Kohlenstoffdichtungsfederhalteanordnung

Details

Veröffentlichungs-Nr.

EP3346097

Aktenzeichen

EP18150902

Anmeldetag

9. Januar 2018

Veröffentlichung

29. April 2020

Erteilung

29. April 2020

Rechtsraum

EP

IPC

F01D11/00F02C7/28F16J15/34

Abstract

A seal assembly for a turbine engine extends along a center axis and includes a seal support (70) and a seal carrier (72) configured to translate relative the seal support (70). A seal (80) is connected to the seal carrier (72) and a spring (74) is disposed between the seal support (70) and the seal carrier (72). A spring carrier (76) is disposed between the spring (74) and the seal support (70). A first end of the spring is connected to the spring carrier (76) and the spring carrier (76) is connected to the seal support (70). The spring (74) includes a second end disposed opposite the first end of the spring. The second end of the spring (74) contacts the annular seal carrier (72).

Anmelder

Firmen

Raytheon Technologies Corporation
United Technologies Corporation

Land

🇺🇸 USA

Fachgebiete