Inventor

BELMONTE OLIVIER

FR67 patents

⚠️ This page may combine multiple inventors who share the name “BELMONTE OLIVIER”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

BELMONTE OLIVIER

BELMONTE OLIVIER

Aircraft turbomachine fan comprising a balancing flange concealed by the inlet cone

Turbomachine rotor disk

Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted

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

Turbine engine fan comprising a balancing system with blind holes for accommodating masses

Unducted propeller with variable pitch blades for a turbomachine

Annular flange for fastening a rotor or stator element in a turbomachine

Fan blade

Turbine engine stator wheel and a turbine or a compressor including such a stator wheel

Turbomachine fan

Device for de-icing a turbomachine separator

Retaining ring assembly and supporting flange for said ring

Annular flange for fastening a rotor or stator element

Turbine engine part forming a compressor stator or a turbine nozzle, and method for fabricating same

Cooling device for cooling the slots of a turbomachine rotor disk downstream from the drive cone

Set of rotor disks for a turbine engine

Deoiler layout

Stator vane for 3D composite blower

Low-pressure turbine

Rotor for a gas turbine engine comprising a rotor spool and a rotor ring

Blade retention disk

SAFRAN AIRCRAFT ENGINES

Guide device for variable pitch stator vanes of a turbine engine, and a method of assembling such a device

Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub

Radial locking of a blade pivot with adjustable orientation for a turbomachine fan hub

Aircraft turbomachine with mechanical reducer and contrarotative turbine

Radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fan

Variable pitch blade pivot for a turbine engine fan hub

Reduction gear having an epicyclic gear train for a turbine engine

Device for recovering lubrication oil ejected by centrifugal effect in a turbine engine

Turbomachine module provided with a propeller and offset stator vanes

Modularity of an aircraft turbomachine

Blade pivot with adjustable orientation and protected integrity for a turbomachine fan hub

Aircraft turbine engine with an off-axis propeller

Recovery of lubricating oil from a reduction gear of an aircraft turbine engine

Pressurising of lubrication chambers in a turbomachine with counter-rotating turbine

Assembly for turbine machine with open rotor contra-rotating propellers, comprising a small duct for the passage of ancillaries

SNECMA

Device for attaching a stator vane to a turbomachine annular casing, turbojet engine incorporating the device and method for mounting the vane

System for changing the pitch of the blades of a propeller

Turbine engine comprising a means for measuring the speed and torque of a shaft of the turbine engine and method for monitoring said shaft

Device for guiding variable pitch diffuser vanes of a turbine engine

Unlockable device for axially arresting a sealing ring with which an aircraft turbomachine module rotor wheel makes contact

Hydraulic and electrical interface ring for a turbine engine

Radial control shaft for a device for controlling the pitch of fan blades of a turbine engine having an unducted fan, and a method of mounting such a shaft

Device for supplying and distributing fluid

Device for transferring oil between two repositories rotating relative to each other, and propeller turbomachine for an aircraft with such a device

Guidance of turbine engine shafts

Device for supplying hydraulic fluid to a ram and mechanism for controlling the pitch of the blades of a turbine engine propeller comprising the ram

Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted

Device for the blind coupling of fluidic, electrical or similar supplies, to a receiving control mechanism

AUBIN STEPHAN

Turbojet compressor