CN216327808U

CN216327808U - Aircraft spare part digital assembly quality convenient to operation

Info

Publication number: CN216327808U
Application number: CN202122737120.8U
Authority: CN
Inventors: 王媛媛
Original assignee: Liaoning Gangtai Aviation Technology Co ltd
Current assignee: Liaoning Gangtai Aviation Technology Co ltd
Priority date: 2021-11-10
Filing date: 2021-11-10
Publication date: 2022-04-19
Anticipated expiration: 2031-11-10

Abstract

The utility model discloses a conveniently-operated airplane part digital assembly device which comprises a workbench, a first fixing plate, a transverse plate and a second fixing plate, wherein the first fixing plate and the second fixing plate are arranged inside the workbench and are connected through the transverse plate; further comprising: the number of the first supporting plates is 2, and the bottom ends of the 2 first supporting plates are respectively connected with a first fixing plate and a second fixing plate; a second support plate disposed at a rear side of the first support plate. This aircraft parts digital assembly device convenient to operation, the bottom of first fixed plate is provided with the rack, and rack and fixed gear meshing are connected, and when fixed gear was rotatory, can drive rack and first fixed plate and carry out the displacement like this, drive the second fixed plate through the diaphragm and remove together, realize the quick adjustment to 2 group's splint intervals, bring convenient for staff's operation.

Description

Aircraft spare part digital assembly quality convenient to operation

Technical Field

The utility model relates to the technical field of airplane part processing, in particular to a digital assembling device for airplane parts, which is convenient to operate.

Background

The use of the airplane brings great convenience for people to go out remotely, the airplane is an important vehicle, a plurality of parts on the airplane are arranged, and when parts are machined, a digital assembly mode is adopted, so that the machining progress is improved.

But the present digital assembly quality still has some weak points in the use, for example, when the assembly quality used, be not convenient for fix a position spare part fast, lead to the spare part to add the phenomenon that the easy appearance of working shifted, influenced the processing effect, and inconvenient staff's operation, in to the spare part assembly course, do not have shock attenuation operation, do not cause vibrations to the operation panel easily, thereby reduced the availability factor to the assembly quality, so we have proposed the aircraft spare part digital assembly quality convenient to operation, so as to solve the problem that proposes in the aforesaid.

Disclosure of Invention

The utility model aims to provide a conveniently-operated airplane part digital assembly device, which solves the problems that when the assembly device in the prior market provided by the background art is used, the parts are not conveniently and quickly positioned, the parts are easy to displace during machining, the machining effect is influenced, the operation of workers is inconvenient, and the assembly device is easy to shake an operation table due to no damping operation during the assembly and machining process of the parts, so that the use efficiency of the assembly device is reduced.

In order to achieve the purpose, the utility model provides the following technical scheme: a digital assembly device of airplane parts convenient to operate comprises a workbench, a first fixing plate, a transverse plate and a second fixing plate, wherein the first fixing plate and the second fixing plate are arranged inside the workbench and are connected through the transverse plate;

further comprising:

the number of the first supporting plates is 2, and the bottom ends of the 2 first supporting plates are respectively connected with a first fixing plate and a second fixing plate;

the second supporting plate is arranged at the rear side of the first supporting plate, and clamping plates are arranged at the tops of the second supporting plate and the first supporting plate;

the rack is arranged at the bottom of the first fixing plate and meshed with the fixed gear, a rotating rod penetrates through the inside of the fixed gear, a connecting disc is installed at the left end of the rotating rod, and a rocker is fixed on the surface of the left side of the connecting disc.

Preferably, the left side of first fixed plate and the right side of second fixed plate all are provided with the stopper, and the through-hole has been seted up to the front side surface of workstation to the high sum that is greater than first fixed plate and rack of through-hole can make first fixed plate normally remove like this, thereby is convenient for put the spare part of not unidimensional.

Preferably, the bottom and the bottom plate of second backup pad are connected, and the inner wall of bottom plate is seted up flutedly to the inside of recess is provided with the buffer block, installs elastic spring between buffer block and the recess simultaneously, when first fixed plate removed to a certain position, can reduce the impact dynamics to the bottom plate through elastic spring like this, and then reduce the vibrations of workstation.

Preferably, splint are provided with 2 groups, and every group splint are provided with 2 to overlook of splint is "7" font, is convenient for carry out better spacing operation to spare part, the convenient processing to spare part.

Preferably, stopper and first fixed plate formula structure as an organic whole, and stopper and second fixed plate formula structure as an organic whole to the connected mode of stopper and workstation is sliding connection, can make first fixed plate and second fixed plate remove more steadily under the effect of stopper, further guarantees going on of whole operation stably.

Preferably, all seted up spacing hole on connection pad and the workstation, and the inside block in spacing hole is connected with the gag lever post to spacing hole is equiangular distribution on the connection pad, is convenient for carry on spacingly to the connection pad like this, thereby is convenient for carry on spacingly to the rotary rod, effectively prevents that self-rotation pivoted phenomenon from appearing in the rotary rod.

Compared with the prior art, the utility model has the beneficial effects that: the digital assembly device for the airplane parts convenient to operate,

(1) the clamping device is provided with a first fixing plate and a second fixing plate which are connected through a transverse plate, a rack is arranged at the bottom of the first fixing plate and meshed with the fixing gear, so that the rack and the first fixing plate can be driven to move when the fixing gear rotates, and the second fixing plate is driven to move through the transverse plate, so that a first supporting plate and clamping plates above the first fixing plate and the second fixing plate can move, the space between 2 groups of clamping plates can be quickly adjusted, parts can be conveniently positioned, the clamping device is suitable for placing parts with different sizes, and convenience is brought to operation of workers;

(2) the bottom and the bottom plate of second backup pad are connected, and the inner wall of bottom plate is seted up flutedly to the inside buffer block that is provided with of recess, install elastic spring simultaneously between the inner wall of buffer block and recess, when first fixed plate removes to be close to like this, can cushion the impact dynamics of first fixed plate through elastic spring, and then reduce the striking dynamics to the bottom plate, stability when guaranteeing bottom plate and workstation use effectively reduces the phenomenon that the amplitude appears.

Drawings

FIG. 1 is a schematic view of an overall main sectional structure of the present invention;

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

FIG. 3 is a schematic top view of a first fixing plate according to the present invention;

FIG. 4 is a schematic cross-sectional view of the first fixing plate of the present invention;

FIG. 5 is an enlarged view of a portion a of FIG. 1 according to the present invention;

FIG. 6 is a schematic diagram of a side view of the connecting pad of the present invention.

In the figure: 1. a work table; 101. a through hole; 2. a first fixing plate; 3. a transverse plate; 4. a second fixing plate; 5. a first support plate; 6. a second support plate; 601. a base plate; 602. a groove; 603. a buffer block; 604. an elastic spring; 7. a splint; 8. a limiting block; 9. a rack; 10. fixing a gear; 11. rotating the rod; 12. a connecting disc; 13. a limiting hole; 14. a limiting rod; 15. a rocker.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-6, the present invention provides a technical solution: a digital assembly device of aircraft parts convenient to operation comprises a workbench 1, a first fixing plate 2, a transverse plate 3 and a second fixing plate 4, wherein the workbench 1 is internally provided with the first fixing plate 2 and the second fixing plate 4 which are connected through the transverse plate 3, the left side of the first fixing plate 2 and the right side of the second fixing plate 4 are both provided with a limiting block 8, the front side surface of the workbench 1 is provided with a through hole 101, the height of the through hole 101 is larger than the sum of the heights of the first fixing plate 2 and a rack 9, the limiting block 8 and the first fixing plate 2 are of an integral structure, the limiting block 8 and the second fixing plate 4 are of an integral structure, the connecting mode of the limiting block 8 and the workbench 1 is sliding connection, parts to be processed are placed on the workbench 1, and the parts and a clamping plate 7 at the rear side are mutually attached, when the first fixing plate 2 moves in the later stage, the first fixing plate can pass through the through hole 101, so that the normal movement of the first fixing plate 2 is ensured;

further comprising:

the number of the first supporting plates 5 is 2, and the bottom ends of the 2 first supporting plates 5 are respectively connected with the first fixing plate 2 and the second fixing plate 4;

the second supporting plate 6 is arranged at the rear side of the first supporting plate 5, clamping plates 7 are arranged at the tops of the second supporting plate 6 and the first supporting plate 5, the bottom of the second supporting plate 6 is connected with the bottom plate 601, a groove 602 is formed in the inner wall of the bottom plate 601, a buffer block 603 is arranged in the groove 602, an elastic spring 604 is arranged between the buffer block 603 and the

groove

602, 2 groups of clamping plates 7 are arranged, 2 clamping plates 7 are arranged in each group, the overlooking surfaces of the clamping plates 7 are in a 7 shape, when the first fixing plate 2 moves to be attached to the buffer block 603 and moves, the elastic spring 604 can be extruded, and the first fixing plate 2 enters the groove 602, so that the impact force of the first fixing plate 2 on the bottom plate 601 can be relieved under the action of the elastic spring 604, the vibration of the workbench 1 is reduced, and the limit operation of parts is not influenced, the use efficiency of the device is improved;

a rack 9 which is arranged at the bottom of the first fixing plate 2, the rack 9 is meshed with the fixed gear 10, a rotating rod 11 penetrates through the fixed gear 10, a connecting disc 12 is arranged at the left end of the rotating rod 11, a rocker 15 is fixed on the left surface of the connecting disc 12, limiting holes 13 are formed in the connecting disc 12 and the workbench 1, a limiting rod 14 is clamped and connected in the limiting holes 13, the limiting holes 13 are distributed on the connecting disc 12 at equal angles, a worker rotates the rocker 15 anticlockwise to enable the rocker 15 to drive the connecting disc 12 and the rotating rod 11 to rotate together, the fixed gear 10 is fixed on the outer wall of the rotating rod 11, the fixed gear 10 is meshed and connected with the rack 9 at the bottom of the first fixing plate 2, so that when the fixed gear 10 rotates anticlockwise, the rack 9 and the first fixing plate 2 can be driven to move backwards, wherein the first fixing plate 2 is connected with the second fixing plate 4 through a transverse plate 3, so when first fixed plate 2 removes, can drive second fixed plate 4 and remove together, just so make first backup pad 5 and splint 7 of first fixed plate 2 and second fixed plate 4 top remove, be close to gradually between the splint 7 of front side and the splint 7 of rear side promptly, along with the removal of rear side splint 7, can press from both sides tight spacing to the spare part, can be applicable to the spacing operation of not unidimensional spare part like this, it is convenient to bring for staff's operation.

The working principle is as follows: when the airplane parts digital assembling device convenient to operate is used, as shown in fig. 1-6, firstly, a worker puts the device at a corresponding position, then places parts to be processed on the workbench 1, and makes the parts and the clamping plate 7 at the rear side mutually attached, then the worker takes the limiting rod 14 out of the limiting hole 13, then rotates the rocker 15 anticlockwise, makes the rocker 15 drive the connecting disc 12, the rotating bar 11 and the fixed gear 10 to rotate together, and drives the rack 9 and the first fixing plate 2 to move backwards through the fixed gear 10, so that the first supporting plate 5 and the clamping plate 7 above the first fixing plate 2 and the second fixing plate 4 move, namely the clamping plate 7 at the front side and the clamping plate 7 at the rear side gradually approach each other, along with the movement of the clamping plate 7 at the rear side, the parts can be clamped and limited, when the first fixing plate 2 moves to be attached to the buffer block 603 and is still moving, the elastic spring 604 can be squeezed, and the first fixing plate 2 enters the groove 602, so that under the action of the elastic spring 604, the impact force of the first fixing plate 2 on the bottom plate 601 can be relieved, further the vibration on the workbench 1 is reduced, and meanwhile, the limiting operation on parts is not affected, which is the working process of the whole device, and the content which is not described in detail in the specification belongs to the prior art known by persons skilled in the art.

Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that various changes in the embodiments and/or modifications of the utility model can be made, and equivalents and modifications of some features of the utility model can be made without departing from the spirit and scope of the utility model.

Claims

1. The airplane part digital assembly device convenient to operate comprises a workbench (1), a first fixing plate (2), a transverse plate (3) and a second fixing plate (4), wherein the first fixing plate (2) and the second fixing plate (4) are arranged inside the workbench (1), and the first fixing plate (2) is connected with the second fixing plate (4) through the transverse plate (3);

it is characterized by also comprising:

the number of the first supporting plates (5) is 2, and the bottom ends of the 2 first supporting plates (5) are respectively connected with the first fixing plate (2) and the second fixing plate (4);

the second supporting plate (6) is arranged on the rear side of the first supporting plate (5), and clamping plates (7) are mounted at the tops of the second supporting plate (6) and the first supporting plate (5);

the rack (9) is arranged at the bottom of the first fixing plate (2), the rack (9) is meshed with the fixed gear (10) and connected with the fixed gear (10), a rotating rod (11) penetrates through the inside of the fixed gear (10), a connecting disc (12) is installed at the left end of the rotating rod (11), and a rocker (15) is fixed on the surface of the left side of the connecting disc (12).

2. The digital assembly device for aircraft parts, which is convenient to operate, according to claim 1, is characterized in that: the left side of first fixed plate (2) and the right side of second fixed plate (4) all are provided with stopper (8), and through-hole (101) have been seted up to the front side surface of workstation (1) to the height of through-hole (101) is greater than the sum of the height of first fixed plate (2) and rack (9).

3. The digital assembly device for aircraft parts, which is convenient to operate, according to claim 1, is characterized in that: the bottom of the second supporting plate (6) is connected with the bottom plate (601), a groove (602) is formed in the inner wall of the bottom plate (601), a buffer block (603) is arranged inside the groove (602), and meanwhile an elastic spring (604) is arranged between the buffer block (603) and the groove (602).

4. The digital assembly device for aircraft parts, which is convenient to operate, according to claim 1, is characterized in that: the clamping plates (7) are provided with 2 groups, each group of clamping plates (7) is provided with 2 clamping plates, and the overlooking of the clamping plates (7) is in a 7 shape.

5. An easy-to-operate digital assembly device for aircraft parts according to claim 2, wherein: stopper (8) and first fixed plate (2) formula structure as an organic whole, and stopper (8) and second fixed plate (4) formula structure as an organic whole to the connected mode of stopper (8) and workstation (1) is sliding connection.

6. The digital assembly device for aircraft parts, which is convenient to operate, according to claim 1, is characterized in that: spacing hole (13) have all been seted up on connection pad (12) and workstation (1), and the inside block of spacing hole (13) is connected with gag lever post (14) to spacing hole (13) equiangular distribution on connection pad (12).