Method of manufacturing a component of a rotary machine and component manufactured using said method
US-2017341178-A1 · Nov 30, 2017 · US
US9375818B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9375818-B2 |
| Application number | US-201313916923-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 13, 2013 |
| Priority date | Jun 13, 2012 |
| Publication date | Jun 28, 2016 |
| Grant date | Jun 28, 2016 |
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A manufacturing method, including: given a predetermined finished part geometry, providing a sacrificial structure preform that simultaneously contains the finished part geometry, minimizes material that must be removed from the sacrificial structure preform to achieve the finished part geometry during machining, and has a sufficient stiffness to resist a machining force that will be applied during machining without allowing the finished part geometry to be compromised; and machining the sacrificial structure preform to achieve the finished part geometry. The manufacturing method also includes preliminarily estimating a stiffness of the finished part geometry and the machining force that will be applied during machining.
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What is claimed is: 1. A manufacturing method, comprising: providing a predetermined finished part geometry; prior to machining a sacrificial structure preform to achieve the finished part geometry, estimating a stiffness of the finished part geometry and a machining force that will be applied while machining the sacrificial structure preform to achieve the finished part geometry; prior to machining the sacrificial structure preform to achieve the finished part geometry, estimating a stiffness of a sacrificial structure preform, wherein the stiffness of the sacrificial structure preform exceeds the stiffness of the finished part geometry, and wherein the sacrificial structure preform simultaneously contains the finished part geometry and additional material, minimizes the additional material that must be removed from the sacrificial structure preform to achieve the finished part geometry, and has a sufficient stiffness to resist the machining force that will be applied without allowing the finished part geometry to be compromised; modifying the additional material of the sacrificial structure preform based on the estimating the stiffness steps; providing the sacrificial structure preform; and machining the sacrificial structure preform to achieve the finished part geometry by applying the machining force. 2. The manufacturing method of claim 1 , wherein the estimating the stiffness steps each comprise estimating the stiffness using one or more of finite element modeling, closed form computation, and physical experimentation. 3. The manufacturing method of claim 1 , wherein the estimating the machining force comprises estimating the machining force using one or more of cutting process modeling and physical experimentation. 4. The manufacturing method of claim 1 , wherein the sacrificial structure preform comprises a plurality of sacrificial stiffening structures one of coupled to and integrally formed with the finished part geometry. 5. The manufacturing method of claim 4 , wherein the plurality of sacrificial stiffening structures comprise a plurality of sacrificial stiffening structures selected from a group consisting of: buttresses, ribs, flanges, corrugations, steps, ridges, beads, and combinations of any thereof. 6. A manufacturing method, comprising: providing a predetermined finished part geometry; prior to machining a sacrificial structure preform to achieve the finished part geometry, using finite element analysis, estimating a stiffness of the finished part geometry and a machining force that will be applied while machining the sacrificial structure preform to achieve the finished part geometry; prior to machining the sacrificial structure preform to achieve the finished part geometry, using finite element analysis, estimating a stiffness of a sacrificial structure preform, wherein the stiffness of the sacrificial structure preform exceeds the stiffness of the finished part geometry, and wherein the sacrificial structure preform simultaneously contains the finished part geometry and additional material, minimizes the additional material that must be removed from the sacrificial structure preform to achieve the finished part geometry, and has a sufficient stiffness to resist the machining force that will be applied without allowing the finished part geometry to be compromised; modifying the additional material of the sacrificial structure preform based on the estimating the stiffness steps; providing the sacrificial structure preform; and machining the sacrificial structure preform to achieve the finished part geometry by applying the machining force. 7. The manufacturing method of claim 6 , wherein the estimating the machining force comprises estimating the machining force using one or more of cutting process modeling and physical experimentation. 8. The manufacturing method of claim 6 , wherein the sacrificial structure preform comprises a plurality of sacrificial stiffening structures one of coupled to and integrally formed with the finished part geometry. 9. The manufacturing method of claim 8 , wherein the plurality of sacrificial stiffening structures comprise a plurality of sacrificial stiffening structures selected from a group consisting of: buttresses, ribs, flanges, corrugations, steps, ridges, beads, and combinations of any thereof.
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