METODO DE FABRICACION DE LARGUERILLOS CON FORMA DE "T" PARA UN AVION Y HERRAMIENTA DE CURADO USADA EN EL MISMO
The invention relates to a method for manufacturing T-shaped aircraft stringers, in which the T-shape stringers have a web and a flange and wherein the method includes: a first step of hot forming a carbon fiber laminate in order to achieve semi-stringers with a geometry with a L-shaped cross-sectio...
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Main Authors | , , |
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Format | Patent |
Language | Spanish |
Published |
28.02.2013
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a method for manufacturing T-shaped aircraft stringers, in which the T-shape stringers have a web and a flange and wherein the method includes: a first step of hot forming a carbon fiber laminate in order to achieve semi-stringers with a geometry with a L-shaped cross-section, a second step of joining the two L-shaped hot formed semi-stringers in order to form a T-shaped stringer, a third step in which the resulting T-shaped stringer is co-cured on a cured lining with an adhesive line separating said stringer and said lining, and a fourth step of curing the T-shaped stringer produced inside a vacuum bag using invar alloy brackets as curing tools. The method is characterized in that the invar alloy brackets are radial cut, eliminating a portion thereof that covers the stringer flange in order to define an invar alloy part having no flange. |
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Bibliography: | Application Number: ES20100030940 |