Abblasventilsystem für Gasturbinenmotor

Details

Veröffentlichungs-Nr.

EP4741645

Anmeldetag

4. November 2025

Veröffentlichung

13. Mai 2026

Rechtsraum

EP

Abstract

A bleed valve system (80, 200, 300) for a gas turbine engine (10, 100, 100', 210, 240, 270), the bleed valve system (80, 200, 300) including a bleed valve (202, 202', 82, 222, 252, 262, 274, 310), a bleed valve exhaust duct (204, 304) fluidly connected to the bleed valve (202, 202', 82, 222, 252, 262, 274, 310), and a bleed valve exhaust nozzle (206, 306) fluidly connected to the bleed valve exhaust duct (204, 304), wherein the bleed valve exhaust duct (204, 304) and the bleed valve exhaust nozzle (206, 306) are fluidly separated from an exhaust nozzle of the gas turbine engine (10, 100, 100', 210, 240, 270) when the bleed valve system (80, 200, 300) is installed in the gas turbine engine (10, 100, 100', 210, 240, 270).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA