US20150174653A1 - System and methods for removing core elements of cast components - Google Patents

System and methods for removing core elements of cast components Download PDF

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Publication number
US20150174653A1
US20150174653A1 US14/572,474 US201414572474A US2015174653A1 US 20150174653 A1 US20150174653 A1 US 20150174653A1 US 201414572474 A US201414572474 A US 201414572474A US 2015174653 A1 US2015174653 A1 US 2015174653A1
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Prior art keywords
vessel
high temperature
solution
autoclave
cycle
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US14/572,474
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Carl R. Verner
John Joseph Marcin
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Raytheon Technologies Corp
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United Technologies Corp
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Priority to US14/572,474 priority Critical patent/US20150174653A1/en
Assigned to UNITED TECHNOLOGIES CORPORATION reassignment UNITED TECHNOLOGIES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MARCIN, JOHN JOSEPH, VERNER, CARL R.
Publication of US20150174653A1 publication Critical patent/US20150174653A1/en
Priority to US15/590,132 priority patent/US9808862B2/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D29/00Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
    • B22D29/001Removing cores
    • B22D29/003Removing cores using heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D29/00Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D29/00Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
    • B22D29/001Removing cores
    • B22D29/002Removing cores by leaching, washing or dissolving
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D29/00Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
    • B22D29/001Removing cores
    • B22D29/006Removing cores by abrasive, water or air blasting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D30/00Cooling castings, not restricted to casting processes covered by a single main group

Definitions

  • the present disclosure relates generally to metal casting, and more particularly to a system and methods for removal of core and pin elements from cast components.
  • Investment casting, or die casting is a known technique for forming metallic components having complex geometries, especially hollow components, and is used in the fabrication of gas turbine engine components.
  • Cast hardware can include one or more core elements to produce internal and external features.
  • internal independent parts can be attached and assembled together. These elements may be difficult to remove after casting, especially for complex cores and long or narrow passages.
  • Casting pins can be used to produce features or strengthen sections of the cores and may be particularly difficult to remove.
  • Conventional core removal methods may employ open vessels, which take a long time and in many cases, such as open pot leach, the process is ineffective for removal of complex cores or casting pins.
  • Conventional sealed autoclaves are typically large and require a complex agitation system to change pressure. In some cases no system for pressure change is used. Accordingly, there is a desire to improve removal of core elements.
  • a method includes controlling a first high temperature autoclave cycle for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component, and controlling a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component.
  • the method also includes controlling one or more low temperature autoclave cycles following the second high temperature cycle to remove core and casting pins from the cast component.
  • a system for removing core elements of cast components includes a vessel and a controller configured to control solution concentration, temperature and pressure in the vessel.
  • the controller is configured to control a first high temperature autoclave cycle for a cast component in the vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component, control a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component, and control one or more low temperature autoclave cycles following the second high temperature cycle to remove core and casting pins from the cast component.
  • FIG. 1 depicts a simplified system diagram of a core removal system according to one or more embodiments
  • FIG. 2 depicts a method for removing core components according to one or more embodiments
  • FIG. 3 depicts a graphical representation of autoclave cycles according to one or more other embodiments.
  • FIG. 4 depicts a graphical representation of a vessel according to one or more embodiments.
  • a method for removing core material and elements from cast components, such as cast blades, vanes and other gas turbine hardware having complex core passages that serpentine through the casting.
  • Core material such as the ceramic core, and other core elements, such as quartz or alumina casting pins, may be removed by a process of one or more autoclave cycles.
  • a method includes high temperature and low temperature autoclave cycles, wherein a solution concentration, temperature and pressure in an autoclave vessel are controlled to loosen and remove one or more core elements from a cast component.
  • a system for removing core elements of cast components includes a vessel and a controller configured to control one or more of a solution concentration, temperature and pressure in the vessel.
  • the vessel may include one or more coiling coils to produce quick temperature and pressure changes in the vessel.
  • the terms “a” or “an” shall mean one or more than one.
  • the term “plurality” shall mean two or more than two.
  • the term “another” is defined as a second or more.
  • the terms “including” and/or “having” are open ended (e.g., comprising).
  • the term “or” as used herein is to be interpreted as inclusive or meaning any one or any combination. Therefore, “A, B or C” means “any of the following: A; B; C; A and B; A and C; B and C; A, B and C”. An exception to this definition will occur only when a combination of elements, functions, steps or acts are in some way inherently mutually exclusive.
  • FIG. 1 depicts a simplified system diagram of a core removal system according to one or more embodiments.
  • System 100 may be configured to remove one or more core elements from a cast component, shown as 101 , including ceramic core elements and casting pins.
  • Cast component 101 may be cast blades, vanes, blade outer air seals, other gas turbine engine components, and other hardware with core passages.
  • system 100 may include autoclave equipment, including vessel 105 for flushing cast component 101 with a solution under controlled, temperatures and pressures to remove core elements from the cast component. As shown in FIG. 1 , system 100 includes vessel 105 and controller 110 . Controller 110 may be electrically coupled to one or more elements of system 100 to control one or more autoclave cycles.
  • Vessel 105 can contain cast component 101 mounted to a component 115 and solution 120 .
  • vessel 105 may have a small capacity, such as a volume within the range of 1-50 gallons (e.g., 3.7 to 189 liters). Using a small volume vessel may allow for lower mass, and lower time to raise and lower temperature of the vessel, and vessel contents (e.g., liquids, solutions, casting parts, etc.). It should be appreciated that in certain embodiments, vessel 105 may be a large vessel with specific controls to allow for rapid heat up and cool down. Vessel 105 is sealed by cover 125 . Solution 120 may be provided to vessel 105 , and replenished by, solution source 130 .
  • Temperature sensor 140 may be configured to monitor the temperature inside vessel 105 and the temperature of solution 120 .
  • Pressure controller/sensor 145 may be configured to detect the pressure inside of vessel 105 .
  • pressure control/sensor 145 may pressurize the vessel.
  • the output of temperature sensor 140 and pressure control/sensor 145 may be employed by controller 110 to control the temperature and/or pressure in vessel 105 .
  • Cooling controls 150 and 155 may each include one or more cooling coils, shown as 160 for rapidly cooling solution 120 .
  • Heating elements 165 may be configured to heat vessel 105 and/or solution 120 .
  • Cooling controls 150 and 155 and heating elements 165 may be controlled by controller 105 .
  • controller 105 may be configured to control solution concentration, temperature and pressure in the vessel for one or more autoclave cycles.
  • Discharge assembly 170 may be configured to flush solution 120 and or removed core material during one or more autoclave cycles.
  • FIG. 2 depicts a method for removing core components according to one or more embodiments.
  • process 200 may be employed to control a system for removing core elements (e.g., system 100 of FIG. 1 ).
  • Process 200 may be employed by a controller (e.g., controller 105 ) to control one or more autoclave cycles.
  • autoclave cycles of process 200 may be controlled to remove core elements including ceramic cores and alumina casting pins.
  • Process 200 may be initiated at block 205 with a first high temperature autoclave cycle.
  • the first high temperature autoclave cycle may be for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements.
  • the first solution concentration, temperature and pressure in the vessel may be controlled during the first high temperature autoclave cycle to expose one or more casting pins in the cast component.
  • the first high temperature autoclave cycle includes heating the vessel to a temperature within the range of 200 to 400 degrees F. (e.g., 95-200 degrees Celsius (C)).
  • first high temperature autoclave cycle may employ a solution of less than 40% KOH or less than 40% NaOH.
  • the first high temperature autoclave cycle may employ a solution of 20%-30% of KOH or 20%-30% of NaOH. In one embodiment, percentages of solutions used here, such as a solution used in an autoclave cycle, may be by mole. In other embodiments, percentages of solutions used herein, such as a solution used in an autoclave cycle, may be by weight.
  • the first high temperature autoclave cycle may be controlled to remove a first leg of core components, such as a serpentine core and expose casting pin. In one embodiment, the first high temperature autoclave cycle may be a 12 hour cycle. It should be appreciated that shorter or longer time periods may be employed for the first high temperature autoclave cycle.
  • a second temperature autoclave cycle at is initiated for the cast component in the vessel with second solution concentration.
  • the second cycle may be directed to components that are difficult to remove due to access or material composition.
  • the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component.
  • the second high temperature autoclave cycle includes heating the vessel to a temperature within the range of 400 to 600 degrees F. (e.g., 200-315 degrees C.).
  • the second high temperature autoclave cycle may employ a solution of at least 40% of KOH or at least 40% of NaOH.
  • the second high temperature autoclave cycle may employ a solution of 40%-50% of KOH or 40%-50% of NaOH.
  • the second high temperature autoclave cycle may be controlled to remove core components and casting pins from the cast component, in particular pins made from aluminum oxide.
  • the second high temperature autoclave cycle may be a 12 hour cycle. It should be appreciated that shorter or longer time periods may be employed for the second high temperature autoclave cycle.
  • Each of the high temperature autoclave cycles in process 200 may include a cooling cycle that is controlled to cycled on and off multiple times during each autoclave cycle to provide repetitive and rapid pressure changes in the vessel, promote agitation, and promote a flushing action in the solution.
  • one or more low temperature cycles may be performed in the vessel. In one embodiment, between 3-5 low temperature autoclave cycles are initiated in the vessel. However, it should be appreciated that additional or fewer low temperature cycles may be performed.
  • the one or more low temperature cycles may include controlling the temperature of a vessel to be below 200 degrees F.
  • each autoclave cycle includes flushing the cast component to remove one or more of core and casting pin material.
  • FIG. 3 depicts a flow diagram of autoclave processing and process parameters according to one or more embodiments.
  • Process 300 may be initiated by positioning a component at block 305 .
  • parts may be alternately positioned root side up or root side down in a vessel at block 305 .
  • the position of cast parts may be alternated during each autoclave cycle.
  • one or more parameters may be controlled during each autoclave cycle.
  • Process 300 includes one or more high temperature autoclave cycles 306 including controlling temperature at block 310 , pressure at block 315 and solution at block 320 .
  • High temperature autoclave cycle 306 includes a cooling cycle 325 which may be cycled on or off multiple times per hour to achieve repetitive and rapid pressure change in the vessel.
  • Cycle 306 may also include discharge of core elements and/or solution during the cycle at block 330 .
  • decision block 335 may determine whether to initiate a low temperature cycle. When additional high temperature cycles are required (e.g., “NO” path out of decision block 335 ), process 300 may continue with a high temperature autoclave cycle, similar to cycle 306 .
  • Process 300 may determine a low temperature cycle is to be performed (e.g., “YES” path out of decision block 335 ) and conduct one or more low temperature cycles at block 340 .
  • FIG. 4 depicts a graphical representation of a vessel according to one or more embodiments.
  • vessel 400 may include one or more elements to rapidly change the temperature (e.g., by heating and/or cooling) within the vessel during one or more cycles.
  • elements of vessel 400 may be employed with the vessel of system 100 of FIG. 1 for removing one or more core elements from a cast component, including ceramic core elements and casting pins.
  • vessel 400 is a cylindrical container including sidewall 405 and vessel lid 410 . Although shown as a cylindrical container it should be appreciated that other configurations and shapes maybe employed with vessel 400 .
  • Vessel 400 includes discharge 415 to flush solution and/or removed core material during one or more autoclave cycles.
  • vessel 400 includes cooling coil 420 .
  • Cooling coil 420 may be positioned in and/or near vessel lid 410 for cooling solution and contents of vessel 400 .
  • Cooling coil 420 may be employed for changing the pressure in vessel 400 .
  • Cooling coil 420 is shown as an individual coil in FIG. 4 , however, it should be appreciated that multiple cooling coils may be used with vessel 400 .
  • vessel 400 includes heating bands 425 1-n .
  • Heating bands 425 1-n may be positioned in and/or near sidewall 405 for heating solution and contents of vessel 400 .
  • Heating bands 425 1-n may be employed for changing the pressure in vessel 400 .
  • Heating bands 425 1-n is shown as multiple bands in FIG. 4 , however, it should be appreciated that a single heating element may be used with vessel 400 in certain embodiments.

Abstract

A system and methods are provided for removing core elements of cast components. In one embodiment, a method includes controlling a first high temperature autoclave cycle for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component. The method may also include controlling a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component, and controlling one or more low temperature autoclave cycles to remove core and casting pins from the cast component.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application claims priority to U.S. Provisional Application No. 61/918,594 filed on Dec. 19, 2013 and titled System and Methods for Removing Core Elements of Cast Components, the disclosure of which is hereby incorporated by reference in its entirety.
  • FIELD
  • The present disclosure relates generally to metal casting, and more particularly to a system and methods for removal of core and pin elements from cast components.
  • BACKGROUND
  • Investment casting, or die casting, is a known technique for forming metallic components having complex geometries, especially hollow components, and is used in the fabrication of gas turbine engine components.
  • Cast hardware can include one or more core elements to produce internal and external features. In some cases, internal independent parts can be attached and assembled together. These elements may be difficult to remove after casting, especially for complex cores and long or narrow passages. Casting pins can be used to produce features or strengthen sections of the cores and may be particularly difficult to remove.
  • Conventional core removal methods may employ open vessels, which take a long time and in many cases, such as open pot leach, the process is ineffective for removal of complex cores or casting pins. Conventional sealed autoclaves are typically large and require a complex agitation system to change pressure. In some cases no system for pressure change is used. Accordingly, there is a desire to improve removal of core elements.
  • BRIEF SUMMARY OF THE EMBODIMENTS
  • Disclosed and claimed herein are a system and methods for removing core elements of cast components. In one embodiment, a method includes controlling a first high temperature autoclave cycle for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component, and controlling a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component. The method also includes controlling one or more low temperature autoclave cycles following the second high temperature cycle to remove core and casting pins from the cast component.
  • In one embodiment, a system for removing core elements of cast components includes a vessel and a controller configured to control solution concentration, temperature and pressure in the vessel. According to one embodiment, the controller is configured to control a first high temperature autoclave cycle for a cast component in the vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component, control a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component, and control one or more low temperature autoclave cycles following the second high temperature cycle to remove core and casting pins from the cast component.
  • Other aspects, features, and techniques will be apparent to one skilled in the relevant art in view of the following detailed description of the embodiments.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The features, objects, and advantages of the present disclosure will become more apparent from the detailed description set forth below when taken in conjunction with the drawings in which like reference characters identify correspondingly throughout and wherein:
  • FIG. 1 depicts a simplified system diagram of a core removal system according to one or more embodiments;
  • FIG. 2 depicts a method for removing core components according to one or more embodiments;
  • FIG. 3 depicts a graphical representation of autoclave cycles according to one or more other embodiments; and
  • FIG. 4 depicts a graphical representation of a vessel according to one or more embodiments.
  • DETAILED DESCRIPTION OF THE EXEMPLARY EMBODIMENTS Overview and Terminology
  • One aspect of the disclosure relates to removal of core material and elements from core passages of a cast component. In one embodiment, a method is provided for removing core material and elements from cast components, such as cast blades, vanes and other gas turbine hardware having complex core passages that serpentine through the casting. Core material, such as the ceramic core, and other core elements, such as quartz or alumina casting pins, may be removed by a process of one or more autoclave cycles. In one embodiment, a method includes high temperature and low temperature autoclave cycles, wherein a solution concentration, temperature and pressure in an autoclave vessel are controlled to loosen and remove one or more core elements from a cast component.
  • According to another embodiment, a system for removing core elements of cast components includes a vessel and a controller configured to control one or more of a solution concentration, temperature and pressure in the vessel. The vessel may include one or more coiling coils to produce quick temperature and pressure changes in the vessel.
  • As used herein, the terms “a” or “an” shall mean one or more than one. The term “plurality” shall mean two or more than two. The term “another” is defined as a second or more. The terms “including” and/or “having” are open ended (e.g., comprising). The term “or” as used herein is to be interpreted as inclusive or meaning any one or any combination. Therefore, “A, B or C” means “any of the following: A; B; C; A and B; A and C; B and C; A, B and C”. An exception to this definition will occur only when a combination of elements, functions, steps or acts are in some way inherently mutually exclusive.
  • Reference throughout this document to “one embodiment,” “certain embodiments,” “an embodiment,” or similar term means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment. Thus, the appearances of such phrases in various places throughout this specification are not necessarily all referring to the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any suitable manner on one or more embodiments without limitation.
  • Exemplary Embodiments
  • Referring now to the figures, FIG. 1 depicts a simplified system diagram of a core removal system according to one or more embodiments. System 100 may be configured to remove one or more core elements from a cast component, shown as 101, including ceramic core elements and casting pins. Cast component 101 may be cast blades, vanes, blade outer air seals, other gas turbine engine components, and other hardware with core passages.
  • According to one embodiment, system 100 may include autoclave equipment, including vessel 105 for flushing cast component 101 with a solution under controlled, temperatures and pressures to remove core elements from the cast component. As shown in FIG. 1, system 100 includes vessel 105 and controller 110. Controller 110 may be electrically coupled to one or more elements of system 100 to control one or more autoclave cycles.
  • Vessel 105 can contain cast component 101 mounted to a component 115 and solution 120. In one embodiment, vessel 105 may have a small capacity, such as a volume within the range of 1-50 gallons (e.g., 3.7 to 189 liters). Using a small volume vessel may allow for lower mass, and lower time to raise and lower temperature of the vessel, and vessel contents (e.g., liquids, solutions, casting parts, etc.). It should be appreciated that in certain embodiments, vessel 105 may be a large vessel with specific controls to allow for rapid heat up and cool down. Vessel 105 is sealed by cover 125. Solution 120 may be provided to vessel 105, and replenished by, solution source 130.
  • Temperature sensor 140 may be configured to monitor the temperature inside vessel 105 and the temperature of solution 120. Pressure controller/sensor 145 may be configured to detect the pressure inside of vessel 105. In certain embodiments, pressure control/sensor 145 may pressurize the vessel. The output of temperature sensor 140 and pressure control/sensor 145 may be employed by controller 110 to control the temperature and/or pressure in vessel 105.
  • Cooling controls 150 and 155 may each include one or more cooling coils, shown as 160 for rapidly cooling solution 120. Heating elements 165 may be configured to heat vessel 105 and/or solution 120. Cooling controls 150 and 155 and heating elements 165 may be controlled by controller 105. In one embodiment, controller 105 may be configured to control solution concentration, temperature and pressure in the vessel for one or more autoclave cycles.
  • Discharge assembly 170 may be configured to flush solution 120 and or removed core material during one or more autoclave cycles.
  • FIG. 2 depicts a method for removing core components according to one or more embodiments. According to one embodiment, process 200 may be employed to control a system for removing core elements (e.g., system 100 of FIG. 1). Process 200 may be employed by a controller (e.g., controller 105) to control one or more autoclave cycles. According to another embodiment, autoclave cycles of process 200 may be controlled to remove core elements including ceramic cores and alumina casting pins.
  • Process 200 may be initiated at block 205 with a first high temperature autoclave cycle. According to one embodiment, the first high temperature autoclave cycle may be for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements. The first solution concentration, temperature and pressure in the vessel may be controlled during the first high temperature autoclave cycle to expose one or more casting pins in the cast component. According to one embodiment, the first high temperature autoclave cycle includes heating the vessel to a temperature within the range of 200 to 400 degrees F. (e.g., 95-200 degrees Celsius (C)). In one embodiment, first high temperature autoclave cycle may employ a solution of less than 40% KOH or less than 40% NaOH. In certain embodiments, the first high temperature autoclave cycle may employ a solution of 20%-30% of KOH or 20%-30% of NaOH. In one embodiment, percentages of solutions used here, such as a solution used in an autoclave cycle, may be by mole. In other embodiments, percentages of solutions used herein, such as a solution used in an autoclave cycle, may be by weight. The first high temperature autoclave cycle may be controlled to remove a first leg of core components, such as a serpentine core and expose casting pin. In one embodiment, the first high temperature autoclave cycle may be a 12 hour cycle. It should be appreciated that shorter or longer time periods may be employed for the first high temperature autoclave cycle.
  • At block 210, a second temperature autoclave cycle at is initiated for the cast component in the vessel with second solution concentration. The second cycle may be directed to components that are difficult to remove due to access or material composition. The second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component. According to one embodiment, the second high temperature autoclave cycle includes heating the vessel to a temperature within the range of 400 to 600 degrees F. (e.g., 200-315 degrees C.). In one embodiment, the second high temperature autoclave cycle may employ a solution of at least 40% of KOH or at least 40% of NaOH. By way of example, the second high temperature autoclave cycle may employ a solution of 40%-50% of KOH or 40%-50% of NaOH. The second high temperature autoclave cycle may be controlled to remove core components and casting pins from the cast component, in particular pins made from aluminum oxide. In one embodiment, the second high temperature autoclave cycle may be a 12 hour cycle. It should be appreciated that shorter or longer time periods may be employed for the second high temperature autoclave cycle.
  • Each of the high temperature autoclave cycles in process 200 may include a cooling cycle that is controlled to cycled on and off multiple times during each autoclave cycle to provide repetitive and rapid pressure changes in the vessel, promote agitation, and promote a flushing action in the solution.
  • At block 215, one or more low temperature cycles may be performed in the vessel. In one embodiment, between 3-5 low temperature autoclave cycles are initiated in the vessel. However, it should be appreciated that additional or fewer low temperature cycles may be performed. The one or more low temperature cycles may include controlling the temperature of a vessel to be below 200 degrees F.
  • The autoclave cycles for removal of core components and casting pins in process 200 may be initiated in a vessel having a volume within the range of 5-10 gallons (e.g., 18-38 liters). According to one embodiment, each autoclave cycle includes flushing the cast component to remove one or more of core and casting pin material.
  • FIG. 3 depicts a flow diagram of autoclave processing and process parameters according to one or more embodiments. Process 300 may be initiated by positioning a component at block 305. According to one embodiment, parts may be alternately positioned root side up or root side down in a vessel at block 305. In certain embodiments, the position of cast parts may be alternated during each autoclave cycle. According to one embodiment, one or more parameters may be controlled during each autoclave cycle. Process 300 includes one or more high temperature autoclave cycles 306 including controlling temperature at block 310, pressure at block 315 and solution at block 320. High temperature autoclave cycle 306 includes a cooling cycle 325 which may be cycled on or off multiple times per hour to achieve repetitive and rapid pressure change in the vessel. Cycle 306 may also include discharge of core elements and/or solution during the cycle at block 330. Following high temperature autoclave cycle 306, decision block 335 may determine whether to initiate a low temperature cycle. When additional high temperature cycles are required (e.g., “NO” path out of decision block 335), process 300 may continue with a high temperature autoclave cycle, similar to cycle 306. Process 300 may determine a low temperature cycle is to be performed (e.g., “YES” path out of decision block 335) and conduct one or more low temperature cycles at block 340.
  • FIG. 4 depicts a graphical representation of a vessel according to one or more embodiments. According to one embodiment, vessel 400 may include one or more elements to rapidly change the temperature (e.g., by heating and/or cooling) within the vessel during one or more cycles. According to another embodiment, elements of vessel 400 may be employed with the vessel of system 100 of FIG. 1 for removing one or more core elements from a cast component, including ceramic core elements and casting pins.
  • As shown in FIG. 4, vessel 400 is a cylindrical container including sidewall 405 and vessel lid 410. Although shown as a cylindrical container it should be appreciated that other configurations and shapes maybe employed with vessel 400. Vessel 400 includes discharge 415 to flush solution and/or removed core material during one or more autoclave cycles.
  • According to one embodiment, vessel 400 includes cooling coil 420. Cooling coil 420 may be positioned in and/or near vessel lid 410 for cooling solution and contents of vessel 400. Cooling coil 420 may be employed for changing the pressure in vessel 400. Cooling coil 420 is shown as an individual coil in FIG. 4, however, it should be appreciated that multiple cooling coils may be used with vessel 400.
  • According to another embodiment, vessel 400 includes heating bands 425 1-n. Heating bands 425 1-n may be positioned in and/or near sidewall 405 for heating solution and contents of vessel 400. Heating bands 425 1-n may be employed for changing the pressure in vessel 400. Heating bands 425 1-n is shown as multiple bands in FIG. 4, however, it should be appreciated that a single heating element may be used with vessel 400 in certain embodiments.
  • While this disclosure has been particularly shown and described with references to exemplary embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the scope of the claimed embodiments.

Claims (20)

What is claimed is:
1. A method for removing core elements of cast components, the method comprising:
controlling a first high temperature autoclave cycle for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component;
controlling a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component; and
controlling one or more low temperature autoclave cycles following the second high temperature cycle to remove core and casting pins from the cast component.
2. The method of claim 1, wherein the first high temperature autoclave cycle includes heating the vessel to a temperature within the range of 95 to 200 degrees Celsius (C).
3. The method of claim 1, wherein the solution of the first high temperature autoclave cycle is solution of less than 40% of KOH or less than 40% of NaOH.
4. The method of claim 1, wherein the second high temperature autoclave cycle includes heating the vessel to a temperature within the range of 200 to 315 degrees Celsius (C).
5. The method of claim 1, wherein the solution of the second high temperature autoclave cycle is solution of at least 40% of KOH or at least 40% of NaOH.
6. The method of claim 1, wherein each high temperature autoclave cycle includes a cooling cycle that is controlled to cycled on and off multiple times during each autoclave cycle to provide repetitive and rapid pressure changes in the vessel, promote agitation, and promote a flushing action in the solution.
7. The method of claim 1, wherein 3-5 low temperature autoclave cycles are initiated in the vessel.
8. The method of claim 1, wherein the autoclave cycles are controlled to remove core elements including ceramic cores and alumina casting pins.
9. The method of claim 1, wherein the autoclave cycles are initiated in a vessel having a volume within the range of 3.7 to 189 liters.
10. The method of claim 1, wherein the each autoclave cycle includes flushing the cast component with a fluid to remove one or more of core and casting pin material.
11. A system for removing core elements of cast components comprising:
a vessel;
a controller configured to control solution concentration, temperature and pressure in the vessel, wherein the controller is configured to
control a first high temperature autoclave cycle for a cast component in the vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component;
control a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component; and
control one or more low temperature autoclave cycles following the second high temperature cycle to remove core and casting pins from the cast component.
12. The system of claim 11, wherein the first high temperature autoclave cycle includes heating the vessel to a temperature within the range of 95 to 200 degrees Celsius (C).
13. The system of claim 11, wherein the solution of the first high temperature autoclave cycle is solution of less than 40% of KOH or less than 40% of NaOH.
14. The system of claim 11, wherein the second high temperature autoclave cycle includes heating the vessel to a temperature within the range of 200 to 315 degrees Celsius (C).
15. The system of claim 11, wherein the solution of the second high temperature autoclave cycle is solution of at least 40% of KOH or at least 40% of NaOH.
16. The system of claim 11, further comprising cooling coils, wherein the controller controls the cooling coils to be cycled on and off multiple times during each autoclave cycle to provide repetitive and rapid pressure changes in the vessel, promote agitation, and promote a flushing action in the solution.
17. The system of claim 11, wherein 3-5 low temperature autoclave cycles are initiated in the vessel.
18. The system of claim 11, wherein the autoclave cycles are controlled to remove core elements including ceramic cores and alumina casting pins.
19. The system of claim 11, wherein the autoclave cycles are initiated in a vessel having a volume within the range of 3.7 to 189 liters.
20. The system of claim 11, wherein the each autoclave cycle includes flushing the cast component with a fluid to remove one or more of core and casting pin material.
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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9579714B1 (en) 2015-12-17 2017-02-28 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
CN106735108A (en) * 2017-01-04 2017-05-31 中国航空工业集团公司北京航空材料研究院 A kind of turbine hollow blade depoling frock
CN107127323A (en) * 2017-06-13 2017-09-05 西安交通大学 A kind of method and apparatus for improving ceramic core depoling efficiency
US9808862B2 (en) 2013-12-19 2017-11-07 United Technologies Corporation System and methods for removing core elements of cast components
CN107866550A (en) * 2017-12-21 2018-04-03 西安欧中材料科技有限公司 A kind of ceramic core removal methods of aero-engine hollow blade
US9968991B2 (en) 2015-12-17 2018-05-15 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
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US10099284B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having a catalyzed internal passage defined therein
US10118217B2 (en) 2015-12-17 2018-11-06 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10137499B2 (en) 2015-12-17 2018-11-27 General Electric Company Method and assembly for forming components having an internal passage defined therein
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US10286450B2 (en) 2016-04-27 2019-05-14 General Electric Company Method and assembly for forming components using a jacketed core
US10335853B2 (en) 2016-04-27 2019-07-02 General Electric Company Method and assembly for forming components using a jacketed core
EP3536418A1 (en) * 2018-03-09 2019-09-11 United Technologies Corporation Casting core removal through thermal cycling
CN112191829A (en) * 2020-10-10 2021-01-08 中国航发北京航空材料研究院 Core removing kettle and method for precisely casting hollow blade core

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11179769B2 (en) 2019-02-08 2021-11-23 Raytheon Technologies Corporation Investment casting pin and method of using same
US11325182B2 (en) 2020-03-12 2022-05-10 Raytheon Technologies Corporation Method for removing refractory metal cores
CN111992695B (en) * 2020-07-13 2022-05-31 中国科学院金属研究所 Method for removing ceramic shell of single crystal high-temperature alloy blade

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3714977A (en) * 1971-07-23 1973-02-06 United Aircraft Corp Method and apparatus for the production of directionally solidified castings
US5779809A (en) * 1995-12-26 1998-07-14 General Electric Company Method of dissolving or leaching ceramic cores in airfoils
US5915452A (en) * 1995-06-07 1999-06-29 Howmet Research Corporation Apparatus for removing cores from castings
US6739380B2 (en) * 2002-04-11 2004-05-25 Rolls-Royce Corporation Method and apparatus for removing ceramic material from cast components
US8056607B2 (en) * 2008-06-24 2011-11-15 Pcc Airfoils, Inc. Method of casting metal articles
US20120222961A1 (en) * 2010-12-30 2012-09-06 Michel Shawn Smallwood System, method, and apparatus for leaching cast components
US8409493B2 (en) * 2009-08-06 2013-04-02 Rolls-Royce Corporation Systems and methods for leaching a material from an object

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2266677B (en) * 1992-05-08 1995-02-01 Rolls Royce Plc Improvements in or relating to the leaching of ceramic materials
US6354310B1 (en) * 1998-11-12 2002-03-12 General Electric Company Apparatus and process to clean and strip coatings from hardware
US20150174653A1 (en) 2013-12-19 2015-06-25 United Technologies Corporation System and methods for removing core elements of cast components

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3714977A (en) * 1971-07-23 1973-02-06 United Aircraft Corp Method and apparatus for the production of directionally solidified castings
US5915452A (en) * 1995-06-07 1999-06-29 Howmet Research Corporation Apparatus for removing cores from castings
US5779809A (en) * 1995-12-26 1998-07-14 General Electric Company Method of dissolving or leaching ceramic cores in airfoils
US6739380B2 (en) * 2002-04-11 2004-05-25 Rolls-Royce Corporation Method and apparatus for removing ceramic material from cast components
US8056607B2 (en) * 2008-06-24 2011-11-15 Pcc Airfoils, Inc. Method of casting metal articles
US8409493B2 (en) * 2009-08-06 2013-04-02 Rolls-Royce Corporation Systems and methods for leaching a material from an object
US20120222961A1 (en) * 2010-12-30 2012-09-06 Michel Shawn Smallwood System, method, and apparatus for leaching cast components

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9808862B2 (en) 2013-12-19 2017-11-07 United Technologies Corporation System and methods for removing core elements of cast components
US10099276B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having an internal passage defined therein
US9968991B2 (en) 2015-12-17 2018-05-15 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
US10099284B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having a catalyzed internal passage defined therein
US10137499B2 (en) 2015-12-17 2018-11-27 General Electric Company Method and assembly for forming components having an internal passage defined therein
US10118217B2 (en) 2015-12-17 2018-11-06 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US9975176B2 (en) 2015-12-17 2018-05-22 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
US9987677B2 (en) 2015-12-17 2018-06-05 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10046389B2 (en) 2015-12-17 2018-08-14 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10099283B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having an internal passage defined therein
US9579714B1 (en) 2015-12-17 2017-02-28 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
US10150158B2 (en) 2015-12-17 2018-12-11 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10286450B2 (en) 2016-04-27 2019-05-14 General Electric Company Method and assembly for forming components using a jacketed core
US10335853B2 (en) 2016-04-27 2019-07-02 General Electric Company Method and assembly for forming components using a jacketed core
US10981221B2 (en) 2016-04-27 2021-04-20 General Electric Company Method and assembly for forming components using a jacketed core
CN106735108A (en) * 2017-01-04 2017-05-31 中国航空工业集团公司北京航空材料研究院 A kind of turbine hollow blade depoling frock
CN107127323A (en) * 2017-06-13 2017-09-05 西安交通大学 A kind of method and apparatus for improving ceramic core depoling efficiency
CN107866550A (en) * 2017-12-21 2018-04-03 西安欧中材料科技有限公司 A kind of ceramic core removal methods of aero-engine hollow blade
EP3536418A1 (en) * 2018-03-09 2019-09-11 United Technologies Corporation Casting core removal through thermal cycling
US20190275583A1 (en) * 2018-03-09 2019-09-12 United Technologies Corporation Casting core removal through thermal cycling
US10710154B2 (en) * 2018-03-09 2020-07-14 Raytheon Technologies Corporation Casting core removal through thermal cycling
CN112191829A (en) * 2020-10-10 2021-01-08 中国航发北京航空材料研究院 Core removing kettle and method for precisely casting hollow blade core

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