CN215203418U

CN215203418U - Female die heating mechanism for producing aircraft surface covering frame

Info

Publication number: CN215203418U
Application number: CN202023277181.2U
Authority: CN
Inventors: 郭强; 吕辉
Original assignee: Hunan Fengchi Machinery Co ltd
Current assignee: Hunan Fengchi Machinery Co ltd
Priority date: 2020-12-30
Filing date: 2020-12-30
Publication date: 2021-12-17
Anticipated expiration: 2030-12-30

Abstract

The utility model discloses an aircraft surface covering frame production is with bed die heating mechanism, including unable adjustment base, unable adjustment base's upper end fixedly connected with box, the T-slot, two have all been seted up with interior bottom at the interior top of box T-slot equal sliding connection has the T-shaped piece, the equal fixedly connected with fixed case of lower extreme of T-shaped piece, two the inside of fixed case all is provided with and is used for carrying out the fixture of centre gripping to the work piece, be provided with in the fixed case and be used for carrying out driven actuating mechanism to fixture, all be provided with on the both ends lateral wall of box and be used for carrying out the heat treatment mechanism that handles to the work piece. The utility model discloses it is rational in infrastructure, through setting up heat treatment mechanism, realize carrying out the concurrent heating to the both sides of work piece, avoid appearing heating inhomogeneous phenomenon, influence the processing in later stage, through setting up fixture, T-shaped piece and T-shaped groove, avoid the manual work to get the material, cause the scald danger easily.

Description

Female die heating mechanism for producing aircraft surface covering frame

Technical Field

The utility model relates to a bed die processing technology field especially relates to an aircraft surface covers production of frame and uses bed die heating mechanism.

Background

For vacuum plastic packaging molding, only one surface of a heated material is contacted with a molding tool, the surface of the material, which is connected with a mold, has the surface contour which is completely the same as that of the molding mold, the contour and the size of the non-contact surface of a molded part only depend on the thickness of the material, and the molding process can be divided into male mold molding and female mold molding according to the difference of the contact surfaces of the molding material and the molding mold.

Among the prior art, traditional heating mechanism can not carry out the omnidirectional heating to the work piece, causes the uneven circumstances of heating easily to influence the production and processing in later stage, among the prior art simultaneously, after heating the work piece, the surface temperature of work piece is higher, causes the condition of scald easily when the manual work is got the material.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the production of an aircraft surface covering frame is with bed die heating mechanism that proposes, through setting up heat treatment mechanism, realize carrying out the concurrent heating to the both sides of work piece, avoid appearing heating inhomogeneous phenomenon, influence the processing in later stage, through setting up fixture, T-shaped piece and T-shaped groove, avoid the manual work to get the material, cause easily that the scald is dangerous.

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

the utility model provides an aircraft surface covers production of frame and uses bed die heating mechanism, includes unable adjustment base, unable adjustment base's upper end fixedly connected with box, the T-slot, two have all been seted up to the interior top and the interior bottom of box T-slot equal sliding connection has the T-shaped piece, the equal fixedly connected with fixed case of lower extreme of T-shaped piece, two the inside of fixed case all is provided with the fixture that is used for carrying out the centre gripping to the work piece, be provided with in the fixed case and be used for carrying out driven actuating mechanism to fixture, all be provided with on the both ends lateral wall of box and be used for carrying out the heat treatment mechanism that heat treats to the work piece.

Preferably, fixture is including seting up the spout on the fixed incasement lateral wall, sliding connection has the slider in the spout, rotate on the lateral wall of slider and connect two alternately arranged dwang, logical groove, two have been seted up to the lower extreme of fixed case the dwang passes logical groove, two the lower extreme of dwang all rotates and is connected with splint.

Preferably, the driving mechanism comprises a double-threaded rod with one end rotatably connected to the inner side wall of the fixed box, the other end of the double-threaded rod penetrates through the side wall of one end of the fixed box, two symmetrically arranged moving blocks are connected to the double-threaded rod in a threaded mode, and the two rotating rods are rotatably connected to the side walls of the two moving blocks respectively.

Preferably, heat treatment mechanism includes the telescopic link of fixed connection on the box both ends inside wall, two the equal fixedly connected with hot plate of flexible end of telescopic link.

Preferably, a fixing frame is fixedly connected between the two fixing boxes, and a handle is fixedly sleeved on the side wall of the fixing frame.

Preferably, two the equal fixedly connected with handle of one end that double-end threaded rod is located the fixed box outside, the cover is equipped with anti-skidding rubber sleeve on hand.

Compared with the prior art, the utility model, its beneficial effect does:

1. through setting up heat treatment mechanism, the drive telescopic link extends, makes two hot plates draw close to the centre to the realization heats simultaneously to the both sides of work piece, avoids appearing heating inhomogeneous phenomenon, influences the processing in later stage.

2. Through setting up fixture, T-shaped piece and T-shaped groove, pulling handle makes two fixed casees of mount 8 drive and removes to take out the work piece from the box in, avoid the manual work to get the material, cause the scald danger easily.

Drawings

Fig. 1 is a schematic structural view of a female mold heating mechanism for producing an aircraft surface covering frame according to the present invention;

FIG. 2 is a cross-sectional view of a fixing mechanism of a female mold heating mechanism for producing an aircraft surface covering frame according to the present invention;

fig. 3 is a sectional top view of a female mold heating mechanism for producing an aircraft surface covering frame according to the present invention.

In the figure: the device comprises a fixed base 1, a box body 2, a telescopic rod 3, a heating plate 4, a T-shaped groove 5, a T-shaped block 6, a fixed box 7, a fixed frame 8, a handle 9, a double-head threaded rod 10, a moving block 11, a rotating rod 12, a clamping plate 13, a sliding chute 14 and a sliding block 15.

Detailed Description

In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. The present invention can be embodied in many different forms other than those specifically described herein, and it will be apparent to those skilled in the art that similar modifications can be made without departing from the spirit and scope of the invention, and it is therefore not to be limited to the specific embodiments disclosed below.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and similar tables are used herein for illustrative purposes only and do not represent the only embodiments.

Referring to fig. 1-3, a female mold heating mechanism is used in production of aircraft surface covering frame, including unable adjustment base 1, unable adjustment base 1's upper end fixedly connected with box 2, T-slot 5 has all been seted up with interior bottom at the interior top of box 2, equal sliding connection has T-shaped piece 6 in two T-slot 5, the equal fixedly connected with fixed case 7 of lower extreme of T-shaped piece 6, common fixedly connected with mount 8 between two fixed cases 7, mount 8 is the U-shaped setting, fixed handle 9 that has cup jointed on the lateral wall of mount 8, handle 9 is high temperature resistant material.

The inside of two fixed casees 7 all is provided with the fixture that is used for carrying out the centre gripping to the work piece, and fixture is including seting up spout 14 on fixed incasement 7 inside walls, and sliding connection has slider 15 in the spout 14, rotates two alternately arranged dwang 12 of connection on slider 15's the lateral wall, and logical groove has been seted up to fixed case 7's lower extreme, and two dwang 12 pass logical groove, and the lower extreme of two dwang 12 all rotates and is connected with splint 13.

Be provided with in the fixed box 7 and be used for carrying out driven actuating mechanism to fixture, actuating mechanism includes that one end rotates the double threaded rod 10 of connection on 7 inside walls of fixed box, the screw thread on the double threaded rod 10 revolves to setting up for opposite, the equal fixedly connected with handle of one end that two double threaded rod 10 are located fixed box 7 outside, the cover is equipped with the anti-skidding rubber sleeve on hand, the other end of double threaded rod 10 passes the one end lateral wall of fixed box 7, threaded connection has the movable block 11 that two symmetries set up on the double threaded rod 10, two dwang 12 rotate respectively and connect on the lateral wall of two movable blocks 11.

All be provided with on the both ends lateral wall of box 2 and be used for carrying out the heat treatment mechanism that heat treats to the work piece, heat treatment mechanism includes telescopic link 3 of fixed connection on the inside wall of box 2 both ends, and the equal fixedly connected with hot plate 4 of the flexible end of two telescopic links 3.

The utility model discloses during the use, the staff places the work piece between a plurality of splint 13, rotate double threaded rod 10, make two movable blocks 11 rather than the meshing remove, thereby promote two dwang 12 and use slider 15 to rotate as the axle, make two splint 13 draw close to the centre, thereby realize carrying out effectual centre gripping to the work piece, start two telescopic links 3 after fixed completion, make two hot plates 4 draw close to the centre, thereby realize heating simultaneously to the both sides of work piece, avoid appearing heating inhomogeneous phenomenon, after the heating is accomplished, pulling handle 9 makes mount 8 drive two fixed casees 7 and removes, thereby take out the work piece conveniently.

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. The utility model provides an aircraft surface covers production of frame and uses bed die heating mechanism, includes unable adjustment base (1), its characterized in that, the upper end fixedly connected with box (2) of unable adjustment base (1), T-slot (5), two have all been seted up with interior bottom at the interior top of box (2) equal sliding connection has T-shaped piece (6) in T-slot (5), the equal fixedly connected with fixed case (7) of lower extreme of T-shaped piece (6), two the inside of fixed case (7) all is provided with and is used for carrying out the fixture of centre gripping to the work piece, be provided with in fixed case (7) and be used for carrying out driven actuating mechanism to fixture, all be provided with the heat treatment mechanism who is used for carrying out heat treatment to the work piece on the both ends lateral wall of box (2).

2. The female die heating mechanism for the production of the aircraft surface covering frame according to claim 1, wherein the clamping mechanism comprises a sliding groove (14) formed in the inner side wall of the fixed box (7), a sliding block (15) is slidably connected in the sliding groove (14), two rotating rods (12) which are arranged in a crossed manner are rotatably connected to the side wall of the sliding block (15), a through groove is formed in the lower end of the fixed box (7), the two rotating rods (12) penetrate through the through groove, and the two rotating rods (12) are rotatably connected to the lower end of a clamping plate (13).

3. The heating mechanism for the female die for producing the aircraft surface covering frame is characterized in that the driving mechanism comprises a double-threaded rod (10) with one end rotatably connected to the inner side wall of the fixed box (7), the other end of the double-threaded rod (10) penetrates through the side wall of one end of the fixed box (7), two symmetrically arranged moving blocks (11) are in threaded connection with the double-threaded rod (10), and two rotating rods (12) are respectively rotatably connected to the side walls of the two moving blocks (11).

4. The female die heating mechanism for the production of the aircraft surface covering frame according to claim 1, wherein the heat treatment mechanism comprises telescopic rods (3) fixedly connected to the inner side walls of the two ends of the box body (2), and the telescopic ends of the two telescopic rods (3) are fixedly connected with heating plates (4).

5. The heating mechanism of the female die for the production of the aircraft surface covering frame as claimed in claim 2, wherein a fixing frame (8) is fixedly connected between the two fixing boxes (7), and a handle (9) is fixedly sleeved on the side wall of the fixing frame (8).

6. The female die heating mechanism for the production of the aircraft surface covering frame as claimed in claim 3, wherein two ends of the double-threaded rod (10) outside the fixed box (7) are fixedly connected with handles, and the handles are sleeved with anti-skid rubber sleeves.