Aerofoil structure and a method of making a rib for an aerofoil structure
A method for making a rib for an aerofoil structure, the aerofoil structure including a skin component, the method including the steps of scanning the inner surface of the skin component to determine the surface profile thereof, providing a rib having a rib body and a rib foot protruding from the body, machining a foot surface profile into the rib foot, the foot surface profile being arranged to complement the skin inner surface profile where the rib foot is intended to abut the skin component.
1. A method for making a rib for an aerofoil structure, the aerofoil structure comprising a skin component, the method comprising the steps of scanning the inner surface of the skin component to determine the surface profile thereof, providing the rib having a rib body and a rib foot protruding from the body, using scanned inner surface profile data from the skin component obtained from the step of scanning the inner surface of the skin component to machine a foot surface profile into the rib foot, the foot surface profile being arranged to complement the skin inner surface profile where the rib foot is intended to abut the skin component.
2. A method for making a rib according to claim 1 , in which the rib has a plurality of rib feet, one or more of the feet having a foot surface profile and comprising the step of machining the or each respective foot surface profiles of the feet to complement the skin inner surface profile where the respective foot is intended to abut the skin component.
3. A method for making a rib according to claim 2 in which the aerofoil structure comprises two skin components and the foot surface profiles of the feet complement, respectively the inner surface profiles of the regions of the skin components where the feet are intended to abut.
4. A method for making a rib according to claim 1 -in which the aerofoil structure has a spar component attached to the skin component, the method comprising the step of forming the rib to complement an inner surface profile of the spar component.
5. A method for making a rib according to claim 1 in which the aerofoil structure comprises an additional skin component having an inner surface profile, the skin components each having an outer surface profile, wherein the aerofoil structure further comprises first and second spar components arranged between the skin components whereby a space envelope is defined by the inner surface profiles of the skin components, and wherein the step of providing the rib comprises providing a rib having a rib body and a plurality of rib feet and the step of machining the foot surface profile comprises machining multiple foot surface profiles to complement the inner surface profiles of the skin components.
6. The method for making a rib according to claim 1 , further the action of providing a plurality of ribs, wherein the ribs are part of a monolithic component.