Pre-Cured Edge Seal
Abstract
The different illustrative embodiments provide a method and apparatus for installing an edge seal. In one illustrative example, a pre-cured edge seal is placed on an edge of a composite structure with a sealant to form a placed pre-cured edge seal. The placed pre-cured edge seal is then cured on the composite structure. In another illustrative embodiment, an edge of a structure is prepared with solvent, and a brush coat of sealant is applied to the top and the edge of the structure. A fillet is applied to the base of the edge of the structure. A pre-cured edge seal is applied to the edge of the structure, and the edge is cured.
Claims
exact text as granted — not AI-modified1 . A method for installing an edge seal, the method comprising:
placing a pre-cured edge seal on an edge of a composite structure with a sealant to form a placed pre-cured edge seal; and curing the placed pre-cured edge seal on the composite structure.
2 . The method of claim 1 , further comprising:
applying a layer of the sealant to the base of the composite structure to form a fillet.
3 . The method of claim 1 , wherein placing the pre-cured edge seal on the edge of the composite structure with the sealant further comprises:
applying a brush coat of the sealant to the composite structure; and placing the pre-cured edge seal on the edge of the composite structure, wherein the brush coat of the sealant adheres the pre-cured edge seal to the composite structure.
4 . The method of claim 1 , wherein the composite structure is selected from one of an aircraft structure, a wing spar, a stringer, a shear-tie, and a rib.
5 . An apparatus comprising:
a structure having an edge, a top, and a base; a pre-cured edge seal having a first end and a second end attached on the edge of the structure; a sealant located between the pre-cured edge seal and the structure, wherein the sealant attaches the pre-cured edge seal to the edge of the structure; and a fillet located at the base of the structure.
6 . The apparatus of claim 5 , wherein the first end of the pre-cured edge seal forms a curved shape at the top of the structure, wherein the curved shape comes over the top of the structure to form a hook shape.
7 . The apparatus of claim 5 , wherein the second end of the pre-cured edge seal forms a straight edge.
8 . A method for installing an edge seal, the method comprising:
preparing an edge of a structure using a solvent; applying a brush coat of a sealant along a top and the edge of the structure; applying a fillet of the sealant at a base of the edge of the structure; applying a pre-cured edge seal; and curing the edge of the structure.
9 . The method of claim 8 , wherein the structure is selected from one of an aircraft structure, a wing spar, a stringer, a shear-tie, and a rib.
10 . The method of claim 8 , wherein the brush coat of the sealant is an application of a thin layer of the sealant in a wet state.
11 . The method of claim 8 , wherein the application of the fillet of the sealant is an application of the sealant in a wet state.
12 . The method of claim 8 , wherein the application of the pre-cured edge seal is an application of the sealant in a fully cured state.
13 . The method of claim 8 , wherein the pre-cured edge seal is formed in accordance with a number of dimensions.
14 . The method of claim 8 , wherein the application of the pre-cured edge seal is an application of the sealant in a partially cured state.
15 . A method for manufacturing a pre-cured edge seal, the method comprising:
identifying a mold for a number of dimensions of the pre-cured edge seal; filling the mold with sealant; and curing the sealant to form the pre-cured edge seal with the number of dimensions.
16 . The method of 15 , wherein the number of dimensions include at least one of a degree of thickness, a shape, and a degree of flexibility.
17 . The method of claim 15 , wherein the pre-cured edge seal is capable of sealing a structure selected from one of an aircraft structure, a wing spar, a stringer, a shear-tie, and a rib.
18 . A method for manufacturing a pre-cured edge seal, the method comprising:
partially curing a sealant to form the pre-cured edge seal; extruding the pre-cured edge seal into a number of shapes and dimensions.
19 . The method of claim 18 , wherein partially curing the sealant further comprises:
applying a curing process to the sealant; and stopping the curing process before the sealant is fully cured to form the pre-cured edge seal, wherein the pre-cured edge seal is the sealant in a partially cured state.
20 . The method of claim 18 , wherein the pre-cured edge seal is capable of sealing a structure selected from one of an aircraft structure, a wing spar, a stringer, a shear-tie, and a rib.Join the waitlist — get patent alerts
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