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1. WO2010094277 - GAS TURBINE MACHINE COMPRISING A DAMPED BLADE CLUSTER

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Publication Number WO/2010/094277
Publication Date 26.08.2010
International Application No. PCT/DE2010/000196
International Filing Date 22.02.2010
IPC
F01D 25/06 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
DNON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
25Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
04Antivibration arrangements
06for preventing blade vibration
F01D 9/04 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
DNON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
9Stators
02Nozzles; Nozzle boxes; Stator blades; Guide conduits
04forming ring or sector
CPC
F01D 25/06
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
25Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
04Antivibration arrangements
06for preventing blade vibration
F01D 5/16
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
5Blades; Blade-carrying members
12Blades
14Form or construction
16for counteracting blade vibration
F01D 9/041
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
9Stators
02Nozzles; Nozzle boxes; Stator blades; Guide conduits ; , e.g. individual nozzles
04forming ring or sector
041using blades
F05D 2260/96
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
2260Function
96Preventing, counteracting or reducing vibration or noise
Applicants
  • MTU AERO ENGINES GMBH [DE]/[DE] (AllExceptUS)
  • HARTUNG, Andreas [DE]/[DE] (UsOnly)
Inventors
  • HARTUNG, Andreas
Common Representative
  • MTU AERO ENGINES GMBH [DE]/[DE]
Priority Data
10 2009 010 185.323.02.2009DE
Publication Language German (DE)
Filing Language German (DE)
Designated States
Title
(DE) GASTURBINENMASCHINE MIT EINEM GEDÄMPFTEN SCHAUFELCLUSTER
(EN) GAS TURBINE MACHINE COMPRISING A DAMPED BLADE CLUSTER
(FR) TURBINE À GAZ
front page image
Abstract
(DE)
Eine Gasturbinenmaschine umfasst mindestens einen Schaufelcluster (10), in dem mehrere Schaufelblätter (12) an einem gemeinsamen Innenring (14) und/oder Außenring (16) angeordnet sind. Der Schaufelcluster (10) weist wenigstens einen Hohlraum (18) auf, wobei im Inneren des Hohlraums (18) mehrere Dämpfungskörper (20, 22, 24) vorgesehen sind, die sich unabhängig voneinander relativ zu den Wänden des Hohlraums (18) und relativ zueinander bewegen können.
(EN)
A gas turbine machine comprises at least one blade cluster (10), in which several blades (12) are arranged on a common inner ring (14) and/or outer ring (16). The blade cluster (10) has at least one hollow space (18), inside which several damping elements (20, 22, 24) are provided that can be independently moved relative to the walls of the hollow space (18) and relative to one another.
(FR)
L'invention concerne une turbine à gaz comprenant au moins un groupe d'aubes (10) dans lequel sont disposées plusieurs aubes (12) sur une bague intérieure (14) et/ou une bague extérieure (16) communes. Le groupe d'aubes (10) présente au moins une cavité (18) à l'intérieur de laquelle sont placés plusieurs éléments d'amortissement (20, 22, 24) qui peuvent se déplacer indépendamment les uns des autres vis-à-vis des parois de la cavité (18) et les uns par rapport aux autres.
Also published as
DE102009010185
Latest bibliographic data on file with the International Bureau
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