CN216049438U - Vacuum leading-in device for missile launching plate - Google Patents

Vacuum leading-in device for missile launching plate Download PDF

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Publication number
CN216049438U
CN216049438U CN202122004871.9U CN202122004871U CN216049438U CN 216049438 U CN216049438 U CN 216049438U CN 202122004871 U CN202122004871 U CN 202122004871U CN 216049438 U CN216049438 U CN 216049438U
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China
Prior art keywords
resin
vacuum
mold
product
glue
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Active
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CN202122004871.9U
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Chinese (zh)
Inventor
于智华
关丽阳
秦伟
王卓
沙振刚
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Jilin Jiangji Industrial Development Co ltd
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Jilin Jiangji Industrial Development Co ltd
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Priority to CN202122004871.9U priority Critical patent/CN216049438U/en
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Abstract

The utility model discloses a vacuum leading-in device for a missile launcher plate, which comprises a mold for manufacturing the launcher plate, a resin tank, a resin collector, a vacuum pump and a temperature control box, wherein the resin tank is communicated with a mold glue inlet through a glue inlet pipe and is filled with resin glue; by adopting the vacuum leading-in technology, the external dimension and the weight of the manufactured transmitting plate product are controlled within the qualified range, the difficulty in subsequent foaming is reduced, the weight requirement of the product after subsequent foaming forming can be controlled within the qualified range, the consistency of the product quality is ensured, and the rejection rate of the product is reduced.

Description

Vacuum leading-in device for missile launching plate
Technical Field
The utility model relates to the field of missile launching equipment, in particular to a vacuum leading-in device for a missile launching plate.
Background
The missile launcher plate is a support plate for supporting missiles, the traditional launcher plate is usually manufactured manually, the consistency of product quality cannot be guaranteed, the product error is large, and the rejection rate is high due to unstable technical state.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects in the prior art, the utility model aims to provide a vacuum leading-in device for a missile launching plate, which reduces the product rejection rate and ensures the quality consistency.
In order to achieve the purpose, the utility model adopts the following technical scheme:
a vacuum leading-in device for a missile launcher comprises a mold for manufacturing the launcher, a resin tank which is communicated with a mold glue inlet through a glue inlet pipe and is filled with resin glue, a resin collector which is communicated with a mold glue outlet through a glue outlet pipe, a vacuum pump which is communicated with the resin collector through a vacuum connecting pipe, and a temperature control box which is communicated with a mold heating port through a heating pipe.
Further, a pressure gauge is mounted on the resin collector.
Further, the heating pipe sets up three.
Compared with the prior art, the utility model has the following technical effects:
according to the utility model, firstly, carbon cloth in an emitter plate product is placed on a mold to be bonded and fixed, the mold is sealed by a sealing bag, prepared resin glue is placed in a resin tank, a vacuum pump is started to pump the resin glue into the mold through vacuum pumping force generated by the vacuum pump, so that the resin glue is filled with the carbon cloth, the prepared emitter plate product has a uniform structure, then redundant resin glue is collected and recycled through a resin collector, and meanwhile, a switch on a temperature control box is opened to heat a heating pipe, so that the product can be better cured on the mold, and the quality consistency of the product is ensured; by adopting the vacuum leading-in technology, the external dimension and the weight of the manufactured transmitting plate product are controlled within the qualified range, the difficulty in subsequent foaming is reduced, the weight requirement of the product after subsequent foaming forming can be controlled within the qualified range, the consistency of the product quality is ensured, and the rejection rate of the product is reduced.
Drawings
FIG. 1 is a schematic view of the present invention;
in the figure: 1. the device comprises a temperature control box, 2, a resin tank, 3, a rubber inlet pipe, 4, a transmitting plate, 5, a mold, 6, a heating pipe, 7, a rubber outlet pipe, 8, a vacuum connecting pipe, 9, a pressure gauge, 10, a resin collector, 11 and a vacuum pump.
Detailed Description
The present invention will be explained in further detail with reference to examples.
As shown in figure 1, the utility model provides a vacuum leading-in device for a missile launcher plate, which comprises a mould 5, wherein carbon cloth used for manufacturing the launcher plate 4 is bonded in the mould 5 and sealed by a sealing bag, a glue inlet of the mould 5 is communicated with a resin tank 2 filled with resin glue through a glue inlet pipe 3, a glue outlet of the mould 5 is communicated with a resin collector 10 provided with a pressure gauge 9 through a glue outlet pipe 7, and the resin collector 10 is communicated with a vacuum pump 11 through a vacuum connecting pipe 8.
The mould 5 is provided with three heating ports at even intervals, and each heating port is communicated with a temperature control box 1 through a heating pipe 6.
The working principle is as follows: firstly, placing carbon cloth in an emission plate 4 on a mold 5 for bonding and fixing, sealing by using a sealing bag, placing prepared resin glue into a resin tank 2, opening a vacuum pump 11 to pump the resin glue into the mold 5 by vacuum suction force generated by the vacuum pump 11 so that the resin glue is filled with the carbon cloth, enabling the prepared emission plate 4 to be uniform in structure, then collecting and recycling redundant resin glue by a resin collector 10, and simultaneously opening a switch on a temperature control box 1 to heat a heating pipe 6, so that a product can be better cured on the mold 5, and the quality consistency of the product is ensured; by adopting the vacuum leading-in technology, the external dimension and the weight of the manufactured transmitting plate 4 are controlled within the qualified range, the difficulty in subsequent foaming is reduced, the weight requirement of the product after subsequent foaming forming can be controlled within the qualified range, the consistency of the product quality is ensured, and the rejection rate of the product is reduced.

Claims (3)

1. A vacuum import device for missile launcher is characterized in that: the device comprises a mold (5) for manufacturing a transmitting plate (4), a resin tank (2) which is communicated with a glue inlet of the mold (5) through a glue inlet pipe (3) and is filled with resin glue, a resin collector (10) which is communicated with a glue outlet of the mold (5) through a glue outlet pipe (7), a vacuum pump (11) which is communicated with the resin collector (10) through a vacuum connecting pipe (8), and a temperature control box (1) which is communicated with a heating port of the mold (5) through a heating pipe (6).
2. The vacuum infusion device for missile launcher plate of claim 1, wherein the resin collector (10) has a pressure gauge (9) mounted thereon.
3. Vacuum infusion device for missile launcher plates as in claim 1, wherein said heating pipes (6) are provided in three.
CN202122004871.9U 2021-08-23 2021-08-23 Vacuum leading-in device for missile launching plate Active CN216049438U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122004871.9U CN216049438U (en) 2021-08-23 2021-08-23 Vacuum leading-in device for missile launching plate

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122004871.9U CN216049438U (en) 2021-08-23 2021-08-23 Vacuum leading-in device for missile launching plate

Publications (1)

Publication Number Publication Date
CN216049438U true CN216049438U (en) 2022-03-15

Family

ID=80560404

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202122004871.9U Active CN216049438U (en) 2021-08-23 2021-08-23 Vacuum leading-in device for missile launching plate

Country Status (1)

Country Link
CN (1) CN216049438U (en)

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