EP 0813669 A1 19971229 - THERMAL SHIELD ARRANGEMENT FOR GAS TURBINE COMBUSTION CHAMBERS
Title (en)
THERMAL SHIELD ARRANGEMENT FOR GAS TURBINE COMBUSTION CHAMBERS
Title (de)
HITZESCHILD-ANORDNUNG FÜR EINE GASTURBINEN-BRENNKAMMER
Title (fr)
AGENCEMENT D'ECRAN THERMIQUE POUR CHAMBRES DE COMBUSTION DE TURBINES A GAZ
Publication
Application
Priority
- DE 19508111 A 19950308
- EP 9600860 W 19960301
Abstract (en)
[origin: DE19508111A1] In order to cool down as efficiently as possible the hot surface of the thermal shield (1) that surrounds the burner of a gas turbine ring-shaped combustion chamber, in particular in the area of the burner outlet (3), a cooling air flow (10) ejected in the direction of the outlet over a continuous web (8) at the edge of the outlet is guided by a guiding rib (9). The guiding rib (9) is substantially parallel to the web (8) and has at the side of the combustion chamber a bent end, so that the cooling air flow that enters the gap between the web and the guiding rib is deflected there towards the hot surface (2b) of the thermal shield (1).
IPC 1-7
IPC 8 full level
CPC (source: EP US)
F23R 3/10 (2013.01 - EP US); F23R 3/283 (2013.01 - EP US)
Citation (search report)
See references of WO 9627765A1
Designated contracting state (EPC)
DE FR GB
DOCDB simple family (publication)
DE 19508111 A1 19960912; CA 2214691 A1 19960912; DE 59603160 D1 19991028; EP 0813669 A1 19971229; EP 0813669 B1 19990922; US 5894732 A 19990420; WO 9627765 A1 19960912
DOCDB simple family (application)
DE 19508111 A 19950308; CA 2214691 A 19960301; DE 59603160 T 19960301; EP 9600860 W 19960301; EP 96906722 A 19960301; US 91312297 A 19970908