Honeycomb cores with splice joints and methods of assembling honeycomb cores

1. A honeycomb core for use in an aerospace application, the honeycomb core comprising:

a first honeycomb core section defining a plurality of first cells, wherein the first honeycomb core section has (i) a first edge generally aligned with longitudinal axes of the first cells, and (ii) a first side generally perpendicular to the longitudinal axes of the first cells;

a second honeycomb core section defining a plurality of second cells, wherein the second honeycomb core section has (i) a second edge generally aligned with longitudinal axes of the second cells and positioned adjacent to and spaced apart from the first edge, and (ii) a second side generally perpendicular to the longitudinal axes of the second cells and generally aligned with the first side;

a sheet of film adhesive including a first portion extending partially along the first side, a second portion extending along the first edge, a third portion extending along the second edge, and a fourth portion extending partially along the second side; and

a foam adhesive positioned between the second portion and the third portion of the sheet of film adhesive.

2. The honeycomb core of claim 1 , wherein the first edge is generally parallel to the second edge.

3. The honeycomb core of claim 1 , wherein the first edge is generally parallel to the longitudinal axes of the first cells.

4. The honeycomb core of claim 1 , wherein the second edge is generally parallel to the longitudinal axes of the second cells.

5. The honeycomb core of claim 1 , wherein the first edge is at an angle relative to the longitudinal axes of the first cells.

6. The honeycomb core of claim 1 , wherein the second edge is at an angle relative to the longitudinal axes of the second cells.

7. The honeycomb core of claim 1 , wherein the first edge is at an angle relative to the second edge.

8. The honeycomb core of claim 1 , wherein the foam adhesive extends at least partially on a portion of the sheet of film adhesive that extends partially along the first side.

9. The honeycomb core of claim 1 ,

wherein the first edge is defined by a plurality of first edge ligaments; and

wherein (i) the plurality of first edge ligaments includes ligaments of different dimensions, and/or (ii) the plurality of first edge ligaments are not uniformly spaced along the first edge.

10. The honeycomb core of claim 1 , wherein the sheet of film adhesive is not planar along the first edge.

11. The honeycomb core of claim 10 , wherein the sheet of film adhesive is not planar along the second edge.

12. The honeycomb core of claim 1 , wherein the first edge is defined by a plurality of partial first edge cells, and wherein at least one partial first edge cell has a different configuration than at least one other partial first edge cell.

13. The honeycomb core of claim 1 , wherein the foam adhesive varies in thickness between the first edge and the second edge.

14. The honeycomb core of claim 1 ,

wherein the first edge is defined by a plurality of partial first edge cells, and wherein walls of at least a subset of the plurality of partial first edge cells and the sheet of film adhesive define voids between the walls of the subset of the plurality of partial first edge cells and the sheet of film adhesive; and

wherein the second edge is defined by a plurality of partial second edge cells, and wherein walls of at least a subset of the plurality of partial second edge cells and the sheet of film adhesive define voids between the walls of the subset of the plurality of partial second edge cells and the sheet of film adhesive.

15. The honeycomb core of claim 1 ,

wherein the first edge is defined by a plurality of partial first edge cells, and wherein the sheet of film adhesive undulates along the first edge, extending partially into at least a subset of the plurality of partial first edge cells; and

wherein the second edge is defined by a plurality of partial second edge cells, and wherein the sheet of film adhesive undulates along the second edge, extending partially into at least a subset of the plurality of partial second edge cells.

16. An acoustic panel, comprising:

the honeycomb core of claim 1 ;

a first skin operatively coupled to the first side and the second side; and

a second skin operatively coupled to the first honeycomb core section and the second honeycomb core section opposite of the first side and the second side;

wherein one of the first skin and the second skin is free of perforations, and wherein the other of the first skin and the second skin defines a plurality of perforations.

17. The acoustic panel of claim 16 , wherein the acoustic panel is tuned for a predetermined purpose.

18. An inner acoustic barrel of an aircraft engine inlet, the inner acoustic barrel comprising the acoustic panel of claim 16 .

19. An aircraft, comprising:

a fuselage;

a wing supported by the fuselage;

at least one engine; and

the honeycomb core of claim 1 .

20. A method of assembling the honeycomb core of claim 1 , the method comprising:

placing the foam adhesive relative to and engaged with the sheet of film adhesive so that the foam adhesive is adhered to the sheet of film adhesive;

following the placing the foam adhesive, folding the sheet of film adhesive over the foam adhesive so that two flanges are defined by the sheet of film adhesive, with the two flanges extending beyond and not adhered to the foam adhesive;

following the folding, positioning the first honeycomb core section relative to the sheet of film adhesive and the foam adhesive so that the sheet of film adhesive is engaged with the first edge;

following the folding, positioning the second honeycomb core section relative to the sheet of film adhesive and the foam adhesive so that the sheet of film adhesive is engaged with the second edge and so that the foam adhesive is positioned between the first edge and the second edge;

following the folding, placing a first of the two flanges against the first side; and

following the folding, placing a second of the two flanges against the second side.