EP 0841520 A3 19991103 - Gas turbine engine combustor
Title (en)
Gas turbine engine combustor
Title (de)
Gasturbinenbrennkammer
Title (fr)
Chambre de combustion pour une turbine à gaz
Publication
Application
Priority
GB 9623195 A 19961107
Abstract (en)
[origin: EP0841520A2] A combustor for a gas turbine engine has a fuel nozzle located in the upstream end thereof and is positioned within a cylinder coaxial with said nozzle. The cylinder comprises at its downstream end an annular flange extending from the cylinder in a generally radial direction. The flange has a plurality of cooling air apertures radially extending therethrough so as to direct cooling air along the face of an adjacent heatshield. <IMAGE>
IPC 1-7
IPC 8 full level
CPC (source: EP)
F23R 3/10 (2013.01); F23R 3/283 (2013.01); F23D 2214/00 (2013.01)
Citation (search report)
- [X] US 4914918 A 19900410 - SULLIVAN DENNIS J [US]
- [X] DE 4427222 A1 19960208 - BMW ROLLS ROYCE GMBH [DE]
- [X] DE 19508111 A1 19960912 - BMW ROLLS ROYCE GMBH [DE]
- [X] US 4934145 A 19900619 - ZEISSER MELVIN H [US]
Designated contracting state (EPC)
AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE
DOCDB simple family (publication)
EP 0841520 A2 19980513; EP 0841520 A3 19991103; EP 0841520 B1 20030312; DE 69719671 D1 20030417; DE 69719671 T2 20030814; GB 9623195 D0 19970108
DOCDB simple family (application)
EP 97308248 A 19971017; DE 69719671 T 19971017; GB 9623195 A 19961107