Gas turbine component

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F - Mech Eng,Light,Heat,Weapons

01

D

F01D 11/12 (2006.01) B22F 5/04 (2006.01) B22F 7/00 (2006.01) C22C 1/08 (2006.01) F01D 25/14 (2006.01) F01D 25/24 (2006.01) F16L 59/14 (2006.01)

Patent

CA 2547619

The invention relates to a gas turbine component, namely a static gas turbine component, especially for an aircraft engine. According to the invention, the static gas turbine component is at least partially formed from metal dross.

L'invention concerne un composant de turbine à gaz, notamment un composant statique de turbine à gaz, en particulier destiné à un groupe motopropulseur. Selon l'invention, le composant de turbine à gaz statique est constitué, au moins dans une zone, d'une mousse métallique.

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