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Ceramic matrix composite airfoil structures for a gas turbine engine

BERCZIK DOUGLAS M / SUCIU GABRIEL L / MERRY BRIAN D / IOANNIS ALVANOS / DYE CHRISTOPHER M

A Ceramic Matrix Composite (CMC) airfoil segment for a gas turbine engine includes a box-shape fiber geometry which defines a rectilinear pressure side bond line and a rectilinear suction side bond line.

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Ceramic matrix composite airfoil structures for a gas turbine engine

BERCZIK DOUGLAS M / SUCIU GABRIEL L / MERRY BRIAN D / IOANNIS ALVANOS / DYE CHRISTOPHER M

Abstract

Ceramic matrix composite airfoil structures for a gas turbine engine

BERCZIK DOUGLAS M / SUCIU GABRIEL L / MERRY BRIAN D / IOANNIS ALVANOS / DYE CHRISTOPHER M

Abstract

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Titel:

Ceramic matrix composite airfoil structures for a gas turbine engine

Beteiligte:

BERCZIK DOUGLAS M (Autor:in) / SUCIU GABRIEL L (Autor:in) / MERRY BRIAN D (Autor:in) / IOANNIS ALVANOS (Autor:in) / DYE CHRISTOPHER M (Autor:in)

Erscheinungsdatum:

13.03.2018

Medientyp:

Patent

Format:

Elektronische Ressource

Sprache:

Englisch

Klassifikation:

IPC: F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / C04B Kalk , LIME

FREEMAN TED J / USKERT RICHARD C | Europäisches Patentamt | 2019

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