Turbinenschaufelrahmenanordnung

Details

Veröffentlichungs-Nr.

EP4818481

Anmeldetag

5. März 2026

Veröffentlichung

7. Oktober 2026

Rechtsraum

EP

IPC

F01D25/24, F01D9/04, F01D11/00

Abstract

A turbine vane frame assembly (200) defining an axial direction, a radial direction, and a circumferential direction includes an outer frame (202) extending from a forward end to an aft end (106, 212, 216, 220, 224), the outer frame (202) including a first connector (234) at the forward end and a second connector (236, 280, 290, 300) at the aft end (106, 212, 216, 220, 224), an outer fairing (204) extending from a forward end to an aft end (106, 212, 216, 220, 224), the outer fairing (204) connected to the outer frame (202) by the first connector (234) and the second connector (236, 280, 290, 300), an inner frame (204, 206) extending from a forward end to an aft end (106, 212, 216, 220, 224), the inner frame (204, 206) including a third connector (238) at the forward end and a fourth connector (240) at the aft end (106, 212, 216, 220, 224), and an inner fairing (208) extending from a forward end to an aft end (106, 212, 216, 220, 224), the inner fairing (208) connected to the inner frame (204, 206) by the third connector (238) and the fourth connector (240), wherein the first connector (234) provides support in the circumferential direction to the outer fairing (204), the second connector (236, 280, 290, 300) provides support in the axial direction to the outer fairing (204), and the fourth connector (240) provides support in both the circumferential direction and axial direction to the inner fairing (208).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA

Fachgebiete