Gas turbine component
The invention relates to a gas turbine component, namely static gas turbine component, especially for an aircraft engine. According to the invention, the static gas turbine component is formed at least region-wise of metal foam.
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
31.05.2007
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a gas turbine component, namely static gas turbine component, especially for an aircraft engine. According to the invention, the static gas turbine component is formed at least region-wise of metal foam. |
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Bibliography: | Application Number: US20040582930 |