EP 2562361 B1 20151209 - Structural composite fan exit guide vane for a turbomachine
Title (en)
Structural composite fan exit guide vane for a turbomachine
Title (de)
Strukturverbundfanleitschaufel für eine Turbomaschine
Title (fr)
Aube directrice de sortie de fan composite structurelle pour turbomachine
Publication
Application
Priority
US 201113217372 A 20110825
Abstract (en)
[origin: EP2562361A1] A structural composite fan exit guide vane assembly uses single component monolithic structural guide vane segments (200) to provide airflow correction and structural support in a gas turbine engine. The segments (200) comprise an inner diameter shroud (258), an outer diameter shroud (256) and a plurality of vanes (252,254) connecting the shrouds (256,258).
IPC 8 full level
F01D 9/04 (2006.01)
CPC (source: EP US)
F01D 9/042 (2013.01 - EP US); F05D 2220/36 (2013.01 - EP US); F05D 2300/603 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 2562361 A1 20130227; EP 2562361 B1 20151209; EP 2562361 B2 20190410; US 2013052004 A1 20130228
DOCDB simple family (application)
EP 12181806 A 20120824; US 201113217372 A 20110825