WO2009144975A1 - ロウ付け補修材料およびその材料を使用したロウ付け補修方法 - Google Patents

ロウ付け補修材料およびその材料を使用したロウ付け補修方法 Download PDF

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Publication number
WO2009144975A1
WO2009144975A1 PCT/JP2009/052649 JP2009052649W WO2009144975A1 WO 2009144975 A1 WO2009144975 A1 WO 2009144975A1 JP 2009052649 W JP2009052649 W JP 2009052649W WO 2009144975 A1 WO2009144975 A1 WO 2009144975A1
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Prior art keywords
brazing repair
alloy powder
brazing
molten alloy
repair material
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Ceased
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PCT/JP2009/052649
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English (en)
French (fr)
Japanese (ja)
Inventor
吉岡　洋明
布施　俊明
斎藤　大蔵
歴 高久
北山　和弘
石橋　和利
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Toshiba Corp
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Toshiba Corp
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Priority to EP09754483.7A priority Critical patent/EP2279826B1/en
Priority to US12/994,396 priority patent/US20110088260A1/en
Publication of WO2009144975A1 publication Critical patent/WO2009144975A1/ja
Anticipated expiration legal-status Critical
Priority to US14/102,610 priority patent/US20140096872A1/en
Ceased legal-status Critical Current

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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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • B23K1/0008—Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • B23K1/0018—Brazing of turbine parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
    • B23K35/0244—Powders, particles or spheres; Preforms made therefrom
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3033—Ni as the principal constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3046—Co as the principal constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/07—Alloys based on nickel or cobalt based on cobalt
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • 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
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10—Processes characterised by the sequence of their steps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • 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
    • 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
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making

Definitions

  • the present invention relates to a brazing repair material and a brazing repair method using the material, and in particular, damage due to thermal fatigue, creep damage, fatigue damage, thermal deterioration due to exposure to high temperatures, Brazing repair material that can effectively repair and regenerate high temperature parts such as gas turbine vanes that have been damaged due to oxidation, corrosion, erosion, or collision with flying foreign objects, and brazing using that material It relates to repair methods.
  • combustion is performed by mixing air by guiding air compressed by driving a compressor provided coaxially with the gas turbine to a combustor, and the generated high-temperature combustion gas is converted into a transition piece and The stationary blade is guided to the moving blade of the gas turbine, and the moving blade is rotationally driven to work on the gas turbine, and the generator is configured to generate electric power.
  • repair welding and diffusion brazing repairs are applied and used continuously. In these repairs, heat treatment for welding and heat treatment for removing residual stress are applied as necessary.
  • Conventional diffusion brazing repair techniques include US Pat. No. 5,320,690 “Co-base superalloy repair method using Co-based brazing material composition” or Japanese Patent Application Laid-Open No. 4-254544 “Improved high temperature brazing alloy and Its use method "has been proposed.
  • Japanese Patent Application Laid-Open No. 57-62884 “Welding Processing Method” is known as a defect elimination method at the time of repair.
  • the method described in this patent document aims to eliminate welding defects that occur during the welding process of the butt portion between the wheel and the moving blade implanted therein by HIP processing.
  • the repair method by diffusion brazing includes a brazing material (molten alloy powder) obtained by adding a melting point lowering material such as Si and B to a material similar to the base material composition, and a composition material having a base equivalent strength (non- Molten alloy powder) is mixed at a predetermined blending ratio, and the cracked portion is filled or the thinned portion is built up at a heat treatment temperature not higher than the melting point of the base material.
  • a brazing material molten alloy powder obtained by adding a melting point lowering material such as Si and B to a material similar to the base material composition
  • a composition material having a base equivalent strength non- Molten alloy powder
  • Al is often added to the repair material, particularly the non-molten alloy powder.
  • the present invention has been made in view of the circumstances as described above, and for non-opening cracks generated on the surface of a component for a high-temperature component such as a gas turbine stationary blade that has been deteriorated or damaged due to actual operation.
  • Brazing that repairs damage by performing diffusion brazing repair in vacuum without completely removing the suspension, and can restore the properties of the original base material by applying pressure treatment in a high-temperature inert atmosphere.
  • An object is to provide a repair material and a brazing repair method using the repair material.
  • the present inventors have obtained the following knowledge and completed the present invention. That is, it is deformation due to welding repair that dominates the life of high-temperature parts such as gas turbine stationary blades.
  • vacuum brazing treatment and pressure densification treatment such as HIP Developed repair technology using
  • an oxide layer of alumina (Al 2 O 3 ) is formed at the interface with the repair material by heat treatment during brazing with a gas in the base material whose content increases by operation, particularly oxygen, and the repair material
  • a gas in the base material whose content increases by operation, particularly oxygen, and the repair material In order to prevent a decrease in bonding strength, and as a repair material that can be hydrogen-cleaned so that repeated repairs are possible, an Al-free (Al-free) material is used.
  • the weight ratio of the non-molten alloy powder is set to 0.
  • the particle size of the non-molten alloy powder is set to twice or more that of the molten alloy powder, the filling degree of the brazed repair material to the repaired portion can be increased.
  • a cold spray method in which the repair material is sprayed onto the repaired portion at a high speed with a carrier gas having a temperature of 800 ° C. or less is used to cover the repair material including the inside of the crack. It can be fixed by spraying and filling the repaired part, eliminating the problem that the accuracy of the repaired part greatly varies due to the difference in the inclination state (installation angle) during the heat treatment of the construction surface of the repaired part. be able to.
  • the brazing repair material according to the present invention is obtained by filling the brazed repair material into the repaired portion of the base material in which defects such as cracks and corrosion have occurred, and performing diffusion heat treatment, thereby applying the brazing repair material to the above-described brazed repair material.
  • the brazing repair material used when the repaired portion is repaired by integrally joining the repaired portion, includes a non-molten alloy powder having a composition similar to the base material, and the diffusion heat treatment.
  • It consists of a mixture with molten alloy powder that melts at a temperature, which is 0.001 to 0.05% C, 2 to 5% Si, 10 to 25% Cr, 15% by mass, It is characterized by being a brazing repair alloy that is composed of ⁇ 25% Co, 1 ⁇ 5% B, and the balance Ni and does not contain Al.
  • the molten alloy powder is 0.01 to 0.05% C, 2.5 to 4.5% Si, 12 to 20% Cr, and 17% by mass. It is preferably composed of ⁇ 23% Co, 2 ⁇ 4% B, and the balance Ni, and the composition ratio [Si + 1.5 ⁇ (C + B)] of the above components is preferably 6 or more and 9 or less.
  • the non-molten alloy powder comprises 10 to 25% Ni, 15 to 45% Cr, 6 to 8% Ta, and 0.1% or less W by mass%. And 0.05% or less of C and the balance Co.
  • the non-molten alloy powder contains 0.001 to 0.01% C and 18 to 25% Cr in mass%.
  • the molten alloy powder may be a powder containing 2 to 5% Si and 1 to 5% B by mass in the non-molten alloy powder.
  • the brazing repair method according to the present invention is a method for inspecting, disassembling, surface cleaning, solution heat treatment, surface portion and through cracks in a gas turbine component that has generated defects such as cracks and corrosion after the gas turbine is operated.
  • the brazing repair material by repeatedly performing a diffusion heat treatment under pressure at a temperature not higher than the melting point of the base material of the gas turbine component and not lower than the melting point of the molten alloy powder. Brazing repair process to join the repair part integrally, inspection process of this brazing repair part, additional repair of partial defective part, finishing process including repair process of cooling hole,
  • the repair portion includes a step of performing solution treatment and aging heat treatment, and a step of reassembling the repaired gas turbine component.
  • the weight ratio of the non-molten alloy powder of the brazing repair material is 0.8 times or more that of the molten alloy powder, and the particle size of the non-molten alloy powder is 2 times that of the molten alloy powder.
  • the weight ratio of the non-molten alloy powder of the brazing repair material is 1 to 1.5 times that of the molten alloy powder.
  • the brazing repair is performed by a hot isostatic pressing (HIP) method, and the heating temperature is 1000 ° C. or more and 1300 ° C. or less, while the applied pressure is 1000 atmospheres or more and 2000 atmospheres or less, It is preferable to perform solution treatment and aging treatment after the brazing repair.
  • HIP hot isostatic pressing
  • the heating temperature in the hot isostatic pressing (HIP) method is preferably 1100 ° C. or higher and 1260 ° C. or lower.
  • a crack is formed in the repaired portion, and the composition of the brazing repair material filled in the crack increases as the molten alloy powder moves from the surface side of the crack toward the tip side. It is preferable to approach the composition of
  • a brazing repair material is used by using a high-speed carrier gas flow of 800 ° C. or lower, which is a temperature at which the alloy powder is not melted and oxidized. It is preferable to set the particle speed of the brazing repair material to be 300 m / second or more so that the brazing repair material adheres to the repaired part or fills in the crack.
  • a repair material comprising a non-molten alloy powder having a composition similar to that of the component base material and a molten alloy powder having a predetermined composition is used. Therefore, it is easy to repair and regenerate high-temperature parts with defects such as cracks and corrosion, and it is possible to greatly improve the operational economy and maintenance management of gas turbines that use high-temperature parts as components. .
  • the material constituting the part to be repaired to which the present invention is applied is mainly a Co-based alloy material that is a high-strength heat-resistant material.
  • a typical material is FSX414 material, which has the composition shown in Table 1 below.
  • the non-molten alloy constituting the brazing repair material defined in the present invention has a composition similar to that of the base material of the part.
  • the molten alloy constituting the brazing repair material defined in the present invention is structurally stable and has various properties even after alloying with a non-molten alloy having a similar composition to the component base material. It is necessary.
  • this molten alloy uses Ni, which is an austenite stabilizing element, as a base component, and is intended to improve oxidation resistance. Containing.
  • the Cr content is specified to be 25% or less so that the austenite structure is in a stable range. Desirably, it is 12% or more and 20% or less.
  • cobalt (Co) is added in the range of 15% or more and 25% or less as a component capable of stabilizing the structure even in the fusion part between the base material and the non-molten alloy powder.
  • Boron (B) is a component that improves the melting point drop of the molten alloy and the wettability and fluidity during diffusion heat treatment of the molten alloy powder, and is contained in a proportion of 1% or more. In order to avoid the formation of a boride phase, the upper limit of the amount added is 5% or less. A preferable content of B is in the range of 2% to 4%.
  • C and Si are also component elements added to obtain the melting point lowering effect of the molten alloy.
  • the amount of C and Si added is the diffusion heat treatment temperature with the goal of obtaining a melting point lower by about ⁇ 50 to ⁇ 100 ° C. than the melting point of the base material in view of the melting point drop due to each element. Is set as follows.
  • the specific C content range is 0.001 to 0.05%
  • Si is 2 to 5%
  • the calculated value of Si + 1.5 ⁇ (C + B) is preferably 6 or more and 9 or less.
  • the composition of the non-molten powder constituting the brazing repair material defined in the present invention is a material similar to the base material FSX414 material, and is caused by a difference in the compatibility with the base material and characteristics after repair. Is prevented.
  • the upper limit of the Cr content is specified to be 45% or less.
  • the Cr content is desirably in the range of 18 to 25%.
  • Ni is an effective element for stabilizing the austenite structure in the low temperature region, and is added at a ratio of 10% or more. However, excessive addition exceeding 25% causes a decrease in strength in the high temperature region. Therefore, the addition amount is set to 25% or less.
  • W is usually added at around 7%. However, in the present invention, an equivalent amount (6 to 8%) of Ta is added instead of the above-mentioned W, whereby a structural failure caused by the formation of ⁇ phase or the like. While preventing stabilization, the melting point of the non-molten powder is adjusted and precipitation strengthening by carbides is attempted.
  • the molten alloy powder it is also possible to use, as the molten alloy, an alloy powder in which the melting point is lowered by further adding 2 to 5% Si and 1 to 5% B to the non-molten alloy powder. .
  • the present invention can be applied not only to the FSX414 material as a base material but also to other Co-based alloys or Ni-based alloys containing 15% to 30% Cr.
  • Example 1 Molten alloy powders for Examples and Comparative Examples having the compositions shown in Table 2 below were prepared.
  • the wettability as a brazing material and the stability of the structure are evaluated based on the gap wetting test method in the brazing material wetting test method prescribed in Japanese Industrial Standard (JIS Z3191). It was. That is, based on the above standards, an inner tube B having an outer diameter of 13.5 mm and an inner diameter of 8.5 mm is inserted into an outer tube A having an outer diameter of 19 mm and an inner diameter of 14 mm, and the lower portion of the outer tube A 10 g of each molten alloy powder is placed in a vacuum, held at a temperature of 1200 ° C.
  • the component ratio defined by Si + 1.5 (C + B) is close to 6 which is the lower limit value.
  • the amount of increase is large at the narrow part of the gap between the inner pipe and the outer pipe, but it is low at the wide part.
  • the difference tended to increase.
  • the test results are shown as ⁇ when both values meet the reference value, ⁇ when one of them is close to the reference value, ⁇ when either does not meet the value, and ⁇ when both values do not satisfy the value. evaluated.
  • Each of the molten alloy powders for each example showed good wettability and was confirmed to have excellent brazing performance as a molten alloy powder. It was also found that the formation of coarse and brittle boride phases in the structure was small and the structure was excellent in stability.
  • Example 2 Non-molten alloy powders for Examples and Comparative Examples having the compositions shown in Table 3 (a) below were prepared. Moreover, the molten alloy powder for an Example and a comparative example which have a composition shown in Table 3 (b) was prepared. Both were mixed so that the weight ratio of each molten alloy powder and non-molten alloy powder was 5: 7, and each brazing repair material was prepared.
  • a groove having a width of 6 mm was formed in a base material made of FSX414 material to form a repaired part for test evaluation, and the brazing repair material (mixed powder) was filled in the groove as the repaired part.
  • the brazing repair material mixed powder
  • the molten alloy powder for the comparative non-molten alloy powder 8 shown in Table 3 (b) an alloy powder obtained by adding the same amount of Al to the molten alloy powder as defined in the present invention was used.
  • the oxidation resistance, the creep strength, and the low cycle fatigue life of the repaired portion subjected to the solution aging heat treatment after performing the diffusion heat treatment on the repaired portion filled with each brazing repair material were measured.
  • the oxidation resistance of the repaired portion is indicated by an increase in oxidation (g) when heated at a temperature of 1000 ° C. for 1000 hours, while the creep strength is a creep in a state where a tensile stress of 103.4 MPa is applied at a temperature of 816 ° C.
  • break time (h) The low cycle fatigue life is expressed as the number of times the operation can be repeated (times) until a total strain of 0.4% occurs at a temperature of 816 ° C.
  • Table 3 (a) The measurement results are shown in Table 3 (a) below and FIGS.
  • Table 3 (a) the result about the case where it is a base material is written together with the result of using each comparative alloy powder.
  • the result about the case where the conventional TIG welding repair was performed was also written together in following Table 3 (a) and FIG.
  • Example 3 Various molten alloy powders having the compositions shown in Table 4 by adding C, B, and Si as melting point depressing elements in the same manner as in Example 1 to the alloy powders shown in Example 2 having a composition similar to that of the substrate. was prepared, and the wettability (bondability) as a brazing material was evaluated. Also in this example, when a gap wetting test based on the brazing material wetting test method specified in JIS Z3191 is performed as in Example 1, a brazing material spreading test is additionally performed, and the wettability as brazing material and The fluidity was evaluated.
  • the spread test of the brazing material is a test method in which 0.1 g of brazing material is held at the brazing temperature for 30 seconds and then rapidly cooled, and the wettability is comparatively evaluated by the size of the spread area. Since the alloy powder material according to the present example was initially concerned about wettability and fluidity, the evaluation by the brazing material spreading test was additionally performed. The measurement evaluation results are shown in Table 4 below.
  • a brazing repair material comprising a mixture of the above-described molten alloy powder comprising a Co-based alloy and a non-molten alloy powder 4 comprising a Co-based alloy having a composition similar to that of the base material was prepared and carried out in Example 2.
  • a similar repair test was conducted.
  • the compositions of the molten alloy powder 8 and the non-molten alloy powder 4 of the present invention used in Table 5 below are shown.
  • the present molten alloy powder 5 shown in Table 4 corresponds to the present molten alloy powder 8 shown in Table 5.
  • both were mixed so that the weight ratio of the molten alloy powder 8 and the non-molten alloy powder 4 would be 5: 7, and each brazing repair material was prepared.
  • a groove of 6 mm width is formed on the base material made of FSX414 material to form a repaired part for test evaluation, and after filling the brazing repair material (mixed powder) into the groove as the repaired part, Diffusion heat treatment was performed under the same conditions as in Example 2, and the characteristics of the repaired part were evaluated.
  • the evaluation results are also shown in Table 5.
  • Example 4 Next, the process flow of the brazing repair method using the brazing repair material according to the present invention will be described, and the processing temperature, a plurality of diffusion heat treatments, the operation of mixing the repair material without using paste in the flat portion, etc. Will be explained.
  • the processing steps of the brazing repair method of the present invention include the following steps as shown in FIG.
  • the brazing repair material has a small apparent viscosity and easily flows. Therefore, in order to prevent the movement of the brazing repair material, the brazing repair material filling process and the diffusion heat treatment are performed by setting the inclination angle of the treatment surface of the repaired part to be within 30 degrees from the horizontal plane. Is preferred.
  • a mixed powder in which a paste agent is mixed with a brazing repair material (mixed powder) to increase the viscosity, or the area to be repaired is surrounded by a heat-resistant tape. Can be adopted.
  • brazing repair processing is executed by the processing steps shown in FIG.
  • the sample (alloy powder) and the reference sample are placed symmetrically in the furnace, the temperature difference between the sample and the reference sample is measured while the temperature is raised at a constant speed, and plotted against time and recorded.
  • a differential thermal analyzer was prepared. The melting point of each molten alloy and non-molten alloy was measured using a differential thermal analysis curve (DTA curve) measured using this differential thermal analyzer. And it shows in following Table 6 with melting
  • the temperature at which local melting occurs from the observation of the structure after heating the sample to a predetermined temperature and rapidly cooling the sample together with the melting point obtained from the DTA curve was also obtained. The local melting temperature was 1261 ° C. From these data, 1200 ° C. was used as the diffusion heat treatment temperature as a temperature higher than the melting point of the molten alloy powder and lower than the local melting temperature of the base material.
  • the ratio of the molten alloy powder increases, the maintenance of the shape of the repair material deteriorates, while when the ratio of the non-molten alloy powder increases, the fluidity of the repair material decreases. As a result of the deterioration, the repair material hardly flows to the crack tip and the filling property is lowered, and the porosity (brazing defect) of the repair portion tends to increase.
  • various brazing repair materials were prepared by changing the mixing ratio of the molten alloy powder and the non-molten alloy powder as shown in Table 7, and the repair material in a state where the inclination angle of the repaired part (treated surface) was changed. The integrity of the shape was confirmed.
  • diffusion heat treatment was performed with the treated surface horizontal (tilt angle 0 degree), the cross-sectional structure of the repaired part was observed, and the occurrence of defects such as pores was investigated. The survey results are shown in Table 7 below.
  • the ratio of the particle size of the non-molten alloy powder constituting the brazing repair material to the particle size of the molten alloy powder also has a large influence on the soundness of the repaired part. While the particle size of the non-molten alloy powder is set to about 45 microns, as shown in Table 8, the particle size of the molten alloy powder is changed from 1/2 to 3 times the particle size of the non-molten alloy powder.
  • a brazing repair material was prepared. Using each of these brazing repair materials, brazing repair was performed under the same conditions as in Example 2. The repaired part was repaired while maintaining the horizontal state (inclination angle 0 degree). And the optimal particle size ratio was examined by observing the structure
  • Example 6 investigated the influence on the structure of the repaired portion when high-temperature brazing repair was performed using a brazing repair material to which a predetermined amount of binder was added.
  • a sufficient amount of repair material is applied to the part to be repaired even if a brazing material for the brazing repair material is formed. It may be difficult to hold. In that case, it is necessary to use a repair material mixed with a binder within a range in which the quality of the repair site can be maintained.
  • each repair material having a different viscosity was prepared by changing the mixing ratio (weight ratio) of the binder to the brazing repair material (mixed powder) from 2 to 20% as shown in Table 9. Furthermore, brazing repair was performed under the same conditions as in Example 2 using each brazing repair material. Then, the influence of the mixing ratio of the binder on the structure after the diffusion heat treatment was examined by observing the structure of each repaired part and comparing the porosity. The survey results are shown in Table 9 below.
  • Example 7 hot isostatic pressing (HIP) processing conditions were examined.
  • a brazing repair material is prepared by mixing the molten alloy powder 1 of the present invention and the non-molten alloy powder 1 of the present invention at a weight ratio of 5: 7, and this repair material is used in the example. Brazing repair was carried out under the same conditions as 2.
  • Each test piece including the repair part was subjected to HIP treatment under the conditions shown in Table 10. Specifically, the HIP treatment was performed by changing the pressure to 1000 atm and the heating temperature in the range of 1000 ° C. to 1350 ° C. The structure of the repaired part was observed for each test piece, and the filling state of the repair material into the cracks was investigated. In addition, a tensile test of the repaired part was performed, and the tensile strength and tensile elongation of the repaired part were measured. The measurement evaluation results are shown in Table 10 below.
  • Example 2 After carrying out brazing repair using the brazing repair material used in Example 2 and Example 3, the test piece which carried out the HIP process on the HIP processing conditions 3 (pressure: 1000 atm, temperature: 1200 degreeC) of this invention, and implementation
  • the brazing repair material prepared by mixing the molten alloy powder 8 of the present invention used in Example 3 and the non-molten alloy powder 4 at a ratio of 5: 7 was used for brazing repair, and then the above HIP processing condition 3 of the present invention was used.
  • the low cycle fatigue life was measured for the HIP-treated specimen.
  • the low cycle fatigue life is represented by the number of times the operation can be repeated (times) until a total strain of 0.4% is generated at a temperature of 816 ° C., as in Example 2.
  • Example 8 Next, in the brazing repair method of the present invention, the influence of the particle size ratio between the molten alloy powder and the non-molten alloy powder on the characteristics of the repaired part will be described based on Example 8 below.
  • the brazing repair material in Example 8 is composed of a molten alloy powder and a non-molten alloy powder having the composition shown in Table 11, and the particle size of the molten alloy powder is set to about half the particle size of the non-molten alloy powder. This improves the fluidity of the molten alloy during diffusion heat treatment.
  • FIG. 6 is a schematic cross-sectional view showing the distribution state of the non-molten alloy and the molten alloy in the repaired portion repaired by the diffusion brazing method.
  • the crack 2 generated in the base material 1 is filled with a brazing repair material 3 composed of molten alloy powder ( ⁇ ) and non-molten alloy powder ( ⁇ ) and subjected to diffusion heat treatment, the fluidity of the molten alloy during the diffusion heat treatment Therefore, the repair material effectively penetrates from the surface portion P1 of the base material through the middle portions P2 and P3 to the tip portion P4 of the crack 2, and the filling property of the repair material to the crack 2 is improved. Was confirmed to be very good.
  • Table 11 below shows the analysis results of the alloy composition at the surface portion P1 of the base material, the middle portions P2 and P3 of the crack 2 and the tip portion P4 of the crack 2 in the repair portion shown in FIG.
  • the alloy composition may be closer to the molten alloy powder composition from the non-molten alloy powder composition as it goes from the surface layer portion P1 of the repaired portion to the tip portion P4 of the crack 2. confirmed.
  • the amounts of Si and B components were slightly lower than the original molten alloy composition by diffusion heat treatment, but showed a tendency to approach the molten alloy powder composition generally toward the tip side of the crack.
  • Example 9 Next, in the brazing repair method of the present invention, an example in which a brazed repair material composed of a molten alloy powder and a non-molten alloy powder is filled in a repaired part by a high-speed gas flow is shown in Example 9 below. This will be explained based on.
  • a non-melt coating apparatus as shown in FIG. 7 is used as a brazing repair material filling apparatus for a repaired part.
  • This non-melt coating apparatus has a configuration similar to a thermal spraying apparatus used for coating treatment of gas turbine blades, a powder supply apparatus 4 for supplying brazing repair material 3, and compression of nitrogen, He gas, etc.
  • the brazing repair material 3 is repaired by a high-speed gas flow below a temperature at which the alloy powder constituting the brazing repair material 3 does not melt and oxidize. Material is dispersed and transported. Then, the repair material is made to collide with the repaired part, and the mixed powder is attached to the non-repaired portion by the energy of the collision, and the repair material is pushed into the deep part of the crack. That is, compressed air or compressed gas such as nitrogen or He gas is supplied to the supersonic nozzle 7 with the flow velocity accelerated through the gas heating device 5 and mixed with the powder of the brazing repair material 3 supplied separately.
  • the gas flow velocity is further accelerated to collide with the portion to be repaired at the supersonic speed to cover it.
  • the brazing repair material can be firmly attached to the base material surface and the inside of the crack by the above filling operation, damage such as a crack occurs over the entire surface of the gas turbine stationary blade. Even in such a case, the number of diffusion heat treatments can be two times, i.e., when the blade surface is facing upward, and when the blade surface is facing downward, and repair work efficiency is greatly improved.
  • FIG. 8 is a graph showing the relationship between the particle velocity and the adhesion efficiency of the particles when the brazing repair material is impacted and adhered to the substrate surface at a high speed using the non-melt coating apparatus.
  • spraying is performed using a carrier gas having a particle speed of 300 m / second or higher. It is very effective to fill the material surface or the inside of the crack with the repair material particles.
  • the adhesion efficiency is defined as the ratio of the amount of the repair material actually adhered to the surface of the base material and the crack to the amount of the repair material conveyed by the high-speed gas flow.
  • FIG. 9 is a graph showing the relationship between the nozzle outlet temperature of compressed gas and the particle velocity in the non-melt coating apparatus. It is apparent that the particle velocity tends to increase in proportion to the increase in the nozzle outlet temperature of the compressed gas. In order to set the particle velocity to 300 m / sec or more, it is sufficient to set the nozzle outlet temperature of the compressed gas as the carrier gas to 200 ° C. or more. However, when the compressed gas temperature is increased to exceed 800 ° C., the upper limit temperature is desirably set to 800 ° C. because the alloy powder constituting the repair material is likely to be deteriorated by melting or oxidation.
  • FIG. 10 is a graph showing the relationship between the thermal spraying efficiency of the brazing repair material powder and the powder particle size when the brazing repair material powder is impacted and adhered to the substrate surface at a high speed using the non-melt coating apparatus. It is. In particular, since it is clear that the thermal spraying efficiency is high when the powder particle size is in the range of 10 ⁇ m to 150 ⁇ m, the particle size of the molten alloy powder and the non-molten alloy powder constituting the brazing repair material should be selected within the above range. Is preferred.
  • the spraying efficiency is defined as the ratio of the amount of the repair material actually sprayed on the substrate surface and inside the crack to the amount of the repair material conveyed by the high-speed gas flow.
  • a repair material comprising a non-molten alloy powder having a composition similar to that of the component base material and a molten alloy powder having a predetermined composition is used. Therefore, it is easy to repair and regenerate high-temperature parts with defects such as cracks and corrosion, and greatly improve the operating economy and maintenance management of gas turbines that use high-temperature parts as components. Can do.

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  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
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PCT/JP2009/052649 2008-05-27 2009-02-17 ロウ付け補修材料およびその材料を使用したロウ付け補修方法 Ceased WO2009144975A1 (ja)

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US12/994,396 US20110088260A1 (en) 2008-05-27 2009-02-17 Brazing repair material and brazing repairing method using the material
US14/102,610 US20140096872A1 (en) 2008-05-27 2013-12-11 Brazing repair material and brazing repairing method using the material

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US20110088260A1 (en) 2011-04-21
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US20140096872A1 (en) 2014-04-10
SA109300323B1 (ar) 2014-10-23
EP2279826A4 (en) 2013-03-20
EP2279826A1 (en) 2011-02-02

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