EP 0870990 B1 20030507 - Gas turbine with toroidal combustor
Title (en)
Gas turbine with toroidal combustor
Title (de)
Gasturbine mit toroidaler Brennkammer
Title (fr)
Turbine à gaz avec chambre de combustion toroidale
Publication
Application
Priority
EP 97810167 A 19970320
Abstract (en)
[origin: EP0870990A1] The combustion chamber (1) has at least one annular toroidal interior (8) actively connected to burners (5) around the periphery of the combustion chamber. The toroidal interior has a hot gas duct (11) branching off in a peripheral direction and positioned on the flow plane of a turbine (3) placed after the gas turbo group. The end of the hot gas duct has guide-blades (12) co-operating with the turbine. The annular toroidal interior is enclosed in a shell (13) in which flows a coolant (15) in the intermediate space (14) formed. Combustion air (7) belonging to a plenum (6) feeds the burners.
IPC 1-7
IPC 8 full level
CPC (source: EP US)
F23R 3/425 (2013.01 - EP US); F23R 3/52 (2013.01 - EP US)
Designated contracting state (EPC)
DE GB
DOCDB simple family (publication)
EP 0870990 A1 19981014; EP 0870990 B1 20030507; CN 1149354 C 20040512; CN 1195088 A 19981007; DE 59710046 D1 20030612; US 6192669 B1 20010227
DOCDB simple family (application)
EP 97810167 A 19970320; CN 98104195 A 19980320; DE 59710046 T 19970320; US 4491098 A 19980320