A layered heating system for heating a leading edge component of an aircraft .

An aircraft leading edge ice protection system.

The beak of the edge of attack of an aircraft is a very important feature for the take-off and landing because it is intended to improve the gliding of air over the wing and therefore the aerodynamics of the aircraft.

The beak of the edge of attack of an aircraft is a very important feature for the take-off and landing because it is intended to improve the gliding of air over the wing and therefore the aerodynamics of the aircraft.

A layered heating system for heating a leading edge component of an aircraft .

A method making a leading edge component for an aircraft.

An aircraft leading edge ice protection system.

An actuation system configured to deploy a high-lift device on a leading edge of an aircraft wing.

The invention also relates to a method of manufacturing a leading edge (1) with a metallic reinforcement (2) for aircraft made of composite material.

A fin having a leading edge, a trailing edge opposing the leading edge, and a plurality of leading holes substantially centered along a leading axis.

Each rotor blade (10) includes an elongate central body (14) that has a leading edge (16) and a flap (20) along the leading edge (16).

A leading edge component (30) for an aircraft.

Each blade includes a leading edge (13) opposite a trailing edge (15).

A metallic leading edge protective strip (12) adapted to provide impact protection for a leading edge of an airfoil of a turbomachine.

The concave leading edge (24) is provided with a coextensive protrusion (26) and the convex leading edge is provided with a coextensive recess (27).