Aircraft structure
View Patent ↗An aircraft structure comprising: a spar; a primary cover attached to the spar and extending on a first side of the spar; and a secondary cover positioned on a second side of the spar and partially overlapping an internal surface of the primary cover. A bracket is attached to the spar, and a spacer is provided between the secondary cover and the bracket. The spacer is sized so that the primary and secondary covers together form a substantially continuous external aerodynamic surface. The structure provides an alternative to conventional butt-strap arrangements.
1. An aircraft structure comprising: a spar; a primary cover attached to the spar and extending on a first side of the spar; a secondary cover positioned on a second side of the spar and partially overlapping an internal surface of the primary cover; a bracket attached to the spar; and a spacer between the secondary cover and the bracket, wherein the spacer can be adjusted to control a distance between the secondary cover and the bracket so that the primary and secondary covers together form a substantially continuous external aerodynamic surface.
2. The structure of claim 1 wherein the spacer is detachable from the secondary cover and the bracket.
3. The structure of claim 1 wherein the spacer passes through a hole in the secondary cover and/or a hole in the bracket.
4. The structure of claim 3 wherein the spacer comprises a head which engages a recess in the external surface of the secondary cover; and a shaft which passes through a hole in the secondary cover and engages the bracket.
5. The structure of claim 4 wherein the shaft comprises a tip which passes through a hole in the bracket; and a shoulder which engages the bracket.
6. The structure of claim 1 wherein the spacer comprises an assembly of parts including a base and a detachable packer.
7. The structure of claim 1 wherein the secondary cover comprises a core sandwiched between internal and external layers, and wherein one or both of the layers overhangs an edge of the core to form a landing portion which overlaps the internal surface of the primary cover.
8. The structure of claim 1 , wherein the secondary cover comprises a laminar composite with a stack of layers, a subset of the layers being extended to form a landing portion which overlaps the internal surface of the primary cover.
9. The structure of claim 1 comprising upper and lower primary covers each attached to the spar and extending on a first side of the spar; wherein the secondary cover comprises a D-nose cover with an upper part which overlaps the internal surface of the upper primary cover and a lower part which overlaps the internal surface of the lower primary cover; upper and lower brackets attached to the spar; and upper and lower spacers, each spacer being positioned between the D-nose cover and a respective upper or lower one of the brackets, wherein each spacer is sized so that a respective upper or lower part of the D-nose cover forms a substantially continuous external aerodynamic surface with a respective upper or lower primary cover.
10. A method of assembling the aircraft structure of claim 1 , the method comprising: attaching the primary cover and the bracket to the spar; installing the secondary cover with the spacer between the secondary cover and the bracket; and adjusting the spacer so that the primary and secondary covers together form a substantially continuous external aerodynamic surface.
11. The method of claim 10 further comprising measuring a height difference between the external surfaces of the covers; and adjusting the size of the spacer in accordance with the measured height difference.
12. The method of claim 11 wherein the size of the spacer is increased by detaching a base from the secondary cover and the bracket; attaching a packer to the base, the packer being sized in accordance with the measured height difference; and re-installing the base and packer between the secondary cover and the bracket.