Aerospace articles made from quasi-isotropic chopped prepreg
View Patent ↗Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames, wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo floor flange supports, storage bin fittings, antenna supports, torque tube pans, handle boxes, side guide fittings, wing box covers and intercostals.
1. A method for making an aerospace assembly, said method comprising the steps of:
providing a first aerospace part; and
connecting a composite aerospace part to said first aerospace part wherein said composite aerospace part comprises cured quasi-isotropic chopped prepreg and wherein said composite aerospace part comprises a surface defining a hole and wherein said hole is used to connect said composite aerospace part.
2. A method for making an aerospace assembly according to claim 1 wherein said composite aerospace part is an aircraft window frame.
3. A method for making an aerospace assembly according to claim 1 wherein said cured quasi-isotropic chopped prepreg comprises a resin selected from the group consisting of epoxy, phenolic, bismaleimide and cyanates.
4. A method for making an aerospace assembly according to claim 1 wherein said cured quasi-isotropic chopped prepreg comprises fibers selected from the group consisting of carbon, glass, aramid and polyethylene.
5. A method for making an aerospace assembly according to claim 1 wherein said cured quasi-isotropic chopped prepreg comprises epoxy resin and carbon fibers.
6. A method for making an aerospace assembly, said method comprising the steps of:
providing a first aerospace part;
providing a second aerospace part; and
joining said first and second aerospace parts together with a composite aerospace part that comprises a cured quasi-isotropic chopped prepreg, wherein said composite aerospace part comprises a first portion for attachment to said first aerospace part and a second portion for attachment to said second aerospace part and wherein said composite aerospace part comprises a surface defining a hole.
7. A method for making an aerospace assembly according to claim 6 wherein said cured quasi-isotropic chopped prepreg comprises a resin selected from the group consisting of epoxy, phenolic, bismaleimide and cyanates.
8. A method for making an aerospace assembly according to claim 6 wherein said cured quasi-isotropic chopped prepreg comprises fibers selected from the group consisting of carbon, glass, aramid and polyethylene.
9. A method for making an aerospace assembly according to claim 6 wherein said cured quasi-isotropic chopped prepreg comprises epoxy resin and carbon fibers.
10. A method for making an aerospace assembly according to claim 6 wherein said first and second portions of said composite aerospace part are not in planar alignment.
11. A method for making an aerospace assembly according to claim 6 wherein said composite aerospace part is selected from the group consisting of wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo flange supports, storage bin fittings, antenna supports and intercostals.
12. A method for making an aerospace assembly according to claim 11 wherein said composite aerospace part is a flange support that is capable of carrying a load of over 6000 pounds.
13. A method for making a composite aerospace part, said method comprising the steps of:
providing a mat of quasi-isotropic chopped prepreg; and
molding said mat of quasi-isotropic chopped prepreg into said composite aerospace part and forming a surface defining a hole in said aerospace part.
14. A method for making a composite aerospace part according to claim 13 wherein said aerospace part is selected from the group consisting of aircraft window frames, wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo floor flange supports, storage bin fittings, antenna supports, torque tube pans, handle boxes, side guide fittings, wing box covers and intercostals.
15. A method for making a composite aerospace part according to claim 13 wherein said aerospace part is an aircraft window frame.
16. A method for making a composite aerospace part according to claim 13 wherein said cured quasi-isotropic chopped prepreg comprises a resin selected from the group consisting of epoxy, phenolic, bismaleimide and cyanates.
17. A method for making a composite aerospace part according to claim 13 wherein said cured quasi-isotropic chopped prepreg comprises fibers selected from the group consisting of carbon, glass, aramid and polyethylene.
18. A method for making a composite aerospace part according to claim 13 wherein said cured quasi-isotropic chopped prepreg comprises epoxy resin and carbon fibers.