SYSTEM AND METHOD FOR PROTECTING STRENGTH OF MOTOR PYLON
Detección de sobrevelocidad de una turbina libre por medición con medidor de par
IMMERSED CORE FLOW INLET BETWEEN ROTOR BLADE AND STATOR VANE FOR AN UNDUCTED FAN GAS TURBINE
IMMERSED CORE FLOW INLET BETWEEN ROTOR BLADE AND STATOR VANE FOR AN UNDUCTED FAN GAS TURBINE
Immersed core flow inlet between rotor blade and stator vane for an unducted fan gas turbine
Rotary assembly of an aeronautical turbomachine comprising an added-on fan blade platform
DUCTED FAN ENGINE, ARRAY OF DUCTED FAN ENGINES, AND AIRCRAFT
DUCTED FAN ENGINE, ARRAY OF DUCTED FAN ENGINES, AND AIRCRAFT
SYSTEME DE CHANGEMENT DE PAS DES PALES D’UNE SOUFFLANTE D’UN ENSEMBLE PROPULSIF
ROTOR HANGING TOOL, ROTOR SUPPORT JIG, ROTOR LIFTING METHOD, AND ROTARY MACHINE DISASSEMBLY METHOD
TURBOPROPULSEUR APTE A FOURNIR UNE FONCTION D’EOLIENNE DE SECOURS ET PROCEDE DE MISE EN ŒUVRE
TURBOPROPULSEUR APTE A FOURNIR UNE FONCTION D'EOLIENNE DE SECOURS ET PROCEDE DE MISE EN ŒUVRE
TURBOPROPULSEUR APTE A FOURNIR UNE FONCTION D’EOLIENNE DE SECOURS ET PROCEDE DE MISE EN ŒUVRE
Method of regulating air pressure in anti-icing system
METHOD OF REGULATING AIR PRESSURE IN ANTI-ICING SYSTEM
LOW INFRARED SIGNATURE EXHAUST THROUGH ACTIVE FILM COOLING ACTIVE MIXING AND ACITVE VANE ROTATION
Method for balancing a turbofan engine or other rotating system
Method for Balancing a Turbofan Engine or Other Rotating System
Unducted propeller turboshaft engine provided with a reinforcing shell integrating pipe segments
UNDUCTED PROPELLER TURBOSHAFT ENGINE PROVIDED WITH A REINFORCING SHELL INTEGRATING PIPE SEGMENTS
Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply
AIRCRAFT COMPRISING A TURBINE ENGINE INCORPORATED INTO THE REAR FUSELAGE WITH VARIABLE SUPPLY
GAS TURBINE SYSTEM AND MOVABLE BODY INCLUDING THE SAME
GAS TURBINE SYSTEM AND MOVABLE BODY INCLUDING THE SAME
Turbogenerator for aircraft, comprising an improved oil system
TURBOGENERATOR FOR AIRCRAFT, COMPRISING AN IMPROVED OIL SYSTEM
HIGH IMPACT-RESISTANT, REINFORCED FIBER FOR LEADING EDGE PROTECTION OF AERODYNAMIC STRUCTURES
High impact-resistant, reinforced fiber for leading edge protection of aerodynamic structures
Joint cover with improved manifold block for duct leak detection system
STRÖMUNGSPROFIL UND DAMIT AUSGESTATTETE MECHANISCHE MASCHINE