Alenia Aeronautica S.p.a.

Alenia Aermacchi S.p.a.

Massimo Riccio

Salvatore Russo

Sabato Inserra Imparato

Vincenzo De Vita

Generoso Iannuzzo

Erika Calvi

Luigi Capasso

Giovanni Sagnella

Giovanni Lanfranco

Marco Fassero

Nicola Miani

Rosario Pecora

Leonardo Lecce

Silvestro Barbarino

Antonio Concilio

Salvatore Ameduri

Ernesto Rinaldi

A method of manufacturing a wing structure includes laying a plurality of layers of preimpregnated material on a first mould half and on a second mold half so as to form a first fresh skin and a second fresh skin of the wing structure. A plurality of layers of preimpregnated material are laid in succession on a shaped apparatus to form a fresh leading edge skin of the wing structure. Fresh spars of preimpregnated material are formed. A wedgelike body of expanded plastics material is formed, this body being designed to be interposed between the first and second skins at the trailing edge of the wing structure. The fresh spars are positioned in a coordinated way on the first fresh skin, removable support members also positioned next to the spars. The second mold half is turned over on to the first mold half so as to position the second fresh skin on the spars and the supports, to produce a fresh wing structure. The fresh wing structure is subjected to a polymerization cycle, using a vacuum bag.

Method of manufacturing an integral profile monolithic wing structure

A wing-flap assembly includes a flap made up of a plurality of flap sections, in which each flap section is connected to the preceding one in a rotatable manner, and one or more actuator devices adapted to control the rotation of the flap sections. Each actuator device includes an extended element made of shape memory alloy and an arch-shaped framework made of elastic material, to which the extended element is fixedly connected under tension. Each end of the extended element is fixed to a respective end of the arch-shaped framework. At least one of the actuator devices is connected at one end to the first of the flap sections, and on the other side it is adapted to be connected to a wing structure.

Actuator device based on a shape memory alloy, and a wing flap assembly fitted with such an actuator device

A leading edge structure includes two or more multilayer panels at least partially overlapping and suitably curved with at least partially congruent concavities. Each multilayer panel includes at least the following three layers: a first metal foil layer metal foil, a second intermediate layer of fiber-glass securely fixed to the first layer, and a third metal honeycomb layer securely fixed to the second layer.

Leading edge for aircraft wings and empennages

Growing community of inventors

Caserta, Italy

Massimo Riccio