Impacts of the Additive Manufacturing Process on the Roughness of Engine Scale Vanes and Cooling Channels

Author:

Wildgoose Alexander J.1,A. Thole Karen2,Subramanian Ramesh3,Kersting Lisa4,Kulkarni Anand5

Affiliation:

1. Pennsylvania State University , State College, PA 16801

2. Pennsylvania State University State College, PA 16801

3. Siemens Energy , Orlando, FL, 32826

4. Siemens Energy , Berlin 10553 , Germany

5. Siemens Corporation , Charlotte, NC 28273

Abstract

Abstract By leveraging the additive manufacturing (AM) platform, development time and costs for turbine component testing can be reduced relative to traditional investment casting. Surface roughness is a key characteristic of the additive manufacturing process that can impact flow, heat transfer, and mechanical integrity of printed components. There are multiple design and build considerations that result in variability in surface roughness, especially when additively fabricating complicated three-dimensional vanes and internal cooling passages. This study characterizes the surface roughness of internal cooling passages, vanes, and flat external surface samples made using additive manufacturing, specifically the direct metal laser sintering process. The samples were manufactured with various wall thicknesses, layer thicknesses, build locations, build directions, and on different AM machines. A combination of computed tomography scanning and optical profilometry was used to evaluate surface roughness levels. The data indicate that the dominant factors in roughness for a given layer thickness are a function of wall thickness, build location, and build direction.

Publisher

ASME International

Subject

Mechanical Engineering

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1. Roughness Related to Cooling Performance of Channels Made Through Additive Manufacturing;Journal of Turbomachinery;2024-01-16

2. Variability in additively manufactured turbine cooling features;Journal of the Global Power and Propulsion Society;2023-07-27

3. Influences of Laser Incidence Angle and Wall Thickness on Additive Components;Journal of Turbomachinery;2023-06-26

4. Advanced Gas Turbine Cooling for the Carbon-Neutral Era;International Journal of Turbomachinery, Propulsion and Power;2023-06-24

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