Inventor

SERGHINE CAMEL

FR28 patents

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

SERGHINE CAMEL

SAFRAN HELICOPTER ENGINES

Assistance device for a free-turbine engine of an aircraft having at least two free-turbine engines

Turbomachine designed to operate in turning gear mode

Propulsion unit with selective coupling means

Integration of a phase-change material for limiting the temperature of fuel from an electronic module

Turbomachine designed to operate in turning gear mode

Turboshaft engine comprising a controlled mechanical coupling device, helicopter equipped with such a turboshaft engine, and method for optimising the zero-power super-idle speed of such a helicopter

Electrical machine of a turbomachine comprising a rotor cooled by a cooling channel

Electric machine with phase change material for a turbomachine starter/generator

Propulsion unit with foldable propeller blades and method for folding the blades

Propulsion unit with foldable propeller blades and method for stopping the propeller in an indexed angular position

Propulsion unit with foldable propeller blades and method for folding the blades

Device and method for testing the integrity of a helicopter turbine engine rapid restart system

Turbogenerator for aircraft, comprising an improved oil system

Hydraulic device for emergency starting a turbine engine, propulsion system of a multi-engine helicopter provided with one such device, and corresponding helicopter

Aircraft electrical machine with improved heat transfer by means of a phase change material and associated method

Electric machine with device for forcibly demagnetising permanent magnets

Hybrid propulsion system and method for controlling such a system

Hybrid propulsion chain for an aircraft comprising an auxiliary mechanical drive system

Pneumatic device for rapidly reactivating a turbine engine, architecture for a propulsion system of a multi-engine helicopter provided with such a device, and corresponding helicopter

Method for starting an aircraft engine

Hybrid-electric propulsion architecture and method for dissipating electrical energy in such an architecture

Propeller for an aircraft propulsion assembly, propulsion assembly, and method for the use of such a propulsion assembly

Magnetohydrodynamic generator

Removable pack for reactivating a turboshaft engine, architecture for a multi-engine system for propelling a helicopter, provided with such a pack, and corresponding helicopter

SAFRAN

Electrical machine winding having improved cooling

Multi-rotor aircraft propulsion system with reconfigurable electric network

TURBOMECA

Hybrid cutoff member for an electric circuit

SNECMA

System and method for emergency starting of an aircraft turbomachine