Wouter Balk

Method for producing a transmission shaft, preferably for an accessory box system of an aircraft turbomachine

TURBINE ENGINE SUPPORT PART OF HYBRID STRUCTURE

System for changing the pitch of the contra-rotating propellers of a turboshaft engine

Device for suspending a turbojet engine

Thrust reverser having locking/unlocking cascade vanes

AIRCRAFT PROPULSION ASSEMBLY

Composite material FADEC box support

Assembly for attaching the hangers from which an aircraft propulsion unit is suspended

Axisymmetric part for an aviation turbine engine rotor

Turbojet engine case, notably intermediate case

Gas turbine engine comprising means for axially retaining a fan of the engine

Acoustic panel for a turbojet engine nacelle, with in-built fasteners

AIRCRAFT TURBOJET ENGINE FAN CASING

AIRFLOW-STRAIGHTENING STRUCTURE FOR THE NACELLE OF AN AIRCRAFT ENGINE

AIR INLET DUCT FOR A TURBOJET NACELLE

Fitting including a composite material bracket and a stiffener

Mechanism for variable adjustment of blades for a system of contra-rotating propellers, and a system of contra-rotating propellers comprising at least one such mechanism

Turboprop provided with a blade-positioning device

Contra-rotating propeller system for an aircraft turbine engine

Movable actuator device for controlling the pitch of fan blades of a turboprop

Device for controlling the pitch of fan blades of a turboprop

Device with counter-rotating propellers having a propeller pitch altering means

System of contra-rotating propellers driven by a planetary gear train providing a balanced distribution of torque between the two propellers

Device adapted to be fitted with propeller blades

Aircraft propulsion system

DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF A TURBOPROP

Attachment of a multiflow turbojet engine to an aircraft

Connecting a propulsion system to a structural element of an aircraft

Pylon for suspending an engine beneath an aircraft wing