Hot gas segment arrangementA hot gas segment arrangement (20), especially for a combustion chamber of a gas turbine, comprises at least one hot gas segment (22), which is removably mounted on a carrier (21), and is subjected at…DRIVE·May 7·2 min readFollowF01D9/02ALSTOM TECHNOLOGY LTD [CH]
Combustor transitionThe disclosure relates combustor transition (24) adapted to guide combustion gases in a hot gas flow path (15) extending between a can combustor (2) and a first stage of turbine (3) in a gas turbine (…DRIVE·Apr 30·2 min readFollowF01D9/02ALSTOM TECHNOLOGY LTD [CH]
Combustor transitionThe disclosure relates combustor transition (24) adapted to guide combustion gases in a hot gas flow path (15) extending between a can combustor (2) and a first stage of turbine (3) in a gas turbine (…DRIVE·Apr 30·2 min readFollowF01D9/02ALSTOM TECHNOLOGY LTD [CH]
Blocked nozzle detection and remedial method and systemSystem and method for controlling a stuck nozzle system installed between first and second turbines connected in series to a compressor. The method includes determining whether the nozzle system is st…DRIVE·Nov 2·1 min readFollowF01D9/02NUOVO PIGNONE SPA [IT]
Aerodynamically shaped support and/or cladding element in the bypass of a gas turbine engineThe element has a supporting structure radially extended between inner and outer walls of a bypass duct and including a front edge part (7) and a rear edge part (8). A connecting rod (9) connects the …DRIVE·Sep 14·2 min readFollowF01D9/02ROLLS ROYCE DEUTSCHLAND [DE]
