Frédéric CHELIN

Engine assembly of an aircraft including a display unit

Panel for the acoustic treatment comprising hot air ducts and at least one annular channel

Process for the destruction of a blind fastener and device for its implementation

Air intake of an aircraft nacelle that incorporates a reinforced lip with a defrost system by joule-effect

Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structure

Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air

Part for and method of repairing a damaged structure, in particular an airframe skin, and a repair kit for implementing it

Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes

Aircraft cover including means for limiting the scoop phenomena of pneumatic type

AIRCRAFT COVER INCLUDING MEANS FOR LIMITING THE SCOOP PHENOMENA OF ELECTROMAGNETIC TYPE

AIRCRAFT NACELLE INCLUDING A CONTINUE JOINT AREA BETWEEN AN OUTER WALL AND A FRONT FRAME

Aircraft nacelle including at least one radial partition between two conducts

Aircraft nacelle including a rear frame inclined to the rear

Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle

Aircraft nacelle comprising a reinforced outer wall

Aircraft nacelle including an optimised acoustic processing system

Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle

Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment

Air outlet system for aircraft leading edge

Turbine engine for aircraft

AIRCRAFT PROPULSION UNIT THAT COMPRISES AN EXHAUST PIPE WITH A SCALLOPED TRAILING EDGE

Turbine engine for aircraft