side wall of the side channel steel under the condition that the extending arm is converted from a vertical state to a horizontal state.
6. A cable landing gear for hoisting an energy storage container as claimed in claim 5 wherein: the lock catch structure comprises a lock catch cover, lock catch short rods, fixed barrels and springs, wherein the two fixed barrels which extend horizontally are respectively fixedly arranged on opposite side faces of the side groove steel, the lock catch covers are nested on the end parts of the fixed barrels, which are far away from corresponding side groove steel, in a threaded manner, the springs and the lock catch short rods are arranged in the fixed barrels, the springs are arranged between the lock catch short rods and the corresponding lock catch covers, the end parts, which are far away from the corresponding lock catch covers, of the lock catch short rods penetrate through the corresponding side groove steel and are propped against the hinging blocks, and the lock catch short rods can be pushed by the springs to be embedded in corresponding lock catch holes under the horizontal state of the extending arms.
7. A cable landing gear for hoisting an energy storage container as claimed in claim 6 wherein: still including middle link board, undercarriage, cloud platform camera, unmanned aerial vehicle base member and mounting crotch, the part that is in cloud platform camera below on the undercarriage of unmanned aerial vehicle base member is equipped with middle link board, the middle center of linking the board is equipped with the mounting crotch that is used for hooking unmanned aerial vehicle mounting ring.
8. A cable landing gear for hoisting an energy storage container as claimed in claim 7 wherein: the end part of the mounting hook, which is far away from the middle connecting plate, is provided with a mounting straight rod which horizontally penetrates through the unmanned aerial vehicle mounting ring.
9. A cable landing device for hoisting an energy storage container as claimed in claim 8 wherein: the cable locking plate is pressed against the rear side surface of the base square cylinder and is locked on the base square cylinder through a plurality of locking bolts, the upper end of the mounting cable is bent to form a helicopter mounting ring, and two ends of the helicopter mounting ring are respectively locked between the cable locking plate and the base square cylinder.
10. A cable landing device for hoisting an energy storage container as claimed in claim 9, wherein: the central lines of the helicopter mounting ring and the unmanned aerial vehicle mounting ring respectively extend front and back, and the two unmanned aerial vehicle mounting rings are respectively positioned on the left side and the right side of the helicopter mounting ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210827864.5A CN115057396B (en) | 2022-07-14 | 2022-07-14 | Cable landing device for hoisting energy storage container |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210827864.5A CN115057396B (en) | 2022-07-14 | 2022-07-14 | Cable landing device for hoisting energy storage container |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115057396A CN115057396A (en) | 2022-09-16 |
| CN115057396B true CN115057396B (en) | 2023-12-15 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202210827864.5A Active CN115057396B (en) | 2022-07-14 | 2022-07-14 | Cable landing device for hoisting energy storage container |
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| CN (1) | CN115057396B (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN116279851A (en) * | 2023-03-30 | 2023-06-23 | 安徽奇瑞瑞弗特种车辆技术有限公司 | Mobile rescue system |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH101282A (en) * | 1996-06-17 | 1998-01-06 | Minato Seiki Kogyo Kk | Container spreader |
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| KR20170054916A (en) * | 2015-11-10 | 2017-05-18 | 주식회사 선진인더스트리 | A folding safty gondola with horizontal control function |
| KR20180052516A (en) * | 2016-11-10 | 2018-05-18 | 삼성전자주식회사 | Lifting device and refrigerator including the same |
| KR20200111874A (en) * | 2019-03-19 | 2020-10-05 | 류재환 | Cargo Loading Port For Cargo Transporting Drone |
| CN111747286A (en) * | 2020-05-18 | 2020-10-09 | 周仁战 | Civil engineering pipeline handling device |
| CN113581995A (en) * | 2021-07-30 | 2021-11-02 | 陕西建工安装集团有限公司 | Hoist device is used in engineering equipment fixing |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US10906783B2 (en) * | 2017-08-25 | 2021-02-02 | Columbia Helicopters, Inc. | Load placement system |
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| JPH101282A (en) * | 1996-06-17 | 1998-01-06 | Minato Seiki Kogyo Kk | Container spreader |
| US6619904B1 (en) * | 1998-03-04 | 2003-09-16 | Leonard Dodge Barry | Container transfer crossover and system |
| JP2002137884A (en) * | 2000-11-01 | 2002-05-14 | Hirotech:Kk | Container suspension device |
| KR101018534B1 (en) * | 2010-05-20 | 2011-03-03 | 김화식 | Manual puller for lifting a manhole frame |
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| KR20180052516A (en) * | 2016-11-10 | 2018-05-18 | 삼성전자주식회사 | Lifting device and refrigerator including the same |
| KR20200111874A (en) * | 2019-03-19 | 2020-10-05 | 류재환 | Cargo Loading Port For Cargo Transporting Drone |
| CN111747286A (en) * | 2020-05-18 | 2020-10-09 | 周仁战 | Civil engineering pipeline handling device |
| CN113581995A (en) * | 2021-07-30 | 2021-11-02 | 陕西建工安装集团有限公司 | Hoist device is used in engineering equipment fixing |
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| Publication number | Publication date |
|---|---|
| CN115057396A (en) | 2022-09-16 |
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