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.

Saved in:
Bibliographic Details
Main Authors STEINHARDT ERICH, MEIER REINHOLD
Format Patent
LanguageEnglish
Published 31.05.2007
Subjects
Online AccessGet full text

Cover

Loading…
More Information
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.
Bibliography:Application Number: US20040582930