CN213353184U

CN213353184U - Aerospace composite material mould strutting arrangement

Info

Publication number: CN213353184U
Application number: CN202021616645.5U
Authority: CN
Inventors: 不公告发明人
Original assignee: Shenzhen Wanxinglong Plastic Electronics Co ltd
Current assignee: Shenzhen Wanxinglong Plastic Electronics Co ltd
Priority date: 2020-08-06
Filing date: 2020-08-06
Publication date: 2021-06-04
Anticipated expiration: 2030-08-06

Abstract

The utility model discloses an aerospace combined material mould strutting arrangement, the utility model relates to the technical field of mould strutting arrangement, aerospace combined material mould strutting arrangement, including operation panel, brace table, support and bottom plate, the operation panel is located the brace table top, and the brace table is located inside the support, and the bottom plate is located the support below, and the welding of operation panel bottom surface four corners has the fixed block, and the welding of fixed block below has a branch, and the four corners of brace table upper surface are opened has first recess, and first recess bottom surface is opened has the second recess, and the branch surface just lies in the joint and has compression spring between fixed block and the first recess bottom surface; the beneficial effects of the utility model reside in that: the height of the supporting table is adjusted through the threaded hole and the first positioning hole. Make the support can the back-and-forth movement through slider and slide rail, do benefit to and shift, increase the convenience of use, play the shock attenuation cushioning effect through magnet and compression spring to the operation panel, protect the operation panel to avoid too big impact, increase of service life.

Description

Aerospace composite material mould strutting arrangement

Technical Field

The utility model belongs to the technical field of the mould strutting arrangement technique and specifically relates to an aerospace combined material mould strutting arrangement is related to.

Background

The aerospace composite material is a high-performance new material system applied to aerospace craft, which is compounded by two or more than two heterogeneous, special-shaped and heterogeneous materials through a special molding process, and the compounding aims to improve the performance of the material or enable the material to meet a certain special physical performance requirement. The existing aerospace composite material mold supporting device is difficult to displace, so that the use convenience is low, various requirements are difficult to deal with, and the service life is short due to the fact that a common supporting device is deficient in shock absorption protection.

SUMMERY OF THE UTILITY MODEL

The utility model aims at the problem that above-mentioned exists with not enough, provide an aerospace combined material mould strutting arrangement, it realizes a supporting bench altitude mixture control through screw hole and first locating hole. Make the support can the back-and-forth movement through slider and slide rail, do benefit to and shift, increase the convenience of use, play the shock attenuation cushioning effect through magnet and compression spring to the operation panel, protect the operation panel to avoid too big impact, increase of service life.

In order to achieve the purpose, the adopted technical scheme is as follows:

the aerospace composite material mold supporting device comprises an operating platform, a supporting platform, a support and a bottom plate, wherein the operating platform is positioned above the supporting platform, the supporting platform is positioned in the support, and the bottom plate is positioned below the support;

the welding of operation panel bottom surface four corners has the fixed block, just the welding of fixed block below has branch, it has first recess to open in supporting bench upper surface four corners, just first recess face is opened there is the second recess, the branch surface just is located the fixed block with the joint has compression spring between the first recess face, two screw holes have all been opened to both sides around both ends about the supporting bench, the support is controlled the inner wall around both sides and all is opened five first spacing holes, just the support bottom surface left and right sides is opened there is the pinhole, the equal fixedly connected with slider in support lower surface left and right sides, the slide rail is all installed to the bottom plate upper surface left and right sides, just slide rail upper surface equidistance is opened there is the spacing hole of a plurality of second.

Preferably, the cross-sectional area of the lower end of the strut is larger than that of the upper end of the strut, and the lower end of the strut is connected in the second groove in a sliding mode.

Preferably, mutually exclusive magnets are embedded into the lower end of the supporting rod and the bottom end of the second groove respectively.

Preferably, the inner wall of the first limiting hole is provided with internal threads, the two first limiting holes corresponding to the first limiting hole and the two threaded holes are connected with bolts in an internal thread mode, and the support table and the support are fixed through the bolts.

Preferably, the slide rail is T-shaped, and the slide block is connected with the slide rail in a sliding manner.

Preferably, the pin hole and the second limit hole corresponding to the position are inserted with a bolt.

By adopting the technical scheme, the beneficial effects are as follows:

the sliding block and the sliding rail enable the position of the device to translate back and forth, the convenience of displacement is improved, the device is suitable for the requirements of various die mounting positions, the supporting table can move up and down in the support, the adjustability of height is improved, the requirements of various die mounting heights are met, and the support and the supporting table are relatively fixed through bolts;

mutual repulsion through producing between the magnet of the branch bottom surface and the magnet of second recess bottom surface for branch can suspend in second recess bottom surface top, because branch and second recess do not have rigid contact, its noise at work will greatly reduced, can cushion the overdraft through compression spring, alleviate the operation panel vibrations that are brought by the overdraft, the protection mould avoids receiving vibrations to influence, prolongs the device's life.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings of the embodiments of the present invention will be briefly described below. The drawings are intended to depict only some embodiments of the invention, and not all embodiments of the invention are limited thereto.

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

fig. 2 is a schematic view of the overall top plan structure of the present invention;

fig. 3 is a schematic view of the overall left-side plan structure of the present invention;

fig. 4 is a schematic diagram of a partially enlarged structure in fig. 1 according to the present invention.

The labels in the figure are: an operation table 1; a support table 2; a support 3; a base plate 4; a first groove 5; a first limit hole 6; a slide rail 7; a slide block 8; a second limit hole 9; a threaded hole 10; a pin hole 11; a fixed block 12; a strut 13; a compression spring 14; a second groove 15; and a magnet 16.

Detailed Description

In order to make the purpose, technical features and technical effects of the technical solution of the present invention clearer, the drawings of the embodiments of the present invention are combined together, and the example solution of the embodiments of the present invention is clearly and completely described.

Referring to fig. 1 to 4, the utility model relates to an aerospace composite mold supporting device, which comprises an operating platform 1, a supporting platform 2, a support 3 and a bottom plate 4, wherein the operating platform 1 is positioned above the supporting platform 2, the supporting platform 2 is positioned inside the support 3, and the bottom plate 4 is positioned below the support 3;

the four corners of the bottom surface of the operating platform 1 are welded with fixed blocks 12, supporting rods 13 are welded below the fixed blocks 12, first grooves 5 are formed in the four corners of the upper surface of the supporting platform 2, second grooves 15 are formed in the bottom surfaces of the first grooves 5, compression springs 14 are clamped between the fixed blocks 12 and the bottom surfaces of the first grooves on the surfaces of the supporting rods 13, two threaded holes 10 are formed in the front and rear sides of the left and right ends of the supporting platform 2, five first limiting holes 6 are formed in the front and rear sides of the left and right inner walls of the support 3, pin holes 11 are formed in the left and right sides of the bottom surface of the support 3, sliding blocks 8 are fixedly connected to the left and right sides of the lower surface of the support 3, sliding rails 7 are mounted on the left and right sides of;

the cross sectional area of the lower end of the supporting rod 13 is larger than that of the upper end of the supporting rod, the lower end of the supporting rod 13 is connected in the second groove 15 in a sliding mode, mutually exclusive magnets 16 are embedded into the lower end of the supporting rod 13 and the bottom end of the second groove 15 respectively, internal threads are arranged on the inner wall of the first limiting hole 6, two first limiting holes 6 and two threaded holes 10 which correspond to the positions are connected with bolts in an internal thread mode, the supporting table 2 and the support 3 are fixed through the bolts, the sliding rail 7 is T-shaped, the sliding block 8 is connected with the sliding rail 7 in a sliding mode, and bolts are;

specifically, a user needs to install the device before using the device, firstly, the support 3 is connected with the two slide rails 7 in a sliding way through the two slide blocks 8, the slide blocks 8 and the slide rails 7 enable the position of the device to translate back and forth, the convenience of displacement is increased, the device is suitable for the requirements of various die installation positions, after the die installation positions are confirmed, inserting the inserted pin into the corresponding pin hole 11 and the second limit hole 9, fixing the support 3 and the bottom plate 4 through the inserted pin, then the supporting platform 2 is placed between the left inner wall and the right inner wall of the support 3, the supporting platform 2 can move up and down in the support 3, the adjustability of the height is increased, the requirements of various die mounting heights are met, adjusting according to the installation height of the die, screwing a bolt into the first limiting hole 6 from a threaded hole 10 in the outer wall of the support 3 after the height is confirmed, fixing the support 3 and the support platform 2 through the bolt at the moment, and fixing the basic height of the operating platform 1;

further, the upper surface of the operating platform 1 is provided with a plurality of mounting holes, a user mounts the die to the surface of the operating platform 1 through the mounting holes on the surface of the operating platform 1, the operating platform 1 generates mutual repulsion force between the magnet 16 on the bottom surface of the supporting rod 13 and the magnet 16 on the bottom surface of the second groove 15, so that the supporting rod 13 can suspend above the bottom surface of the second groove 15, the supporting rod 13 does not have rigid contact with the second groove 15, the working noise is greatly reduced, the operating platform 1 presses down the supporting rod 13 during working, the pressing force can be buffered through the compression spring 14, the vibration of the operating platform 1 caused by the pressing force is reduced, the die is protected from being influenced by vibration, and the service life of the device is prolonged.

In the present specification, each embodiment is described with emphasis on differences from other embodiments, and the same or similar parts between the embodiments may be referred to each other. Unless otherwise defined, technical or scientific terms used in the present embodiments should have the ordinary meaning as understood by those having ordinary skill in the art to which the present invention belongs.

Exemplary embodiments of the present invention have been described in detail with reference to the preferred embodiments, however, it will be understood by those skilled in the art that various modifications and changes may be made to the above specific embodiments without departing from the scope of the present invention, and various combinations of the technical features and structures of the present invention may be implemented without departing from the scope of the present invention, which is defined by the appended claims.

Claims

1. The utility model provides an aerospace combined material mould strutting arrangement, includes operation panel (1), brace table (2), support (3) and bottom plate (4), its characterized in that:

the operating platform (1) is positioned above the supporting platform (2), the supporting platform (2) is positioned inside the support (3), and the bottom plate (4) is positioned below the support (3);

the operating table is characterized in that a fixed block (12) is welded at four corners of the bottom surface of the operating table (1), a supporting rod (13) is welded below the fixed block (12), a first groove (5) is formed in four corners of the upper surface of the supporting table (2), a second groove (15) is formed in the bottom surface of the first groove (5), the surface of the supporting rod (13) is located between the fixed block (12) and the bottom surface of the first groove (5), a compression spring (14) is clamped between the fixed block (12) and the bottom surface of the first groove (5), two threaded holes (10) are formed in the front side and the rear side of the left end and the right end of the supporting table (2), five first limiting holes (6) are formed in the front side and the rear side of the left inner wall and the right inner wall of the support (3), pin holes (11) are formed in the left side and the right side of the bottom, and a plurality of second limiting holes (9) are formed in the upper surface of the sliding rail (7) at equal intervals.

2. An aerospace composite mold support apparatus as claimed in claim 1, wherein: the cross sectional area of the lower end of the supporting rod (13) is larger than that of the upper end of the supporting rod, and the lower end of the supporting rod (13) is connected in the second groove (15) in a sliding mode.

3. An aerospace composite mold support apparatus as claimed in claim 2, wherein: mutually exclusive magnet (16) are respectively embedded into the lower end of the supporting rod (13) and the bottom end of the second groove (15).

4. An aerospace composite mold support apparatus as claimed in claim 1, wherein: the inner wall of the first limiting hole (6) is provided with internal threads, the two first limiting holes (6) and the two threaded holes (10) which correspond to each other in position are connected with bolts in an internal thread mode, and the support table (2) and the support (3) are fixed through the bolts.

5. An aerospace composite mold support apparatus as claimed in claim 1, wherein: the slide rail (7) is T-shaped, and the slide block (8) is connected with the slide rail (7) in a sliding manner.

6. An aerospace composite mold support apparatus as claimed in claim 1, wherein: the pin hole (11) and the second limit hole (9) which correspond to the positions are internally inserted with a bolt.