EP 0964206 B1 20041208 - Variable geometry gas turbine combustor chamber
Title (en)
Variable geometry gas turbine combustor chamber
Title (de)
Brennkammer einer Gasturbine mit verstellbarer Geometrie
Title (fr)
Chambre de combustion de turbine à gaz à géométrie variable
Publication
Application
Priority
FR 9807409 A 19980611
Abstract (en)
[origin: EP0964206A1] The combustion chamber has pilot (11) and main (12) combustion zones with separate injectors (3,7;4,8) for fuel and oxidant, the assembly being held under pressure (P1) inside a housing (14). The system incorporates a regulating mechanism for the main oxidant flow which reacts to the pressure difference between the internal pressure (P1) and the atmospheric pressure outside the housing.
IPC 1-7
IPC 8 full level
CPC (source: EP US)
F23R 3/26 (2013.01 - EP US); F23R 3/346 (2013.01 - EP US)
Designated contracting state (EPC)
BE DE GB IT NL
DOCDB simple family (publication)
EP 0964206 A1 19991215; EP 0964206 B1 20041208; DE 69922437 D1 20050113; DE 69922437 T2 20051208; FR 2779807 A1 19991217; FR 2779807 B1 20000713; JP 2000009319 A 20000114; JP 4435331 B2 20100317; US 6263663 B1 20010724
DOCDB simple family (application)
EP 99401204 A 19990518; DE 69922437 T 19990518; FR 9807409 A 19980611; JP 16130699 A 19990608; US 33019999 A 19990611