CN109162918B - Vortex disk of oil-free vortex air compressor - Google Patents

Vortex disk of oil-free vortex air compressor Download PDF

Info

Publication number
CN109162918B
CN109162918B CN201811119322.2A CN201811119322A CN109162918B CN 109162918 B CN109162918 B CN 109162918B CN 201811119322 A CN201811119322 A CN 201811119322A CN 109162918 B CN109162918 B CN 109162918B
Authority
CN
China
Prior art keywords
static
radiator
vortex
main body
disc
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.)
Expired - Fee Related
Application number
CN201811119322.2A
Other languages
Chinese (zh)
Other versions
CN109162918A (en
Inventor
高相家
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201811119322.2A priority Critical patent/CN109162918B/en
Publication of CN109162918A publication Critical patent/CN109162918A/en
Application granted granted Critical
Publication of CN109162918B publication Critical patent/CN109162918B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0215Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form where only one member is moving
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/04Heating; Cooling; Heat insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2230/00Manufacture
    • F04C2230/20Manufacture essentially without removing material
    • F04C2230/23Manufacture essentially without removing material by permanently joining parts together
    • F04C2230/231Manufacture essentially without removing material by permanently joining parts together by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2230/00Manufacture
    • F04C2230/20Manufacture essentially without removing material
    • F04C2230/25Manufacture essentially without removing material by forging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2230/00Manufacture
    • F04C2230/90Improving properties of machine parts
    • F04C2230/91Coating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2230/00Manufacture
    • F04C2230/90Improving properties of machine parts
    • F04C2230/92Surface treatment

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Abstract

Oil-free vortex air compressor machine vortex dish divide into quiet vortex dish and move the vortex dish, quiet vortex dish with move the vortex dish and split respectively into 2 parts, quiet dish main part, quiet dish radiator promptly with driving disk main part, driving disk radiator. The static plate radiator is welded on the radiating surface of the static plate main body, the movable plate radiator is welded on the radiating surface of the movable plate main body, the static plate main body and the movable plate main body are produced by an alloy aluminum semi-solid forging process, and the static plate radiator and the movable plate radiator are produced by an alloy aluminum extrusion process. The radiator manufactured by adopting the alloy aluminum extrusion process not only improves the mechanical strength of the radiating fins, but also increases the number of the radiating fins and the total radiating area by more than 1 time under the condition that the heat source collecting area is the same as the sectional area of the cooling radiating channel, thereby greatly reducing the operating temperature of the scroll plate, improving the operating condition of the air compressor, obviously improving the performance of the air compressor, reducing the failure rate and improving the reliability.

Description

Vortex disk of oil-free vortex air compressor
The technical field is as follows:
the invention relates to the technical field of scroll compressors, in particular to a scroll plate of an oil-free scroll air compressor.
Background art:
the oil-free scroll air compressor is divided into a static scroll and a movable scroll, the oil-free scroll air compressor is molded by adopting a casting process at present, the size of the outer diameter dimension is mainly determined by the air displacement and the driving power of the air compressor, the outer diameter of the scroll does not exceed 400mm with respect to the current technical level and the manufacturing capability, and the driving power does not exceed 11 kW. Due to the casting process, the thickness, number and spacing of the fins are significantly constrained when casting the heat sink on the back of the scroll. Meanwhile, the air holes and the air holes are difficult to overcome, and further influence the heat dissipation performance of the scroll and the strength of the heat dissipation fins.
The invention content is as follows:
the technical problem to be solved by the invention is to overcome the defects of the prior art, and the novel oil-free vortex air compressor scroll is suitable for an oil-free vortex air compressor with the outer diameter smaller than 400mm and the driving power not exceeding 11 kW.
The technical problem to be solved by the invention is realized by adopting the following technical scheme.
There is not oily vortex air compressor machine vortex dish divide into static vortex dish and move the vortex dish, its characterized in that: the static vortex plate and the movable vortex plate are respectively split into 2 parts, namely a static plate main body, a static plate radiator, a movable plate main body and a movable plate radiator, the static plate main body and the movable plate main body are produced by a semi-solid forging process, and the static plate radiator and the movable plate radiator are produced by an alloy aluminum extrusion process.
Further technology: the forging process adopts an aluminum alloy semi-solid forging process for forging, the defects of air holes, loosening defects, low qualified rate of finished products and the like which are difficult to avoid in the conventional cast alloy aluminum are completely avoided, and the vortex disc main body forged by the process has high density, high strength and high reliability. Meanwhile, compared with the production cost and the production rate of a cast alloy aluminum vortex plate, the production cost of the vortex plate forged by the semi-solid forging process is lower, and the production efficiency is higher.
Further technology: the static disc radiator and the movable disc radiator produced by adopting the alloy aluminum extrusion process have the advantages that the number of radiating fins on the radiating surface of the static disc radiator and the number of radiating fins on the radiating surface of the movable disc radiator are increased by more than 1 time compared with the number of radiating fins on the original cast radiator, so that the radiating area is increased by more than 1 time under the condition that the heat source collecting area and the sectional area of a cooling air duct are the same, the working temperature of a vortex disc is greatly reduced, and the operating efficiency and the reliability of a vortex. In addition, the strength of the radiating fin is greatly improved.
Further technology: the static dish radiator welds the cooling surface at static dish main part, and the welding of driving disk radiator is at the cooling surface of driving disk main part.
Further technology: the movable and static disc main bodies are subjected to T6 heat treatment process flow treatment
Further technology: locally and chemically plating nickel on the welding surface, wherein the thickness of the nickel plating is not less than 10 mu m, solidifying a layer of metal nickel on the welding surface of the movable and static disk main bodies and the radiating fins on the movable and static radiators after welding pretreatment, then placing a welding piece which is completely the same as the welding surface in shape and has the thickness of about 0.5mm between the welding surfaces of the movable and static disk main bodies and the movable and static radiators, putting the welding piece and the movable and static radiators and the static disk main bodies and the movable and static radiators in a horizontal state to carry out alloy aluminum high-temperature vacuum plane welding, controlling the furnace temperature to reach 300 ℃ for not less than 1 hour, keeping the temperature at 300 ℃ for not less than 5 minutes, and then.
Further technology: the movable and static disk main bodies and the movable and static radiators are welded by adopting a soldering flux welding process.
Further technology: the welding lug material adopted by the invention allows the working temperature of the welded scroll whole body to be not less than 230 ℃.
Further technology: and performing aging treatment on the welded static vortex plate and the welded movable vortex plate, then performing precision machining, and finally performing surface hardening treatment.
Compared with the prior art, the invention has the following advantages and positive effects
1. The structure of the scroll plate blank is simplified, the difficulty of the manufacturing process of the scroll plate blank is reduced, the yield of the scroll plate blank is improved, and the manufacturing cost of the scroll plate blank is reduced.
2. After the blank of the scroll plate is changed from a casting process to a forging process, the defects of air holes, sand holes and the like easily generated by the casting process are overcome, the mechanical strength of the scroll plate is greatly improved, the thermal deformation of the scroll plate is reduced, and therefore the stability and the reliability of the operation of the oil-free scroll air compressor are improved.
3. The radiator manufactured by adopting the alloy aluminum extrusion process not only greatly improves the strength of the radiating fins, but also increases the number of the radiating fins and the total radiating area by more than 1 time under the condition that the heat source collecting area is the same as the sectional area of the cooling radiating channel, thereby greatly reducing the operating temperature of the scroll plate, improving the operating condition of the air compressor, obviously improving the performance of the air compressor, reducing the failure rate and improving the reliability.
4. The invention not only improves the performance of the air compressor, reduces the failure rate and improves the reliability, but also improves the bottleneck value of the prior oil-free vortex air compressor on the air displacement.
Description of the drawings:
FIG. 1 is an explosion schematic diagram of a scroll structure of an oil-free scroll air compressor;
FIG. 2 is a schematic structural view of a stationary plate main body and a stationary plate radiator;
FIG. 3 is a schematic view of the structure of the movable plate main body and the movable plate heat sink;
FIG. 4 is a schematic view of a static scroll compression cavity surface configuration;
FIG. 5 is a schematic view of a heat dissipating surface of the stationary plate;
FIG. 6 is a schematic view of a compression cavity surface structure of a orbiting scroll;
FIG. 7 is a schematic view of a heat dissipating surface of the rotor plate.
The specific implementation mode is as follows:
in order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
Example 1: oil-free vortex air compressor machine vortex dish divide into quiet vortex dish and moves the vortex dish, quiet vortex dish with move the vortex dish split respectively and be 2 parts, quiet dish main part 1 promptly, quiet dish radiator 2, and driving disk main part 3, driving disk radiator 4, quiet dish radiator is fixed at quiet dish main part lateral wall, the cooling surface in driving disk main part is fixed to the driving disk radiator, and quiet dish main part and driving disk main part adopt alloy aluminium semi-solid state forging technology production, quiet dish radiator and driving disk radiator adopt alloy aluminium extrusion technology production.
The forging process adopts the alloy aluminum semi-solid forging process to forge, the defects of air holes, loosening defects, low qualified rate of finished products and the like which are difficult to avoid in the prior casting of alloy aluminum are completely avoided, and the vortex disc main body forged by the process has high density, high strength and high reliability. Meanwhile, compared with the production cost and the production rate of a cast alloy aluminum vortex plate, the production cost of the vortex plate forged by the semi-solid forging process is lower, and the production efficiency is higher.
The radiator manufactured by adopting the alloy aluminum extrusion process not only greatly improves the strength of the radiating fins, but also increases the quantity of the radiating fins on the static disc radiator and the dynamic disc radiator by more than 1 time compared with the original cast radiator, so that the radiating area is increased by more than 1 time under the condition that the heat source collecting area is the same as the sectional area of the cooling air duct, thereby greatly reducing the working temperature of the vortex disc and improving the operating efficiency and the reliability of the vortex air compressor. The static dish radiator welds the cooling surface at static dish main part, and the welding of driving disk radiator is at the cooling surface of driving disk main part.
And carrying out T6 heat treatment process flow treatment on the movable disc body and the static disc body.
Locally and chemically plating nickel on the welding surface, wherein the thickness of the nickel plating is not less than 10 mu m, solidifying a layer of metal nickel on the welding surface of the movable and static disk main bodies and the radiating fins on the movable and static radiators after welding pretreatment, then placing a welding piece which is completely the same as the welding surface in shape and has the thickness of about 0.5mm between the welding surfaces of the movable and static disk main bodies and the movable and static radiators, putting the welding piece and the movable and static radiators and the static disk main bodies and the movable and static radiators in a horizontal state to carry out alloy aluminum high-temperature vacuum plane welding, controlling the furnace temperature to reach 300 ℃ for not less than 1 hour, keeping the temperature at 300 ℃ for not less than 5 minutes, and then.
The welding lug material adopted by the invention allows the working temperature of the welded scroll whole body to be not less than 230 ℃.
And performing aging treatment on the welded static vortex plate and the welded movable vortex plate, then performing precision machining, and finally performing surface hardening treatment.
Example 2: there is not oily vortex air compressor machine vortex dish, divide into quiet vortex dish and move the vortex dish, quiet vortex dish with move the vortex dish split respectively and be 2 parts, quiet dish main part 1 promptly, quiet dish radiator 2, and driving disk main part 3, driving disk radiator 4, the radiating surface in quiet dish main part is fixed to quiet dish radiator, the radiating surface in driving disk main part is fixed to the driving disk radiator to quiet dish main part and driving disk main part adopt semi-solid state forging technology production, quiet dish radiator and driving disk radiator adopt alloy aluminium extrusion technology production.
The forging process adopts an aluminum alloy semi-solid forging process for forging, the defects of air holes, loosening defects, low qualified rate of finished products and the like which are difficult to avoid in the conventional cast alloy aluminum are completely avoided, and the vortex disc main body forged by the process has high density, high strength and high reliability. Meanwhile, compared with the production cost and the production rate of a cast alloy aluminum vortex plate, the production cost of the vortex plate forged by the semi-solid forging process is lower, and the production efficiency is higher.
The radiator manufactured by adopting the alloy aluminum extrusion process not only greatly improves the strength of the radiating fins, but also increases the quantity of the radiating fins on the static disc radiator and the dynamic disc radiator by more than 1 time compared with the original cast radiator, so that the radiating area is increased by more than 1 time under the condition that the heat source collecting area is the same as the sectional area of the cooling air duct, thereby greatly reducing the working temperature of the vortex disc and improving the operating efficiency and the reliability of the vortex air compressor.
The static dish radiator welds the cooling surface at static dish main part, and the welding of driving disk radiator is at the cooling surface of driving disk main part.
The movable disc body, the static disc body, the movable disc radiator and the static disc radiator are welded by adopting a soldering flux welding process.
The welding lug material adopted by the invention allows the working temperature of the welded scroll whole body to be not less than 230 ℃.
And performing aging treatment on the welded static vortex plate and the welded movable vortex plate, then performing precision machining, and finally performing surface hardening treatment.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (4)

1. There is not oily vortex air compressor machine vortex dish divide into static vortex dish and move the vortex dish, its characterized in that: the static vortex disc and the movable vortex disc are respectively split into 2 parts, namely a static disc main body, a static disc radiator, a movable disc main body and a movable disc radiator, wherein the static disc radiator is welded on the radiating surface of the static disc main body, the movable disc radiator is welded on the radiating surface of the movable disc main body, the static disc main body and the movable disc main body are produced by adopting an alloy aluminum semi-solid forging process, and the static disc radiator and the movable disc radiator are produced by adopting an alloy aluminum extrusion process;
carrying out T6 heat treatment process flow treatment on the movable disc main body and the static disc main body; locally and chemically plating nickel on the welding surface, wherein the thickness of the nickel plating is not less than 10 mu m, solidifying a layer of metal nickel on the welding surface on the moving and static disk main bodies and the moving and static disk radiators after welding pretreatment, then placing a soldering lug with the shape completely identical to the shape of the welding surface and the thickness of about 0.5mm between the welding surfaces of the moving and static disk main bodies and the moving and static disk radiators, putting the soldering lug and the moving and static disk radiators and the soldering lug into a vacuum furnace in a horizontal state to carry out high-temperature vacuum plane welding on the alloy aluminum, controlling the furnace temperature to reach 300 ℃ for not less than 1 hour, keeping the temperature at 300 ℃ for not less than 5 minutes, and then stopping heating and naturally.
2. The oil-free scroll air compressor scroll of claim 1, wherein: the forging process adopts an aluminum alloy semi-solid forging process.
3. The oil-free scroll air compressor scroll of claim 1, wherein: the movable disc body, the static disc body, the movable disc radiator and the static disc radiator are welded by adopting a soldering flux welding process.
4. The oil-free scroll air compressor scroll of claim 1, wherein: and performing aging treatment on the welded static vortex plate and the welded movable vortex plate, then performing precision machining, and finally performing surface hardening treatment.
CN201811119322.2A 2018-09-25 2018-09-25 Vortex disk of oil-free vortex air compressor Expired - Fee Related CN109162918B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811119322.2A CN109162918B (en) 2018-09-25 2018-09-25 Vortex disk of oil-free vortex air compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811119322.2A CN109162918B (en) 2018-09-25 2018-09-25 Vortex disk of oil-free vortex air compressor

Publications (2)

Publication Number Publication Date
CN109162918A CN109162918A (en) 2019-01-08
CN109162918B true CN109162918B (en) 2019-12-27

Family

ID=64880488

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811119322.2A Expired - Fee Related CN109162918B (en) 2018-09-25 2018-09-25 Vortex disk of oil-free vortex air compressor

Country Status (1)

Country Link
CN (1) CN109162918B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110118181A (en) * 2019-06-18 2019-08-13 南京永升新能源技术有限公司 A kind of oil-free scroll air compressor machine that heat dissipation performance is excellent

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05172066A (en) * 1991-12-20 1993-07-09 Toshiba Corp Scroll fluid compressor
JPH10118734A (en) * 1996-10-17 1998-05-12 Nippon Light Metal Co Ltd Forging die, forging method and its product
JP2006192450A (en) * 2005-01-12 2006-07-27 Mitsubishi Heavy Ind Ltd Forging die for scroll, method for forging scroll and scroll
JP2006193765A (en) * 2005-01-12 2006-07-27 Mitsubishi Heavy Ind Ltd Method for producing member made of aluminum alloy
CN203488380U (en) * 2013-07-11 2014-03-19 复盛股份有限公司 Scroll type compressor structure and radiator of scroll type compressor
CN104561852A (en) * 2014-12-26 2015-04-29 西安交通大学 Process for preparing semi-solid state aluminum alloy scroll plate by radial forging strain induction method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05172066A (en) * 1991-12-20 1993-07-09 Toshiba Corp Scroll fluid compressor
JPH10118734A (en) * 1996-10-17 1998-05-12 Nippon Light Metal Co Ltd Forging die, forging method and its product
JP2006192450A (en) * 2005-01-12 2006-07-27 Mitsubishi Heavy Ind Ltd Forging die for scroll, method for forging scroll and scroll
JP2006193765A (en) * 2005-01-12 2006-07-27 Mitsubishi Heavy Ind Ltd Method for producing member made of aluminum alloy
CN203488380U (en) * 2013-07-11 2014-03-19 复盛股份有限公司 Scroll type compressor structure and radiator of scroll type compressor
CN104561852A (en) * 2014-12-26 2015-04-29 西安交通大学 Process for preparing semi-solid state aluminum alloy scroll plate by radial forging strain induction method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
大功率LED灯具散热铝型材挤压模具设计及数值模拟;郑宪阳;《中国优秀硕士学位论文全文数据库 工程科技Ⅰ辑》;20150915(第9期);第2-4页 *

Also Published As

Publication number Publication date
CN109162918A (en) 2019-01-08

Similar Documents

Publication Publication Date Title
US8472188B2 (en) Semiconductor power module, inverter, and method of manufacturing a power module
CN113695597B (en) High-performance alloy steel solid-phase additive forming device and process based on induction heating compensation
CN102126023A (en) Powder hot isostatic pressing (HIP) forming method for titanium (Ti) alloy blisk
CN109162918B (en) Vortex disk of oil-free vortex air compressor
CN101752945A (en) Motor shell with radiating fins and manufacturing method thereof
CN102172771A (en) Remelting heating process in semisolid thixotropic processing of aluminium alloy
CN104551545A (en) Strain-induced semi-solid forming device and process for fine-grained bearing pad
CN104712371A (en) Aero-engine double-alloy double-performance turbine disc and manufacturing method thereof
CN203949540U (en) A kind of flat-plate heat pipe
CN109158573A (en) A kind of almag die casting from preheating
CN107083509B (en) For the combined type liquid metal thermal interface material of IGBT heat dissipations
CN202527508U (en) Extrusion die of pipe billet
CN106584012A (en) Shaping method for amorphous alloy
CN105397050A (en) Semi-solid forming method for copper alloy
CN208945144U (en) A kind of casting forging device for metal pan manufacture
CN108015285A (en) A kind of quick molding method of the high temperature alloy diskware of aero-engine
CN103831313A (en) Manufacturing method of low-cost semi-solid thixotropic precisely-formed compressor impeller
CN105632674A (en) Method for sintering neodymium iron boron magnetic tile and discharge plasma sintering device thereof
CN202602445U (en) Aluminum motor housing
CN112211817A (en) Novel high-efficient oilless vortex air compressor machine vortex dish
CN111014618B (en) Method for preparing aluminum alloy scroll by adopting radial forging technology
KR20150139134A (en) Manufacturing methode of pin type heat-radiating substrate using cabon based metal matrix composite
CN217129804U (en) Scroll compressor heat abstractor
CN109648030A (en) A kind of TiAl-base alloy cogging forging mold
CN114603141B (en) TiAl alloy blade die forging forming method

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20191227

CF01 Termination of patent right due to non-payment of annual fee