EP 0795682 B1 20000503 - Blade containment system for a turbofan engine
Title (en)
Blade containment system for a turbofan engine
Title (de)
Berstschutzeinrichtung für ein Bläsertriebwerk
Title (fr)
Anneau de protection pour une turbosoufflante
Publication
Application
Priority
GB 9605284 A 19960313
Abstract (en)
[origin: EP0795682A1] Casing assembly for a gas turbine engine comprising an annular cross section casing around which a plurality of flexible material are wound. One or more rigid panels are positioned between the wound flexible material and the annular casing. The rigid panel provides enhanced containment of a detached fan blade or part of a fan blade by distributing the load of the detached blade across the wound flexible material. <IMAGE>
IPC 1-7
IPC 8 full level
F01D 21/04 (2006.01)
CPC (source: EP)
F01D 21/045 (2013.01); F05B 2260/3011 (2013.01); F05D 2300/224 (2013.01); F05D 2300/603 (2013.01)
Designated contracting state (EPC)
DE FR GB
DOCDB simple family (publication)
EP 0795682 A1 19970917; EP 0795682 B1 20000503; DE 69701831 D1 20000608; DE 69701831 T2 20000817; GB 9605284 D0 19960515
DOCDB simple family (application)
EP 97300729 A 19970205; DE 69701831 T 19970205; GB 9605284 A 19960313