Inventor

JORET JEAN-PHILIPPE

FR29 patents

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

JORET JEAN-PHILIPPE

SAFRAN NACELLES

Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure

Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing method

Front frame and deflection grid of a thrust reverser of an aircraft nacelle

Thrust reverser for an aircraft bypass turbojet engine nacelle

Air inlet of a turbomachine nacelle including a circulation conduit of a hot air flow between a movable upstream part and a fixed downstream part

Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing method

Thrust reverser with door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior

Fastening of an exhaust cone in a turbomachine nozzle

Nacelle for an aircraft propulsion assembly comprising a flap for closing a recess for the passage of an actuator

Fastening of an exhaust cone in a turbomachine nozzle

Exhaust cone for a turbomachine

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

Rear assembly of a turbojet engine nacelle including a fireproof sealing device

AIRCELLE SA

Turbojet engine nacelle including a device for absorbing circumferential stresses

Composite panel having a built-in duct

Thrust reverser having an aerodynamic coupling for a front frame

Front frame for a cascade thrust reverser structure

Flattened nacelle of a turbojet engine

Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure

Control device for a turbojet engine thrust reverser, blocking the reverser

Air inlet structure for a turbojet engine nacelle of laminar type

JORET JEAN-PHILIPPE

Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device

Turbojet engine nacelle with translatable upstream cowl

CARUEL PIERRE

Assembly for an aircraft turbojet engine comprising a thrust reversal cowl

Guiding system for aircraft nacelle maintenance

VAUCHEL GUY BERNARD

Structural nacelle

JORET JEAN PHILIPPE

Turbojet engine nacelle

VAUCHEL GUY

Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator

SAFRAN CERAM

Fastening of an exhaust cone in a turbomachine turbine