Hot Gas Path Component With Arced Cooling and Hybrid Manufacture
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Solution Overview
Problem
The increasing cost of materials and difficulty in manipulating them pose challenges in producing gas turbomachine components that can withstand significant temperatures and maintain a desired lifespan, as conventional methods are inefficient and costly.
Innovation Solution
The approach involves forming a turbomachine component using a combination of conventional forging or casting for one portion and additive manufacturing for another portion, where the latter includes cooling features, with the two portions being bonded together, allowing for the use of less expensive materials with similar thermal expansion coefficients, and incorporating arced cooling pathways to enhance heat transfer.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If conventional methods are used to produce gas turbomachine components with desired lifespan, then thermal endurance is achieved, but production cost increases significantly
Solution Approach 1:
The component is divided into two distinct portions: a first portion formed by conventional forging or casting methods, and a second portion formed by additive manufacturing. This segmentation allows each portion to be optimized for its specific manufacturing requirements, reducing overall production costs while maintaining the thermal endurance needed for component lifespan
Solution Approach 2:
The invention uses two different materials with similar thermal expansion coefficients but different cost and manufacturing characteristics. The first material is suitable for conventional manufacturing, while the second material is optimized for additive manufacturing and includes cooling features. This composite approach enables cost reduction without compromising the thermal performance required for desired lifespan
2Duration of action of stationary object
If expensive materials with high heat endurance are used, then component lifespan is extended, but material cost and manipulation difficulty increase
Solution Approach 1:
The component is divided into two distinct portions: a first portion formed by conventional forging or casting methods, and a second portion formed by additive manufacturing. This segmentation allows each portion to be optimized for its specific manufacturing requirements, reducing overall production costs while maintaining the thermal endurance needed for component lifespan
Solution Approach 2:
The cooling features are localized in the second portion of the component where thermal management is most critical. By concentrating cooling capabilities in specific areas rather than using expensive heat-enduring materials throughout the entire component, the invention reduces material costs and manipulation difficulty while extending component lifespan through effective heat management
3Ease of manufacture
If simple cooling features are incorporated, then manufacturing is easier, but heat transfer effectiveness is reduced
Solution Approach 1:
The additive manufacturing process enables the creation of three-dimensional arced cooling pathways that follow the curvature of the component surface. These pathways extend into the depth of the component, creating a multi-dimensional cooling network that significantly enhances heat transfer effectiveness compared to simple surface-level cooling features, while maintaining ease of manufacture through additive processes
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 method reduces production costs while maintaining thermal performance by utilizing additive manufacturing to create complex cooling features with similar thermal expansion characteristics, effectively managing heat transfer and extending the lifespan of gas turbomachine components.
Implementation Method 1
incorporating arced cooling pathways to enhance heat transfer
Implementation Method 2
allows coolant to flow through the component, effectively transferring heat away from the component
Implementation Method 3
bonding comprises heating the member and the layer
Data Source
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AI summary
Various embodiments of the disclosure include a turbomachine component (2) and methods of forming such a component (2). Some embodiments include a turbomachine component (2) including: a first portion (4) including at least one of a stainless steel or an alloy steel; and a second portion (6) joined with the first portion (4), the second portion (6) including a nickel alloy including an arced cooling feature (10) extending therethrough, the second portion (6) having a thermal expansion coefficient substantially similar to a thermal expansion coefficient of the first portion (4), wherein the arced cooling feature (10) is located within the second portion (6) to direct a portion of a coolant to a leakage area (18) of the turbomachine component (2).