Jacketed Core Casting for Complex Internal Passages
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Solution Overview
Problem
Existing methods for forming components with internal passages are costly, time-consuming, and prone to fragility, especially when using ceramic cores, and struggle to produce complex or curved passage designs efficiently.
Innovation Solution
A method involving the formation of a jacketed core with a hollow structure and an inner core, where the precursor core is shaped to match the internal passage, and the jacketed core is positioned within a mold for casting, allowing the molten material to absorb the hollow structure and define the internal passage, using additive manufacturing for precision and reducing core fragility.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If traditional ceramic cores are used to form internal passages, then the internal passage can be formed in the component, but the cores are fragile and difficult/expensive to produce and handle without damage
Solution Approach 1:
The patent applies composite materials by combining a ceramic core with a metallic jacket to create a hybrid core structure. The ceramic portion maintains its ability to define the internal passage geometry, while the metallic jacket provides mechanical strength and damage resistance. This composite approach resolves the contradiction by integrating the advantages of both materials: the ceramic's geometric precision and the metal's structural integrity, making the core both functional and manufacturable.
Solution Approach 2:
The patent changes the physical and chemical parameters of the core structure by applying a metallic coating or jacket to the ceramic core. This parameter change transforms the core from a purely ceramic, fragile structure to a composite structure with enhanced mechanical properties. The metallic layer modifies the core's strength, toughness, and handling characteristics while preserving the ceramic's ability to define the internal passage shape.
2Productivity
If drilling processes are used to form internal passages, then passages can be created in the component, but the process is time-consuming and expensive
Solution Approach 1:
The patent applies preliminary action by forming the internal passage geometry during the initial casting process itself, rather than requiring subsequent drilling operations. The ceramic core is positioned in the mold cavity before the molten metal is introduced, so the passage is created as the metal solidifies around the core. This eliminates the need for time-consuming post-casting drilling operations, significantly improving productivity and reducing total manufacturing time.
Solution Approach 2:
The patent merges the core formation function with the casting process. Instead of separating the passage creation into distinct steps (casting followed by drilling), the method combines these operations by using the ceramic core as a permanent mold feature during casting. The internal passage is formed simultaneously with the component body, integrating multiple manufacturing functions into a single operation and eliminating redundant process steps.
3Adaptability or versatility
If drilling processes are used to form internal passages, then passages can be created, but complex curvatures required by certain designs cannot be produced
Solution Approach 1:
The patent applies copying by using the ceramic core itself as a negative template or mold for the internal passage. The core is shaped to precisely match the desired passage geometry, including complex curvatures, and this geometry is copied into the final component during casting. The molten metal takes the shape of the space around the core, accurately reproducing the passage design without the limitations of drilling tool paths or tool access constraints.
4Reliability
If investment casting molds are used, then components can be formed, but the ceramic cores lack sufficient strength to withstand injection of wax material to form patterns
Solution Approach 1:
The patent applies composite materials by combining a ceramic core with a metallic jacket to create a hybrid core structure. The ceramic portion maintains its ability to define the internal passage geometry, while the metallic jacket provides mechanical strength and damage resistance. This composite approach resolves the contradiction by integrating the advantages of both materials: the ceramic's geometric precision and the metal's structural integrity, making the core both functional and manufacturable.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
This approach reduces fragility issues, enables the production of complex and curved internal passages, and lowers manufacturing costs by using a reinforced core that can handle more intricate designs and larger components effectively.
Implementation Method 1
introducing a component material in a molten state into a cavity of the mold such that the component material in the molten state at least partially absorbs the hollow structure from a portion of the jacketed core within the cavity
Data Source
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AI summary
A method (1200) of forming a component (80) having an internal passage (82) defined therein includes forming (1202) a precursor core (524) having a shape corresponding to a shape of the internal passage (82), and forming (1204) a hollow structure (320) around the precursor core (524). The method also includes removing (1206) the precursor core (524) from within the hollow structure (320), and disposing (1208) an inner core (324) within the hollow structure (320) to form a jacketed core (310). The method further includes positioning (1210) the jacketed core (310) with respect to a mold (300), and introducing (1212) a component material (78) in a molten state into a cavity (304) of the mold (300), such that the component material (78) in the molten state at least partially absorbs the hollow structure (320) from a portion (315) of the jacketed core (310) within the cavity (304). Additionally, the method includes cooling (1214) the component material (78) in the cavity (304) to form the component (80). The inner core (324) defines the internal passage (82) within the component (80).