Method of fabricating a thrust reverser cascade assembly
A method of fabricating a thrust reverser cascade assembly including positioning a first frame section on an assembly fixture, positioning a first set of turning vanes on a first elongated stiffener of the first frame section, securing the first set of turning vanes to the elongated stiffener, positioning a second frame section on the assembly fixture adjacent to the first frame section such that the first set of turning vanes are between the elongated stiffeners of the first and second frame section, adding additional sets of turning vanes and frame sections, and fastening the frame sections together.
1. A method of fabricating a thrust reverser cascade assembly, the method comprising the steps of:
positioning a plurality of independent frame sections adjacent to each other, each having a single elongated stiffener and a plurality of flanges extending laterally from the elongated stiffener, some of the frame sections being intermediate frame sections having opposing flanges;
overlapping the flanges of each frame section with a flange of an adjacent frame section such that elongated stiffeners of adjacent frame sections are laterally spaced from each other and such that the intermediate frame sections are spaced between two adjacent frame sections via the opposing flanges;
positioning a plurality of turning vanes between the elongated stiffeners of adjacent frame sections;
securing the turning vanes to the elongated stiffeners of adjacent frame sections; and
securing the adjacent frame sections to each other via the overlapping flanges.
2. The method of claim 1 , further comprising the step of inspecting the plurality of independent frame sections and turning vanes via non-destructive inspection before positioning the plurality of independent frame sections adjacent to each other and before positioning the turning vanes between the elongated stiffeners of the adjacent frame sections.
3. The method of claim 1 , wherein the turning vanes include flanges configured to abut the elongated stiffeners of the plurality of independent frame sections and the step of securing the turning vanes to the elongated stiffeners includes applying an adhesive or double-sided tape between the flanges of the turning vanes and the elongated stiffeners.
4. The method of claim 1 , wherein the step of securing the adjacent frame sections to each other includes inserting fasteners through aligned fastener holes of the overlapping flanges.
5. The method of claim 1 , wherein the step of securing the adjacent frame sections to each other includes applying an adhesive or double-sided tape to at least portions of the overlapping flanges.
6. The method of claim 1 , further comprising the step of aligning the turning vanes via interlocking geometry.
7. The method of claim 1 , further comprising the step of aligning the turning vanes via welding or fastening.
8. The method of claim 1 , further comprising the step of applying a bonding agent to the plurality of independent frame sections and turning vanes for improving bonding therebetween.
9. The method of claim 1 , further comprising the step of trimming the plurality of independent frame sections.
10. The method of claim 1 , further comprising the step of removing material from the elongated stiffeners of the plurality of independent frame sections for increasing a strength-to-weight ratio of the plurality of independent frame sections.
11. The method of claim 1 , wherein the plurality of independent frame sections includes a first end section, a second end section, and a plurality of inner sections, the inner sections being substantially identical to each other, the end sections being different from each other and different from the inner sections.
12. The method of claim 1 , wherein the thrust reverser cascade assembly includes at least ten frame sections and at least nine rows of turning vanes.
13. The method of claim 1 , further comprising the step of forming the plurality of independent frame sections via pultrusion or extrusion.
14. The method of claim 1 , further comprising the step of forming the plurality of independent frame sections on steel tooling.
15. The method of claim 1 , wherein the plurality of independent frame sections includes elongated stiffeners having at least two geometries.
16. The method of claim 15 , wherein some of the plurality of independent frame sections are radially extending frame sections and some of the plurality of independent frame sections are side turning frame sections.
17. The method of claim 1 , wherein the steps of positioning the plurality of independent frame sections and positioning the plurality of turning vanes include the steps of: positioning a first frame section of the plurality of frame sections on an assembly fixture; positioning a first set of turning vanes of the plurality of turning vanes on a first elongated stiffener of the first frame section; after positioning the first frame section, positioning a second frame section of the plurality of frame sections on the assembly fixture adjacent to the first frame section so as to align the second frame section with the first frame section such that a second elongated stiffener of the second frame section is spaced from the first elongated stiffener of the first frame section and adjacent the first set of turning vanes; and positioning a second set of turning vanes of the plurality of turning vanes on the second elongated stiffener of the second frame section; and after positioning the second frame section, positioning additional frame sections of the plurality of independent frame sections on the assembly fixture so as to align the additional frame sections with previously placed frame sections and positioning additional turning vanes of the plurality of turning vanes on previously placed frame sections in alternating fashion.
18. The method of claim 17 , wherein the steps of positioning frame sections on the assembly fixture include aligning alignment geometry of the plurality of independent frame sections with alignment geometry of the assembly fixture.
19. The method of claim 17 , wherein the steps of positioning turning vanes on elongated stiffeners include aligning the turning vanes with indexing geometry on the assembly fixture.
20. A method of fabricating a thrust reverser cascade assembly, the method comprising the steps of:
positioning a first frame section on an assembly fixture, the first frame section having a single elongated stiffener and a plurality of flanges extending laterally from the elongated stiffener;
positioning a first set of turning vanes on the elongated stiffener of the first frame section;
securing the first set of turning vanes to the elongated stiffener of the first frame section;
positioning a second frame section on the assembly fixture adjacent to the first frame section, the second frame section having a single elongated stiffener and a plurality of opposing flanges extending laterally from the elongated stiffener so that the second frame section is an intermediate frame section, such that flanges of the first and second frame sections overlap each other so that the elongated stiffener of the second frame section is spaced from the elongated stiffener of the first frame section and adjacent the first set of turning vanes, the second frame section being independent from the first frame section;
positioning a second set of turning vanes on the elongated stiffener of the second frame section;
securing the second set of turning vanes to the elongated stiffener of the second frame section;
positioning additional frame sections on the assembly fixture adjacent to previously placed frame sections, the additional frame sections each having a single elongated stiffener and a plurality of flanges, such that flanges of the additional frame sections and previously placed frame sections overlap each other and such that the second frame section is spaced between two adjacent frame sections via the opposing flanges, the additional frame sections being independent from the first and second frame sections and from each other;
positioning additional turning vanes on elongated stiffeners of previously placed frame sections;
securing the additional turning vanes to the previously placed frame sections in alternating fashion; and
inserting cascade basket fasteners through aligned fastener holes of the overlapping flanges of the adjacent frame sections so as to secure the adjacent frame sections together and secure the thrust reverser cascade assembly to a cascade basket.