Inventor

BOILEAU PATRICK

FR31 patents

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

BOILEAU PATRICK

SAFRAN NACELLES

Nacelle air intake and nacelle comprising such an air intake

Nacelle air intake and nacelle comprising such an air intake

Nacelle air intake and nacelle comprising such an air intake

Grid-type thrust reverser for turbojet engine

Assembly and method for handling an aircraft propulsion unit

Aircraft propulsion unit and method for ventilating an engine enclosure

Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle

Propulsion unit for aircraft comprising an assembly box-type structure in the six o&#39;clock position

Propulsion unit including lifting points disposed on thrust reverser cylinder supports

Aircraft nacelle and associated air intake

Drive unit for an aircraft having lifting points, and carriages for supporting such a unit

Upper axial retention for a cascade-type thrust reverser with sliding vanes of D-shaped structure

Nacelle for an aircraft turbojet engine with hybrid air inlet and fan cowl

Turbojet nacelle provided with a thrust reverser, including cut-outs to avoid the movable slat of an aircraft wing

Defrosting and acoustic treatment device for an air intake lip of a turbojet engine nacelle

Aircraft propulsion unit

Air inflow lip for turbojet nacelle

Thrust reverser with a c-shaped movable structure for an aircraft propulsion unit, and method for maintaining the same

Bypass propulsion unit, comprising a thrust reverser with movable cascades

Thrust reverser with cascades of mobile vanes, comprising a rear structure supporting the cascades of vanes and incorporating an acoustic function

System for installing and removing a propulsion unit on a pylon of an aircraft

Nacelle rear assembly for a turbojet engine comprising a suspension cradle

Thrust reverser for nacelle of aircraft turbofan

Propulsion unit for an aircraft and method for opening a movable cowl of said propulsion unit

Nacelle rear assembly for a turbojet engine comprising a cradle for a core-type mast

AIRCELLE SA

Turbojet engine nacelle having a variable nozzle

Thrust reverser device

Thrust reverser of a turbojet engine nacelle, comprising control cylinders of movable cowls and a variable secondary nozzle

Thrust reverser of a turbofan pod comprising a single control for movable cowlings and a variable nozzle

Air intake structure for turbojet engine nacelle

Propulsion unit for an aircraft

Propulsion unit for aircraft comprising an assembly box-type structure in the six o'clock position