TW201524640A - Method for bonding metal powder injection molded bodies - Google Patents
Method for bonding metal powder injection molded bodies Download PDFInfo
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- TW201524640A TW201524640A TW103134399A TW103134399A TW201524640A TW 201524640 A TW201524640 A TW 201524640A TW 103134399 A TW103134399 A TW 103134399A TW 103134399 A TW103134399 A TW 103134399A TW 201524640 A TW201524640 A TW 201524640A
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- metal powder
- powder injection
- injection molded
- molded body
- coating agent
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- 229910052751 metal Inorganic materials 0.000 title claims abstract description 157
- 239000002184 metal Substances 0.000 title claims abstract description 157
- 239000000843 powder Substances 0.000 title claims abstract description 115
- 238000002347 injection Methods 0.000 title claims abstract description 74
- 239000007924 injection Substances 0.000 title claims abstract description 74
- 238000000034 method Methods 0.000 title claims abstract description 25
- 239000011248 coating agent Substances 0.000 claims abstract description 57
- 238000005245 sintering Methods 0.000 claims abstract description 37
- 238000005238 degreasing Methods 0.000 claims abstract description 29
- 239000011230 binding agent Substances 0.000 claims abstract description 27
- 238000001746 injection moulding Methods 0.000 claims abstract description 25
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 18
- 239000000460 chlorine Substances 0.000 claims abstract description 16
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910052801 chlorine Inorganic materials 0.000 claims abstract description 10
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 9
- 238000004898 kneading Methods 0.000 claims abstract description 7
- 238000005304 joining Methods 0.000 claims description 24
- 229920005989 resin Polymers 0.000 claims description 20
- 239000011347 resin Substances 0.000 claims description 20
- 239000007767 bonding agent Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 abstract description 8
- 239000001993 wax Substances 0.000 description 18
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000000576 coating method Methods 0.000 description 7
- -1 polyethylene Polymers 0.000 description 5
- DQXBYHZEEUGOBF-UHFFFAOYSA-N but-3-enoic acid;ethene Chemical compound C=C.OC(=O)CC=C DQXBYHZEEUGOBF-UHFFFAOYSA-N 0.000 description 4
- 239000005038 ethylene vinyl acetate Substances 0.000 description 4
- 229920006244 ethylene-ethyl acrylate Polymers 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 4
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 description 4
- 238000005476 soldering Methods 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 125000006850 spacer group Chemical group 0.000 description 3
- 239000004698 Polyethylene Substances 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- 239000004793 Polystyrene Substances 0.000 description 2
- 229920002472 Starch Polymers 0.000 description 2
- 235000021355 Stearic acid Nutrition 0.000 description 2
- 239000012298 atmosphere Substances 0.000 description 2
- 239000004203 carnauba wax Substances 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000005042 ethylene-ethyl acrylate Substances 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 238000007654 immersion Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 2
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 2
- 239000012188 paraffin wax Substances 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- 229920002223 polystyrene Polymers 0.000 description 2
- 235000019698 starch Nutrition 0.000 description 2
- 239000008107 starch Substances 0.000 description 2
- 239000008117 stearic acid Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- JOYRKODLDBILNP-UHFFFAOYSA-N urethane group Chemical group NC(=O)OCC JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 2
- VZXTWGWHSMCWGA-UHFFFAOYSA-N 1,3,5-triazine-2,4-diamine Chemical group NC1=NC=NC(N)=N1 VZXTWGWHSMCWGA-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000007865 diluting Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000012748 slip agent Substances 0.000 description 1
- 239000002195 soluble material Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
- B22F7/064—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts using an intermediate powder layer
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
- F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/22—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
- B22F3/225—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/22—Manufacture essentially without removing material by sintering
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Powder Metallurgy (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
Description
本發明是關於金屬粉末射出成型體之接合方法[method for jointing metal injection molded parts],特別是關於用來將複數個金屬粉末射出成型體予以接合而製作金屬製品的金屬粉末射出成型體之接合方法。 The present invention relates to a method for joining a metal powder injection molded article, and more particularly to a method for joining a metal powder injection molded body for joining a plurality of metal powder injection molded bodies to produce a metal product. .
金屬粉末射出成型法(MIM:Metal Injection Molding),是將金屬粉末和結合劑混煉後以具有既定形狀的方式進行射出成型而獲得成型體(坯體[green part]),藉由將該成型體在真空中或氣體氛圍中進行脫脂及燒結而製作出密度超過95%的金屬製品。作為結合劑,是使用將複數的樹脂、蠟混合而成者。藉由使複數的結合劑成分依序飛散,以維持成型體的形狀。 MIM (Metal Injection Molding) is a method in which a metal powder and a binder are kneaded and then injection-molded in a predetermined shape to obtain a molded body (green part). The body is degreased and sintered in a vacuum or in a gas atmosphere to produce a metal product having a density of more than 95%. As the binder, a mixture of a plurality of resins and waxes is used. The shape of the molded body is maintained by sequentially scattering a plurality of binder components.
結合劑較佳為使用不會殘留在金屬中的成分。例如,一般是混合使用:在250℃以下的較低溫容易揮發之硬脂酸、石蠟、棕櫚蠟等的蠟、和在500℃以下的溫度容易分解飛散之聚乙烯、聚丙烯、聚苯乙烯、EVA(乙烯醋酸乙烯酯)、EEA(乙烯-丙烯酸乙酯共聚物樹 脂)等的樹脂。 The binder is preferably a component that does not remain in the metal. For example, it is generally used in combination: a wax such as stearic acid, paraffin wax or palm wax which is easily volatilized at a temperature lower than 250 ° C, and a polyethylene, polypropylene, polystyrene which is easily decomposed and scattered at a temperature of 500 ° C or lower. EVA (ethylene vinyl acetate), EEA (ethylene-ethyl acrylate copolymer tree Resin such as grease).
然而,渦輪壓縮機的定子葉片,如下述專利文獻1所揭示,是配置在環狀的內殼體和環狀的外殼體之間。此外,定子葉片是由主成分為Ti或Ni的合金所形成,是將在周方向分割成複數個的定子葉片扇區[stator blade sectors]組合而構成。一般而言,將構成外殼體的一部分之外帶體、將構成內殼體的一部分之內帶體、及葉片分別個別地製作,再在葉片上焊接外帶體及內帶體而形成定子葉片扇區。 However, the stator blade of the turbo compressor is disposed between the annular inner casing and the annular outer casing as disclosed in Patent Document 1 below. Further, the stator blade is formed of an alloy having a main component of Ti or Ni, and is configured by dividing a plurality of stator blade sectors in a circumferential direction. In general, a belt body constituting a part of the outer casing, an inner belt body constituting a part of the inner casing, and blades are separately formed, and the outer belt body and the inner belt body are welded to the blade to form a stator blade sector. .
近年,基於功能提昇的觀點,有使葉片更薄、且將葉片面做成複雜的三維曲面的傾向,但利用鑄造或塑性加工很難確保葉片的形狀精度。因此,關於葉片的製造方法,使用上述金屬粉末射出成型法被提出。 In recent years, from the viewpoint of function improvement, there is a tendency to make the blade thinner and to make the blade surface into a complicated three-dimensional curved surface. However, it is difficult to ensure the shape accuracy of the blade by casting or plastic working. Therefore, regarding the method of manufacturing the blade, the above-described metal powder injection molding method is proposed.
在外帶體和內帶體之間具有複數個葉片之上述定子葉片扇區,要利用射出成型(金屬粉末射出成型法的一步驟)來形成可能會發生困難。因此,形成定子葉片扇區的分割體,該分割體是在外帶體和內帶體之間具有一個葉片,將複數個分割體接合而形成定子葉片扇區的技術被提出。 The stator blade sector having a plurality of blades between the outer belt body and the inner belt body may be difficult to be formed by injection molding (a step of the metal powder injection molding method). Therefore, a split body of a stator blade sector is formed which has a blade between the outer tape body and the inner tape body, and a technique of joining a plurality of divided bodies to form a stator blade sector has been proposed.
下述專利文獻2揭示金屬粉末射出成型體之接合方法,其目的是為了抑制接合強度的降低。在該接合方法使用:將與構成成型體的金屬粉末相同種類的金屬粉末和水溶性糊狀物質[gelatinized soluble material]用水稀釋而成的糊劑。首先,將上述糊劑塗布在燒結前的成型體 之接合面,將成型體彼此藉由糊劑暫時接合。然後,將暫時接合的成型體燒結,使成型體彼此藉由糊劑所含的金屬粉末進行接合。又在下述專利文獻2揭示,在脫脂後將糊劑塗布於接合面之後進行燒結的情況,以及在將糊劑塗布於接合面之後進行脫脂及燒結的情況。 Patent Document 2 listed below discloses a joining method of a metal powder injection molded body, which is intended to suppress a decrease in joint strength. In the joining method, a paste obtained by diluting a metal powder of the same kind as the metal powder constituting the molded body and a gelatinized soluble material with water is used. First, the above paste is applied to a molded body before sintering. The joint faces temporarily bond the molded bodies to each other by the paste. Then, the temporarily joined molded body is sintered, and the molded bodies are joined to each other by the metal powder contained in the paste. Further, Patent Document 2 listed below discloses a case where the paste is applied to the joint surface after degreasing, followed by sintering, and after the paste is applied to the joint surface, degreasing and sintering are performed.
[專利文獻] [Patent Literature]
[專利文獻1]日本特開2004-197622號公報 [Patent Document 1] Japanese Patent Laid-Open Publication No. 2004-197622
[專利文獻2]日本特開2010-236042號公報 [Patent Document 2] Japanese Patent Laid-Open Publication No. 2010-236042
上述專利文獻2所記載的糊劑,是使用以澱粉質作為原料之水溶性糊狀物質。澱粉是由碳(C)、氫(H)及氧(O)所構成的高分子,容易受熱而分解。此外,在金屬粉末射出成型法,是從金屬粉末和結合劑所構成的坯體讓結合劑飛散而製作出成型體,因此成型體的大小是從坯體的大小產生收縮。在此,要控制收縮所造成的接合面變形是困難的。因此,若使用容易發生熱分解的糊劑(接著劑),在脫脂步驟或燒結步驟會使糊劑提早進行分解、飛散,要維持收縮後之接合面彼此的密合狀態是困難的。因此,抑制接合強度降低的效果不佳。 The paste described in Patent Document 2 is a water-soluble paste-like material using starch as a raw material. Starch is a polymer composed of carbon (C), hydrogen (H), and oxygen (O), and is easily decomposed by heat. Further, in the metal powder injection molding method, a binder is formed by scattering a binder from a green body composed of a metal powder and a binder, and thus the size of the molded body is shrunk from the size of the green body. Here, it is difficult to control the deformation of the joint surface caused by the shrinkage. Therefore, when a paste (adhesive) which is susceptible to thermal decomposition is used, it is difficult to prematurely decompose and scatter the paste in the degreasing step or the sintering step, and it is difficult to maintain the adhesion state between the joined surfaces after shrinkage. Therefore, the effect of suppressing the decrease in the joint strength is not good.
本發明的目的是為了提供一種可提高接合強度的金屬粉末射出成型體之接合方法。 An object of the present invention is to provide a joining method of a metal powder injection molded body which can improve joint strength.
本發明的特徵,是提供一種金屬粉末射出成型體之接合方法,該金屬粉末射出成型體之接合方法,是使分別將金屬粉末和結合劑混煉後經由射出成型而得之至少二個金屬粉末射出成型體互相抵接,在前述至少二個金屬粉末射出成型體相抵接之接合部上塗布含有氮或氯之塗布劑,將在前述接合部塗布有前述塗布劑之前述至少二個金屬粉末射出成型體實施脫脂或燒結,使前述至少二個金屬粉末射出成型體在前述接合部進行接合而製作出金屬製品。 A feature of the present invention is to provide a joining method of a metal powder injection molded body, wherein the metal powder injection molded body is joined by a method in which at least two metal powders obtained by kneading the metal powder and the binder after injection molding are respectively obtained by injection molding. The injection molded bodies are in contact with each other, and a coating agent containing nitrogen or chlorine is applied to the joint portion where the at least two metal powder injection molded bodies are in contact with each other, and the at least two metal powders coated with the coating agent on the joint portion are emitted. The molded body is degreased or sintered, and the at least two metal powder injection molded bodies are joined at the joint portion to produce a metal product.
依據上述特徵,藉由使用含有氮或氯的塗布劑,能使塗布劑的分解速度變慢,在實施金屬粉末射出成型體的脫脂或燒成時,在接合部能使金屬粉末射出成型體的密合狀態更長久地維持,可提高接合部的接合強度。 According to the above feature, by using a coating agent containing nitrogen or chlorine, the decomposition rate of the coating agent can be slowed, and when the metal powder injection molded body is degreased or fired, the metal powder can be injected into the molded body at the joint portion. The close contact state is maintained for a longer period of time, and the joint strength of the joint portion can be improved.
在此較佳為,前述結合劑係含有:在既定溫度範圍會揮發的蠟、以及在比前述既定溫度範圍更高的溫度範圍會飛散的樹脂,前述塗布劑之至少一部分,在實施前述至少二個金屬粉末射出成型體的脫脂時或燒結時,比前述蠟更慢揮發且比前述樹脂更快飛散。 Preferably, the binder contains a wax which volatilizes in a predetermined temperature range and a resin which scatters in a temperature range higher than the predetermined temperature range, and at least a part of the coating agent is at least two When the metal powder injection molded body is degreased or sintered, it is more slowly volatilized than the above wax and scatters faster than the aforementioned resin.
此外較佳為,前述塗布劑塗布於前述接合部之接觸面或周側面。 Further preferably, the coating agent is applied to a contact surface or a circumferential side surface of the joint portion.
此外較佳為,在前述接合部之間隙保持為0.1mm以下的狀態下,將前述至少二個金屬粉末射出成型體實施脫脂或燒結。 Further, it is preferable that the at least two metal powder injection molded bodies are degreased or sintered while the gap of the joint portion is maintained at 0.1 mm or less.
此外較佳為,前述金屬製品是具備有複數個 葉片及用來支承前述複數個葉片的帶體部之葉片扇區,前述至少二個金屬粉末射出成型體分別為具有單一葉片的前述葉片扇區之分割體。 Further preferably, the metal product is provided with a plurality of And a blade segment of the blade body for supporting the plurality of blades, wherein the at least two metal powder injection molding bodies are each a segment of the blade sector having a single blade.
再者較佳為,在前述帶體部之豎設有前述葉片的一面之背面上,形成有朝與前述葉片的葉片弦線交叉的方向延伸之肋部。 Further preferably, a rib extending in a direction intersecting the blade chord of the blade is formed on a back surface of one surface of the belt body on which the blade is vertically disposed.
在此較佳為,將前述分割體中之前述帶體部的延伸方向和前述肋部的延伸方向所成的角度設為θ時,角度θ大於0°且為前述葉片的交錯角以下。 Here, it is preferable that when the angle formed by the extending direction of the belt body portion and the extending direction of the rib portion in the divided body is θ , the angle θ is larger than 0° and is equal to or less than the stagger angle of the blade.
或是較佳為,將前述分割體中之前述帶體部的延伸方向和前述肋部的延伸方向之間的角度設為θ時,0°<θ≦12°。 Or preferably when the angle between the extending direction of the strip portion and the divided body of the rib is defined as θ, 0 ° <θ ≦ 12 °.
1‧‧‧金屬製品 1‧‧‧Metal products
2‧‧‧金屬粉末射出成型體 2‧‧‧Metal powder injection molded body
3‧‧‧接合部 3‧‧‧ joints
3a‧‧‧接觸面 3a‧‧‧Contact surface
3b‧‧‧周側面 3b‧‧‧ week side
4‧‧‧塗布劑 4‧‧‧ Coating agent
5‧‧‧支承塊 5‧‧‧Support block
6‧‧‧金屬粉末射出成型板 6‧‧‧Metal powder injection molding board
7‧‧‧間隔件 7‧‧‧ spacers
11‧‧‧外帶體 11‧‧‧External body
11a‧‧‧殼體部 11a‧‧‧Shell Department
11b‧‧‧鉤扣部 11b‧‧‧ hooking
11c‧‧‧肋部 11c‧‧‧ ribs
11d‧‧‧段差 11d‧‧‧ paragraph difference
12‧‧‧內帶體 12‧‧‧Inner body
12a‧‧‧殼體部 12a‧‧‧Shell Department
12b‧‧‧狹縫部 12b‧‧‧Slits
13‧‧‧定子葉片 13‧‧‧ stator blades
14‧‧‧轉子葉片 14‧‧‧Rotor blades
A‧‧‧外帶體的橫寬 A‧‧‧ transverse width of the outer body
B‧‧‧外帶體的高度 B‧‧‧ Height of the outer body
C‧‧‧能夠實現充分的接合強度之間隙 C‧‧‧Able to achieve sufficient joint strength gap
g‧‧‧接合部的間隙 g‧‧‧Gap of the joint
h‧‧‧外帶體的段差高度(內帶體的端緣高度) h‧‧‧The height of the step of the outer body (the height of the edge of the inner body)
θ‧‧‧帶體部的延伸方向和肋部的延伸方向之間的角度 θ ‧‧‧An angle between the extension of the body and the direction in which the rib extends
λ‧‧‧交錯角 λ‧‧‧Interlace angle
La‧‧‧渦輪軸方向 La‧‧‧ Turbine axis direction
Lc‧‧‧葉片弦線 Lc‧‧‧blade string
Le‧‧‧外帶體的延伸方向 Le‧‧‧Extension of the outer body
Lr‧‧‧肋部的延伸方向 Lr‧‧‧ extension of the rib
OH1、OH2‧‧‧懸伸部 OH1, OH2‧‧‧ overhang
S1‧‧‧混煉步驟 S1‧‧‧ mixing step
S2‧‧‧射出成型步驟 S2‧‧‧ injection molding step
S3‧‧‧塗布步驟 S3‧‧‧ Coating step
S4‧‧‧脫脂步驟 S4‧‧‧ Degreasing step
S5‧‧‧燒結步驟 S5‧‧‧Sintering step
圖1係實施形態的金屬粉末射出成型體之接合方法的流程圖。 Fig. 1 is a flow chart showing a method of joining metal powder injection molded articles of an embodiment.
圖2係藉由上述金屬粉末射出成型體之接合方法所製作的金屬製品之立體圖,(a)為第一例,(b)為第二例,(c)為第三例。 2 is a perspective view of a metal product produced by the above-described joining method of the metal powder injection molded body, wherein (a) is a first example, (b) is a second example, and (c) is a third example.
圖3(a)係顯示射出成型後的金屬粉末射出成型體之立體圖,圖3(b)係顯示塗布有塗布劑之金屬粉末射出成型體的立體圖。 Fig. 3 (a) is a perspective view showing the metal powder injection molded body after injection molding, and Fig. 3 (b) is a perspective view showing the metal powder injection molded body coated with the coating agent.
圖4係顯示塗布劑的塗布方法之說明剖面圖,(a)為第 一例,(b)為第二例,(c)為第三例,(d)為第四例。 Figure 4 is a cross-sectional view showing the coating method of the coating agent, (a) being the first For example, (b) is the second case, (c) is the third case, and (d) is the fourth case.
圖5(a)係外帶體的前視圖,圖5(b)顯示肋部的延伸角度θ和安定度S的關係圖。 Fig. 5(a) is a front view of the outer band, and Fig. 5(b) is a view showing the relationship between the extending angle θ of the rib and the stability S.
圖6係外帶體的變形例之前視圖。 Fig. 6 is a front view showing a modification of the outer belt body.
圖7係接合部的間隙試驗方法之說明圖,(a)顯示間隙調整狀態的側視圖,(b)顯示接合完成狀態之側視圖。 Fig. 7 is an explanatory view showing a gap test method of the joint portion, (a) showing a side view of the gap adjustment state, and (b) a side view showing the joint completion state.
以下,針對金屬粉末射出成型體之接合方法的實施形態,參照圖式作說明。 Hereinafter, an embodiment of a joining method of a metal powder injection molded body will be described with reference to the drawings.
本實施形態的金屬粉末射出成型體之接合方法,是使將金屬粉末和結合劑混煉後經由射出成型而得的金屬粉末射出成型體2彼此接合,進行脫脂[degreasing](脫結合劑[debinding])或燒結[sintering](燒成[calcining])而製作出金屬製品1。在此,是在金屬粉末射出成型體2的接合部3上塗布含有氮(N)或氯(Cl)的塗布劑4之後,使金屬粉末射出成型體2彼此接合並進行脫脂或燒結。 In the joining method of the metal powder injection molded body of the present embodiment, the metal powder injection molded body 2 obtained by kneading the metal powder and the bonding agent is joined to each other to perform degreasing (debinding) [debinding] ]) or sintering [sintering] (calcining) to produce metal product 1. Here, after the coating agent 4 containing nitrogen (N) or chlorine (Cl) is applied onto the joint portion 3 of the metal powder injection molded body 2, the metal powder injection molded body 2 is joined to each other and degreased or sintered.
具體而言,如圖1所示般,是經由混煉步驟S1、射出成型步驟S2、塗布步驟S3、脫脂步驟S4、燒結步驟S5而製作出金屬製品1。混煉步驟S1,是將金屬粉末和結合劑予以混煉;射出成型步驟S2,是將混煉後的原料加熱熔融後朝模具內射出;塗布步驟S3,是將從模具取出後的金屬粉末射出成型體2彼此組合,在接合部3 將塗布劑4利用烙鐵等進行塗布;脫脂步驟S4,是將塗布有塗布劑4之金屬粉末射出成型體2利用加熱爐進行脫脂;燒結步驟S5,是將脫脂後的金屬粉末射出成型體2利用加熱爐進行燒結。 Specifically, as shown in FIG. 1, the metal product 1 is produced through the kneading step S1, the injection molding step S2, the coating step S3, the degreasing step S4, and the sintering step S5. In the kneading step S1, the metal powder and the binder are kneaded; in the injection molding step S2, the kneaded material is heated and melted and then ejected into the mold; and the coating step S3 is to eject the metal powder taken out from the mold. The molded bodies 2 are combined with each other at the joint portion 3 The coating agent 4 is applied by a soldering iron or the like; the degreasing step S4 is to degrease the metal powder injection molded body 2 coated with the coating agent 4 by a heating furnace; and the sintering step S5 is to use the degreased metal powder to be molded into the molded body 2 The furnace is sintered.
金屬製品1,例如是渦輪壓縮機的定子葉片單元的一部分。定子葉片單元,是由環狀的內殼體、環狀的外殼體、以及配置於其等之間的複數個定子葉片所構成。定子葉片單元,是將在周方向分割成複數個的定子葉片扇區組合而製作出。上述金屬製品1為定子葉片扇區。 The metal product 1 is, for example, part of a stator blade unit of a turbo compressor. The stator vane unit is composed of an annular inner casing, an annular outer casing, and a plurality of stator vanes disposed between the stator vane. The stator blade unit is produced by dividing a plurality of stator blade sector combinations in the circumferential direction. The above metal product 1 is a stator blade sector.
圖2(a)所示的金屬製品1(定子葉片扇區),是由構成外殼體的一部分之外帶體11、構成內殼體的一部分之內帶體12、以及配置在外帶體11和內帶體12之間的複數個定子葉片13所構成。又圖2(a)中的一點鏈線表示接合部3。 The metal product 1 (stator blade sector) shown in Fig. 2(a) is a belt body 11 which is a part of the outer casing, an inner belt body 12 which forms a part of the inner casing, and is disposed in the outer belt body 11 and The plurality of stator blades 13 are formed between the belt bodies 12. Further, the one-dot chain line in Fig. 2(a) indicates the joint portion 3.
外帶體11係具有:用來形成定子葉片13的外周側流路面之殼體部11a、及分別形成於殼體部11a的兩端緣之鉤扣部11b。在鉤扣部11b和殼體部11a之間形成有段差11d,段差11d卡止在渦輪外殼上所形成的軌道。在外帶體11之豎設有定子葉片13之一面的背面(與流路面為相反側的面),利用殼體部11a及鉤扣部11b而形成凹部。在凹部內,用來連結一對的鉤扣部11b之肋部11c形成在殼體部11a上。 The outer casing 11 has a casing portion 11a for forming an outer peripheral side flow surface of the stator blade 13, and a hook portion 11b formed at both end edges of the casing portion 11a. A step 11d is formed between the hook portion 11b and the casing portion 11a, and the step 11d is locked to the rail formed on the turbine casing. A rear surface (a surface opposite to the flow path surface) on one surface of the stator blade 13 is vertically provided on the outer tape body 11, and a concave portion is formed by the case portion 11a and the hook portion 11b. In the recess, a rib 11c for coupling the pair of hook portions 11b is formed on the casing portion 11a.
內帶體12係具有:用來形成定子葉片13的內周側流路面之殼體部12a、及分別形成於殼體部12a之 軸方向的兩端緣之狹縫部12b。狹縫部12b,是將殼體部12a的側緣折回而形成的。藉由在一對的狹縫部12b之間插穿板構件,使複數個定子葉片扇區的內周端互相連結,使由複數個殼體部12a所形成的內帶體12保持為環狀。上述肋部11c,是用來補強外帶體11而抑制脫脂步驟S4、燒結步驟S5中之外帶體11發生變形。關於肋部11c的效果隨後敘述。 The inner belt body 12 has a casing portion 12a for forming an inner peripheral side flow surface of the stator blade 13, and a casing portion 12a formed in the casing portion 12a, respectively. The slit portion 12b at both end edges in the axial direction. The slit portion 12b is formed by folding back the side edge of the casing portion 12a. By inserting the plate member between the pair of slit portions 12b, the inner peripheral ends of the plurality of stator blade segments are connected to each other, and the inner band body 12 formed by the plurality of casing portions 12a is held in a ring shape. The rib portion 11c is for reinforcing the outer band body 11 to suppress the degreasing step S4 and the outer band body 11 is deformed in the sintering step S5. The effect of the rib 11c will be described later.
金屬製品1並不限定於上述構造。如圖2(b)所示般,金屬製品1亦可為不具有肋部11c之定子葉片扇區。此外,如圖2(c)所示般,金屬製品1亦可為渦輪壓縮機之轉子葉片單元的一部分、即轉子葉片扇區。作為轉子葉片扇區之金屬製品1,是由構成外殼體的一部分之外帶體11、及結合於外帶體11之複數個轉子葉片14所構成。又圖2(b)及圖2(c)中的一點鏈線表示接合部3。 The metal product 1 is not limited to the above configuration. As shown in Fig. 2(b), the metal product 1 may also be a stator blade sector having no ribs 11c. Further, as shown in FIG. 2(c), the metal product 1 may also be a part of a rotor blade unit of a turbo compressor, that is, a rotor blade sector. The metal product 1 as a rotor blade sector is composed of a plurality of rotor blades 14 that are a part of the outer casing and a plurality of rotor blades 14 that are coupled to the outer casing 11. Further, the one-dot chain line in FIGS. 2(b) and 2(c) indicates the joint portion 3.
此外,金屬製品1並不限定於定子葉片扇區、轉子葉片扇區,是包含將複數個金屬粉末射出成型體2接合而製作出的所有構件。此外,上述外帶體11、內帶體12的構造僅是一例,並不限定為上述形狀。 Further, the metal product 1 is not limited to the stator blade sector and the rotor blade sector, and is a member including all of the members produced by joining a plurality of metal powder injection molded bodies 2. Further, the structures of the outer tape body 11 and the inner tape body 12 are merely examples, and are not limited to the above shapes.
上述金屬製品1,具有複雜的形狀,要維持形狀精度而藉由一次射出成型製作出可能會發生困難。此外,當金屬製品1大型化的情況,其重量增加,在脫脂或燒結中可能發生變形。於是,在本實施形態,如圖3(a)所示般,藉由將複數個金屬粉末射出成型體2(葉片扇區的分割體)接合,製作出如圖2(a)所示般的金屬製品1。各金屬 粉末射出成型體2,是在外帶體11和內帶體12之間具有單一的定子葉片13而形成為較簡單的形狀,因此可維持形狀精度而藉由一次射出成型製作出。 The metal product 1 described above has a complicated shape, and it may be difficult to produce it by one injection molding in order to maintain the shape accuracy. Further, in the case where the metal product 1 is enlarged, its weight is increased, and deformation may occur in degreasing or sintering. Then, in the present embodiment, as shown in Fig. 3(a), a plurality of metal powder injection molded bodies 2 (divided bodies of blade sectors) are joined to each other, as shown in Fig. 2(a). Metal products 1. Various metals The powder injection molded body 2 has a single stator blade 13 between the outer tape body 11 and the inner tape body 12, and is formed into a relatively simple shape. Therefore, the powder injection molded body 2 can be produced by one injection molding while maintaining shape accuracy.
將複數個金屬粉末射出成型體2接合而製作出的金屬製品1,是具備有複數個葉片(定子葉片13)及用來支承葉片的帶體部(外帶體11及內帶體12)之葉片扇區(例如,定子葉片扇區)。金屬粉末射出成型體2,是將葉片扇區按照葉片而分割的構件。因此,縱使金屬製品1具有複雜的形狀,金屬粉末射出成型體2成為容易射出成型的形狀,而能夠維持形狀精度。又在以下的說明中,關於金屬粉末射出成型體2也是,使用與金屬製品1的各部位相同的符號(外帶體11、內帶體12、定子葉片13等)。 The metal product 1 produced by joining a plurality of metal powder injection molded bodies 2 is a blade including a plurality of blades (stator blades 13) and a belt portion (the outer belt body 11 and the inner belt body 12) for supporting the blades. Sector (eg, stator blade sector). The metal powder injection molded body 2 is a member that divides the blade sector into blades. Therefore, even if the metal product 1 has a complicated shape, the metal powder injection molded body 2 has a shape that is easily injection molded, and the shape accuracy can be maintained. In the following description, the metal powder injection molded body 2 is also the same as the respective portions of the metal product 1 (the outer tape body 11, the inner tape body 12, the stator blade 13, and the like).
針對圖1的流程圖之各步驟作說明。在混煉步驟S1,將成為金屬粉末射出成型體2的原料之金屬粉末和結合劑予以混煉而使其造粒化。作為金屬粉末,例如是將不鏽鋼(SUS)、鈦、各種合金、各種陶瓷等做成粒徑10~20μm左右的粉末。 The steps of the flowchart of Fig. 1 will be described. In the kneading step S1, the metal powder which is the raw material of the metal powder injection molded body 2 and the binder are kneaded and granulated. As the metal powder, for example, stainless steel (SUS), titanium, various alloys, various ceramics, or the like is used as a powder having a particle diameter of about 10 to 20 μm.
此外,結合劑係含有:在既定溫度範圍會揮發的蠟、及在比蠟更高的溫度範圍會飛散的樹脂。蠟,例如為在250℃以下的較低溫下容易揮發之硬脂酸、石蠟、棕櫚蠟等。此外,樹脂例如為在500℃以下的溫度容易分解飛散之聚乙烯、聚丙烯、聚苯乙烯、EVA(乙烯醋酸乙烯酯)、EEA(乙烯-丙烯酸乙酯共聚物樹脂)等(其等可混合使用)。又在結合劑中,除了蠟及樹脂以外,視需要可添 加滑劑、界面活性劑等。 Further, the binder contains a wax which volatilizes in a predetermined temperature range, and a resin which scatters in a temperature range higher than the wax. The wax is, for example, stearic acid, paraffin wax, palm wax or the like which is easily volatilized at a lower temperature of 250 ° C or lower. Further, the resin is, for example, polyethylene, polypropylene, polystyrene, EVA (ethylene vinyl acetate), EEA (ethylene-ethyl acrylate copolymer resin) which is easily decomposed and scattered at a temperature of 500 ° C or lower (these may be mixed) use). In addition to the wax and resin in the bonding agent, it can be added as needed. Add a slip agent, a surfactant, and the like.
在射出成型步驟S2,是形成圖3(a)所示的金屬粉末射出成型體2。金屬粉末射出成型體2也稱為坯體。金屬粉末射出成型體2中,除了構成金屬製品1的金屬粉末以外還含有結合劑,因此金屬粉末射出成型體2的大小比金屬製品1更大。 In the injection molding step S2, the metal powder injection molded body 2 shown in Fig. 3(a) is formed. The metal powder injection molded body 2 is also referred to as a green body. The metal powder injection molded body 2 contains a binder in addition to the metal powder constituting the metal product 1, and therefore the size of the metal powder injection molded body 2 is larger than that of the metal product 1.
在塗布步驟S3,如圖3(b)所示般,將複數個金屬粉末射出成型體2以成為金屬製品1的形狀的方式進行組裝,在接合部3上塗布塗布劑4。塗布劑4例如為含有氮(N)、氯(Cl)之蠟或樹脂。此外,塗布劑4的至少一部分含有:在脫脂或燒結時比結合劑所含的蠟更慢飛散的材料、或在脫脂或燒結時比結合劑所含的樹脂更快飛散的材料。在此,「塗布劑4的至少一部分」是指,塗布劑4所含的成分之一部分比結合劑所含的蠟更快飛散、或比結合劑所含的樹脂更慢飛散。 In the coating step S3, as shown in FIG. 3(b), a plurality of metal powder injection molded bodies 2 are assembled so as to have the shape of the metal product 1, and the coating agent 4 is applied onto the joint portion 3. The coating agent 4 is, for example, a wax containing N (N) or chlorine (Cl) or a resin. Further, at least a part of the coating agent 4 contains a material which scatters more slowly than the wax contained in the binder during degreasing or sintering, or a material which scatters faster than the resin contained in the binder during degreasing or sintering. Here, "at least a part of the coating agent 4" means that one of the components contained in the coating agent 4 is scattered faster than the wax contained in the binder or more slowly than the resin contained in the binder.
具體而言,作為塗布劑4,可使用帶有氨甲酸乙酯基(-NHCOO-)、醯胺基(-CONH2)之蠟、氯化蠟等,或帶有氨甲酸乙酯基之熱熔接著劑。作為商品,可使用[Hi-Bon](註冊商標:日立化成聚合物公司[Hitachi Kasei Polymer Co.,Ltd.])、[Macromelt](註冊商標:漢高公司[Henkel AG & Co.KGaA])、[EMPARA](註冊商標:味之素精密科技公司[Ajinomoto Fine-Techno Co.,Inc.])等。 Specifically, as the coating agent 4, a wax having a urethane group (-NHCOO-), a guanamine group (-CONH 2 ), a chlorinated wax, or the like, or a heat having a urethane group can be used. A fluxing agent. As a product, [Hi-Bon] (registered trademark: Hitachi Kasei Polymer Co., Ltd.), [Macromelt] (registered trademark: Henkel AG & Co. KGaA) can be used. [EMPARA] (registered trademark: Ajinomoto Fine-Techno Co., Inc.).
假使,在後述脫脂步驟S4、燒結步驟S5之較早階段就使塗布劑4飛散,會在金屬粉末射出成型體2的 接合部3產生間隙,使燒結後的金屬製品1的強度降低。但是,本實施形態的塗布劑4由於是不容易受熱而分解的材料,亦即含有氮(N)及/或氯(Cl)之蠟或樹脂,在脫脂步驟S4、燒結步驟S5之較早階段不會飛散。又塗布劑4亦可為含有氮(N)及/或氯(Cl)之蠟、和含有氮(N)及/或氯(Cl)的樹脂之混合物。 If the coating agent 4 is scattered at an earlier stage of the degreasing step S4 and the sintering step S5, which will be described later, the metal powder is injected into the molded body 2 The joint portion 3 generates a gap to lower the strength of the sintered metal product 1. However, the coating agent 4 of the present embodiment is a material which is not easily decomposed by heat, that is, a wax or a resin containing nitrogen (N) and/or chlorine (Cl), at an earlier stage of the degreasing step S4 and the sintering step S5. Will not fly. Further, the coating agent 4 may be a mixture of a wax containing nitrogen (N) and/or chlorine (Cl) and a resin containing nitrogen (N) and/or chlorine (Cl).
藉由使用上述塗布劑4,能使塗布劑4的至少一部分在脫脂或燒結時比結合劑所含的蠟更慢飛散、或在脫脂或燒結時比結合劑所含的樹脂更快飛散。塗布劑4由於含有比應脫脂的結合劑的蠟更慢飛散的材料,在脫脂步驟S4中可抑制塗布劑4的飛散,可長時間維持塗布劑4的接著(暫時接合)功能。 By using the above-mentioned coating agent 4, at least a part of the coating agent 4 can be more slowly scattered at the time of degreasing or sintering than the wax contained in the binder, or can be scattered faster than the resin contained in the binder at the time of degreasing or sintering. Since the coating agent 4 contains a material which scatters more slowly than the wax of the binder to be degreased, the scattering of the coating agent 4 can be suppressed in the degreasing step S4, and the subsequent (temporary bonding) function of the coating agent 4 can be maintained for a long period of time.
此外,塗布劑4由於含有在脫脂或燒結時比結合劑所含的樹脂更快飛散的材料(亦即,使塗布劑4的至少一部分在結合劑的樹脂之飛散前後能夠殘留),因此在燒結步驟S5中,結合劑的樹脂不致阻塞飛散路徑,能整體均衡良好地將金屬粉末實施燒結。結果,可抑制金屬製品1的變形(又在此的「變形」,並不包含燒結所造成之金屬粉末射出成型體2往金屬製品1的收縮。)。此外,由於脫脂步驟S4後的金屬粉末射出成型體2(也稱為棕坯)之接合部3可保持密合狀態,能使燒結後的金屬製品1的強度提高。 Further, since the coating agent 4 contains a material which disperses faster than the resin contained in the binder at the time of degreasing or sintering (that is, at least a part of the coating agent 4 can remain before and after scattering of the resin of the binder), it is sintered. In the step S5, the resin of the bonding agent does not block the scattering path, and the metal powder can be sintered in a well-balanced manner as a whole. As a result, the deformation of the metal product 1 (the "deformation" here) can be suppressed, and the shrinkage of the metal powder injection molded body 2 to the metal product 1 caused by the sintering is not included. Further, since the joint portion 3 of the metal powder injection molded body 2 (also referred to as a brown compact) after the degreasing step S4 can be kept in an adhered state, the strength of the sintered metal product 1 can be improved.
上述塗布劑4,在加熱熔融的狀態下,藉由烙鐵[soldering iron]、刷毛[brush]、輥子[roller]、噴吹 [spraying]、浸漬[immersion coating]等來塗布於接合部3。例如,在使用烙鐵的情況,是採用在烙鐵的使用溫度330℃以下具有軟化點之塗布劑4。塗布劑4是塗布在接合部3的接觸面[contact surfaces]3a或周側面[circumferential side surface]3b。 The coating agent 4 is heated and melted by a soldering iron, a brush, a roller, and a spray. [spraying], immersion [immersion coating] or the like is applied to the joint portion 3. For example, in the case of using a soldering iron, a coating agent 4 having a softening point at a use temperature of 330 ° C or lower of the soldering iron is used. The coating agent 4 is applied to the contact surface 3a or the circumferential side surface 3b of the joint portion 3.
在圖4(a)所示的第一例,是在接觸面3a上塗布塗布劑4。在接觸面3a上塗布塗布劑4的情況,能使接合部3的接著力(接合力)提高。但接合部3的間隙g宜保持在0.1mm以下。若間隙g變寬,會成為金屬製品1之接合部3的強度降低、金屬製品1發生變形的主要原因。 In the first example shown in Fig. 4 (a), the coating agent 4 is applied onto the contact surface 3a. When the coating agent 4 is applied to the contact surface 3a, the adhesion (joining force) of the joint portion 3 can be improved. However, the gap g of the joint portion 3 is preferably kept at 0.1 mm or less. When the gap g is widened, the strength of the joint portion 3 of the metal product 1 is lowered, and the metal product 1 is deformed.
在圖4(b)所示的第二例,是在接觸面3a及周側面3b上塗布塗布劑4。接觸面3a是金屬粉末射出成型體2之接合部3中的對置面,周側面3b則是金屬粉末射出成型體2之接合部3中的側面。除了接觸面3a以外,在周側面3b也塗布有塗布劑4,能減少對於接觸面3a的塗布量,容易將間隙g調整為0.1mm以下。此外,因為能使接著(接合)面積增大,可提高接合部3的接著力(接合)。 In the second example shown in Fig. 4(b), the coating agent 4 is applied onto the contact surface 3a and the circumferential side surface 3b. The contact surface 3a is an opposing surface of the joint portion 3 of the metal powder injection molded body 2, and the circumferential side surface 3b is a side surface of the joint portion 3 of the metal powder injection molded body 2. In addition to the contact surface 3a, the coating agent 4 is also applied to the circumferential side surface 3b, and the amount of application to the contact surface 3a can be reduced, and the gap g can be easily adjusted to 0.1 mm or less. Further, since the subsequent (joining) area can be increased, the adhesion (joining) of the joint portion 3 can be improved.
在圖4(c)所示的第三例,是在周側面3b上塗布塗布劑4。在此,塗布劑4塗布於接合部3之周側面3b的全周。僅在周側面3b上塗布塗布劑4,容易將間隙g調整為0.1mm以下。此外,塗布於周側面3b之塗布劑4,在脫脂步驟S4或燒結步驟S5中被加熱而熔融,自然 會滲透到接觸面3a。因此,能將間隙g維持在期望值以下,且藉由接觸面3a也能提高接合部3的接著力(接合力)。 In the third example shown in Fig. 4(c), the coating agent 4 is applied to the peripheral side surface 3b. Here, the coating agent 4 is applied to the entire circumference of the circumferential side surface 3b of the joint portion 3. The coating agent 4 is applied only to the circumferential side surface 3b, and the gap g is easily adjusted to 0.1 mm or less. Further, the coating agent 4 applied to the circumferential side surface 3b is heated and melted in the degreasing step S4 or the sintering step S5, naturally Will penetrate into the contact surface 3a. Therefore, the gap g can be maintained below the desired value, and the adhesion force (joining force) of the joint portion 3 can also be increased by the contact surface 3a.
在圖4(d)所示的第四例,是在周側面3b的一部分塗布塗布劑4。當接合部3具有複雜形狀的情況,可僅在容易塗布的場所塗布塗布劑4。此外,如圖4(d)所示般當接觸面3a是朝鉛直方向延伸的情況,塗布於上方的周側面3b之塗布劑4,可利用重力而滲透到接觸面3a。 In the fourth example shown in Fig. 4(d), the coating agent 4 is applied to a part of the circumferential side surface 3b. When the joint portion 3 has a complicated shape, the coating agent 4 can be applied only at a place where coating is easy. Further, as shown in FIG. 4(d), when the contact surface 3a extends in the vertical direction, the coating agent 4 applied to the upper circumferential side surface 3b can penetrate the contact surface 3a by gravity.
如圖3(b)所示般,塗布有塗布劑4之金屬粉末射出成型體2,被載置在支承塊5上而送往脫脂步驟S4。在此,藉由使外帶體11的段差11d的高度h和內帶體12的端緣的高度h一致,能在將段差11d抵接於支承塊5之角部的狀態下,將定子葉片13呈水平地載置。 As shown in Fig. 3 (b), the metal powder injection molded body 2 coated with the coating agent 4 is placed on the support block 5 and sent to the degreasing step S4. Here, by matching the height h of the step 11d of the outer band 11 and the height h of the end edge of the inner band body 12, the stator blade 13 can be placed in a state where the step 11d is brought into contact with the corner portion of the support block 5. Placed horizontally.
此外,當上述高度h不一致的情況,若在將外帶體11的段差11d抵接於支承塊5之角部的狀態下將定子葉片13呈水平地載置,在內帶體12的端緣和支承塊5之間可能會發生間隙。在這種情況,可在內帶體12的端緣和支承塊5之間插入用來填補間隙之輔助支承塊(未圖示)。或是,若在讓內帶體12的端緣與支承塊5接觸的狀態下將定子葉片13呈水平地載置,在外帶體11的段差11d和支承塊5的角部之間可能會發生間隙。在這種情況,可在段差11d和支承塊5(的角部)之間插入用來填補間隙之輔助支承塊(未圖示)。 Further, when the height h does not match, the stator blade 13 is placed horizontally in a state where the step 11d of the outer tape 11 abuts against the corner portion of the support block 5, and the end edge of the inner tape body 12 is A gap may occur between the support blocks 5. In this case, an auxiliary support block (not shown) for filling the gap can be inserted between the end edge of the inner band body 12 and the support block 5. Alternatively, if the stator blade 13 is horizontally placed in a state where the end edge of the inner tape body 12 is brought into contact with the support block 5, a difference may occur between the step 11d of the outer tape body 11 and the corner portion of the support block 5. gap. In this case, an auxiliary support block (not shown) for filling the gap can be inserted between the step 11d and the corner portion of the support block 5.
在脫脂步驟S4及燒結步驟S5中,因為結合 劑被除去,燒結後的金屬製品1的大小,比起金屬粉末射出成型體2的大小其整體上形成收縮。因此,藉由將定子葉片13呈水平地載置,能使定子葉片13呈大致水平地收縮。結果,能夠使接著後的金屬粉末射出成型體2整體均衡良好地收縮,可抑制收縮時的應變所造成的變形。 In the degreasing step S4 and the sintering step S5, because of the combination The agent is removed, and the size of the sintered metal product 1 is contracted as a whole as compared with the size of the metal powder injection molded body 2. Therefore, by placing the stator blades 13 horizontally, the stator blades 13 can be contracted substantially horizontally. As a result, the entire metal powder injection molded body 2 can be contracted in a well-balanced manner, and deformation due to strain at the time of shrinkage can be suppressed.
在脫脂步驟S4,將結合劑所含的蠟予以除去。脫脂步驟S4的加熱溫度,一般而言是比燒結步驟S5的加熱溫度低。因此,可利用與燒結步驟S5所使用的燒結爐不同的脫脂裝置將金屬粉末射出成型體2實施加熱。當然,在燒結步驟S5,藉由控制所使用之燒結爐的溫度來將金屬粉末射出成型體2實施脫脂亦可。 In the degreasing step S4, the wax contained in the binder is removed. The heating temperature of the degreasing step S4 is generally lower than the heating temperature of the sintering step S5. Therefore, the metal powder can be injected into the molded body 2 by heating, which is different from the sintering furnace used in the sintering step S5. Of course, in the sintering step S5, the metal powder may be injected into the molded body 2 by controlling the temperature of the sintering furnace to be used for degreasing.
在燒結步驟S5,結合劑所含的樹脂被除去,而使金屬粉末燒結。例如,使用Ni基合金IN718[IN:[Inconel](註冊商標:特殊金屬公司[Special Metals Corporation])]作為金屬粉末的情況,較佳為在超過1200℃之非氧化氛圍下進行燒結。關於燒結後的金屬製品1,作為其後處理,為了確認燒結的進展程度可測定其密度,或為了實施尺寸的微調可進行衝壓加工,或為了實施端面處理可進行放電加工,或為了調整表面粗糙度可實施研削或研磨處理。 In the sintering step S5, the resin contained in the binder is removed to sinter the metal powder. For example, in the case of using a Ni-based alloy IN718 [IN: [Inconel] (registered trademark: Special Metals Corporation)] as the metal powder, it is preferred to carry out sintering in a non-oxidizing atmosphere exceeding 1200 °C. Regarding the metal product 1 after sintering, as the post-treatment, the density can be measured in order to confirm the progress of the sintering, or the press processing can be performed for fine-tuning the size, or the electric discharge machining can be performed for the end surface treatment, or the surface roughness can be adjusted. The grinding or grinding treatment can be carried out.
針對上述肋部11c(參照圖2(a)、圖3(a)及圖3(b))作說明。如圖5(a)所示般,在外帶體11(帶體部)的背面延伸設置有肋部11c。肋部11c的延伸方向Lr是與定子葉片13的葉片弦線[chord line]Lc呈交叉。相對於外帶體 11的延伸方向Le(圖5(a)的情況為鉛直方向)將肋部11c的角度設為θ(>0:角度大小)、將金屬粉末射出成型體2之外帶體11的橫寬設為A、將其高度設為B時,金屬粉末射出成型體2(金屬製品1)的尺寸安定度S(dB:decibel)可由S=10.log10(B/A)來求出。 The rib 11c (see FIGS. 2(a), 3(a), and 3(b)) will be described. As shown in Fig. 5 (a), a rib portion 11c is provided on the back surface of the outer tape body 11 (belt portion). The extending direction Lr of the rib 11c is intersected with the chord line Lc of the stator blade 13. The angle of the rib 11c is θ (>0: angular size) with respect to the extending direction Le of the outer tape 11 (in the case of the vertical direction of FIG. 5(a)), and the metal powder is emitted from the outer body 11 of the molded body 2. When the width is set to A and the height is set to B, the dimensional stability S (dB: decibel) of the metal powder injection molded body 2 (metal product 1) can be S = 10. Log 10 (B/A) to find out.
分別成型出肋部11c的上述角度θ為0°,6°及12°之金屬粉末射出成型體2,對燒結後之外帶體11的形狀進行三維測定,與均一收縮後之理想的金屬粉末射出成型體2(金屬製品1)的形狀作比較。比較結果如圖5(b)所示。安定度S高時,與均一收縮後的金屬粉末射出成型體2之尺寸差小。相反地,安定度S低時,與均一收縮後的金屬粉末射出成型體2之尺寸差大。 The metal powder injection molded body 2 in which the angle θ of the rib 11c is 0°, 6°, and 12° is formed, and the shape of the outer belt 11 after sintering is three-dimensionally measured, and the desired metal powder is uniformly shrunk. The shape of the molded body 2 (metal product 1) was compared. The comparison results are shown in Figure 5(b). When the stability S is high, the difference in size from the metal powder injection molded body 2 after uniform shrinkage is small. On the other hand, when the stability S is low, the difference in size from the metal powder injection molded body 2 after the uniform shrinkage is large.
如圖5(b)所示般,比起θ=0°的情況,θ=6°或12°之安定度S較高。因此,較佳為將肋部11c之上述角度θ增大(亦即,將相對於葉片弦線Lc之交叉角增大)。但縱使是θ=0°的情況,按照金屬粉末射出成型體2之大小、形狀、重量等的條件,也可能成為可維持金屬製品1的形狀精度之高安定度S的情況。因此,並不排除上述角度θ=0°的情況。 As shown in Fig. 5(b), the stability S of θ = 6° or 12° is higher than in the case of θ =0°. Therefore, it is preferable to increase the above-described angle θ of the rib 11c (that is, to increase the crossing angle with respect to the blade string Lc). However, even when θ =0°, the condition of the size, shape, weight, and the like of the metal powder injection molded body 2 may be a high degree of stability S in which the shape accuracy of the metal product 1 can be maintained. Therefore, the case where the above angle θ = 0° is not excluded.
此外,若肋部11c的角度θ過大,肋部11c本身的重量可能會促進燒結時的變形。因此,較佳為對於上述角度θ設定上限。考慮到這點,上述角度θ的上限較佳為定子葉片13之交錯角[stagger angle]λ(>0:角度大小)。「交錯角λ」,如圖5(a)所示般,是相對於渦輪軸方 向La(圖5(a)的情況,是與上述延伸方向Le平行)之葉片弦線Lc的角度。具體而言,上述角度θ的上限,根據上述試驗結果,較佳為6°~12°的範圍內的數值。但上述角度θ的上限並不限定為該數值(範圍),可因應肋部11c本身的重量,而對每個金屬粉末射出成型體2進行設定。 Further, if the angle θ of the rib 11c is excessively large, the weight of the rib 11c itself may promote deformation at the time of sintering. Therefore, it is preferable to set an upper limit for the above angle θ. In view of this, the upper limit of the above-described angle θ is preferably the stagger angle λ (>0: angular size) of the stator blade 13. As shown in Fig. 5(a), the "staggered angle λ" is an angle of the blade string Lc with respect to the turbine axis direction La (in the case of Fig. 5(a), which is parallel to the extending direction Le). Specifically, the upper limit of the angle θ is preferably a value within a range of 6° to 12° based on the above test results. However, the upper limit of the angle θ is not limited to the numerical value (range), and each of the metal powder injection molded bodies 2 can be set in accordance with the weight of the rib 11c itself.
亦即,外帶體11之延伸方向Le和肋部11c的延伸方向Lr之間的角度θ,較佳為比0°大且為交錯角λ以下。特別是若僅考慮收縮所造成的變形,上述角度θ更佳為設定成與交錯角λ的大小相同。在此,因為定子葉片13之交錯角λ在某種程度上是一定的,具體而言較佳為0°<θ≦12°。又,從外帶體11的延伸方向Le往肋部11c的延伸方向Lr之上述角度θ的方向,是與從渦輪軸方向La往葉片弦線Lc之交錯角λ的方向相反。 That is, the angle θ between the extending direction Le of the outer tape body 11 and the extending direction Lr of the rib portion 11c is preferably larger than 0° and equal to or less than the stagger angle λ . In particular, if only the deformation caused by the contraction is considered, the angle θ is preferably set to be the same as the size of the stagger angle λ . Here, since the stagger angle λ of the stator blade 13 is constant to some extent, it is preferably 0° < θ ≦ 12°. Further, the direction of the angle θ from the extending direction Le of the outer belt body 11 to the extending direction Lr of the rib portion 11c is opposite to the direction of the stagger angle λ from the turbine axis direction La toward the blade string line Lc.
圖6所示的變形例,金屬粉末射出成型體2的端面相對於渦輪軸方向La呈傾斜。如圖6所示般,按照與定子葉片13之交錯角λ的關係,肋部11c可能會形成如此般的傾斜。在本變形例,外帶體11的延伸方向Le和渦輪軸方向La並非平行。圖6所示的的情況,外帶體11之懸伸部OH1及OH2相對於肋部11c的差可縮小,能有效抑制金屬粉末射出成型體2(金屬製品1)收縮時的應變所造成的變形。 In the modification shown in FIG. 6, the end surface of the metal powder injection molded body 2 is inclined with respect to the turbine axis direction La. As shown in Fig. 6, the rib 11c may be formed to have such a tilt in accordance with the stagger angle λ of the stator blade 13. In the present modification, the extending direction Le of the outer band 11 and the turbine axis direction La are not parallel. In the case shown in Fig. 6, the difference between the overhanging portions OH1 and OH2 of the outer tape body 11 with respect to the rib portion 11c can be reduced, and the deformation caused by the strain at the time of shrinkage of the metal powder injection molded body 2 (metal product 1) can be effectively suppressed. .
接下來,針對上述接合部3的間隙g(參照圖4(a))作說明。如圖7(a)所示般,準備二片的金屬粉末射出成型板6,在其中一方的金屬粉末射出成型板6上,使用 間隔件7使另一方的金屬粉末射出成型板6呈傾斜,而在二片金屬粉末射出成型板6之間形成間隙。藉由改變間隔件7的水平位置,可調整間隙大小。在該間隙塗布塗布劑4後,將金屬粉末射出成型板6實施脫脂及燒結,測定出能讓二片金屬粉末射出成型板6以充分的強度接合時的間隙C。能夠實現充分的接合強度之間隙C為0.1mm。因此,接合部3的間隙g較佳為0.1mm以下。 Next, the gap g (see FIG. 4(a)) of the joint portion 3 will be described. As shown in Fig. 7 (a), two metal powder injection molding sheets 6 are prepared, and one of the metal powder injection molding sheets 6 is used. The spacer 7 causes the other metal powder injection molding plate 6 to be inclined, and a gap is formed between the two metal powder injection molding plates 6. The gap size can be adjusted by changing the horizontal position of the spacer 7. After the application of the coating agent 4 to the gap, the metal powder is injected into the molding plate 6 to perform degreasing and sintering, and the gap C when the two metal powders are injected into the molding plate 6 at a sufficient strength is measured. The gap C capable of achieving sufficient joint strength was 0.1 mm. Therefore, the gap g of the joint portion 3 is preferably 0.1 mm or less.
又,按照成為金屬粉末射出成型板6的原料之金屬粉末及結合劑等,上述間隙C是可改變的。亦即,接合部3的間隙g不一定限定為0.1mm以下,經驗上較佳為0.1mm~0.5mm以下。 Further, the gap C can be changed in accordance with the metal powder, the binder, and the like which are the raw materials of the metal powder injection molding plate 6. That is, the gap g of the joint portion 3 is not necessarily limited to 0.1 mm or less, and empirically preferably 0.1 mm to 0.5 mm or less.
依據本實施形態的接合方法,由於塗布劑4含有氮(N)或氯(Cl),能使塗布劑4的分解速度變慢。因此,在脫脂或燒結時能使金屬粉末射出成型體2彼此的密合狀態更長久地維持,可提高接合部3的接合強度。 According to the bonding method of the present embodiment, since the coating agent 4 contains nitrogen (N) or chlorine (Cl), the decomposition rate of the coating agent 4 can be made slow. Therefore, at the time of degreasing or sintering, the adhesion state of the metal powder injection molded body 2 can be maintained for a longer period of time, and the joint strength of the joint portion 3 can be improved.
本發明並不限定於上述實施形態,在不脫離本發明的趣旨之範圍可作各種變更。例如,在內帶體12形成肋部亦可。又,肋部11c是為了在脫脂或燒結時提高金屬製品1(金屬粉末射出成型體2)的形狀精度而設置的,在完成定子葉片單元之前可能會被施以切削(縱使肋部11c被切削,根據切削痕也能判別肋部11c的角度θ)。此外,肋部11c在一個金屬粉末射出成型體2上設有複數個亦可。 The present invention is not limited to the above-described embodiments, and various modifications can be made without departing from the spirit and scope of the invention. For example, the inner band body 12 may be formed with a rib. Further, the rib 11c is provided to improve the shape accuracy of the metal product 1 (metal powder injection molded body 2) at the time of degreasing or sintering, and may be subjected to cutting before the stator blade unit is completed (even if the rib 11c is cut) The angle θ of the rib 11c can also be determined based on the cutting marks. Further, the ribs 11c may be provided in plural in one metal powder injection molded body 2.
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DE102015210770A1 (en) * | 2015-06-12 | 2016-12-15 | Rolls-Royce Deutschland Ltd & Co Kg | Component construction, component for a gas turbine and method for producing a component of a gas turbine by metal powder injection molding |
FR3039839B1 (en) * | 2015-08-06 | 2019-12-20 | Safran Aircraft Engines | PROCESS FOR MANUFACTURING A PART OF COMPOSITE MATERIAL |
CN105562696A (en) * | 2016-01-11 | 2016-05-11 | 江西理工大学 | Metal 3D printing method |
CN106735170B (en) * | 2016-12-20 | 2019-01-25 | 佛山铂利镁特金属科技有限公司 | A kind of injection moulding method of big part metalwork |
JP2020517830A (en) * | 2017-04-27 | 2020-06-18 | フェデラル−モーグル バルブトレイン ゲーエムベーハーFederal−Mogul Valvetrain Gmbh | Poppet valve and manufacturing method thereof |
WO2018220213A1 (en) * | 2017-06-01 | 2018-12-06 | Safran | Method for improved manufacturing of a dual microstructure part |
FR3066936B1 (en) * | 2017-06-01 | 2019-11-01 | Safran | IMPROVED CO-CLEANING WELDING PROCESS |
KR102013256B1 (en) | 2017-11-23 | 2019-10-21 | 두산중공업 주식회사 | Steam turbine |
CN108326308A (en) * | 2017-12-25 | 2018-07-27 | 杭州铭赫科技有限公司 | A kind of hollow and thin-walled structural metal powder fission injection moulding splicing sintering method |
CN108687348A (en) * | 2018-05-25 | 2018-10-23 | 合肥汇智新材料科技有限公司 | A kind of Novel valve core production technology |
FR3096912B1 (en) * | 2019-06-07 | 2021-10-29 | Safran Aircraft Engines | A method of manufacturing a turbomachine part by MIM molding |
KR102289703B1 (en) | 2019-12-31 | 2021-08-17 | 한국과학기술원 | Chip-scale atomic clock |
JP7435161B2 (en) * | 2020-03-30 | 2024-02-21 | セイコーエプソン株式会社 | Manufacturing method of metal composite sintered body |
DE102020133998A1 (en) * | 2020-12-17 | 2022-06-23 | Rolls-Royce Deutschland Ltd & Co Kg | Blade component, method of manufacture thereof and gas turbine |
CN114289996B (en) * | 2021-12-15 | 2023-04-11 | 北京航星机器制造有限公司 | Large-size platform manufacturing and creep control method |
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Publication number | Priority date | Publication date | Assignee | Title |
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JPH0711305A (en) * | 1993-06-28 | 1995-01-13 | Seiko Instr Inc | Method for joining injection molded articles of metallic powder and ceramic powder |
JP3647066B2 (en) * | 1994-07-06 | 2005-05-11 | オリンパス株式会社 | Manufacturing method of sintered body |
JP2004197622A (en) | 2002-12-17 | 2004-07-15 | Ishikawajima Harima Heavy Ind Co Ltd | Turbine compressor stationary blade |
DE10331599A1 (en) * | 2003-07-11 | 2005-02-03 | Mtu Aero Engines Gmbh | Component for a gas turbine and method for producing the same |
JP2006249943A (en) * | 2005-03-08 | 2006-09-21 | Honda Motor Co Ltd | Centrifugal impeller |
CN1873245A (en) * | 2005-05-31 | 2006-12-06 | 李茂碷 | Circulator and manufactureing method |
JP2007117306A (en) * | 2005-10-26 | 2007-05-17 | Sri Sports Ltd | Golf club shaft |
FR2918702B1 (en) * | 2007-07-13 | 2009-10-16 | Snecma Sa | CLINKING FOR TURBOMACHINE BLADE |
JP5091615B2 (en) * | 2007-10-15 | 2012-12-05 | 三菱重工業株式会社 | Stator blade ring segment assembly method, stator blade ring segment, connecting member, welding method |
TWI383561B (en) * | 2008-11-24 | 2013-01-21 | Arx Group | Injection molding of the bobbin and its manufacturing method |
JP5277426B2 (en) | 2009-03-31 | 2013-08-28 | 日本ピストンリング株式会社 | Method for joining metal powder injection molded body and method for producing metal composite sintered body |
CA2797746C (en) * | 2009-04-29 | 2021-12-07 | Maetta Sciences Inc. | A method for co-processing components in a metal injection molding process, and components made via the same |
JP5751415B2 (en) * | 2011-07-13 | 2015-07-22 | 株式会社Ihi | Manufacturing method of blade for gas turbine engine |
DE102011082484A1 (en) * | 2011-09-12 | 2013-03-14 | Robert Bosch Gmbh | Manufacturing a powder injection molded-composite component, comprises e.g. providing powder injection molded-green sheets to be connected into a composite component, applying an adhesive system on a joining point |
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