Process for manufacturing composite material structures with collapsible tooling
A process for manufacturing stiffened structures ( 11 ) in composite materials formed by an outer skin ( 13 ) and a plurality of stiffeners or stringers ( 15 ) the cross-section of which has a closed form delimiting an inner opening ( 23 ), comprising the following steps: a) Providing a shaping tool ( 31 ); b) Providing auxiliary male tools ( 37 ) of a material capable of varying its volume due to the effect of temperature and/or pressure, covered with membranes suitable for curing c) Providing stiffeners or stringers ( 15 ); d) Arranging the stiffeners or stringers ( 15 ) in the tool ( 31 ) and the auxiliary male tools ( 37 ) in their inner openings ( 23 ); e) Laminating the outer skin ( 13 ); f) Curing the stiffened structure ( 11 ) with high temperature and pressure; g) Removing the auxiliary male tools ( 37 ) after reducing their volume; h) Separating the cured stiffened structure ( 11 ) from the tool ( 31 ). The invention also relates to the auxiliary male tools.
1 . A process for manufacturing stiffened structures ( 11 ) in composite materials formed by an outer skin ( 13 ) and a plurality of stiffeners or stringers ( 15 ) whose cross-section has a broken contour with at least one flange ( 17 ) joined to the skin ( 13 ), said contour delimiting an inner opening ( 23 ), characterized in that it comprises the following steps:
a) Providing a tool ( 31 ) with an outer surface with a shape similar to that of structure ( 11 ) on the side of the stiffeners or stringers ( 15 ), including slots ( 33 ) to house the stiffeners or stringers ( 15 );
b) Providing auxiliary male tools ( 37 ) consisting of elements made of a material capable of varying its volume due to the effect of temperature and/or pressure, shaped with a geometry similar to the inner opening ( 23 ) of the stiffeners or stringers and covered with membranes suitable for curing composite materials;
c) Providing stiffeners or stringers ( 15 ) in fresh or cured condition;
d) Arranging the stiffeners or stringers ( 15 ) in the slots ( 33 ) of tool ( 31 ), adapting them to the geometry of the slots and arranging in their inner openings ( 23 ) the auxiliary male tools ( 37 ), adapted to their geometry;
e) Laminating the outer skin ( 13 ) on the surface formed by the tool ( 31 ), the stiffeners or stringers ( 15 ) and the auxiliary male tools ( 37 );
f) Curing the stiffened structure ( 11 ) at high temperature and pressure conditions;
g) Removing the auxiliary male tools ( 37 );
h) Separating the cured stiffened structure ( 11 ) from the tool ( 31 ).
2 . A process for manufacturing stiffened structures ( 11 ) in composite materials according to claim 1 , characterized in that the stiffened structure ( 11 ) is a tubular piece.
3 . A process for manufacturing stiffened structures ( 11 ) in composite materials according to claim 1 , characterized in that the stiffeners or stringers ( 15 ) have an omega shape.
A process for manufacturing stiffened structures ( 11 ) in composite materials according to claim 1 , characterized in that in step d) the stiffeners or stringers are arranged in the slots ( 33 ) of the tool ( 31 ) having previously coupled the auxiliary male tools ( 37 ) in their inner openings ( 23 ).
5 . A process for manufacturing stiffened structures ( 11 ) in composite materials according to claim 1 , characterized in that step e) is carried out by a head ( 35 ) of a taping machine.
6 . A process for manufacturing stiffened structures ( 11 ) in composite materials according to claim 1 , characterized in that before step f) a caul-plate ( 43 ) is placed on the skin ( 13 ).
7 . An auxiliary male tool ( 37 ) used in a process for manufacturing stiffened structures ( 11 ) according to claim 1 , characterized in that it is made of polyurethane.
8 . An auxiliary male tool ( 37 ) used in a process for manufacturing stiffened structures ( 11 ) according to claim 1 , characterized in that it is made of polystyrene.