Multi-component composite structures
View Patent ↗A composite assembly that can be cured to form a multi-component composite structure which does not have micro cracks along the boundaries between the various components. The composite assembly includes a structural component and a moldable component wherein the coefficients of thermal expansion of the structural component and the moldable component at the interface or boundary between the two components are such that micro cracks do not form along the interface when the composite assembly is cured to form the multi-component composite structure.
1. A multiple-component composite window frame assembly which is curable to form a window frame structure in which an elliptical wall extends perpendicularly from a base plate, said window frame assembly-comprising:
a structural component which forms a lower portion of said base plate, said structural component comprising a modified unidirectional continuous fiber body that comprises alternating layers of unidirectional continuous fibers and multi-directional continuous fibers, said modified unidirectional continuous fiber body having a top and an interior side, said structural component further comprising a multi-directional continuous fiber body that comprises multi-directional continuous fibers and an uncured thermosetting resin, said multi-directional continuous fiber body having a top and an interior side wherein the interior sides of said modified unidirectional continuous fiber body and said multi-directional continuous fiber body are in contact with each other and wherein the tops of said modified unidirectional continuous fiber body and said multi-directional continuous fiber body form a top of the lower portion of said base plate; and
a moldable component which comprises a moldable body comprising an uncured thermosetting resin and discontinuous fibers, said moldable body forming an upper portion of said base plate wherein the upper portion of said base plate has a bottom and a top, said moldable body also forming the elliptical wall that extends from said top of the upper portion of said base plate, said moldable component being in contact with said structural component so as to form an interface between said moldable component and said structural component, said interface being located where the bottom of the upper portion of said base plate contacts the top of the lower portion of said base plate and wherein micro cracks do not form along said interface during curing of said window fame assembly to form said window frame structure.
2. A multi-component composite window frame assembly according to claim 1 wherein said multi-directional continuous fibers in the modified unidirectional continuous fiber body or the multi-directional continuous fiber body comprise woven fibers.
3. A multi-component composite window frame assembly according to claim 1 wherein said discontinuous fibers comprise randomly oriented segments of unidirectional tape.
4. A multi-component window frame assembly according to claim 1 wherein said uncured thermosetting resin in said structural component is an epoxy resin and wherein said uncured thermosetting resin in said moldable component is an epoxy resin.
5. A multi-component window frame assembly according to claim 4 wherein the epoxy resin in said structural component is the same as the epoxy resin in said moldable component.
6. A multi-component window frame assembly according to claim 1 wherein the amount of uncured thermosetting resin in said structural component is between 20 to 45 weight percent of the overall weight of said structural component and wherein the amount of uncured thermosetting resin in said moldable component is between 20 to 45 weight percent of the overall weight of said moldable component.
7. A multi-component composite window frame structure which is formed by curing a multi-component composite window frame assembly according to claim 1 .
8. A multi-component composite window frame structure according to claim 7 wherein said multi-directional continuous fibers in the modified unidirectional continuous fiber body or the multi-directional continuous fiber body comprise woven fibers.
9. A multi-component composite window frame structure according to claim 7 which is an aircraft window frame.
10. A multi-component composite window frame structure according to claim 7 wherein said discontinuous fibers comprise randomly oriented segments of unidirectional tape.
11. A method for making a multiple-component composite window frame assembly which is curable to form a window frame structure in which an elliptical wall extends perpendicularly from a base plate, said method comprising the steps of:
providing a structural component which forms a lower portion of said base plate, said structural component comprising a modified unidirectional continuous fiber body that comprises alternating layers of unidirectional continuous fibers and multi-directional continuous fibers, said modified unidirectional continuous fiber body having a top and an interior side, said structural component further comprising a multi-directional continuous fiber body that comprises multi-directional continuous fibers and an uncured thermosetting resin, said multi-directional continuous fiber body having a top and an interior side;
providing a moldable component which comprises a moldable body comprising an uncured thermosetting resin and discontinuous fibers, said moldable body forming an upper portion of said base plate wherein the upper portion of said base plate has a bottom and a top, said moldable body also forming the elliptical wall that extends from said top of the upper portion of said base plate; and
combining said structural component and said moldable component together to form said multiple-component composite window frame assembly such that the interior sides of said modified unidirectional continuous fiber body and said multi-directional continuous fiber body are in contact with each other and wherein the tops of said modified unidirectional continuous fiber body and said multi-directional continuous fiber body form a top of said lower portion of said base plate and wherein said moldable component is in contact with said structural component so as to form an interface between said moldable component and said structural component, said interface being located where the bottom of the upper portion of said base plate contacts the top of the lower portion of said base plate and wherein micro cracks do not form along said interface during curing of said multiple-component composite window frame assembly to form said window frame structure.
12. A method for making a multi-component composite window frame structure comprising the step of curing a composite assembly according to claim 1 .
13. A method for making a multi-component composite window frame assembly according to claim 11 wherein said multi-directional continuous fibers in the modified unidirectional continuous fiber body or the multi-directional continuous fiber body comprise woven fibers.
14. A method for making a composite assembly according to claim 11 wherein said multi-component composite window frame assembly is a preform of an aircraft window frame.