Systems and methods for controlling blade tip clearances
Systems and methods for controlling blade tip clearances
MODULE DE TURBOMACHINE EQUIPE D'UNE HELICE ET D'AUBES DE STATOR DEPORTEES
MODULE DE TURBOMACHINE EQUIPE D'UNE HELICE ET D'AUBES DE STATOR DEPORTEES
Device and method for influencing the temperatures in inner ring segments of a gas turbine
DEVICE AND METHOD FOR INFLUENCING THE TEMPERATURES IN INNER RING SEGMENTS OF A GAS TURBINE
Endwall component for a turbine stage of a gas turbine engine
Endwall component for a turbine stage of a gas turbine engine
Aircraft propulsion assembly comprising an air flow valve with a variable flow rate
AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN AIR FLOW VALVE WITH A VARIABLE FLOW RATE
ENGINE TURNING MOTOR VIA PNEUMATIC OR HYDRAULIC MOTOR
Engine turning motor via pneumatic or hydraulic motor
ENGINE TURNING MOTOR VIA PNEUMATIC OR HYDRAULIC MOTOR
Movement-limiting device for a turbine engine and associated method
MOVEMENT-LIMITING DEVICE FOR A TURBINE ENGINE AND ASSOCIATED METHOD
Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same
Propeller ring made of composite material for a turbomachine
Turbine engine assembly and method of manufacturing thereof
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF
Turbine engine assembly and method of manufacturing thereof
Simplified pitch actuation system for a turbine engine propeller
FLEXIBLE BAND ELECTRICAL COMPONENT MOUNTS AND METHODS
Flexible band electrical component mounts and methods
TURBOFAN-TRIEBWERK MIT ÜBERDRUCKKLAPPE AN EINER IM SEKUNDÄRSTROMKANAL LIEGENDEN VERKLEIDUNG
Method of monitoring at least one freewheel of a rotary wing aircraft, and an aircraft
METHOD OF MONITORING AT LEAST ONE FREEWHEEL OF A ROTARY WING AIRCRAFT, AND AN AIRCRAFT
Airfoil assembly with ceramic airfoil pieces and seal
AIRFOIL ASSEMBLY WITH CERAMIC AIRFOIL PIECES AND SEAL
GUIDING RING FOR VARIABLE-PITCH BLADES AND METHOD OF MOUNTING SAID RING
Guiding ring for variable-pitch blades and method of mounting said ring
IN-FLIGHT HYBRID-ELECTRIC ENGINE SHUTDOWN AND RESTART