CN218861623U - Accumulator loader - Google Patents
Accumulator loader Download PDFInfo
- Publication number
- CN218861623U CN218861623U CN202221634444.7U CN202221634444U CN218861623U CN 218861623 U CN218861623 U CN 218861623U CN 202221634444 U CN202221634444 U CN 202221634444U CN 218861623 U CN218861623 U CN 218861623U
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- China
- Prior art keywords
- support frame
- loader
- bearing frame
- lifter
- battery
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a storage battery loading machine, including the battery box, the battery box front end is provided with the driver's cabin, the driver's cabin front end is installed balanced mechanism, balanced mechanism front end is installed rotary mechanism, the rotary mechanism top is installed the bearing frame, first support frame is all installed at bearing frame top both ends, two first support frame bottom middle sections are all connected and installed first lifter, the bearing frame top intermediate position is installed the second lifter, second lifter one end is installed the second support frame, install the backup pad between two first support frames, second support frame bottom middle section movable mounting is in the backup pad top, second support frame one end is connected and installed the third support frame; battery loader, be convenient for the side load, reduce the unnecessary operation and improve work efficiency, prevent simultaneously that the during operation that loads from taking place to turn on one's side, improve the security performance.
Description
Technical Field
The utility model relates to a loader field, in particular to battery loader.
Background
The loader is used for loading bulk materials such as soil, sand stone, lime, coal and the like, and can also carry out slight shoveling and loading operation on ores, hard soil and the like, and the scheme particularly relates to a storage battery loader; however, the existing storage battery loader has certain disadvantages to be improved when in use, the existing storage battery loader loads materials to a stacking area, and the materials cannot be laterally loaded, and the loader needs to be operated and adjusted to carry out loading on the front side, so that the work efficiency is reduced by repeated unnecessary operation; when the existing storage battery loader is used, if the storage battery loader meets an uneven site and is loaded with overweight materials, the storage battery loader is not safe to turn on one's side, and certain influence is brought to actual use.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims at providing a storage battery loader, which can effectively solve the problems that when the existing storage battery loader in the background technology is used, the materials are loaded to a stacking area and can not be loaded at the side position, the loader needs to be operated and adjusted to load in the front side, and the unnecessary operation is repeated in such a way to reduce the working efficiency; when current battery loader used, if meet unevenness's place and load overweight material and take place to turn on one's side, be unfavorable for safe problem.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
storage battery loading machine, including the battery box, the battery box front end is provided with the driver's cabin, balance mechanism is installed to the driver's cabin front end, rotary mechanism is installed to the balance mechanism front end, the bearing frame is installed at the rotary mechanism top, first support frame, two are all installed at bearing frame top both ends first support frame bottom middle section is all connected and is installed first lifter, the second lifter is installed to bearing frame top position placed in the middle, the second support frame is installed to second lifter one end, two install the backup pad between the first support frame, second support frame bottom middle section movable mounting is in the backup pad top, second support frame one end is connected and is installed the third support frame, two same loader is installed at the top that first support frame top leaned on front end and third support frame.
As a further scheme of the utility model, rotary mechanism includes preceding base, and the rotation axis is installed between two parties at preceding base top, all installs the swing pinion near four limits of rotation axis, and the motor is installed to one of them swing pinion one side, and the rotary disk is installed at the rotation axis top, and the rotary disk bottom is located the rotation axis periphery and is provided with gear clamping groove.
As a further scheme of the utility model, the balance mechanism includes the fuselage fixed plate, and the connecting block is all installed by the bottom to fuselage fixed plate both sides, and two equal movable mounting of connecting block have a mount in the rotating block, and two equal fixed mounting of rotating block one end have a mount, and two mount tops are close to one end and all connect and install hydraulic telescoping rod, and the hydraulic pump of two hydraulic telescoping rod one ends is peripheral equal fixed mounting has fixed cover, and the fixed block is all installed at fuselage fixed plate top both ends, and two equal movable mounting in fixed cover front and back ends are in the fixed block.
As a further scheme of the utility model, first support frame is movable mounting with bearing frame, loader, and first lifter is movable mounting with bearing frame, first support frame, and the second lifter is movable mounting with bearing frame, second support frame.
As a further scheme of the utility model, gear clamping groove's trench specification and rotating gear phase-match, the bearing frame is fixed mounting with the rotary disk, and the rotary disk is rotatory activity setting with the rotation axis.
As the utility model discloses a further scheme, two the mount is the arc motion, and two hydraulic telescoping rod are synchronous concertina movement, and the distance of mount one end to hydraulic telescoping rod junction equals with the distance of connecting block to fixed cover.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model discloses a set up rotary mechanism, the loader loads the material to the loader in from the material district, the straight line orders about to the stacking district, the rotatory rotary gear that drives of control motor, rotary gear drives the rotary disk and rotates to the stacking district entry, use the flexible lift and the rotation that control loader of control cabinet control first lifter and second lifter to make the material unload, accomplish the loading work, need not to carry out the automobile body and transfer to openly unload in the stacking district and load, the loading is accomplished and is continued to carry out next loading work, reduced the adjustment operation to loading the fuselage, improve the loading efficiency;
through setting up balance mechanism, use two hydraulic telescoping rod of control cabinet control to stretch out and drive two mounts and be the arc motion, make mount bottom contact ground and fix, two hydraulic telescoping rod contractions of control after the loading work is accomplished make mount one end upwards lift up and draw in, are favorable to avoiding the loading during operation to take place to turn on one's side, have improved the security of loading work.
Drawings
Fig. 1 is a schematic view of the overall structure of the battery loader of the present invention;
fig. 2 is a schematic structural view of a rotating mechanism in the battery loader of the present invention;
FIG. 3 is a bottom view of the turntable of the battery loader of the present invention;
FIG. 4 is a schematic structural view of a balancing mechanism in the battery loader of the present invention;
fig. 5 is a left side view of the battery loader of the present invention.
In the figure: 1. a battery case; 2. a driver's cab; 3. a balancing mechanism; 4. a rotation mechanism; 5. a bearing frame; 6. a first lifting rod; 7. a first support frame; 8. a second lifting rod; 9. a second support frame; 10. a loader; 11. a front base; 12. a rotating gear; 13. a rotating shaft; 14. a motor; 15. rotating the disc; 16. a gear slot; 17. a machine body fixing plate; 18. connecting blocks; 19. rotating the block; 20. a fixed mount; 21. a hydraulic telescopic rod; 22. a fixed block; 23. fixing a sleeve; 24. and a third support frame.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
As shown in fig. 1-5, the storage battery loader comprises a storage battery box 1, a driving platform 2 is arranged at the front end of the storage battery box 1, a balancing mechanism 3 is installed at the front end of the driving platform 2, a rotating mechanism 4 is installed at the front end of the balancing mechanism 3, a bearing frame 5 is installed at the top of the rotating mechanism 4, first supporting frames 7 are installed at two ends of the top of the bearing frame 5, first lifting rods 6 are installed at the middle sections of the bottoms of the two first supporting frames 7 in a connected mode, a second lifting rod 8 is installed at the middle position of the top of the bearing frame 5, a second supporting frame 9 is installed at one end of the second lifting rod 8, a supporting plate is installed between the two first supporting frames 7, the middle section of the bottom of the second supporting frame 9 is movably installed at the top of the supporting plate, a third supporting frame 24 is installed at one end of the second supporting frame 9, and the same loader 10 is installed at the top of the two first supporting frames 7 close to the front end and the top of the third supporting frame 24.
In the scheme, in order to facilitate the rotation of the rotating disc 15 for performing side loading work, the rotating mechanism 4 comprises a front base 11, a rotating shaft 13 is installed in the middle of the top of the front base 11, rotating gears 12 are installed on four sides close to the rotating shaft 13, a motor 14 is installed on one side of one rotating gear 12, the rotating disc 15 is installed on the top of the rotating shaft 13, and a gear clamping groove 16 is formed in the periphery of the rotating shaft 13 at the bottom of the rotating disc 15.
In this scheme, in order to facilitate avoiding loading during operation the overweight material of loading to take place to turn on one's side, balance mechanism 3 includes fuselage fixed plate 17, connecting block 18 is all installed by the bottom in fuselage fixed plate 17 both sides, two equal movable mounting of connecting block 18 are in rotatory piece 19, the equal fixed mounting of two rotatory piece 19 one ends has mount 20, two mount 20 tops are close to one end and all connect and install hydraulic telescoping rod 21, the equal fixed mounting in hydraulic pump periphery of two hydraulic telescoping rod 21 one ends has fixed cover 23, fixed block 22 is all installed at fuselage fixed plate 17 top both ends, the equal movable mounting in fixed block 22 of two fixed cover 23 front and back ends.
In the scheme, in order to facilitate the loader 10 to move up and down and rotate, the first support frame 7 is movably mounted with the bearing frame 5 and the loader 10, the first lifting rod 6 is movably mounted with the bearing frame 5 and the first support frame 7, and the second lifting rod 8 is movably mounted with the bearing frame 5 and the second support frame 9.
In this scheme, in order to facilitate the reinforcing rotary disk 15 to the gravity of bearing frame 5 and material, the trench specification and the rotating gear 12 phase-match of gear draw-in groove 16, bearing frame 5 is fixed mounting with rotary disk 15, and rotary disk 15 is rotatory activity setting with rotation axis 13.
In this scheme, for the convenience of mount 20 can contract simultaneously, two mounts 20 are the arc motion, and two hydraulic telescoping rod 21 are synchronous concertina movement, and the distance of mount 20 one end to the 21 junction of hydraulic telescoping rod equals with the distance of connecting block 18 to fixed cover 23.
It should be noted that, the utility model discloses a storage battery loader, when using, at first start-up machine drives to the material district, 6 shrink through two first lifters of driver's cabin 2 control, make two first support frames 7 drive loader 10 descend, control the shrink of second lifter 8 through driver's cabin 2 afterwards, make second support frame 9 drive third support frame 24 and be opposite movement, make loader 10 rotatory forward to suitable position, the drive advances to be equipped with the material splendid attire in loader 10, lift up loader 10 balance afterwards, order about loader straight to stacking district or goods car side, start two hydraulic telescoping rod 21 and drive mount 20 and move to contact ground and fix, control motor 14 through driver's cabin 2 and rotate, motor 14 axis of rotation drives a rotary gear 12 and rotates, all the other rotary gear 12 support rotary disk 15 cooperation rotations, make rotary disk 15 drive loader 10 rotate to stacking district front or goods car fill entrance, the flexible of control first lifter 6 and second lifter 8 unloads the material in the loader 10, accomplish the material and resume the shrink rotary disk 15, hydraulic telescoping rod drives the rotary disk 21 and carry out the telescopic rod under the work of drawing in the load.
The utility model discloses a set up rotary mechanism 4, the loader loads the material to loader 10 in from the material district, the straight line is ordered to the stacking district, control motor 14 is rotatory to drive a rotary gear 12 and is rotated, rotary gear 12 drives rotary disk 15 and rotates to the stacking district entry, use the flexible of driver's cabin 2 control first lifter 6 and second lifter 8 to control the lift and the rotation of loader 10 and make the material unload, accomplish the loading work, need not to carry out the automobile body and transfer to the front and unload and load in the stacking district, the loading is accomplished and is continued to carry out next loading work, reduced the adjustment operation to loading fuselage, improve loading efficiency; through setting up balance mechanism 3, use two hydraulic telescoping rod 21 of driver's cabin 2 control to stretch out and drive two mounts 20 and be the arc motion, make mount 20 bottom contact ground and fix, control two hydraulic telescoping rod 21 contractions after the loading work is accomplished, make mount 20 one end upwards lift up and draw in, be favorable to avoiding the loading work time to take place to turn on one's side, improved the security of loading work.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It should be understood by those skilled in the art that the present invention is not limited to the above embodiments, and the above embodiments and descriptions are only illustrative of the principles of the present invention, and that various changes and modifications may be made without departing from the spirit and scope of the present invention, and all such changes and modifications fall within the scope of the present invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. Storage battery loader, its characterized in that: including battery box (1), battery box (1) front end is provided with driver's cabin (2), balance mechanism (3) are installed to driver's cabin (2) front end, rotary mechanism (4) are installed to balance mechanism (3) front end, rotary mechanism (4) top is installed bearing frame (5), first support frame (7), two are all installed at bearing frame (5) top both ends first support frame (7) bottom middle section is all connected and is installed first lifter (6), second lifter (8) are installed to bearing frame (5) top position placed in the middle, second support frame (9), two are installed to second lifter (8) one end install backup pad between first support frame (7), second support frame (9) bottom middle section movable mounting is in backup pad top, second support frame (9) one end is connected and is installed third support frame (24), two same loader (10) are installed by the top of front end and third support frame (24) in first support frame (7) top.
2. The battery loader of claim 1, wherein: rotary mechanism (4) are including front base (11), and front base (11) top is installed rotation axis (13) in the middle of, and rotating gear (12) are all installed on four limits near rotation axis (13), and motor (14) are installed to one of them rotating gear (12) one side, and rotary disk (15) are installed at rotation axis (13) top, and rotary disk (15) bottom is located rotation axis (13) periphery and is provided with gear clamping groove (16).
3. The battery loader of claim 1, wherein: balance mechanism (3) include fuselage fixed plate (17), connecting block (18) are all installed by the bottom to fuselage fixed plate (17) both sides, connecting block (18) one side movable mounting has rotatory piece (19), two equal fixed mounting of rotatory piece (19) one end have mount (20), two mount (20) tops are close to one end and all connect and install hydraulic telescoping rod (21), the peripheral equal fixed mounting of hydraulic pump of two hydraulic telescoping rod (21) one end has fixed cover (23), fixed block (22) are all installed at fuselage fixed plate (17) top both ends, the equal movable mounting in fixed block (22) of two fixed cover (23) front and back ends.
4. The battery loader of claim 1, wherein: the first support frame (7) is movably mounted with the bearing frame (5) and the loader (10), the first lifting rod (6) is movably mounted with the bearing frame (5) and the first support frame (7), and the second lifting rod (8) is movably mounted with the bearing frame (5) and the second support frame (9).
5. The battery loader of claim 2, wherein: the slot position specification and the rotating gear (12) phase-match of gear draw-in groove (16), bearing frame (5) are fixed mounting with rotary disk (15), and rotary disk (15) are rotatory movable setting with rotation axis (13).
6. The battery loader of claim 3, wherein: two mount (20) are the arc motion, and two hydraulic telescoping rod (21) are synchronous concertina movement, and the distance of mount (20) one end to hydraulic telescoping rod (21) junction equals with the distance of connecting block (18) to fixed cover (23).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221634444.7U CN218861623U (en) | 2022-06-28 | 2022-06-28 | Accumulator loader |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221634444.7U CN218861623U (en) | 2022-06-28 | 2022-06-28 | Accumulator loader |
Publications (1)
Publication Number | Publication Date |
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CN218861623U true CN218861623U (en) | 2023-04-14 |
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ID=87376585
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202221634444.7U Active CN218861623U (en) | 2022-06-28 | 2022-06-28 | Accumulator loader |
Country Status (1)
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CN (1) | CN218861623U (en) |
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2022
- 2022-06-28 CN CN202221634444.7U patent/CN218861623U/en active Active
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