CN214031617U

CN214031617U - Adjustable lifting machine aircraft nose structure

Info

Publication number: CN214031617U
Application number: CN202023226639.1U
Authority: CN
Inventors: 王庆海; 王平超; 杨宝; 李江信
Original assignee: Qingdao Jinyichang Electromechanical Co ltd
Current assignee: Qingdao Jinyichang Electromechanical Co ltd
Priority date: 2020-12-28
Filing date: 2020-12-28
Publication date: 2021-08-24
Anticipated expiration: 2030-12-28

Abstract

The utility model relates to a lifting machine technical field just discloses an adjustable lifting machine aircraft nose structure, including organism, clamp, screw shaft and flexible cover, organism one side is provided with the spout, and the inside electronic slider that is provided with of spout, electronic slider one side is provided with the draw-in groove, and the draw-in groove inboard is provided with the fixture block, fixture block one side is provided with the mounting bracket, and mounting bracket one side is provided with the cylinder, cylinder one side is provided with the aircraft nose, and aircraft nose outer wall one side is provided with rotatory piece, the clamp sets up in the draw-in groove outside, and clamp one side is provided with fixing bolt. This adjustable lifting machine aircraft nose structure through setting up organism, spout, electronic slider, draw-in groove, fixture block, mounting bracket, clamp and fixing bolt, can play the effect of height-adjusting of being convenient for to the device, can adjust the height of device according to the demand of using to in the different in service behavior of adaptation, make the use of device more convenient.

Description

Adjustable lifting machine aircraft nose structure

Technical Field

The utility model relates to a lifting machine technical field specifically is an adjustable lifting machine aircraft nose structure.

Background

The hoist is the large-scale mechanical equipment that transports through changing potential energy, such as mine hoist, dam-crossing hoist etc. broadly speaking, the elevator, the overhead traveling crane, the hoist, the firm car, the crane, hoist and so on all can be called the hoist, the hoist generally indicates the large-scale mechanical equipment that power is great, the lifting power is stronger, drag flexible piece wire rope and the goods of transporting to move from top to bottom through power machinery and accomplish the transportation, wire rope is the indispensable important part of hoisting machinery, but present hoist aircraft nose most do not possess adjustable effect, can't adjust the position and the angle of aircraft nose according to the demand of using when using, it is convenient inadequately during the use, thereby greatly reduced the result of use of the device.

But the aircraft nose structure that uses at present, most do not possess adjustable effect, can't adjust the position and the angle of aircraft nose according to the demand of using when using, and the aircraft nose is convenient inadequately when using, influences the controllability of device to greatly reduced the result of use of device.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an adjustable lifting machine aircraft nose structure possesses the effect of being convenient for to adjust advantages such as, the aircraft nose structural effect of the present use of solution is not good problem.

(II) technical scheme

For the purpose of realizing that above-mentioned aircraft nose structure is convenient for adjust, the utility model provides a following technical scheme: an adjustable hoister head structure comprises a hoister body, a hoop, a threaded shaft and a telescopic sleeve, wherein one side of the hoister body is provided with a chute, an electric slide block is arranged in the sliding groove, a clamping groove is arranged at one side of the electric slide block, a clamping block is arranged at the inner side of the clamping groove, a mounting frame is arranged at one side of the clamping block, and one side of the mounting frame is provided with an air cylinder, one side of the air cylinder is provided with a machine head, one side of the outer wall of the machine head is provided with a rotating block, the clamp is arranged outside the clamping groove, and one side of the hoop is provided with a fixing bolt, the threaded shafts are all arranged on one side of the chute, one side of the threaded shafts is provided with a baffle plate, the telescopic sleeves are all arranged on two sides of the inner wall of the machine head, and the inner side of the telescopic sleeve is provided with a telescopic rod, one side of the telescopic rod is provided with an inner container, a buffer sponge is arranged below the inner container, one side of the buffer sponge is provided with a movable hook, and one side of the movable hook is provided with a movable block.

Preferably, the mounting rack, the electric slider and the machine body form a sliding structure, and the mounting rack and the machine body are distributed in parallel.

Preferably, the mounting bracket is connected with the electric slider in a clamping manner through a clamping block, and the mounting bracket is distributed in parallel with the electric slider.

Preferably, the machine head, the cylinder and the mounting frame form a lifting structure, and the size of the cylinder is smaller than that of the machine head.

Preferably, the baffle, the threaded shaft and the chute form a rotating structure, and the baffle is distributed at equal intervals on one side of the chute.

Preferably, the inner container, the telescopic rod and the machine head form a telescopic structure, and the telescopic rod is symmetrically distributed on the central axis of the inner container.

Preferably, the buffering sponge passes through movable hook and aircraft nose swing joint, and the movable hook is equidistant distribution in buffering sponge one side.

(III) advantageous effects

Compared with the prior art, the utility model provides an adjustable lifting machine aircraft nose structure possesses following beneficial effect:

1. this adjustable lifting machine aircraft nose structure, through setting up the organism, the spout, electronic slider, the draw-in groove, the fixture block, the mounting bracket, clamp and fixing bolt, can play the effect of a height-adjusting of being convenient for to the device, can adjust the height of device according to the demand of using, so as to adapt to different in service behavior, make the use of device more convenient, the setting of fixture block and draw-in groove simultaneously, can play a convenient to detach's effect to the mounting bracket of the device, prevent that the device from taking place to damage and can't in time dismantle the maintenance, influence the subsequent use of device, clamp and fixing bolt's setting, install more firmly during, thereby the effectual regulation efficiency who promotes the device.

2. This adjustable lifting machine aircraft nose structure through being provided with mounting bracket, cylinder, aircraft nose and rotatory piece, can play the effect of the angle regulation of being convenient for to the device, can open the cylinder when using and make the cylinder drive the aircraft nose and carry out the lifting, and the aircraft nose drives rotatory piece simultaneously and rotates to adjust the angle, use more convenient, thereby effectual the result of use that has promoted the device.

3. This adjustable lifting machine aircraft nose structure, through being provided with the telescope tube, the telescopic link, the inner bag, the buffering sponge, movable hook and movable block, can play the effect of a change inner bag of being convenient for to the device, prevent that the inside long-time use of aircraft nose from taking place wearing and tearing or damage, can need not to change the aircraft nose, direct change to inner bag and retrograde motion, the setting of telescope tube and telescopic link, can play a fixed spacing effect to the inner bag of the device, prevent that the inner bag from rocking back and forth in the aircraft nose is inside, the influence is used, the buffering sponge, the setting of movable hook and movable block, can be better protect the bottom of inner bag, prevent that pressure is too big when the installation, lead to inner bag and aircraft nose to take place to collide with, lead to damaging, thereby the effectual life who promotes the device.

Drawings

FIG. 1 is a schematic view of a front cross-sectional structure of the present invention;

FIG. 2 is a schematic front view of the present invention;

FIG. 3 is a connection diagram of the threaded shaft and the baffle plate of the present invention;

fig. 4 is a connection diagram of the telescopic sleeve and the telescopic rod of the utility model.

In the figure: 1. a body; 2. a chute; 3. an electric slider; 4. a card slot; 5. a clamping block; 6. a mounting frame; 7. a cylinder; 8. a machine head; 9. rotating the block; 10. clamping a hoop; 11. fixing the bolt; 12. a threaded shaft; 13. a baffle plate; 14. a telescopic sleeve; 15. a telescopic rod; 16. an inner container; 17. a buffer sponge; 18. a movable hook; 19. a movable block.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, an adjustable elevator machine head structure comprises a machine body 1, a clamp 10, a threaded shaft 12 and a telescopic sleeve 14, wherein a sliding groove 2 is arranged on one side of the machine body 1, an electric slider 3 is arranged inside the sliding groove 2, a clamping groove 4 is arranged on one side of the electric slider 3, a clamping block 5 is arranged on the inner side of the clamping groove 4, a mounting frame 6 is arranged on one side of the clamping block 5, an air cylinder 7 is arranged on one side of the mounting frame 6, a machine head 8 is arranged on one side of the air cylinder 7, a rotating block 9 is arranged on one side of the outer wall of the machine head 8, the clamp 10 is arranged outside the clamping groove 4, a fixing bolt 11 is arranged on one side of the clamp 10, the threaded shaft 12 is arranged on one side of the sliding groove 2, a baffle 13 is arranged on one side of the threaded shaft 12, the telescopic sleeve 14 is arranged on both sides of the inner wall of the machine head 8, a telescopic rod 15 is arranged on the inner side of the telescopic sleeve 14, an inner container 16 is arranged on one side of the telescopic rod, and a buffer sponge 17 is arranged below the inner container 16, one side of the buffer sponge 17 is provided with a movable hook 18, and one side of the movable hook 18 is provided with a movable block 19.

Further, mounting bracket 6, electronic slider 3 constitute sliding structure with organism 1, and mounting bracket 6 and organism 1 parallel distribution, through setting up organism 1, spout 2 and electronic slider 3, can play the effect of height-adjusting of being convenient for to the device, can adjust the height of device according to the demand of using to in the different in service behavior of adaptation, it is more convenient to make the use of device, thereby the effectual result of use that has promoted the device.

Further, mounting bracket 6 passes through fixture block 5 and is connected with 3 blocks of electronic slider, and mounting

bracket

6 and 3 parallel distribution of electronic slider, through being provided with draw-in groove 4, fixture block 5, mounting bracket 6, clamp 10 and fixing bolt 11, can play a convenient to detach's effect to the device's mounting bracket 6, prevent that the device from taking place to damage and can't in time dismantling the maintenance, influence the subsequent use of device, clamp 10 and fixing bolt 11's setting, the time installation is more firm, thereby the effectual regulation efficiency that has promoted the device.

Further, aircraft nose 8, cylinder 7 constitutes elevation structure with mounting bracket 6, and the size of cylinder 7 is less than aircraft nose 8's size, through being provided with mounting bracket 6, cylinder 7, aircraft nose 8 and rotatory piece 9, can play the effect of the angle regulation of being convenient for to the device, can open cylinder 7 when using and make cylinder 7 drive aircraft nose 8 and carry out the lifting, aircraft nose 8 drives rotatory piece 9 simultaneously and rotates, thereby adjust the angle, it is more convenient to use, thereby the effectual result of use that has promoted the device.

Further, baffle 13, threaded shaft 12 and spout 2 constitute revolution mechanic, and baffle 13 is equidistant distribution in spout 2 one side, through being provided with baffle 13 and threaded shaft 12, can play a fixed effect of being convenient for to the device, because aircraft nose 8's weight is too big, prevent that aircraft nose 8 from making a round trip to rock in spout 2 inside when using, and is unable stable, aircraft nose 8's stability can be ensured in baffle 13 and threaded shaft 12's setting, thereby the effectual result of use that has promoted the device.

Further, inner bag 16, telescopic link 15 and aircraft nose 8 constitute extending structure, and telescopic link 15 is with 16 axis symmetric distributions of inner bag, through being provided with telescope tube 14, telescopic link 15 and inner bag 16, can play the effect of a being convenient for change inner bag 16 to the device, prevent that aircraft nose 8 is inside to be used for a long time and take place wearing and tearing or damage, can need not to change aircraft nose 8, it is direct to inner bag 16 and the converse change, the setting of telescope tube 14 and telescopic link 15, can play a fixed spacing effect to the device's inner bag 16, prevent that inner bag 16 from rocking back and forth in aircraft nose 8 inside, influence the use.

Further, buffering sponge 17 passes through movable hook 18 and aircraft nose 8 swing joint, and movable hook 18 is equidistant distribution in buffering sponge 17 one side, through being provided with buffering sponge 17, movable hook 18 and activity piece 19, can be better protect the bottom of inner bag 16, prevent that pressure is too big when the installation, lead to inner bag 16 and aircraft nose 8 to take place to collide with, lead to damaging to the effectual life who promotes the device.

The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.

When the device is used, firstly, an external power supply is switched on, the machine head 8 is pushed to enable the machine head 8 to drive the clamping block 5 to be clamped and connected with the clamping groove 4, so that the machine head 8 is fixedly connected with the electric sliding block 3, then the clamping hoop 10 is sleeved outside the clamping block 5 and the clamping groove 4 and is screwed and fixed by the fixing bolt 11, then the electric sliding block 3 is opened to enable the electric sliding block 3 to drive the machine head 8 to move up and down to a proper position in the sliding groove 2, then the baffle 13 is pulled to enable the baffle 13 to drive the threaded shaft 12 to rotate and fix inwards, then the buffer sponge 17 is pushed to enable the buffer sponge 17 to drive the movable hook 18 to be fixedly connected with the movable block 19, so that the buffer sponge 17 is fixed in the machine head 8, then the inner container 16 is pushed to enable the inner container 16 to drive the telescopic rod 15 to move back and forth in the telescopic sleeve 14, finally the air cylinder 7 is opened to enable the air cylinder 7 to drive one side of the machine head 8 to lift upwards, so that the machine head 8 drives the rotary block 9 to rotate to a proper angle, the model of the electric sliding block 3 is as follows: PKH40, model number of cylinder 7: YS-NZ100-12A, which makes the use more convenient.

In conclusion, the adjustable hoister head structure can achieve the effect of being convenient to adjust, and enables people to be more convenient to use.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an adjustable lifting machine aircraft nose structure, includes organism (1), clamp (10), threaded shaft (12) and flexible cover (14), its characterized in that: the machine body (1) is provided with a sliding groove (2) on one side, an electric slider (3) is arranged inside the sliding groove (2), a clamping groove (4) is arranged on one side of the electric slider (3), a clamping block (5) is arranged on the inner side of the clamping groove (4), a mounting frame (6) is arranged on one side of the clamping block (5), an air cylinder (7) is arranged on one side of the mounting frame (6), a machine head (8) is arranged on one side of the air cylinder (7), a rotating block (9) is arranged on one side of the outer wall of the machine head (8), a clamp (10) is arranged outside the clamping groove (4), a fixing bolt (11) is arranged on one side of the clamp (10), threaded shafts (12) are arranged on one side of the sliding groove (2), a baffle (13) is arranged on one side of the threaded shafts (12), telescopic sleeves (14) are arranged on two sides of the inner wall of the machine head (8), and telescopic rods (15) are arranged on the inner side of the telescopic sleeves (14), the telescopic rod (15) is provided with inner bag (16) one side, and is provided with buffering sponge (17) below inner bag (16), buffering sponge (17) one side all is provided with movable hook (18), and is provided with movable block (19) on one side of movable hook (18).

2. The adjustable elevator machine head structure of claim 1, wherein: the mounting frame (6), the electric sliding block (3) and the machine body (1) form a sliding structure, and the mounting frame (6) and the machine body (1) are distributed in parallel.

3. The adjustable elevator machine head structure of claim 1, wherein: the mounting rack (6) is connected with the electric sliding block (3) in a clamping mode through the clamping block (5), and the mounting rack (6) and the electric sliding block (3) are distributed in parallel.

4. The adjustable elevator machine head structure of claim 1, wherein: the machine head (8), the air cylinder (7) and the mounting frame (6) form a lifting structure, and the size of the air cylinder (7) is smaller than that of the machine head (8).

5. The adjustable elevator machine head structure of claim 1, wherein: the baffle (13), the threaded shaft (12) and the chute (2) form a rotating structure, and the baffle (13) is distributed at equal intervals on one side of the chute (2).

6. The adjustable elevator machine head structure of claim 1, wherein: the inner container (16), the telescopic rod (15) and the machine head (8) form a telescopic structure, and the telescopic rod (15) is symmetrically distributed along the central axis of the inner container (16).

7. The adjustable elevator machine head structure of claim 1, wherein: the buffer sponge (17) is movably connected with the machine head (8) through the movable hooks (18), and the movable hooks (18) are distributed at equal intervals on one side of the buffer sponge (17).