EP 2383518 A2 20111102 - Tangential combustor
Title (en)
Tangential combustor
Title (de)
Tangentialbrennkammer
Title (fr)
Chambre de combustion tangentielle
Publication
Application
Priority
US 76838510 A 20100427
Abstract (en)
A combustion section for a gas turbine includes a casing (32) defining a chamber, a plurality of combustor cans (34) disposed in the casing and oriented in an annular pattern, and a plurality of transition pieces (36) each coupled with one of the combustor cans. The transition pieces direct products of combustion from the combustor cans into contact with rotating buckets of the gas turbine. Each of the transition pieces is angled in two planes to effect turning of the products of combustion and to shorten the gas turbine.
IPC 8 full level
CPC (source: EP US)
F23R 3/425 (2013.01 - EP US); F23R 3/58 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
EP 2383518 A2 20111102; EP 2383518 A3 20141119; CN 102252345 A 20111123; JP 2011232022 A 20111117; US 2011259015 A1 20111027
DOCDB simple family (application)
EP 11163440 A 20110421; CN 201110116512 A 20110427; JP 2011089656 A 20110414; US 76838510 A 20100427