Verbindungsanordnung für Gehäuse einer Gasturbine

Details

Veröffentlichungs-Nr.

EP2884057

Aktenzeichen

EP14195746

Anmeldetag

2. Dezember 2014

Veröffentlichung

12. April 2017

Erteilung

12. April 2017

Rechtsraum

EP

IPC

F01D21/04F01D25/24// F04D29/52F04D29/64

Abstract

A joint assembly between a first gas turbine engine casing and a second gas turbine casing, the first gas turbine engine casing having a plurality of circumferentially spaced attachment points and the second gas turbine casing having a plurality of circumferentially spaced attachment points for securing the first gas turbine casing and the second gas turbine casing together, wherein each attachment point on the first gas turbine casing is circumferentially offset from a respective attachment point on the second gas turbine casing, and connected by a flexure member that permits limited relative movement of the attachment point on the first gas turbine engine casing and its respective attachment point on the second gas turbine casing.

Anmelder

Firma

Rolls-Royce Deutschland Ltd & Co KG

Land

🇩🇪 Deutschland

Fachgebiete