CN214448691U - Forming device for producing thermosetting composite material for aerospace - Google Patents

Abstract

The utility model discloses a forming device of aerospace thermosetting combined material production, including supporting mechanism, placement mechanism, cooling body, supporting mechanism's upper portion is provided with cooling body, cooling body's upper portion is provided with placement mechanism still preheats fashioned forming mechanism including being used for the material, forming mechanism includes cylinder, connecting rod, pressure disk, battery, wire, heating plate, the cylinder passes through bolted connection and is in supporting mechanism's lower part, there is the connecting rod lower part of cylinder through bolted connection, there is the lower part of connecting rod through bolted connection the pressure disk. The utility model discloses utilize the setting of heating plate can guarantee to preheat before the raw materials shaping, guaranteed the raw materials easily shaping to after the shaping, can cool down rapidly under the effect of condenser pipe, make the part can be cooled down rapidly, can take out.

Description

Forming device for producing thermosetting composite material for aerospace

Technical Field

The utility model relates to a combined material production technical field especially relates to a forming device of aerospace thermosetting combined material production.

Background

The composite material is a material formed by combining two or more different substances in different modes, can exert the advantages of various materials, overcomes the defect of a single material, and expands the application range of the material. The composite material has the characteristics of light weight, high strength, convenient processing and forming, excellent elasticity, chemical corrosion resistance, good weather resistance and the like, gradually replaces wood and metal alloy, is widely applied to the fields of aerospace, automobiles, electronics and electrical, buildings, body-building equipment and the like, and is developed rapidly in recent years. However, in the case of composite materials, the shaping is difficult or slow.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a forming device of aerospace thermosetting composite production in order to solve above-mentioned problem.

The utility model discloses a following technical scheme realizes above-mentioned purpose:

the utility model provides a forming device of thermosetting combined material production for aerospace, includes supporting mechanism, placement mechanism, cooling body, supporting mechanism's upper portion is provided with cooling body, cooling body's upper portion is provided with placement mechanism still preheats fashioned forming mechanism including being used for the material, forming mechanism includes cylinder, connecting rod, pressure disk, battery, wire, heating plate, the cylinder passes through bolted connection and is in supporting mechanism's lower part, there is the connecting rod lower part of cylinder through bolted connection, there is the pressure disk lower part of connecting rod through bolted connection, the battery passes through the screw connection and is in supporting mechanism's lower surface, the lower part of battery passes through the wire is connected with the heating plate, the heating plate with the pressure disk is connected.

Preferably, the supporting mechanism comprises a base plate, a fixed disc, a fixed block and a supporting rod, the edge of the upper surface of the base plate is connected with the supporting rod through a bolt, the upper portion of the supporting rod is connected with the fixed disc through a bolt, and the upper portion of the fixed disc is connected with the fixed block through a bolt.

Preferably, the supporting mechanism comprises a base plate, a hydraulic rod, a fixed disc and a fixed block, the edge of the upper surface of the base plate is connected with the hydraulic rod through a bolt, the upper portion of the hydraulic rod is connected with the fixed disc through a bolt, and the upper portion of the fixed disc is connected with the fixed block through a bolt.

Preferably, the placing mechanism comprises a bearing disc, a connecting frame, a bearing ring and a placing cylinder, the bearing disc is connected to the upper surface of the supporting mechanism through bolts, the upper portion of the bearing disc is connected with the connecting frame through bolts, the connecting frame is connected with the bearing ring through the bearing ring, and the placing cylinder is arranged inside the bearing ring.

Preferably, the cooling mechanism comprises a cooling liquid tank, a connecting pipe, a circulating pump and a condensing pipe, the cooling liquid tank is connected to the upper portion of the placing mechanism through bolts, the two sides of the cooling liquid tank are connected with the connecting pipe through flanges, the circulating pump is installed on the connecting pipe, and the connecting pipes are connected through the condensing pipe.

Has the advantages that: the preheating can be guaranteed to utilize the setting of heating plate before the raw materials shaping, has guaranteed the raw materials easily shaping to after the shaping, can cool down rapidly under the effect of condenser pipe, make the part can be cooled down rapidly, can take out.

Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention.

Drawings

The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:

FIG. 1 is an isometric view of a first embodiment of a molding apparatus for aerospace thermoset composite production, in accordance with the present invention;

FIG. 2 is a front view of a molding apparatus for aerospace thermoset composite production according to the present invention;

FIG. 3 is an isometric view of a second embodiment of a molding apparatus for aerospace thermoset composite production according to the present invention;

fig. 4 is a front view of a molding device for aerospace thermosetting composite material production according to the present invention.

The reference numerals are explained below:

1. a support mechanism; 101. a base plate; 102. a hydraulic lever; 103. fixing the disc; 104. a fixed block; 105. a support bar; 2. a molding mechanism; 201. a cylinder; 202. a connecting rod; 203. a platen; 204. a storage battery; 205. a wire; 206. heating the plate; 3. a placement mechanism; 301. a carrier tray; 302. a connecting frame; 303. a load ring; 304. placing the cylinder; 4. a cooling mechanism; 401. a cooling liquid tank; 402. a connecting pipe; 403. a circulating pump; 404. a condenser tube.

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.

The present invention will be further explained with reference to the accompanying drawings:

a forming device for producing thermosetting composite materials for aerospace comprises a supporting mechanism 1, a placing mechanism 3 and a cooling mechanism 4, wherein the cooling mechanism 4 is arranged at the upper part of the supporting mechanism 1, the placing mechanism 3 is arranged at the upper part of the cooling mechanism 4, the forming mechanism 2 is used for preheating and forming materials, the forming mechanism 2 comprises a cylinder 201, a connecting rod 202, a pressure plate 203, a storage battery 204, a lead 205 and a heating plate 206, the cylinder 201 is connected to the lower part of a fixed plate 103 through a bolt and provides power for the action of the pressure plate 203, the lower part of the cylinder 201 is connected with the connecting rod 202 through a bolt and acts together with the pressure plate 203 in a linkage manner, the lower part of the connecting rod 202 is connected with the pressure plate 203 through a bolt and contacts with raw materials for forming, the storage battery 204 is connected to the lower surface of the fixed plate 103 through a bolt and provides electric energy for the heating plate 206, the lower part of the storage battery 204 is connected with the heating plate 206 through the lead 205, the heating wire inside can generate heat, and the heating plate 206 is connected with the pressure plate 203, and transfers the heat to the pressure plate 203 to preheat the raw material.

Example 1

As shown in fig. 1 and 2, the supporting mechanism 1 includes a base plate 101, a fixing plate 103, a fixing block 104, and a support rod 105, wherein the edge of the upper surface of the base plate 101 is connected with the support rod 105 through a bolt, so that the fixing plate 103 is kept stable, the upper portion of the support rod 105 is connected with the fixing plate 103 through a bolt, so that the forming mechanism 2 can stably work, and the upper portion of the fixing plate 103 is connected with the fixing block 104 through a bolt; the placing mechanism 3 comprises a bearing disc 301, a connecting frame 302, a bearing ring 303 and a placing cylinder 304, wherein the bearing disc 301 is connected to the upper surface of the base plate 101 through bolts, so that the placing mechanism 3 is kept stable, the upper part of the bearing disc 301 is connected with the connecting frame 302 through bolts, the connecting frames 302 are connected through the bearing ring 303, the placing cylinder 304 is arranged inside the bearing ring 303, and the inside is a position for placing and forming raw materials; cooling body 4 includes coolant liquid jar 401, connecting pipe 402, circulation pump 403, condenser pipe 404, coolant liquid jar 401 passes through bolted connection in the upper portion of bearing dish 301, and the coolant liquid is stored to inside, and flange joint has connecting pipe 402 through the both sides of coolant liquid jar 401, can see the coolant liquid out, installs circulation pump 403 on the connecting pipe 402 for the coolant liquid can the circulation flow, connects through condenser pipe 404 between the connecting pipe 402, and inside coolant liquid can the circulation flow keep low temperature.

The working principle is as follows: let in the raw materials and place a section of thick bamboo 304, then, make it can produce the heat under the effect of heating plate 206 and pressure disk 203, and give the raw materials with the heat transfer, make the raw materials can easily the shaping, pressure disk 203 can make the raw materials pressure forming after then, make the raw materials after the shaping rapidly cool down under condenser pipe 404 and circulation pump 401's effect, the final shaping is required part, simultaneously because the setting of bracing piece 105, make forming mechanism 2 can the steady operation, thereby guarantee production quality.

Example 2

As shown in fig. 3 and 4, embodiment 2 differs from embodiment 1 in that: the supporting mechanism 1 comprises a base plate 101, a hydraulic rod 102, a fixed disc 103 and a fixed block 104, the hydraulic rod 102 is connected to the edge of the upper surface of the base plate 101 through a bolt, the working height of a machine can be adjusted, the fixed disc 103 is connected to the upper portion of the hydraulic rod 102 through a bolt, so that the forming mechanism 2 can stably work, the fixed block 104 is connected to the upper portion of the fixed disc 103 through a bolt, when the forming mechanism works, raw materials are introduced into a placing cylinder 304, then the raw materials can generate heat under the action of a heating disc 206 and a pressure disc 203, the heat is transferred to the raw materials, so that the raw materials can be easily formed, then the pressure disc 203 can press the raw materials, then the formed raw materials can be rapidly cooled under the action of a condensing pipe 404 and a circulating pump 401, finally the formed raw materials are required parts, and meanwhile, due to the arrangement of the hydraulic rod 102, the forming mechanism 2 can adjust the working height to stably work, thereby ensuring the production quality.

The foregoing illustrates and describes the principles, general features, and advantages of the present invention. 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 (5)

1. The utility model provides a forming device of aerospace thermosetting composite production, includes supporting mechanism (1), places mechanism (3), cooling body (4), the upper portion of supporting mechanism (1) is provided with cooling body (4), the upper portion of cooling body (4) is provided with place mechanism (3), its characterized in that: still including being used for preheating fashioned forming mechanism (2) to the material, forming mechanism (2) include cylinder (201), connecting rod (202), pressure disk (203), battery (204), wire (205), heating plate (206), cylinder (201) pass through bolted connection the lower part of supporting mechanism (1), there is connecting rod (202) lower part of cylinder (201) through bolted connection, there is pressure disk (203) lower part of connecting rod (202) through bolted connection, battery (204) pass through the screw connection the lower surface of supporting mechanism (1), the lower part of battery (204) passes through wire (205) is connected with heating plate (206), heating plate (206) with pressure disk (203) are connected.

2. A molding apparatus for the production of thermoset composite materials for aerospace applications as claimed in claim 1, wherein: supporting mechanism (1) includes backing plate (101), fixed disk (103), fixed block (104), bracing piece (105), there is bracing piece (105) at the upper surface edge of backing plate (101) through bolted connection, there is fixed disk (103) on the upper portion of bracing piece (105) through bolted connection, there is fixed block (104) on the upper portion of fixed disk (103) through bolted connection.

3. A molding apparatus for the production of thermoset composite materials for aerospace applications as claimed in claim 1, wherein: supporting mechanism (1) includes backing plate (101), hydraulic stem (102), fixed disk (103), fixed block (104), there is hydraulic stem (102) upper surface edge of backing plate (101) through bolted connection, there is fixed disk (103) on the upper portion of hydraulic stem (102) through bolted connection, there is fixed disk (103) on the upper portion of fixed disk (103) through bolted connection fixed block (104).

4. A molding apparatus for the production of thermoset composite materials for aerospace applications as claimed in claim 1, wherein: the placing mechanism (3) comprises a bearing disc (301), a connecting frame (302), a bearing ring (303) and a placing barrel (304), wherein the bearing disc (301) is connected to the upper surface of the supporting mechanism (1) through a bolt, the upper part of the bearing disc (301) is connected to the connecting frame (302) through a bolt, the connecting frame (302) is connected to the bearing ring (303), and the placing barrel (304) is arranged inside the bearing ring (303).

5. A molding apparatus for the production of thermoset composite materials for aerospace applications as claimed in claim 1, wherein: the cooling mechanism (4) comprises a cooling liquid tank (401), a connecting pipe (402), a circulating pump (403) and a condensing pipe (404), the cooling liquid tank (401) is connected to the upper portion of the placing mechanism (3) through bolts, the two sides of the cooling liquid tank (401) are connected with the connecting pipe (402) through flanges, the circulating pump (403) is installed on the connecting pipe (402), and the connecting pipe (402) is connected with the condensing pipe (404).

Images