High-temperature mold pressing device for production of spare and accessory parts for aviation equipment

Abstract

The utility model relates to the technical field of production of spare and accessory parts, in particular to a high-temperature mold pressing device for production of spare and accessory parts for aviation equipment, which comprises a base, a lower mold is arranged at the upper end of the base, two vertical plates are arranged at the upper end of the base, cavities are arranged in the vertical plates, and a plurality of holes are distributed in the side walls of the vertical plates in a rectangular array manner; a movable plate is arranged at the lower end of the plate block, two supports are connected to the lower end of the movable plate in a sliding mode, a heating lamp is arranged between the inner walls of the two sides of each support, and an upper mold is arranged at the lower end of the movable plate. The movable plate is pulled to slide upwards through the output end of the hydraulic cylinder, so that the upper mold and the lower mold are separated, air flow in the cavity flows into the cavity, the air flow in the cavity is sprayed out to the surface of the part through the multiple holes, and therefore the part is cooled; and the quality problems of deformation, cracking and the like of the spare and accessory parts due to high temperature are prevented through timely cooling treatment, so that the integrity and the performance of the spare and accessory parts are protected.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of spare and accessory production, especially relates to a spare and accessory production high-temperature compression mould device for aviation equipment. BACKGROUND

[0002] The spare and accessory production high-temperature compression mould device for aviation equipment is a special device designed for the production of aviation equipment spare parts, which is used for compression moulding of metal or other materials under high temperature conditions.

[0003] The existing high-temperature compression mould device, the position of the heating source (such as heating plate, heating rod, etc.) is often fixed, and it is difficult to flexibly adjust according to the size, shape and heating requirements of the material, which may cause uneven heating of the material, overheating in some areas and insufficient heating in some areas. UTILITY MODEL CONTENT

[0004] The utility model aims at providing a spare and accessory production high-temperature compression mould device for aviation equipment, which can realize the effect of uniform heating of materials of different sizes, so as to solve the problem of inconvenient uniform heating of materials of different sizes in the prior art.

[0005] In order to achieve the above-mentioned purpose, the utility model adopts the following technical scheme:

[0006] A spare and accessory production high-temperature compression mould device for aviation equipment, comprising a base, a lower mould is arranged at the upper end of the base, two vertical plates are arranged at the upper end of the base, a cavity is arranged in the vertical plate, a plurality of holes are arranged in the vertical plate in a rectangular array, the holes are communicated with the cavity, the holes are arranged obliquely, a plurality of vertical rods are arranged in a rectangular array at the upper end of the base; a plate is arranged at the upper end of the vertical rod, a movable plate is arranged at the lower end of the plate, the movable plate is connected with the vertical rod through sliding connection, two supports are connected with the lower end of the movable plate through sliding connection, a heating lamp is arranged between the inner walls of the two supports, and an upper mould is arranged at the lower end of the movable plate.

[0007] Preferably, two grooves are arranged at the upper end of the base, and the grooves are connected with the lower end of the support through sliding connection.

[0008] Preferably, a gas pump is fixedly connected to the lower end of the base, a cavity is arranged in the base, the output end of the gas pump is communicated with the inside of the cavity, and the upper end of the cavity is communicated with the lower end of the cavity.

[0009] Preferably, a hydraulic cylinder is fixedly connected to the upper end of the plate, and the output end of the hydraulic cylinder is fixedly connected with the upper end of the movable plate.

[0010] Preferably, the movable plate side wall is fixedly connected with a motor, a screw rod is rotatably connected inside the movable plate, and the motor output end is fixedly connected with the screw rod end.

[0011] Preferably, two through grooves are arranged inside the movable plate and are in through sliding connection with the vertical plate.

[0012] Compared with the prior art, the aviation equipment spare production high-temperature press molding device has the advantages that:

[0013] 1. The motor drives the screw rod to rotate, the two supports slide relative to each other, the heating lamps are located above the material, the material is uniformly heated by the two heating lamps, after the material is heated to a proper temperature, the two supports drive the two heating lamps to slide relative to each other to the two sides of the upper mold, the movable plate is pushed downward by the hydraulic cylinder output end, so that the upper mold and the lower mold are in contact, the material is pressed and forged into the required horizontal space equipment spare, the sliding of the supports and the heating lamps makes the device adapt to materials of different sizes and shapes, and the flexibility of the production line is increased.

[0014] 2. The movable plate is pulled upward by the hydraulic cylinder output end, so that the upper mold and the lower mold are separated, the external airflow is delivered to the cavity inside by the air pump, the airflow in the cavity flows to the chamber inside, and the airflow in the chamber is sprayed to the surface of the spare through the multiple holes, so that the spare is cooled, the timely cooling prevents the spare from being deformed, cracked and other quality problems due to high temperature, and the integrity and performance of the spare are protected. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is a front view of the external structure of the aviation equipment spare production high-temperature press molding device.

[0016] Figure 2 It is a front view of the external structure of the aviation equipment spare production high-temperature press molding device.

[0017] Figure 3 It is a rear view of the external structure of the aviation equipment spare production high-temperature press molding device.

[0018] Figure 4 It is a side view of the external structure of the aviation equipment spare production high-temperature press molding device.

[0019] In the figure: 001 base, 101 lower mold, 102 groove, 103 air pump, 104 cavity, 105 vertical plate, 106 chamber, 107 hole, 108 vertical rod, 002 plate, 201 hydraulic cylinder, 202 movable plate, 203 motor, 204 screw rod, 205 support, 206 heating lamp, 207 upper mold. DETAILED DESCRIPTION

[0020] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments.

[0021] Referring to Figures 1-4 A high-temperature pressure mold device for producing spare parts for aviation equipment, comprising a base 001, a lower mold 101 is arranged at the upper end of the base 001, two vertical plates 105 are arranged at the upper end of the base 001, a chamber 106 is arranged in the vertical plate 105, a plurality of holes 107 are arranged in the side wall of the vertical plate 105 in a rectangular array, the holes 107 are communicated with the chamber 106, the holes 107 are arranged obliquely, a plurality of vertical rods 108 are arranged at the upper end of the base 001 in a rectangular array; a plate 002 is arranged at the upper end of the vertical rod 108, a movable plate 202 is arranged at the lower end of the plate 002, the movable plate 202 is slidably connected with the vertical rod 108, two supports 205 are slidably connected at the lower end of the movable plate 202, a heating lamp 206 is arranged between the inner walls of the two supports 205, an upper mold 207 is arranged at the lower end of the movable plate 202, an operator places materials on the upper end of the lower mold 101, the two supports 205 are relatively slid to make the heating lamps 206 above the materials, the materials are uniformly heated by the two heating lamps 206, after the materials are heated to a proper temperature, the two supports 205 relatively slide with the two heating lamps 206 to the two sides of the upper mold 207, the movable plate 202 drives the upper mold 207 to slide downward, so that the upper mold 207 contacts with the lower mold 101, the materials are pressed and forged into the required spare parts for aviation equipment, after the materials are pressed and forged, the movable plate 202 slides upward, so that the upper mold 207 is separated from the lower mold 101, air flows in the chamber 106 arranged in the vertical plate 105, and the air flows are sprayed to the surface of the spare parts through the plurality of holes 107, so that the spare parts are cooled.

[0022] Two grooves 102 are arranged at the upper end of the base 001, the grooves 102 are slidably connected with the lower end of the support 205, after the upper mold 207 is combined with the lower mold 101, the lower end of the support 205 and the heating lamp 206 slide into the grooves 102, and the two are stored through the grooves 102.

[0023] An air pump 103 is fixedly connected to the lower end of the base 001. A cavity 104 is provided inside the base 001. The output end of the air pump 103 is connected to the inside of the cavity 104. The upper end of the cavity 104 is connected to the lower end of the chamber 106. The air pump 103 delivers external airflow to the inside of the cavity 104, and the airflow inside the cavity 104 flows into the inside of the chamber 106.

[0024] A hydraulic cylinder 201 is fixedly connected to the upper end of the plate 002. The output end of the hydraulic cylinder 201 is fixedly connected to the upper end of the movable plate 202. The movable plate 202 is pushed or pulled longitudinally by the hydraulic cylinder 201.

[0025] A motor 203 is fixedly connected to the side wall of the movable plate 202. A screw 204 is rotatably connected inside the movable plate 202. The output end of the motor 203 is fixedly connected to the end of the screw 204. The screw 204 is threadedly connected to two brackets 205. The side wall of the screw 204 is provided with positive and negative threads. The two brackets 205 correspond to the positive and negative threads. The motor 203 drives the screw 204 to rotate, so that the two brackets 205 slide relative to each other.

[0026] The movable plate 202 has two through slots 208 inside, which are slidably connected to the vertical plate 105. After the upper mold 207 and the lower mold 101 are closed, the vertical plate 105 slides through into the through slot 208.

[0027] In this invention, the operator places the material on the upper end of the lower mold 101, and drives the screw 204 to rotate via the motor 203, causing the two supports 205 to slide relative to each other, so that the heating lamp 206 is positioned above the material. The two heating lamps 206 heat the material evenly. After the material is heated to a suitable temperature, the two supports 205 drive the two heating lamps 206 to slide relative to each other to both sides of the upper mold 207. The output end of the hydraulic cylinder 201 pushes the movable plate 202 to slide downward, so that the upper mold 207 contacts the lower mold 101, pressing and forging the material into the required horizontal equipment parts. At the same time, the vertical plate 105 slides through into the through groove 208, and the lower end of the support 205 and the heating lamp 206 slide into the groove 102, where the groove 102 stores them.

[0028] After the material is pressed and forged, the hydraulic cylinder 201 pulls the movable plate 202 upward to slide, so that the upper mold 207 is separated from the lower mold 101. The air pump 103 delivers external airflow to the cavity 104. The airflow inside the cavity 104 flows into the chamber 106. The airflow inside the chamber 106 is sprayed out through multiple holes 107 onto the surface of the parts, thereby cooling the parts.

[0029] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and the inventive concept of the present utility model, should be included within the protection scope of the present utility model.

Claims

1. A high-temperature molding device for producing spare parts for aerospace equipment, characterized in that, include A base (001) is provided with a lower mold (101) at its upper end. Two vertical plates (105) are provided at the upper end of the base (001). A cavity (106) is provided inside the vertical plate (105). Multiple holes (107) are arranged in a rectangular array on the side wall of the vertical plate (105). The holes (107) are connected to the cavity (106). The holes (107) are inclined. Multiple vertical rods (108) are arranged in a rectangular array at the upper end of the base (001). Plate (002), the plate (002) is located at the upper end of the vertical rod (108), and a movable plate (202) is provided at the lower end of the plate (002). The movable plate (202) is slidably connected to the vertical rod (108). Two supports (205) are slidably connected at the lower end of the movable plate (202). Heating lamps (206) are provided between the inner walls on both sides of the supports (205). An upper mold (207) is provided at the lower end of the movable plate (202).

2. The high-temperature molding device for producing spare parts for aviation equipment according to claim 1, characterized in that, The upper end of the base (001) is provided with two grooves (102), and the grooves (102) are slidably connected to the lower end of the bracket (205).

3. The high-temperature molding device for producing spare parts for aviation equipment according to claim 1, characterized in that, An air pump (103) is fixedly connected to the lower end of the base (001). A cavity (104) is provided inside the base (001). The output end of the air pump (103) is connected to the inside of the cavity (104). The upper end of the cavity (104) is connected to the lower end of the chamber (106).

4. A high-temperature molding device for producing spare parts for aviation equipment according to claim 1, characterized in that, A hydraulic cylinder (201) is fixedly connected to the upper end of the plate (002), and the output end of the hydraulic cylinder (201) is fixedly connected to the upper end of the movable plate (202).

5. A high-temperature molding device for producing spare parts for aviation equipment according to claim 1, characterized in that, A motor (203) is fixedly connected to the side wall of the movable plate (202), and a screw (204) is rotatably connected inside the movable plate (202). The output end of the motor (203) is fixedly connected to the end of the screw (204), and the screw (204) is threadedly connected to two brackets (205).

6. A high-temperature molding device for producing spare parts for aviation equipment according to claim 1, characterized in that, The movable plate (202) has two through slots (208) inside, and the through slots (208) are slidably connected to the vertical plate (105).

Images