WO2005123302A1 - Process for manufacturing rotor-compressors of turbo-compressors and other difficult-to-extract parts, and corresponding mould - Google Patents

Process for manufacturing rotor-compressors of turbo-compressors and other difficult-to-extract parts, and corresponding mould Download PDF

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Publication number
WO2005123302A1
WO2005123302A1 PCT/BR2005/000118 BR2005000118W WO2005123302A1 WO 2005123302 A1 WO2005123302 A1 WO 2005123302A1 BR 2005000118 W BR2005000118 W BR 2005000118W WO 2005123302 A1 WO2005123302 A1 WO 2005123302A1
Authority
WO
WIPO (PCT)
Prior art keywords
drawers
mould
blocks
product
channels
Prior art date
Application number
PCT/BR2005/000118
Other languages
French (fr)
Inventor
Élio de Mello CASTANHO JÚNIOR
Original Assignee
FELIPPI, Ezídio
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 FELIPPI, Ezídio filed Critical FELIPPI, Ezídio
Publication of WO2005123302A1 publication Critical patent/WO2005123302A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/40Removing or ejecting moulded articles
    • B29C45/44Removing or ejecting moulded articles for undercut articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • B22D17/20Accessories: Details
    • B22D17/22Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • B22D17/20Accessories: Details
    • B22D17/22Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
    • B22D17/24Accessories for locating and holding cores or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/087Propellers

Definitions

  • the present patent of invention refers to a process for manufact ⁇ ing rotors of turbochargers and other parts difficult to extract by injection of aluminum or other metals or metallic blends or polymers in a mould specially designed to open three-dimensionally and to provide easy extraction of the molded product within a totally new concept, aiming a better quality and a better fmishing for the product, without needing for hardening, with a better reproducibility of the products using a same non-destructive mould, possibility of extracting complex geometry products without deformation, homogeneous and flat, having obtained products with greater mechanical and thermal resistance, larger durability, smaller friction and smaller working temperature in case of rotors for turbochargers.
  • FIGURE 1. which shows the block diagram with the sequence of the manufactrjring process of the present patent
  • FIGURE 2. which shows perspective view of the corresponding mould for die-casting a rotor with twelve blades
  • FIGURE 3. which shows a superior view of the corresponding mould for die-casting a rotor with twelve blades, with drawers in the closed position
  • FIGURE 4. which shows a superior view of the corresponding mould for die-casting a rotor with twelve blades, with drawers in the open position
  • FIGURE 5. which shows a side view of the corresponding mould for die-casting a rotor with twelve blades, with drawers in the closed position
  • the packing process has the following sequence: a) The mould is assembled, by positioning the segmented blocks ( 1 ) to perform the geometry of the product ( P ), in case of compression rotors with two or more blades, fastened in the sliding drawers ( 2
  • the mould corresponding to the process of the present patent is constituted of segmented blocks ( 1 ) of complementary formats with hollows and prominences, which when being placed side by side in circular fashion form a cavity ( C ) with the same format as the format of the wished product ( P ), fastened in the shding drawers ( 2 ) through the screws ( 2 A ) or another mean for conventional fixation, sliding drawers ( 2 ) in form of wedge, straight or helical, with the same number of sections as the blocks ( 1 ), endowed of guides ( 2-B ) with a transversal section in " T " form, straight or helical, consolidated in its external part in a radial form and cased in drawers ( 3 ) through the guides ( 2-B ) and a set of drawers ( 3 ) of cylindrical or polygonal format, distributing the channels ( 3 A) in a radial form, with channels ( 3 A ) with the same number of sections as that from the blocks ( 1 ) and as that from the drawers ( 2

Abstract

The present patent refers to a process for manufacturing rotors of turbochargers and other parts difficult to extract by injection of aluminum or other metals or metallic leagues or polymers in a mould with segmented insert (1), sliding drawers (2) and drawing sets (3), aiming a better quality and a better finishing for the piece, without needing for hardening, with a better reproducibility of the pieces using a same nondestructive mould, possibility of extracting complex geometry pieces without deformation, homogeneous and flat, having obtained pieces greater mechanical and thermal resistance, larger durability, smaller friction and smaller working temperature in case of rotors for turbochargers.

Description

"PROCESS FOR MANUFACTURING ROTOR-COMPRESSOR OF TURBO-COMPRESSORS AND OTHER DIFFICULT-TO-EXTRACT PARTS, AND CORRESPONDING MOULD". The present patent of invention refers to a process for manufactøing rotors of turbochargers and other parts difficult to extract by injection of aluminum or other metals or metallic blends or polymers in a mould specially designed to open three-dimensionally and to provide easy extraction of the molded product within a totally new concept, aiming a better quality and a better fmishing for the product, without needing for hardening, with a better reproducibility of the products using a same non-destructive mould, possibility of extracting complex geometry products without deformation, homogeneous and flat, having obtained products with greater mechanical and thermal resistance, larger durability, smaller friction and smaller working temperature in case of rotors for turbochargers. As it is well known by technicians in the branch of manufacture of rotors for vehicular turbochargers, currently the rotors-compressors have a design with complex geometry, endowed of blades helically twisted in the axial direction, that increase diameter, in an axial direction and decrease in the other ones. Presently, for manufacturing this kind of rotors or others products of complex geometries, there are basically the following processes and corresponding moulds: 1) Aluminum casting in an ingot mould with sand or another previously formatted mineral material starting from a polymeric mould, which is difficult to extract when the product geometry is complex with curves fins, needing hardening, besides producing a low-quality product with high porosity that generate much friction at high revolution speeds with elevation of temperature and bubbles that decrease its mechanical resistance, limit shelf life of the product and have a high cost due to the necessary workmanship and to disposability of the die; and 2) More recently, arose an evolution in the branch, through a device that previously manufactures dies of plaster under vacuum, in which the products are cast in aluminum, still with high cost, although time expense has decreased by corresponding decrease in workmanship, but still with the need for a disposable die and hardening process, besides producing low quality products with porosity that much friction at high revolution speeds with elevation of temperature and bubbles that decrease its mechanical resistance, and limit shelf life of the product, due to occurrence of fatigue, disintegration and cracking. "PROCESS FOR MANUFACTURING ROTOR- COMPRESSOR OF TURBO-COMPRESSOR AND OTHER DIFFICULT-TO- EXTRACT PARTS, AND CORRESPONDING MOULD", object of the present patent, was developed to solve the problems and inconvenient of the current products and processes and, by using injection process with a mould especially designed to open three-dimensionally and to provide easy extraction of the molded product with a totally new concept, aiming a better quality and a better finishing for the product, without needing for hardening, with a better reproducibility of the products using a same non- destructive mould, possibility of extracting complex geometry products without deformation, homogeneous and flat, having obtained products with greater mechanical and thermal resistance, larger durability, smaller friction and smaller working temperature in case of rotors for turbochargers. For a better understanding of the present Invention, the following drawings are attached: FIGURE 1., which shows the block diagram with the sequence of the manufactrjring process of the present patent; FIGURE 2., which shows perspective view of the corresponding mould for die-casting a rotor with twelve blades; FIGURE 3., which shows a superior view of the corresponding mould for die-casting a rotor with twelve blades, with drawers in the closed position; FIGURE 4., which shows a superior view of the corresponding mould for die-casting a rotor with twelve blades, with drawers in the open position; and FIGURE 5., which shows a side view of the corresponding mould for die-casting a rotor with twelve blades, with drawers in the closed position; According to the referred figures, the packing process has the following sequence: a) The mould is assembled, by positioning the segmented blocks ( 1 ) to perform the geometry of the product ( P ), in case of compression rotors with two or more blades, fastened in the sliding drawers ( 2 ) with the same number of sections as that from the blocks ( 1 ) and these blocks cased in drawer sets ( 3 ) with the same number of sections as that from the blocks
( i ); b) The reservoir of molten aluminum, or another metal or metallic(s) alloy(s) or polymer conventionally spills the previously calibrated quantity of material in the injection sleeve and the injection machine conventionally injects the molten material in the cavity ( C ) formed inside the mould; c) The mould with the injected product is dislocated removing the machine injection sleeve, which remains in a resting position, from the mould, in so exposing the product ( P ); and d) The conventional extractor hydraulic piston softly activates the bottom of the drawers ( 2 ) dislocating the same in the channels ( 3-A ) of the respective drawers ( 3 ), occurring a three-dimensional opening with retreat of the blocks ( 1 ) that form injection channels for the product ( P ), due to the angle of the channels ( 3-A ) of the drawers ( 2 ) which gradually retreat from the injected product, completing the extraction and liberating the injected product (
P ). The mould corresponding to the process of the present patent is constituted of segmented blocks ( 1 ) of complementary formats with hollows and prominences, which when being placed side by side in circular fashion form a cavity ( C ) with the same format as the format of the wished product ( P ), fastened in the shding drawers ( 2 ) through the screws ( 2 A ) or another mean for conventional fixation, sliding drawers ( 2 ) in form of wedge, straight or helical, with the same number of sections as the blocks ( 1 ), endowed of guides ( 2-B ) with a transversal section in " T " form, straight or helical, consolidated in its external part in a radial form and cased in drawers ( 3 ) through the guides ( 2-B ) and a set of drawers ( 3 ) of cylindrical or polygonal format, distributing the channels ( 3 A) in a radial form, with channels ( 3 A ) with the same number of sections as that from the blocks ( 1 ) and as that from the drawers ( 2 ) and with a transversal section in form of " T " straight or helical.

Claims

1 "PROCESS FOR MANUFACTURING
ROTOR-COMPRESSOR OF TURBO-COMPRESSORS AND OTHER DIFFICULT-TO-EXTRACT PARTS ", characterized by the following sequence: a) The mould is assembled, by positioning the segmented blocks ( 1 ) to perform the geometry of the product ( P ), in case of compression rotors with two or more blades, fastened in the shding drawers ( 2 ) with the same number of sections as that from the blocks ( 1 ) and these blocks cased in drawer sets ( 3 ) with the same number of sections as that from the blocks
( i ); b) The reservoir of molten alunώium, or another metal or metalhc(s) alloy(s) or polymer conventionally spills the previously calibrated quantity of material in the injection sleeve and the injection machine conventionally injects the molten material in the cavity ( C ) formed inside the mould; c) The mould with the injected product is dislocated removing the machine injection sleeve, which remains in a resting position, from the mould, in so exposing the injected product ( P ); and d) The conventional extractor hydraulic piston softly activates the bottom of the drawers ( 2 ) dislocating the same in the channels ( 3-A ) of the respective drawers ( 3 ), occurring a toee-dimensional opening with retreat of the blocks ( 1 ) that form injection channels for the product ( P ), due to the angle of the channels ( 3-A ) of the drawers ( 2 ) which gradually retreat from the injected product, completing the extraction and liberating the injected product (
P )-
2. "MOULD", characterized by, segmented blocks (
1 ) of complementary formats with hollows and prominences, which when being placed side by side in circular fashion form a cavity ( C ) with the same format as the format of the wished product ( P ), fastened in the sliding drawers ( 2 ) through the screws ( 2 A ) or another mean for conventional fixation, sliding drawers ( 2 ) in form of wedge, straight or helical, with the same number of sections as the blocks ( 1 ), endowed of guides ( 2-B ) with a transversal section in " T " form, straight or helical, consolidated in its external part in a radial form and cased in drawers ( 3 ) through the guides ( 2-B ) and a set of drawers ( 3 ) of cylindrical or polygonal format, distributing the channels ( 3-A ) in a radial form, with channels ( 3-A ) with the same number of sections as that from the blocks ( 1 ) and as that from the drawers ( 2 ) and with a transversal section in form of " T " straight or helical.
PCT/BR2005/000118 2004-06-18 2005-06-17 Process for manufacturing rotor-compressors of turbo-compressors and other difficult-to-extract parts, and corresponding mould WO2005123302A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BRPI0402480-0 2004-06-18
BRPI0402480 BRPI0402480A (en) 2004-06-18 2004-06-18 Turbocharger compressor rotor manufacturing process and other difficult-to-extract parts and corresponding mold

Publications (1)

Publication Number Publication Date
WO2005123302A1 true WO2005123302A1 (en) 2005-12-29

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/BR2005/000118 WO2005123302A1 (en) 2004-06-18 2005-06-17 Process for manufacturing rotor-compressors of turbo-compressors and other difficult-to-extract parts, and corresponding mould

Country Status (2)

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BR (1) BRPI0402480A (en)
WO (1) WO2005123302A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012152579A1 (en) * 2011-05-11 2012-11-15 Zf Lenksysteme Gmbh Injection moulding device for a globoid toothing and method for producing a globoid toothing
CN103418754A (en) * 2013-08-30 2013-12-04 中国南方航空工业(集团)有限公司 Manufacturing method for casting mold used for casting aircraft engine crankcase component
CN110410362A (en) * 2019-08-23 2019-11-05 固特科工业塑料件科技(深圳)有限公司 A kind of injection mold of turbine and turbine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2347773A (en) * 1941-12-06 1944-05-02 Western Electric Co Molding apparatus
GB2067441A (en) * 1981-01-09 1981-07-30 Nissan Motor Pressure die casting method and apparatus for production of rotor having radial vanes
EP0392347A2 (en) * 1989-04-12 1990-10-17 Thyssen Polymer Gmbh Injection mould
EP1136225A2 (en) * 2000-03-24 2001-09-26 Ramesh Chandra Batra Injection moulding tool and method for producing the inner mould

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2347773A (en) * 1941-12-06 1944-05-02 Western Electric Co Molding apparatus
GB2067441A (en) * 1981-01-09 1981-07-30 Nissan Motor Pressure die casting method and apparatus for production of rotor having radial vanes
EP0392347A2 (en) * 1989-04-12 1990-10-17 Thyssen Polymer Gmbh Injection mould
EP1136225A2 (en) * 2000-03-24 2001-09-26 Ramesh Chandra Batra Injection moulding tool and method for producing the inner mould

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012152579A1 (en) * 2011-05-11 2012-11-15 Zf Lenksysteme Gmbh Injection moulding device for a globoid toothing and method for producing a globoid toothing
CN103418754A (en) * 2013-08-30 2013-12-04 中国南方航空工业(集团)有限公司 Manufacturing method for casting mold used for casting aircraft engine crankcase component
CN103418754B (en) * 2013-08-30 2015-12-02 中国南方航空工业(集团)有限公司 A kind of manufacture method of the casting mold for casting aircraft engine crankcase component
CN110410362A (en) * 2019-08-23 2019-11-05 固特科工业塑料件科技(深圳)有限公司 A kind of injection mold of turbine and turbine

Also Published As

Publication number Publication date
BRPI0402480A (en) 2006-02-07

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