Alarm method for avoiding inappropriate rudder bar actuation
AssigneeAirbus Operations GmbH
InventorsBernard Honnons, Stephane Boissenin
Life of this patent
Estimating the term…
Abstract
A method for producing a connector, in particular for repair, in particular in the field of aviation and aerospace, including the steps of: providing a base layer; attaching a first layer of fibre composite material having a first rigidity to the base layer; attaching a second layer of fibre composite material having a second rigidity to the first layer, offset therefrom, the second rigidity being greater than the first rigidity; and riveting the first layer to the base layer and riveting the second layer to the first layer and to the base layer.
Claims12
A method for producing a connector, comprising the steps of:
- providing a base layer;
- attaching a first layer of fibre composite material having a first rigidity to the base layer;
- attaching a second layer of fibre composite material having a second rigidity to the first layer, offset therefrom, the second rigidity being greater than the first rigidity;
- and
- riveting the first layer to the base layer and riveting the second layer to the first layer and to the base layer.
A connector for an aircraft or spacecraft, comprising:
- a base layer;
- a first layer of fibre composite material having a first rigidity being attached to the base layer;
- a second layer of fibre composite material having a second rigidity being attached to the first layer, offset therefrom, the second rigidity being greater than the first rigidity;
- and
- a plurality of rivets connecting the first layer to the base layer and connecting the second layer to the first layer and the base layer.
Dependencies are inferred from the claim text.