CN220613782U - Fixing clamp for overhauling aviation parts - Google Patents

Abstract

The utility model discloses a fixing clamp for overhauling aviation parts, which comprises a clamp, a bottom ring and a clamping head, wherein a bottom plate is arranged at the bottom of the clamp, two sides of the bottom plate are fixedly connected with a fixing plate, a rotating shaft is sleeved above the fixing plate, a handle is arranged in the rotating shaft, the bottom of the handle is sleeved with the clamp, a shaft column is arranged in the fixing plate, the surface of the shaft column is sleeved with the clamp, the surface of the fixing plate is provided with a plate groove, a baffle is inserted in the plate groove, and the surface of the baffle is fixedly connected with a handle. This kind of mounting fixture for aviation spare part overhauls lets this kind of anchor clamps can rotate through pulling out the handle from the frame inslot portion, then rotates the handle and rotates the convenient detection of suitable position with anchor clamps, can see the most places of spare part when using, more conveniently observes and overhauls aviation spare part.

Description

Fixing clamp for overhauling aviation parts

Technical Field

The utility model belongs to the technical field of clamps, and particularly relates to a fixing clamp for overhauling aviation parts.

Background

Aviation is an emerging field which occurs along with the development of the era, and is often referred to as the flying movement of an aircraft in the earth atmosphere, due to the utilization of an air space and the aircraft, because of the special nature of the aviation field, the precision and precision of the aviation field need to be ensured, when the aviation parts need to be overhauled, the aviation parts need to be fixed through a clamp, and then the parts need to be overhauled, the clamp is used for fixing a processing object in the mechanical manufacturing and overhauling process so as to occupy the correct position, and in the broad sense, any procedure in the manufacturing and overhauling process is also referred to as a clamp for fixing and clamping.

The following problems exist in the conventional fixing clamp for overhauling aviation parts in the market:

1. when the traditional fixing clamp for overhauling the aviation parts is applied, a worker can not see the whole appearance of the parts when overhauling because the clamp can not flexibly rotate when clamping the aviation parts, but can not comprehensively see the parts, and the parts are more inconvenient to overhaul;

2. most of the fixing clamps for overhauling aviation parts are used, when the clamping heads of the clamps fix the aviation parts, for example, instability of clamping of the clamps can occur, or slipping of the parts with irregular clamping can occur, so that the clamps are poor in stability during clamping.

Disclosure of Invention

The utility model aims to provide a fixing clamp for overhauling aviation parts, which aims to solve the technical problems in the background technology.

In order to achieve the above purpose, the specific technical scheme of the utility model is as follows: the utility model provides an aviation spare part overhauls and uses mounting fixture, includes anchor clamps, foundation ring and chuck, the bottom of anchor clamps is equipped with the bottom plate, the both sides fixed connection fixed plate of bottom plate, the pivot is cup jointed to the top of fixed plate, the internally mounted handle of pivot, anchor clamps are cup jointed to the bottom of handle, the internally mounted spliced axle post of fixed plate, anchor clamps are cup jointed on the surface of axle post, the board groove is seted up on the surface of fixed plate, the inside grafting baffle of board groove, the fixed surface connection handle of baffle, the fixed surface connection picture peg of baffle.

Preferably, the telescopic device is arranged above the clamp, the sleeve of the telescopic device is sleeved with the fixed cylinder, the chuck is arranged at the front end of the telescopic device, the anti-skid blocks are arranged on the surfaces of the chucks, the convex grooves are formed in the surfaces of the chucks, anti-skid stripes are embedded on the surfaces of the anti-skid blocks, the rear faces of the anti-skid blocks are fixedly connected with the convex blocks, the convex blocks are slidingly connected with the surfaces of the convex blocks, the anti-skid blocks are arranged on the surfaces of the chucks in an equidistant distribution mode.

Preferably, the surface of the telescopic device is fixedly connected with a sleeve, the telescopic rod is sleeved in the sleeve, and the other end of the telescopic rod is fixedly connected with the clamping head.

Preferably, a bottom ring is arranged above the clamp, a fixed cylinder is fixedly connected above the bottom ring, a bottom column is fixedly connected below the bottom ring, a base is fixedly connected below the bottom column, and the bottom of the base is embedded into the clamp.

Preferably, a control device is installed above the clamp, and a button is installed above the control device.

The fixing clamp for overhauling the aviation parts has the following advantages:

1. the fixing clamp for overhauling the aviation parts is characterized in that a bottom plate is arranged on the clamp, the bottom plate is fixedly connected with two side fixing plates, the fixing plates are sleeved with a rotating shaft internally provided with handles, the handles are sleeved with the clamp, one end of each fixing plate is provided with a shaft post sleeved with the clamp, the other end of each fixing plate is provided with a plate groove for plugging a baffle, the baffle is fixedly connected with a handle and a plugboard, the rotating shaft and the handles which are arranged through the clamp are used for clamping the parts, the handle is pulled out of the frame groove firstly, the clamp can be rotated, then the handles are rotated to rotate the clamp to a proper position for convenient detection, most of parts can be seen during use, and the aviation parts can be observed and overhauled more conveniently;

2. this mounting fixture for aviation spare part overhauls, install telescoping device through the top of anchor clamps and cup joint fixed section of thick bamboo, the tongue is seted up on telescopic mounting chuck surface, antiskid strip is inlayed to the antiskid block, antiskid block fixed connection lug sliding connection tongue, through chuck surface mounting antiskid block, antiskid strip above the antiskid block is being added, three chuck has in addition, simultaneously distribute in different positions, triangle-shaped has stable effect moreover, when the irregular spare part of anchor clamps centre gripping and easy gliding spare part, the antiskid block can reduce the friction on object surface, the phenomenon of clamp instability appears when the centre gripping spare part has been improved to most anchor clamps.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present utility model and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

FIG. 1 is a schematic diagram of the overall structure of the present utility model;

FIG. 2 is a schematic diagram of a base plate structure according to the present utility model;

FIG. 3 is a schematic view of the bottom ring structure of the present utility model;

FIG. 4 is a schematic diagram of a shaft stud according to the present utility model;

FIG. 5 is a schematic view of a baffle structure according to the present utility model;

FIG. 6 is a schematic view of a chuck according to the present utility model;

FIG. 7 is a schematic view of a telescopic device according to the present utility model;

the figure indicates: 1. a clamp; 2. a bottom ring; 3. a chuck; 4. a control device; 5. a handle; 6. a bottom plate; 7. a fixing plate; 8. a baffle; 9. a button; 10. a rotating shaft; 11. a fixed cylinder; 12. a telescoping device; 13. a base; 14. a bottom post; 15. a telescopic rod; 16. a plate groove; 17. a shaft post; 18. a sleeve; 19. a grip; 20. inserting plate; 21. an anti-skid block; 22. anti-slip stripes; 23. a convex groove; 24. and a bump.

Detailed Description

Hereinafter, only certain exemplary embodiments are briefly described. As will be recognized by those of skill in the pertinent art, the described embodiments may be modified in numerous different ways without departing from the spirit or scope of the embodiments of the present utility model. Accordingly, the drawings and description are to be regarded as illustrative in nature and not as restrictive.

In the description of the embodiments of the present utility model, it should be understood that the terms "length," "vertical," "horizontal," "top," "bottom," and the like indicate an orientation or a positional relationship based on that shown in the drawings, and are merely for convenience in describing the embodiments of the present utility model and to simplify the description, rather than to indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the embodiments of the present utility model.

Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the embodiments of the present utility model, the meaning of "plurality" is two or more, unless explicitly defined otherwise.

In the embodiments of the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured" and the like are to be construed broadly and include, for example, either permanently connected, removably connected, or integrally formed; the device can be mechanically connected, electrically connected and communicated; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the embodiments of the present utility model will be understood by those of ordinary skill in the art according to specific circumstances.

The following disclosure provides many different implementations, or examples, for implementing different configurations of embodiments of the utility model. In order to simplify the disclosure of embodiments of the present utility model, components and arrangements of specific examples are described below. Of course, they are merely examples and are not intended to limit embodiments of the present utility model. Furthermore, embodiments of the present utility model may repeat reference numerals and/or letters in the various examples, which are for the purpose of brevity and clarity, and which do not themselves indicate the relationship between the various embodiments and/or arrangements discussed.

In order to better understand the purpose, structure and function of the utility model, the utility model relates to a fixing clamp for overhauling aviation parts, which is further described in detail below with reference to the accompanying drawings.

As shown in figures 1-7, the fixing clamp for overhauling an aviation part comprises a clamp 1, a bottom ring 2 and a clamping head 3, wherein the bottom of the clamp 1 is provided with a bottom plate 6, two sides of the bottom plate 6 are fixedly connected with a fixing plate 7, a rotating shaft 10 is sleeved above the fixing plate 7, a handle 5 is arranged in the rotating shaft 10, the bottom of the handle 5 is sleeved with the clamp 1, a shaft column 17 is arranged in the fixing plate 7, the surface of the shaft column 17 is sleeved with the clamp 1, a plate groove 16 is formed in the surface of the fixing plate 7, a baffle plate 8 is inserted in the plate groove 16, a handle 19 is fixedly connected with the surface of the baffle plate 8, the part clamped by the clamp 1 is rotated through the rotating shaft 10 and the handle 5 which are arranged by the clamp 1, the handle 19 is firstly held to be pulled out from the inside of the frame groove, then the handle 5 is rotated to rotate the clamp 1 to a proper position for convenient detection, the whole of the part can not be seen when the traditional aviation part overhauling fixing clamp 1 is overhauled, and the whole part can be seen when the aviation part overhauling is overhauled.

The telescopic device 12 is arranged above the clamp 1, the fixed cylinder 11 is sleeved on the telescopic device 12, the clamp head 3 is arranged at the front end of the telescopic device, the anti-slip block 21 is arranged on the surface of the clamp head 3, the convex groove 23 is formed in the surface of the clamp head 3, the anti-slip stripes 22 are embedded in the surface of the anti-slip block 21, the convex block 24 is fixedly connected with the convex groove 23 in a sliding manner on the rear surface of the anti-slip block 21, the anti-slip blocks 21 are arranged on the surface of the clamp head 3 in an equidistant distribution mode, the anti-slip stripes 22 on the anti-slip blocks 21 are arranged on the surface of the clamp head 3, the anti-slip stripes are arranged on the clamp head 3 at different positions, the triangle has a stable effect, when the clamp head 1 clamps irregular parts and easily-sliding parts, the anti-slip blocks 21 can reduce friction on the surfaces of objects, the phenomenon that most clamps 1 are unstable in clamping the parts is improved, and the stability in clamping is improved.

The telescopic device 12 surface fixed connection sleeve 18, telescopic link 15 is cup jointed to sleeve 18's inside, and the chuck 3 is connected to the other fixed connection of telescopic link 15, carries out the centre gripping with spare part through the preceding chuck 3 of telescopic device 12, and stability is stronger.

The top of anchor clamps 1 is equipped with foundation ring 2, and the fixed section of thick bamboo of top fixed connection of foundation ring 2 11, the below fixed connection foundation post 14 of foundation ring 2, the lower fixed connection base 13 of foundation post 14, the bottom embedding anchor clamps 1 of base 13, owing to the three group foundation ring 2 structures that are equipped with, better realization three direction centre gripping's effect, its intensity of centre gripping is higher.

The control device 4 is installed above the clamp 1, the button 9 is installed above the control device 4, and due to the control device 4, an operator can conveniently control the clamp, and the operation is convenient.

The working principle of the fixing clamp for overhauling the aviation parts is as follows: firstly, aeronautical parts are placed into a clamp, the telescopic device 12 is controlled by the control device 4, the telescopic device 12 can be linked with the telescopic rod 15 to fix aeronautical parts, when the clamp 1 clamps irregular parts and parts easy to slide, the clamp head 3 is provided with the anti-skid blocks 21, the anti-skid stripes 22 on the anti-skid blocks 21 are added, the three clamps 3 are distributed at different positions at the same time, the triangle has a stable effect, the anti-skid blocks 21 can reduce friction on the surfaces of objects, the clamp 1 has the phenomenon of unstable clamping when clamping the parts, the clamp 1 is increased to clamp various parts, when the aeronautical parts are used for overhauling the clamp 1, the clamp 1 is arranged between the two fixing plates 7, the rotating shafts 10 and the handles 5 arranged on two sides of the clamp 1 can rotate the aeronautical parts clamped by the clamp 1, the clamp 1 is firstly held to be pulled out from the inside of a frame groove, the fixed clamp 1 can be moved, then the clamp 1 is rotated to a proper position for convenient detection, thus the aeronautical parts can be overhauled, and the whole parts can be more clearly observed and overhauled when the aeronautical parts are overhauled.

It will be understood that the utility model has been described in terms of several embodiments, and that various changes and equivalents may be made to these features and embodiments by those skilled in the art without departing from the spirit and scope of the utility model. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the utility model without departing from the essential scope thereof. Therefore, it is intended that the utility model not be limited to the particular embodiment disclosed, but that the utility model will include all embodiments falling within the scope of the appended claims.

Claims (5)

1. The utility model provides an aviation spare part overhauls and uses mounting fixture, includes anchor clamps (1), bottom ring (2) and chuck (3), its characterized in that: the bottom of anchor clamps (1) is equipped with bottom plate (6), both sides fixed connection fixed plate (7) of bottom plate (6), pivot (10) are cup jointed to the top of fixed plate (7), internally mounted handle (5) of pivot (10), anchor clamps (1) are cup jointed to the bottom of handle (5), internally mounted pedestal (17) of fixed plate (7), anchor clamps (1) are cup jointed on the surface of pedestal (17), board groove (16) are seted up on the surface of fixed plate (7), inside grafting baffle (8) of board groove (16), fixed surface connection handle (19) of baffle (8), fixed surface connection picture peg (20) of baffle (8).

2. The fixture for overhauling an aerospace component according to claim 1, wherein: the telescopic device is characterized in that the telescopic device (12) is arranged above the clamp (1), the telescopic device (12) is sleeved with the fixed cylinder (11), the chuck (3) is arranged at the front end of the telescopic device (12), the anti-slip block (21) is arranged on the surface of the chuck (3), the convex groove (23) is formed in the surface of the chuck (3), the anti-slip stripes (22) are inlaid on the surface of the anti-slip block (21), the convex blocks (24) are fixedly connected at the back of the anti-slip block (21), the convex grooves (23) are slidingly connected with the surface of the convex blocks (24), the anti-slip blocks (21) are slidingly connected with the surface of the chuck (3), and the chuck (3) is in an equidistant distribution mode.

3. The fixture for overhauling an aerospace component according to claim 2, wherein: the telescopic device is characterized in that a sleeve (18) is fixedly connected to the surface of the telescopic device (12), a telescopic rod (15) is sleeved in the sleeve (18), and the other end of the telescopic rod (15) is fixedly connected with the clamping head (3).

4. The fixture for overhauling an aerospace component according to claim 2, wherein: the upper side of anchor clamps (1) is equipped with foundation ring (2), the top fixed connection of foundation ring (2) is fixed a section of thick bamboo (11), the below fixed connection foundation post (14) of foundation ring (2), the lower fixed connection base (13) of foundation post (14), anchor clamps (1) are embedded to the bottom of base (13).

5. The fixture for overhauling an aerospace component according to claim 1, wherein: a control device (4) is arranged above the clamp (1), and a button (9) is arranged above the control device (4).