CN216831814U

CN216831814U - Aerospace combined material positioner for mould

Info

Publication number: CN216831814U
Application number: CN202220460613.3U
Authority: CN
Inventors: 马永霞
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-03-04
Filing date: 2022-03-04
Publication date: 2022-06-28
Anticipated expiration: 2032-03-04

Abstract

The utility model discloses an aerospace combined material positioner for mould, including the die mounting platform, the outside of die mounting platform is equipped with rotating base, rotating base's the outside is equipped with the fixed ring, the inside of fixed ring is equipped with the hexagon socket head cap screw, the die mounting platform includes fixed round platform, a spout, No. two spouts, electric telescopic handle, a slide bar, No. two slide bars, spud pile, splint, rubber slipmat and slider, rotating base includes hollow underframe, a ring gear, rack piece, spring leaf, flexible cover and solid fixed ring. A positioner for aerospace combined material mould, can clip equidimension aerospace combined material mould not automatically through the die mounting platform, and be difficult to the slippage, make the mould after fixed can carry out the folk prescription to carrying out rotatory adjustment position, operation process is simple and convenient through rotating base.

Description

Aerospace combined material positioner for mould

Technical Field

The utility model relates to a mould positioner technical field, in particular to aerospace positioner for combined material mould.

Background

The mould, various moulds and tools for obtaining required products by injection moulding, blow moulding, extrusion, die casting or forging forming, smelting, stamping and other methods in industrial production, and the mould positioning device is a clamp or a base for fixing the mould and is responsible for fixing the mould on a workbench of equipment.

Patent numbers: 202121881195.7, the box disappearance mould of being convenient for quick drawing of patterns that publishes, can "through setting up shedder, effectively separate the drawing of patterns with the mould, and then avoided equipment when using, the location is installed through the mode of bolt to most moulds, need use the hard thing to strike the operation during the drawing of patterns, cause the condition of damage to easily appear in equipment, and then reduced the use degree of difficulty of equipment, the ease of use of equipment has been improved, but positioner wherein can not fix the mould of variation in size, and the mould after fixing can not rotate, the direction of adjustment.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a main aim at provides an aerospace positioner for combined material mould can effectively solve the problem in the background art.

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

the utility model provides an aerospace combined material positioner for mould, includes the die holding platform, the outside of die holding platform is equipped with rotating base, rotating base's the outside is equipped with fixed ring, the inside of fixed ring is equipped with the hexagon socket head cap screw, the die holding platform is including fixed round platform, a spout, No. two spouts, electric telescopic handle, No. one slide bar, No. two slide bars, spud pile, splint, rubber slipmat and slider, rotating base includes hollow underframe, a ring gear, rack piece, spring leaf, flexible cover and solid fixed ring.

Preferably, the upper surface of fixed round platform is seted up to a spout, No. two spouts are seted up in the upper surface of fixed round platform and are located between the spout, electric telescopic handle is fixed in the lower surface of fixed round platform, a slide bar is fixed in the non-adjacent one end of electric telescopic handle, No. two slide bars are fixed in the outside of a slide bar, the spud pile is fixed in the upper end of No. two slide bars, splint are fixed in the spud pile and keep away from the one end of No. two slide bars, the rubber slipmat is fixed in adjacent one side between the splint, the slider is fixed in the position that the splint lower surface is close to both ends.

Preferably, the upper end of the first sliding rod penetrates through the inside of the second sliding groove, the second sliding rod is located inside the second sliding groove, and the sliding block is located inside the first sliding groove.

Preferably, a ring gear is fixed in the position of the inboard lower surface of hollow underframe, the rack piece is fixed in the position that fixed round platform lower surface is close to the edge, the spring leaf is fixed in the position that hollow underframe lower surface is close to the edge, flexible cover is fixed in the upper end of spring leaf and is located the inside of hollow underframe, fixed ring is fixed in the outside of fixed round platform.

Preferably, the upper end of the telescopic sleeve is located between the fixing rings, the clamping teeth at the lower end of the rack block are clamped in the clamping grooves in the upper surface of the first gear ring, and the rotating base is arranged on the outer side of the die mounting table through the fixing rings.

Preferably, the fixed ring is fixed on the outer side of the hollow bottom frame, and the fixed ring is arranged on the outer side of the rotating base through the hollow bottom frame.

Compared with the prior art, the utility model discloses following beneficial effect has:

the utility model discloses in, through the die holding platform that sets up, the die holding platform can clip not equidimension aerospace combined material mould automatically, and is difficult to the slippage, and through the rotating base who sets up, rotating base makes the mould after fixed can carry out the folk prescription to rotating the adjustment position, and operation process is simple and convenient.

Drawings

Fig. 1 is a schematic view of the overall structure of a positioning device for an aerospace composite material mold according to the present invention;

fig. 2 is a schematic sectional view of a mold mounting table of the positioning device for an aerospace composite material mold of the present invention;

fig. 3 is an exploded schematic view of a rotary base of the positioning device for an aerospace composite material mold of the present invention;

fig. 4 is an enlarged schematic view of a portion a in fig. 1 of the positioning device for an aerospace composite material mold according to the present invention;

fig. 5 is an enlarged schematic view of a part B in fig. 3 of the positioning device for an aerospace composite material mold according to the present invention.

In the figure: 1. a die mounting table; 101. fixing the round table; 102. a first chute; 103. a second chute; 104. an electric telescopic rod; 105. a first sliding rod; 106. a second sliding bar; 107. fixing the pile; 108. a splint; 109. a rubber non-slip mat; 110. a slider; 2. rotating the base; 201. a hollow bottom frame; 202. a first gear ring; 203. a rack block; 204. a spring plate; 205. a telescopic sleeve; 206. a fixing ring; 3. fixing the circular ring; 4. a hexagon socket head cap screw.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

The first embodiment is as follows:

as shown in fig. 1-5, a positioning device for aerospace composite material molds comprises a mold mounting table 1, a rotary base 2 is arranged on the outer side of the mold mounting table 1, a fixed ring 3 is arranged on the outer side of the rotary base 2, a hexagon socket head cap screw 4 is arranged inside the fixed ring 3, the mold mounting table 1 comprises a fixed circular table 101, a first sliding groove 102, a second sliding groove 103, an electric telescopic rod 104, a first sliding rod 105, a second sliding rod 106, a fixed pile 107, a clamping plate 108, a rubber anti-skid pad 109 and a sliding block 110, the rotary base 2 comprises a hollow bottom frame 201, a first gear ring 202, a rack block 203, a spring plate 204, a telescopic sleeve 205 and a fixed ring 206, the mold mounting table 1 can automatically clamp aerospace composite material molds with different sizes, the die is not easy to slip, the fixed die can rotate in a single direction to adjust the position by rotating the base 2, and the operation process is simple and convenient; the first sliding groove 102 is formed in the upper surface of the fixed circular truncated cone 101, the second sliding groove 103 is formed in the upper surface of the fixed circular truncated cone 101 and is located between the first sliding grooves 102, the electric telescopic rod 104 is fixed to the lower surface of the fixed circular truncated cone 101, the first sliding rod 105 is fixed to one end, which is not adjacent, of the electric telescopic rod 104, the second sliding rod 106 is fixed to the outer side of the first sliding rod 105, the fixing pile 107 is fixed to the upper end of the second sliding rod 106, the clamping plate 108 is fixed to one end, which is far away from the second sliding rod 106, of the fixing pile 107, the rubber anti-skid pad 109 is fixed to one side, which is adjacent, of the clamping plate 108, and the sliding block 110 is fixed to the position, which is close to two ends, of the lower surface of the clamping plate 108; the upper end of the first sliding rod 105 penetrates through the inside of the second sliding groove 103, the second sliding rod 106 is positioned inside the second sliding groove 103, and the sliding block 110 is positioned inside the first sliding groove 102; a first gear ring 202 is fixed at the lower surface of the inner side of a hollow bottom frame 201, a rack block 203 is fixed at the position, close to the edge, of the lower surface of a fixed circular truncated cone 101, a spring piece 204 is fixed at the position, close to the edge, of the lower surface of the hollow bottom frame 201, a telescopic sleeve 205 is fixed at the upper end of the spring piece 204 and is positioned inside the hollow bottom frame 201, and a fixed ring 206 is fixed at the outer side of the fixed circular truncated cone 101; the upper end of the telescopic sleeve 205 is positioned between the fixing rings 206, the latch at the lower end of the rack block 203 is clamped in the clamping groove on the upper surface of the first gear ring 202, and the rotating base 2 is arranged on the outer side of the die mounting table 1 through the fixing rings 206; the fixed ring 3 is fixed on the outer side of the hollow bottom frame 201, and the fixed ring 3 is arranged on the outer side of the rotating base 2 through the hollow bottom frame 201.

Example two:

it should be noted that the utility model relates to a positioner for aerospace composite material mould, when using, install the positioner on the workstation through the inside hexagon socket head cap screw 4 of fixed ring 3, in the die mounting platform 1, through the shrink of electric telescopic handle 104, remove No. two slide bars 106 in No. two spouts 103, splint 108 follows and moves, slider 110 moves in No. one spout 102 along with splint 108, clip the mould that needs to be fixed through splint 108, rubber slipmat 109 plays the antiskid effect, die mounting platform 1 can clip different size aerospace composite material moulds automatically, and be difficult to the slippage, when needing the rotary die, in rotating base 2, rotate fixed round platform 101, the slope surface upward movement of slope in the draw-in groove along No. one ring gear 202 upper surface of rack piece 203, block to next draw-in groove afterwards, the position of the telescopic sleeve 205 and the die mounting table 1 can continuously rise or fall, the spring piece 204 can be continuously stretched and then restored to the original state, the rack block 203 is always moved into the clamping groove corresponding to the upper surface of the first rotating angle gear ring 202, the fixed circular truncated cone 101 can only rotate in one direction, the rotating base 2 enables the fixed die to rotate in one direction to adjust the position, and the operation process is simple and convenient.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides an aerospace positioner for combined material mould which characterized in that: including die holding platform (1), the outside of die holding platform (1) is equipped with rotating base (2), the outside of rotating base (2) is equipped with stationary circular ring (3), the inside of stationary circular ring (3) is equipped with hexagon socket head cap screw (4), die holding platform (1) is including stationary circular table (101), spout (102), No. two spout (103), electric telescopic handle (104), slide bar (105), No. two slide bar (106), spud pile (107), splint (108), rubber slipmat (109) and slider (110), rotating base (2) are including hollow underframe (201), ring gear (202), rack piece (203), spring leaf (204), flexible cover (205) and solid fixed ring (206).

2. The aerospace composite mold positioning device as claimed in claim 1, wherein: the upper surface of fixed round platform (101) is seted up to a spout (102), No. two spout (103) are seted up to the upper surface of fixed round platform (101) and are located between a spout (102), electric telescopic handle (104) are fixed in the lower surface of fixed round platform (101), slide bar (105) are fixed in electric telescopic handle (104) non-adjacent one end, No. two slide bar (106) are fixed in the outside of a slide bar (105), spud pile (107) are fixed in the upper end of No. two slide bars (106), splint (108) are fixed in spud pile (107) and keep away from the one end of No. two slide bars (106), rubber slipmat (109) are fixed in the adjacent one side between splint (108), slider (110) are fixed in the position that splint (108) lower surface is close to both ends.

3. The aerospace composite mold positioning device as claimed in claim 2, wherein: the upper end of the first sliding rod (105) penetrates through the inside of the second sliding groove (103), the second sliding rod (106) is located inside the second sliding groove (103), and the sliding block (110) is located inside the first sliding groove (102).

4. The aerospace composite mold positioning device as claimed in claim 3, wherein: no. one ring gear (202) is fixed in the position of the inboard lower surface of hollow underframe (201), rack block (203) are fixed in the position that fixed round platform (101) lower surface is close to the edge, spring leaf (204) are fixed in the position that hollow underframe (201) lower surface is close to the edge, flexible cover (205) are fixed in the upper end of spring leaf (204) and are located the inside of hollow underframe (201), gu fixed ring (206) are fixed in the outside of fixed round platform (101).

5. The aerospace composite mold positioning device as claimed in claim 4, wherein: the upper end of flexible cover (205) is located between solid fixed ring (206), the latch card of rack piece (203) lower extreme is in the draw-in groove of a ring gear (202) upper surface, the outside of mould mount table (1) is located through solid fixed ring (206) in rotating base (2).

6. The aerospace composite mold positioning device as claimed in claim 5, wherein: the fixed ring (3) is fixed on the outer side of the hollow bottom frame (201), and the fixed ring (3) is arranged on the outer side of the rotating base (2) through the hollow bottom frame (201).