CN209773384U - Aviation titanium alloy casting molding material wax production equipment - Google Patents
Aviation titanium alloy casting molding material wax production equipment Download PDFInfo
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- CN209773384U CN209773384U CN201920523266.2U CN201920523266U CN209773384U CN 209773384 U CN209773384 U CN 209773384U CN 201920523266 U CN201920523266 U CN 201920523266U CN 209773384 U CN209773384 U CN 209773384U
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Abstract
An aviation titanium alloy casting molding wax production device belongs to the field of aviation titanium alloy casting molding wax production devices. Comprises a crushing mechanism, a storage barrel, a collecting barrel and a weighing device; the crushing mechanism, the storage barrel, the collecting barrel and the weighing device are all mounted on the support, the crushing mechanism, the storage barrel, the collecting barrel and the weighing device are sequentially arranged from top to bottom, two crushing hobs which are arranged in parallel are mounted in a box body of the crushing mechanism through bearings and are connected in a matched mode through gears, one crushing hob is connected with a motor through a chain transmission mode, a plurality of groups of cutter tooth groups are arranged on the crushing hob, and each cutter tooth group is composed of a plurality of plate-shaped crushing cutter teeth which are arranged at intervals. The utility model discloses a pair of broken hobbing cutter in the broken mechanism is direct with the raw materials cutting shaping, and the wax after the cutting directly falls into the bucket, makes retractable barrier realize the switching function to discharge gate B through switching solenoid valve B, makes the wax of required weight fall into the collecting vessel.
Description
Technical Field
The utility model relates to an aviation titanium alloy casting moulding material wax production facility field especially relates to an aviation titanium alloy casting moulding material wax production facility.
background
At present, when strip-shaped or block-shaped aviation titanium alloy casting wax is produced, molten wax liquid is usually poured into a mold for cooling and molding, and solidified aviation titanium alloy casting wax is taken out of the mold for weighing and packaging.
SUMMERY OF THE UTILITY MODEL
Occupy the big and problem that expend time in place when solving current aviation titanium alloy casting molding material wax production packing, the utility model provides an aviation titanium alloy casting molding material wax production facility.
In order to achieve the above object, the utility model adopts the following technical scheme: the aviation titanium alloy casting molding wax production equipment comprises a crushing mechanism, a storage barrel, a collecting barrel and a weighing device; the crushing mechanism, the storage barrel, the collecting barrel and the weighing device are sequentially arranged on the support from top to bottom, two crushing hobs which are arranged in parallel are arranged in a box body of the crushing mechanism through bearings, the two crushing hobs are connected in a matched mode through gears, one side of one crushing hob extends out of the box body and is provided with a chain wheel A, the chain wheel A and a chain wheel B of a motor form a chain transmission structure, a plurality of rows of cutter tooth groups are arranged on the crushing hobs, each row of cutter tooth group is formed by a plurality of plate-shaped crushing cutter teeth which are arranged at intervals, a feeding opening is formed in the top of the box body, a discharging opening A is formed in the bottom of the box body; an opening at the top of the storage barrel is positioned below the discharge port A, a discharge port B is arranged at the bottom of the storage barrel, a clamping plate is attached below the discharge port B, the clamping plate is fixed on the bracket, an opening corresponding to the discharge port B is arranged on the clamping plate, and a telescopic baffle is arranged in a gap in the middle of the clamping plate; the opening at collecting vessel top is located discharge gate B below, and the collecting vessel bottom is provided with the discharging pipe, and the collecting vessel is fixed on the support, and the support is put on weighing device.
furthermore, the bottom surface of the storage barrel is of a conical structure and is provided with an air hammer, the air hammer is connected with an air pump through a pipeline A, an electromagnetic valve A installed on the support is arranged on the pipeline A, supporting legs are arranged on the barrel wall of the storage barrel, and the supporting legs are welded on the support.
Furthermore, the splint are two steel sheets arranged in parallel, a gap is reserved between the two steel sheets, the splint is connected with the support column through a bolt, and the support column is welded on the support.
Further, telescopic baffle one side and telescopic cylinder's hub connection, telescopic cylinder fixes on the support, and the air pump is through installing solenoid valve B's pipe connection telescopic cylinder, and solenoid valve B fixes on the support, and telescopic baffle and two upper and lower steel sheet laminating can block the opening on the splint when telescopic baffle stretches out, and the opening on the splint is released when telescopic baffle retracts.
furthermore, an opening for inserting the material baffle plate is formed in the discharge pipe, the weighing device adopts an electronic scale, and the weighing device is placed on a weighing platform of the support.
Further, the motor and the crushing mechanism are placed on the same support platform.
The utility model has the advantages that: directly cut the shaping with the raw materials through a pair of broken hobbing cutters in the crushing mechanism, the wax after the cutting directly falls into the bucket, makes retractable barrier realize the switching function to discharge gate B through switching solenoid valve B, makes the wax of required weight fall into the collecting vessel.
Drawings
Fig. 1 is a schematic structural diagram a of the present invention;
Fig. 2 is a schematic structural diagram B of the present invention;
Fig. 3 is a schematic structural diagram C of the present invention;
Fig. 4 is a schematic structural diagram D of the present invention.
In the figure, 1 is a crushing mechanism, 2 is a storage barrel, 3 is a collecting barrel, 4 is a weighing device, 5 is a motor, 6 is an air hammer, 7 is an air pump, 8 is a telescopic baffle, 9 is a telescopic cylinder, 10 is a crushing hob and 11 is a clamping plate.
Detailed Description
The aviation titanium alloy casting molding wax production equipment comprises a crushing mechanism 1, a storage barrel 2, a collecting barrel 3 and a weighing device 4; the wax cutting machine is characterized in that the crushing mechanism 1, the storage barrel 2, the collecting barrel 3 and the weighing device 4 are all installed on a support and sequentially comprise the crushing mechanism 1, the storage barrel 2, the collecting barrel 3 and the weighing device 4 from top to bottom, two crushing hobs 10 which are arranged in parallel are installed in a box body of the crushing mechanism 1 through bearings, the two crushing hobs 10 are connected through gear matching and rotate relatively, one side of one crushing hob 10 extends out of the box body and is provided with a chain wheel A, the chain wheel A and a chain wheel B of a motor 5 form a chain transmission structure, a plurality of rows of hob tooth groups are arranged on the crushing hob 10, each row of hob tooth groups are arranged in a circumferential mode around an axis of the crushing hob 10 and are used for controlling the length of cut wax, each hob tooth group is composed of a plurality of plate-shaped crushing hob teeth which are axially arranged at intervals, the hob teeth on the two crushing hobs 10 are matched and are, the top of the box body is provided with a feeding port, the bottom of the box body is provided with a discharge port A, and a support platform for placing the box body is provided with a passage at a position corresponding to the discharge port A; an opening in the top of the storage barrel 2 is located below the discharge port A, a discharge port B is arranged at the bottom of the storage barrel 2, a clamping plate 11 is attached to the lower portion of the discharge port B, the clamping plate 11 is fixed on the support, an opening corresponding to the discharge port B is formed in the clamping plate 11, and a telescopic baffle 8 is placed in a gap in the middle of the clamping plate 11; the opening at the top of collecting vessel 3 is located discharge gate B below, and collecting vessel 3 bottom is provided with the discharging pipe, and collecting vessel 3 is fixed on the support, and the support is put on weighing device 4.
2 bottom surfaces of storage bucket set up to the toper structure and install air hammer 6, appear when the wax in storage bucket 2 and can use the vibrations of air hammer 6 to drop with pasting of section of thick bamboo wall, and air hammer 6 passes through pipeline A and connects air pump 7, is provided with the solenoid valve A of installing on the support on the pipeline A, is equipped with the supporting legs on the section of thick bamboo wall of storage bucket 2, and the supporting legs welds on the support, and 2 top opening parts of storage bucket can pass through buckle installation screen cloth.
The splint 11 is two steel sheets of parallel arrangement, has the space between two steel sheets, and splint 11 passes through the bolt to be connected with the pillar, and the pillar welding is on the support.
The telescopic baffle 8 one side is connected with telescopic cylinder 9's hub connection, and telescopic cylinder 9 fixes on the support, and air pump 7 is through the pipe connection telescopic cylinder 9 of installing solenoid valve B, and solenoid valve B fixes on the support, and telescopic baffle 8 can block the opening on splint 11 with two upper and lower steel sheet laminating when telescopic baffle 8 stretches out, releases the opening on splint 11 when telescopic baffle 8 retracts.
The discharging pipe is provided with an opening for inserting the material baffle, the weighing device 4 adopts an electronic scale, the weighing device 4 is placed on a weighing platform of the support, and switches of the electromagnetic valve A and the electromagnetic valve B are both arranged on the support on one side of the material baffle, so that one worker can conveniently operate the material baffle.
The motor 5 and the crushing mechanism 1 are placed on the same support platform.
When the wax-removing device is used, wax is only required to be put into the device from a feeding port at the top of the box body, a crushing hob in the crushing mechanism directly cuts and shapes raw materials, the cut wax directly falls into the storage barrel, the electromagnetic valve B is operated to enable the telescopic baffle 8 to retract, the wax falls into the collecting barrel from the storage barrel at the moment, the material baffle is in an inserted state, when the electronic scale displays that the weight meets the requirement, the electromagnetic valve B is operated to enable the telescopic baffle 8 to extend out, the discharge port B is closed to prevent the wax from continuously falling into the collecting barrel from the storage barrel, then the material baffle is taken out, and the wax; the operation is convenient, and the manpower and the equipment floor space are saved.
The above description is only the specific implementation manner 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 can substitute or change the technical solution of the present invention and the design of the present invention within the technical scope of the present invention.
Claims (6)
1. The production equipment for the aviation titanium alloy casting wax is characterized by comprising a crushing mechanism (1), a storage barrel (2), a collecting barrel (3) and a weighing device (4); the crushing mechanism (1), the storage barrel (2), the collecting barrel (3) and the weighing device (4) are sequentially arranged on a support from top to bottom, two crushing hobs (10) which are arranged in parallel are arranged in a box body of the crushing mechanism (1) through bearings, the two crushing hobs (10) are connected in a matched mode through gears, one side of one crushing hob (10) extends out of the box body and is provided with a chain wheel A, the chain wheel A and a chain wheel B of a motor (5) form a chain transmission structure, a plurality of rows of cutter tooth groups are arranged on the crushing hobs (10), each row of cutter tooth group is formed by a plurality of plate-shaped crushing cutter teeth which are arranged at intervals, a feeding opening is formed in the top of the box body, a discharge opening A is formed in the bottom of the box body; an opening at the top of the storage barrel (2) is positioned below the discharge port A, a discharge port B is arranged at the bottom of the storage barrel (2), a clamping plate (11) is attached below the discharge port B, the clamping plate (11) is fixed on the bracket, an opening corresponding to the discharge port B is arranged on the clamping plate (11), and a telescopic baffle (8) is arranged in a gap in the middle of the clamping plate (11); the opening at the top of the collecting barrel (3) is positioned below the discharge port B, the discharge pipe is arranged at the bottom of the collecting barrel (3), the collecting barrel (3) is fixed on the support, and the support is placed on the weighing device (4).
2. The aviation titanium alloy casting material wax production equipment as claimed in claim 1, wherein the bottom surface of the storage barrel (2) is set to be a conical structure and is provided with an air hammer (6), the air hammer (6) is connected with an air pump (7) through a pipeline A, the pipeline A is provided with an electromagnetic valve A installed on a support, and the wall of the storage barrel (2) is provided with support legs welded on the support.
3. The aviation titanium alloy casting wax production equipment as claimed in claim 1, wherein the clamping plate (11) is two steel plates arranged in parallel, a gap is formed between the two steel plates, the clamping plate (11) is connected with the support through a bolt, and the support is welded on the support.
4. The aviation titanium alloy casting material wax production equipment as claimed in claim 3, wherein one side of the telescopic baffle (8) is connected with a shaft of a telescopic cylinder (9), the telescopic cylinder (9) is fixed on a bracket, an air pump (7) is connected with the telescopic cylinder (9) through a pipeline provided with an electromagnetic valve B, the electromagnetic valve B is fixed on the bracket, the telescopic baffle (8) is attached to the upper steel plate and the lower steel plate, an opening on the clamping plate (11) can be blocked when the telescopic baffle (8) extends, and the opening on the clamping plate (11) can be released when the telescopic baffle (8) retracts.
5. The aviation titanium alloy casting mold wax production equipment according to claim 1, wherein an opening for inserting the material baffle is formed in the material discharge pipe, the weighing device (4) adopts an electronic scale, and the weighing device (4) is placed on a weighing platform of the support.
6. The aviation titanium alloy casting wax production equipment as claimed in claim 1, wherein the motor (5) and the crushing mechanism (1) are placed on the same support platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920523266.2U CN209773384U (en) | 2019-04-17 | 2019-04-17 | Aviation titanium alloy casting molding material wax production equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920523266.2U CN209773384U (en) | 2019-04-17 | 2019-04-17 | Aviation titanium alloy casting molding material wax production equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209773384U true CN209773384U (en) | 2019-12-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920523266.2U Active CN209773384U (en) | 2019-04-17 | 2019-04-17 | Aviation titanium alloy casting molding material wax production equipment |
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| Country | Link |
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| CN (1) | CN209773384U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111534647A (en) * | 2020-05-11 | 2020-08-14 | 黄志芳 | Leather batch polisher during erhu manufacturing |
-
2019
- 2019-04-17 CN CN201920523266.2U patent/CN209773384U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111534647A (en) * | 2020-05-11 | 2020-08-14 | 黄志芳 | Leather batch polisher during erhu manufacturing |
| CN111534647B (en) * | 2020-05-11 | 2021-09-03 | 吴丽君 | Leather batch polisher during erhu manufacturing |
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