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Partition damper seal configurations for segmented internal cooling hardware
Free accessEuropean Patent Office | 2024| -
PROCÉDÉ ET MODULE DE DÉTECTION DE L'ÉTAT D'UN DISPOSITIF D'ACCOUPLEMENT, TURBOMACHINE ET AÉRONEF ASSOCIÉS
Free accessEuropean Patent Office | 2024| -
Turbine with a shroud ring around rotor blades and method of limiting leakage of working fluid in a turbine
Free accessEuropean Patent Office | 2024| -
Closed Brayton cycle power generation device with multi-layer flow guide sleeve structure
Free accessEuropean Patent Office | 2024| -
300MW reaction type single-cylinder shaft row one-time reheating air turbine and operation method
Free accessEuropean Patent Office | 2024| -
ROTOR ASSEMBLY WITH ACTIVE DAMPING FOR GAS TURBINE ENGINES
Free accessEuropean Patent Office | 2024| -
Turbine engine stator control valve comprising a continuous and free sealing ring
Free accessEuropean Patent Office | 2024| -
GAS TURBINE ENGINE WITH TURBINE VANE CARRIER COOLING FLOW PATH
Free accessEuropean Patent Office | 2024| -
AIRFOIL ASSEMBLY WITH FIBER-REINFORCED COMPOSITE RINGS AND TOOTHED EXIT SLOT
Free accessEuropean Patent Office | 2024| -
CLEARANCE CONTROL SYSTEM AND METHOD FOR A GAS TURBINE COMPRESSOR
Free accessEuropean Patent Office | 2024| -
Aircraft engine having stator vanes made of different materials
Free accessEuropean Patent Office | 2024| -
GAS TURBINE ENGINE STATOR VANE FORMED OF CERAMIC MATRIX COMPOSITES AND HAVING ATTACHMENT FLANGES
Free accessEuropean Patent Office | 2024| -
VANE ARC SEGMENT WITH FLANGE HAVING STEP AND METHOD OF FABRICATING A VANE ARC SEGMENT
Free accessEuropean Patent Office | 2024| -
Turbomachine including a rotor connected to a plurality of blades having an arm and a seal
Free accessEuropean Patent Office | 2024| -
Integral cooling system for turbine casing and guide vanes in aeroengine
Free accessEuropean Patent Office | 2024| -
TURBINE ASSEMBLY OF AN AXIAL-FLOW TURBINE AND AXIAL-FLOW TURBINE
Free accessEuropean Patent Office | 2024| -
Steam inlet structure with steam turbine connected in parallel with second steam source
Free accessEuropean Patent Office | 2024| -
BLADE EDGE PLATES, BLADE RING, IMPELLER DISK, AND GAS TURBINE ENGINE
Free accessEuropean Patent Office | 2024| -
PRE-CERAMIC THERMAL BARRIER FOR GAS TURBINE ENGINE COMPONENTS
Free accessEuropean Patent Office | 2024| -
HIGH-EFFICIENCY AXIAL FLOW TURBINE HAVING IMPROVED FUNCTION
Free accessEuropean Patent Office | 2024| -
PLATFORM FLOW TURNING ELEMENTS FOR GAS TURBINE ENGINE COMPONENTS
Free accessEuropean Patent Office | 2024| -
SPOKED THERMAL CONTROL RING FOR A HIGH PRESSURE COMPRESSOR CASE CLEARANCE CONTROL SYSTEM
Free accessEuropean Patent Office | 2024|
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