CN213164977U

CN213164977U - Rapid clamp for aviation material machining

Info

Publication number: CN213164977U
Application number: CN202021633664.9U
Authority: CN
Inventors: 肖茶生
Original assignee: Suzhou Yuhang Aviation Technology Co ltd
Current assignee: Suzhou Yuhang Aviation Technology Co ltd
Priority date: 2020-08-08
Filing date: 2020-08-08
Publication date: 2021-05-11
Anticipated expiration: 2030-08-08

Abstract

The utility model is suitable for the technical field of aviation material processing, and discloses a quick clamp for aviation material processing, which comprises a processing table; the left side and the right side of the bottom end of the processing table are both fixed with a support plate, the middle part of the bottom end of the processing table is provided with an electric push rod, the tail end of the push rod of the electric push rod is fixed with a press plate, two sides of the top end of the press plate are both connected with rod fixing plates, the rod fixing plates are provided with four groups, the inner walls of the rod fixing plates are fixed with slide rods, and the slide rods are provided with two; logical groove has all been seted up on the left side and the right side on processing platform top, and it has the grip block to lead to the inslot, and the pole groove has been seted up to the inside of grip block, and two sets of have been seted up in the pole groove, and the slide bar is pegged graft in the inside in pole groove. The utility model discloses a grip block setting is on the moving mechanism, when carrying out the centre gripping to different aeronautical materials, can adjust in advance to do benefit to greatly and carry out quick centre gripping effect to the aeronautical materials of different sizes, it is convenient when improving the centre gripping.

Description

Rapid clamp for aviation material machining

Technical Field

The utility model is suitable for an aeronautical material processing technology field especially relates to an aeronautical material processing is with swift anchor clamps.

Background

Currently, aerospace materials are a general term for various materials used in the manufacture of aircraft, aircraft engines, and airborne equipment.

The aviation material is generally high in strength and low in quality, meanwhile, the aviation material needs to be fixed in the machining process, but in the normal clamping process, the type and the shape of the aviation material are different greatly, so that clamping is inconvenient, quick clamping of the aviation material is not facilitated, and production is inconvenient.

SUMMERY OF THE UTILITY MODEL

The utility model provides a pair of swift anchor clamps are used in processing of aviation material sets up on the moving mechanism through the grip block, when carrying out the centre gripping to different aviation materials, can adjust in advance to do benefit to greatly and carry out quick centre gripping effect to the aviation material of different sizes of volumes, convenient when improving the centre gripping has solved the problem of proposing in the background art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

a rapid clamp for processing aviation materials comprises a processing table;

the left side and the right side of the bottom end of the processing table are both fixed with a support plate, the middle part of the bottom end of the processing table is provided with an electric push rod, the tail end of the push rod of the electric push rod is fixed with a press plate, two sides of the top end of the press plate are both connected with rod fixing plates, the rod fixing plates are provided with four groups, the inner walls of the rod fixing plates are fixed with slide rods, and the slide rods are provided with two;

logical groove has all been seted up on the left side and the right side on processing platform top, and it has the grip block to lead to the inslot, and the pole groove has been seted up to the inside of grip block, and two sets of have been seted up in the pole groove, and the slide bar is pegged graft in the inside in pole groove, and the board groove has all been seted up on the inside left side of clamp plate and right side, and the backup pad is pegged graft in the.

Preferably, the clamping plate has an inverted L-shape.

Preferably, the sliding rod and the rod groove are matched in size to form the sliding mechanism.

Preferably, the inner wall of the clamping plate is wrapped with a non-slip mat, and the non-slip mat is made of rubber.

Preferably, the outer wall of the processing table is provided with a switch, and the switch is electrically connected with the electric push rod.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses a grip block setting is on the moving mechanism, when carrying out the centre gripping to different aeronautical materials, can adjust in advance to do benefit to greatly and carry out quick centre gripping effect to the aeronautical materials of different sizes, it is convenient when improving the centre gripping.

2. The utility model discloses an inner wall parcel of grip block has the slipmat, when grip block and aviation material contact, will increase the friction of contact surface greatly, guarantees the stability of centre gripping, and the slipmat is the rubber material simultaneously, has also played the protection effect to the centre gripping department.

Drawings

Fig. 1 is a schematic view of the overall structure of a quick clamp for processing aviation materials provided by the present invention;

fig. 2 is a schematic structural view of a top portion of a processing table of the rapid clamp for processing aviation materials according to the present invention;

fig. 3 is the utility model provides a clamp plate bottom structure schematic diagram of swift anchor clamps is used in aviation material processing.

In the figure: 1. a processing table; 2. a support plate; 3. an electric push rod; 4. pressing a plate; 5. a plate groove; 6. a rod fixing plate; 7. a slide bar; 8. a clamping plate; 9. a rod groove; 10. a switch; 11. a through groove; 12. a non-slip mat.

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.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the description of the present invention, it should be noted that, unless explicitly stated or limited otherwise, the terms "mounted," "connected" and "disposed" are to be interpreted broadly, and may be, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed; the utility model discloses in the model of providing with electrical apparatus only refer to, can be through changing the different models that the function is the same according to the actual use condition with electrical apparatus, to the ordinary technical personnel in this field, can understand that above-mentioned term is in by particular case the utility model provides a concrete meaning.

Referring to fig. 1-3, a quick clamp for processing aviation materials comprises a processing table 1;

the left side and the right side of the bottom end of the processing table 1 are both fixed with a support plate 2, the middle part of the bottom end of the processing table 1 is provided with an electric push rod 3, the tail end of the push rod of the electric push rod 3 is fixed with a press plate 4, two sides of the top end of the press plate 4 are both connected with a bar fixing plate 6, the bar fixing plates 6 are provided with four groups in total, the inner wall of the bar fixing plate 6 is fixed with slide bars 7, and the slide bars 7 are;

logical groove 11 has all been seted up on the left side and the right side on 1 top of processing platform, and logical groove 11 embeds there is grip block 8, and the pole groove 9 has been seted up to the inside of grip block 8, and two sets of have been seted up to pole groove 9, and slide bar 7 is pegged graft in the inside of pole groove 9, and board groove 5 has all been seted up on the left side and the right side of 4 inside portions of clamp plate, and backup pad 2 is pegged graft in the inside of board groove 5.

Please refer to fig. 1 in this embodiment, the clamping plate 8 is disposed on the moving mechanism, and can be adjusted in advance when clamping different aviation materials, so as to greatly facilitate rapid clamping effect of aviation materials with different sizes, and improve convenience in clamping.

Wherein the holding plate 8 is in an inverted L shape.

The sliding rod 7 is matched with the rod groove 9 in size to form a sliding mechanism.

Wherein, the inner wall of grip block 8 wraps up and has non-slip mat 12, and non-slip mat 12 is the rubber material.

Wherein, the outer wall of the processing table 1 is provided with a switch 10, and the switch 10 is electrically connected with the electric push rod 3.

The utility model discloses during the use: aeronautical material places at the top of processing platform 1, remove two sets of grip blocks 8, grip block 8 will be located and remove about moving on slide bar 7, when two sets of grip blocks 8 are located the top of aeronautical material tip, switch 10 starts electric putter 3, electric putter 3 drives clamp plate 4 and descends, two sets of grip blocks 8 descend thereupon, last grip block 8 will tightly push down aeronautical material, the completion is to aeronautical material's quick centre gripping effect, the design is simple, and is comparatively practical.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. A rapid clamp for processing aviation materials is characterized by comprising a processing table (1);

the left side and the right side of the bottom end of the processing table (1) are both fixed with a support plate (2), the middle part of the bottom end of the processing table (1) is provided with an electric push rod (3), the tail end of the push rod of the electric push rod (3) is fixed with a press plate (4), two sides of the top end of the press plate (4) are both connected with rod fixing plates (6), four groups of the rod fixing plates (6) are arranged, the inner wall of each rod fixing plate (6) is fixed with a slide rod (7), and two groups of the slide rods (7);

processing platform (1) top left side and right side have all been seted up and have been led to groove (11), lead to that groove (11) embeds there is grip block (8), pole groove (9) have been seted up to the inside of grip block (8), two sets of have been seted up in pole groove (9), slide bar (7) are pegged graft in the inside of pole groove (9), board groove (5) have all been seted up on the left side and the right side of clamp plate (4) inside, backup pad (2) are pegged graft in the inside of board groove (5).

2. The rapid clamp for processing aviation materials as claimed in claim 1, wherein the clamping plate (8) is in an inverted L shape.

3. The rapid clamp for processing the aviation material as claimed in claim 1, wherein the slide rod (7) and the rod groove (9) are matched in size to form a slide mechanism.

4. The rapid clamp for processing the aviation material as claimed in claim 1, wherein the inner wall of the clamping plate (8) is wrapped with a non-slip mat (12), and the non-slip mat (12) is made of rubber.

5. The rapid clamp for processing the aviation material as claimed in claim 1, wherein a switch (10) is arranged on the outer wall of the processing table (1), and the switch (10) is electrically connected with the electric push rod (3).