Inventor

CZAPLA LIONEL

FR43 patents

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

CZAPLA LIONEL

AIRBUS OPERATIONS SAS

Assembly forming an acoustic insulator

Thrust reverser system having limited aerodynamic disturbance

Turbofan engine comprising a system for blocking the flow path of the bypass stream comprising veils

Jet engine comprising a nacelle equipped with reverser flaps

Jet engine comprising a nacelle equipped with reverser flaps

Aircraft pylon comprising a tubular primary structure including at least one twin-walled pipe, and aircraft comprising at least one such pylon

Device for coupling a propulsion system to an engine pylon of an aircraft, and corresponding aircraft

Aircraft nacelle comprising a connection between ducts comprising flanges which are oriented towards the interior, and aircraft comprising at least one nacelle of this type

Propeller propulsion system with T-shaped chassis

Propeller propulsion unit for an aircraft

Jet engine comprising a nacelle equipped with a reverser system comprising inner doors and outer flaps

Assembly for an aircraft nacelle and comprising a support panel, a thermal protection element and a fastening system

Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means

Aircraft nacelle comprising a sealed box structure and a door which opens the box structure to the outside

Device for coupling a propulsion system to an engine pylon of an aircract, and corresponding aircraft

Propulsion assembly for an aircraft

Aircraft propulsive assembly comprising a nacelle with a t-shaped frame

Aircraft propulsion assembly equipped with a thrust-reversing device comprising at least one inflatable barrier, and aircraft comprising at least one such propulsion assembly

Bypass turbofan including a system for blocking the secondary flow including veils

Turbojet including a nacelle equipped with a thrust reverser system including a hinged structure

Aircraft propulsion system having a linear electric motor

Dihydrogen supply system for an aircraft engine

Reinforced lattice structure and aircraft comprising at least one such structure

Dihydrogen supply system for an aircraft engine

Aircraft propulsion system comprising an internal fixed structure with a discharge slot

Powerplant for an aircraft

Propulsion assembly for an aircraft

Propulsion unit with propeller and electric motor comprising an adapted primary structure, and aircraft having at least one such propulsion unit

Powerplant for an aircraft

Casing system containing a heat exchanger for reheating dihydrogen

Aircraft cowl locking system

Acoustic absorption structure comprising a liquid drainage system and propulsive assembly comprising such an acoustic absorption structure

Turbofan comprising a system comprising a screen for closing off the bypass duct

Turbofan comprising a system comprising flexible screens for closing off the bypass duct

Turbojet engine comprising a nacelle equipped with reverser flaps

AIRBUS SAS

Propulsion assembly for an aircraft

Aircraft comprising at least one hydrogen supply device and at least one sealed container, in which at least one item of equipment of said hydrogen supply device is positioned

Propulsive assembly for aircraft

Aircraft propulsion unit comprising at least one pressure relief device and aircraft having at least one such propulsion unit

Powerplant for an aircraft

Module for a dihydrogen supply system for an aircraft engine

Heat exchanger limiting the risk of contamination between two fluids and aircraft comprising at least one such heat exchanger

Aircraft comprising a hydrogen supply device incorporating a hydrogen heating system positioned in the fuselage of the aircraft