CN210498240U - Fixed frock of preparation impeller wax matrix - Google Patents

Fixed frock of preparation impeller wax matrix Download PDF

Info

Publication number
CN210498240U
CN210498240U CN201921316094.8U CN201921316094U CN210498240U CN 210498240 U CN210498240 U CN 210498240U CN 201921316094 U CN201921316094 U CN 201921316094U CN 210498240 U CN210498240 U CN 210498240U
Authority
CN
China
Prior art keywords
template
lock
impeller
wax
branch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201921316094.8U
Other languages
Chinese (zh)
Inventor
王显宇
吴向龙
张树河
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dalian Gerui Precision Industry Co Ltd
Original Assignee
Dalian Gerui Precision Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dalian Gerui Precision Industry Co Ltd filed Critical Dalian Gerui Precision Industry Co Ltd
Priority to CN201921316094.8U priority Critical patent/CN210498240U/en
Application granted granted Critical
Publication of CN210498240U publication Critical patent/CN210498240U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The utility model discloses a fixed frock of preparation impeller wax matrix, include: base, rotation axis, lower lock template, guide bracket, lock template, locking screw, be equipped with the rotation axis on the base, the rotation axis top is connected with the centre bore cooperation of lower lock template, and the both sides of locking the template under are equipped with guide bracket, are equipped with the poroid slide on every guide bracket, lock the template and be located lock template top down, be equipped with branch in last lock template both sides, branch is located the poroid slide that corresponds, is equipped with locking screw at the outer tip of branch. The tool effectively fixes the split wax mold, is simple in structure and high in practicability, can obtain a wax pattern with high dimensional and slide tolerance precision in the impeller combining process, and lays a solid foundation for obtaining good casting products subsequently.

Description

Fixed frock of preparation impeller wax matrix
Technical Field
The utility model belongs to the technical field of the precision casting impeller, a fixed frock of preparation impeller wax matrix specifically says so.
Background
The impeller machine is a power machine which takes continuous rotating blades as a body and enables energy to be converted between fluid working media and shaft power. It can be divided into axial flow, radial flow, mixed flow, combined type, etc. according to the moving direction of the fluid. Generally, axial flow has high efficiency and large flow rate, but the pressure ratio (expansion ratio) is low; the radial flow efficiency, flow rate is slightly low, but the pressure ratio (expansion ratio) is large. The power generation system can be classified into a prime mover such as a steam turbine, a gas turbine, etc. (output power) according to functions; working machines, such as water pumps, fans, compressors, propellers, etc. (power consumption). Common working media comprise air, water, hydrogen, ammonia, carbon dioxide and the like, and the characteristics of the turbines with different working media are different.
The device belongs to two secondary disciplines of power machinery and fluid machinery under the disciplines of power engineering and engineering thermophysics, and has wide application, including a gas compressor, a turbine, a rotor wing and the like in military aircrafts and ship engines; a marine propeller thruster; a water pump, a fan, a steam turbine, a wind turbine and a water turbine in the power generation system; the turbines used in the refrigeration industry are compressors and expanders; compressors, fans, etc. in the chemical industry, turbomachinery are often one of the most critical, most important components in these industries.
Impeller machines hold a very important position in national economy, especially in the whole heavy industrial system. Among them, the gas turbine has been widely used as the core power in high-end fields such as aviation, power station, ship, missile, tank, heavy-duty locomotive, etc., and the main or auxiliary power in general industrial fields such as metallurgy, exploration, chemical industry, civil engineering, etc., so that more and more people think that the production level of the gas turbine has become one of the most important marks for measuring the whole strength of a national industry. The turbine can realize higher single machine power (up to million kW level), higher rotating speed, reliable operation, low fuel (multipurpose coal) cost and relatively mature technology, so the turbine has irreplaceable effect on the aspect of being used as the main power of a central power station, a large ship and a warship. The higher reliability also makes the application of the steam turbine more common than the combustion engine in the industries of metallurgy, chemical engineering and the like.
The impeller machine is the largest sending equipment in the energy field at present (a thermal power plant, a gas turbine power plant, a hydropower station, a nuclear power station and the like are all used), and the research on improving the efficiency of the impeller machine is one of important methods for solving the energy problem. The production difficulty of complex impeller products in precision casting is high, and in order to produce the castings by an investment casting method, a high-precision, complex and integral wax pattern is obtained firstly. The traditional combined wax pattern is formed by melting and butting the joint parts of the wax patterns together by means of a heated soldering lug, the operation is only manual combination, the shape and the size of the wax pattern combination are greatly changed, the precision is low, and the accuracy of the wax pattern combination is greatly different due to human factors.
SUMMERY OF THE UTILITY MODEL
In order to solve the problem that manual operation is adopted in the combination of impeller wax matrix among the prior art, and its size and precision can't effectively be guaranteed, this application provides a fixed frock of preparation impeller wax matrix, has promoted the quality of impeller combination product.
In order to achieve the purpose, the technical scheme of the application is as follows: the utility model provides a fixed frock of preparation impeller wax matrix, includes: base, rotation axis, lower lock template, guide bracket, lock template, locking screw, be equipped with the rotation axis on the base, the rotation axis top is connected with the centre bore cooperation of lower lock template, and the both sides of locking the template under are equipped with guide bracket, are equipped with the poroid slide on every guide bracket, lock the template and be located lock template top down, be equipped with branch in last lock template both sides, branch is located the poroid slide that corresponds, is equipped with locking screw at the outer tip of branch.
Furthermore, the bottom of the rotating shaft is rotatably connected with a central hole of the base.
Further, the base is fixed on the workbench.
Further, the lower cover plate of the impeller wax mould is positioned on the lower lock-type plate, and the upper cover plate of the impeller wax mould is contacted with the bottom surface of the upper lock-type plate.
The utility model discloses owing to adopt above technical scheme, can gain following technological effect: the utility model provides a frock has carried out effectual fixed with components of a whole that can function independently wax matrix, and its simple structure, practicality are strong, have saved the time, can obtain the higher wax matrix of size and slide tolerance precision at impeller composite process, lays solid foundation for the follow-up good foundry goods product that obtains.
Drawings
FIG. 1 is a schematic structural view of a fixture for manufacturing a wax mold of an impeller;
the sequence numbers in the figures illustrate: 1. the base, 2, rotation axis, 3, lower plate of locking, 4, guide bracket, 5, poroid slide, 6, the plate of locking, 7, locking screw.
Detailed Description
The invention will be described in further detail with reference to the following figures and specific embodiments: the present application is further described by taking this as an example.
As shown in fig. 1, the present embodiment provides a fixed tooling for manufacturing an impeller wax mold, including: the bottom of the rotating shaft is rotatably connected with a central hole of the base, the top of the rotating shaft is matched and connected with the central hole of the lower lock-type plate, and the lower lock-type plate can rotate along with the rotating shaft; the two sides of the lower lock-type plate are provided with guide supports, each guide support is provided with a porous slideway, the upper lock-type plate is positioned above the lower lock-type plate, the two sides of the upper lock-type plate are provided with supporting rods, the supporting rods are positioned in the corresponding porous slideways, and the outer end parts of the supporting rods are provided with locking screws.
In the actual operation process, the base (1) is fixed on the workbench; firstly, respectively carrying out wax injection on an upper cover plate, a lower cover plate and blades of an impeller product. Then, an upper cover plate, a lower cover plate and blades of an impeller product which is subjected to wax injection are preliminarily combined and placed on a lower lock plate of the tool, an upper lock plate (6) is guided by a guide support to fall (at the moment, the upper cover plate of an impeller wax mold is in contact with the bottom surface of the upper lock plate), a locking screw (7) is used for locking to fix the impeller wax mold in the tool, a rotating shaft is manually operated to drive the impeller wax mold to rotate and perform combined welding, so that the combined operation of the impeller wax mold can be completed, and the time for combining the wax mold is saved.
Then, the above-mentioned, only for the utility model creates the concrete implementation mode of preferred, but the utility model discloses the scope of protection that creates is not limited to this, and any person skilled in this technical field is in the utility model discloses create the technical scope of disclosure, according to the utility model discloses the technical scheme that creates and utility model design equivalence substitution or change all should be covered in the scope of protection that the utility model created.

Claims (4)

1. The utility model provides a fixed frock of preparation impeller wax matrix which characterized in that includes: base, rotation axis, lower lock template, guide bracket, lock template, locking screw, be equipped with the rotation axis on the base, the rotation axis top is connected with the centre bore cooperation of lower lock template, and the both sides of locking the template under are equipped with guide bracket, are equipped with the poroid slide on every guide bracket, lock the template and be located lock template top down, be equipped with branch in last lock template both sides, branch is located the poroid slide that corresponds, is equipped with locking screw at the outer tip of branch.
2. The fixture for manufacturing the wax mold of the impeller according to claim 1, wherein the bottom of the rotating shaft is rotatably connected with the central hole of the base.
3. The fixed tooling for manufacturing the wax mold of the impeller according to claim 1, wherein the base is fixed on a workbench.
4. The fixture for manufacturing the wax mold of the impeller according to claim 1, wherein the lower cover plate of the wax mold of the impeller is positioned on the lower lock mold plate, and the upper cover plate of the wax mold of the impeller is contacted with the bottom surface of the upper lock mold plate.
CN201921316094.8U 2019-08-14 2019-08-14 Fixed frock of preparation impeller wax matrix Active CN210498240U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921316094.8U CN210498240U (en) 2019-08-14 2019-08-14 Fixed frock of preparation impeller wax matrix

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921316094.8U CN210498240U (en) 2019-08-14 2019-08-14 Fixed frock of preparation impeller wax matrix

Publications (1)

Publication Number Publication Date
CN210498240U true CN210498240U (en) 2020-05-12

Family

ID=70589224

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921316094.8U Active CN210498240U (en) 2019-08-14 2019-08-14 Fixed frock of preparation impeller wax matrix

Country Status (1)

Country Link
CN (1) CN210498240U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114713761A (en) * 2022-03-31 2022-07-08 西安航天发动机有限公司 Interference-free auxiliary tool for bonding wax molds of aerospace liquid engine wheel products

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114713761A (en) * 2022-03-31 2022-07-08 西安航天发动机有限公司 Interference-free auxiliary tool for bonding wax molds of aerospace liquid engine wheel products
CN114713761B (en) * 2022-03-31 2024-02-09 西安航天发动机有限公司 Interference-free auxiliary tool for bonding wax patterns of wheel products of aerospace liquid engines

Similar Documents

Publication Publication Date Title
CN100574989C (en) Two-sided synchronous high-efficiency milling and casting machine tool for impeller vane
CN105252224B (en) A kind of aero-engine outer duct outlet guide vanes processing method
CN210498240U (en) Fixed frock of preparation impeller wax matrix
CN2859041Y (en) Water supplying pump for pressure boiler
CN114688100B (en) Assembly method of gas compressor of gas turbine engine
CN110821712B (en) Low temperature turbine pump high temperature gas outlet end connection structure
CN112115576A (en) Variable efficiency correction method and system for axial flow compressor scale reducing process
Richerson et al. Ceramic gas turbine engine demonstration program
CN115401406A (en) Finish machining method for CPP (casting polypropylene) variable pitch propeller hub assembly
Eckardt et al. Advanced gas turbine technology: ABB/BCC historical firsts
Reddy et al. Analysis of steam turbines
CN207154669U (en) It is pneumatic to open turbine mould
US11806894B2 (en) Method and apparatus for improving core manufacturing for gas turbine components
CN209614559U (en) Cast turbine friction welding clamp
CN210113386U (en) Split type power turbine structure containing static pressure seal
Lin et al. Applications of additively manufactured adjustable vaned diffusers in centrifugal compressor
CN207892708U (en) A kind of gas turbine retrofited by fanjet
CN112595657A (en) Salt spray corrosion experiment table for turbine of micro gas turbine
Zheng et al. Design of a centrifugal compressor with low specific speed for automotive fuel cell
CN213437425U (en) Slot milling machine for field reconstruction of steam turbine cylinder
WO2022116790A1 (en) Method for obtaining force and torque and doing work on load, and apparatus and application thereof
CN219113679U (en) Turbocharger blade processing device
CN102699264A (en) One-piece-forged processing method of centrifugal fan of 400 MW level gas turbine generator
CN115238370B (en) Rapid assessment method for single-stage turbine through-flow scale of marine gas turbine
CN214489043U (en) High-precision trimming die for blade of aero-engine

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant