SEAL IN A GAS TURBINE ENGINE AND CORRESPONDING CREATING METHOD

A seal (200) in a gas turbine engine (100) includes a shim base (202) and a honeycomb structure having a number of cavities (204) are formed as a single unitary structure, for example by using additive manufacturing. Furthermore, a method of creating a seal (200) in a gas turbine engine (100), the m...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	KIRTLEY, Kevin Richard, SEZER, Ibrahim, LACY, Benjamin Paul
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MAKING METALLIC POWDER MANUFACTURE OF ARTICLES FROM METALLIC POWDER MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS POWDER METALLURGY STEAM ENGINES TRANSPORTING WEAPONS WORKING METALLIC POWDER
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A seal (200) in a gas turbine engine (100) includes a shim base (202) and a honeycomb structure having a number of cavities (204) are formed as a single unitary structure, for example by using additive manufacturing. Furthermore, a method of creating a seal (200) in a gas turbine engine (100), the mehtod comprising the steps of forming a shim base (202) and forming a plurality of cavities (204) on the shim base (202) as a single unitary structure with the shim base (202).