Aircraft flooring and methods of manufacturing the same

1. A floor panel for installation in an aircraft, comprising:

a plurality of thermoplastic C-shaped stringers disposed in a parallel arrangement with one another, a pair of the plurality of stringers together defining a longitudinally-extending notch;

a consolidated thermoplastic deltoid filler disposed within the notch;

a thermoplastic upper facing sheet covering an upper surface of each the plurality of stringers and the deltoid filler; and

a thermoplastic lower facing sheet covering a lower surface of each of the plurality of stringers and the deltoid filler,

the plurality of stringers define walls which are vertical and perpendicular to both the upper facing sheet and the lower facing sheet, the walls of each of the plurality of stringers define a pair of vertical backs corresponding to a pair of horizontal flanges extending substantially perpendicularly from opposing ends of the pair of vertical backs; and

the plurality of stringers includes outermost stringers such that the upper facing sheet wraps around an upper half of a vertical back of each of the outermost stringers and the lower facing sheet wraps around a lower half of the vertical backs of the outermost stringers;

wherein the upper and lower facing sheets together surround an entire outer peripheral surface of the stringers and deltoid filler, such that the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are integrally consolidated forming a unitary construction.

2. The floor panel according to claim 1 , wherein the pair of the plurality of stringers is disposed back-to-back.

3. The floor panel according to claim 2 , wherein the horizontal flanges of adjacent stringers have adjoined edges.

4. The floor panel according to claim 1 , wherein the deltoid filler includes a plurality of thermoplastic sheets, consolidated and machined to a deltoid shape.

5. The floor panel according to claim 1 , wherein each of the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are fabricated from carbon and/or glass fibers with a thermoplastic polymer selected from the group consisting of Poly-Ether-Ether-Ketone (PEEK), Poly Ether-Ketone-Ketone (PEKK), polyether sulfide (PES), and polyphenylene sulfide (PPS) or similar materials.

6. The floor panel according to claim 1 , wherein the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are integrally consolidated via a uniformly-applied compressive force.

7. The floor panel according to claim 6 , wherein the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are integrally consolidated by being heated to a temperature between approximately 700° F. and approximately 800° F. while simultaneously undergoing the uniformly-applied compressive force.

8. A floor panel for installation in an aircraft, comprising:

a plurality of thermoplastic C-shaped stringers disposed in a parallel arrangement with one another, a pair of the plurality of stringers together defining a longitudinally-extending notch, the plurality of stringers includes outermost stringers;

a consolidated thermoplastic deltoid filler disposed within the notch;

a thermoplastic upper facing sheet covering an upper surface of each the plurality of stringers and the deltoid filler; and

a thermoplastic lower facing sheet covering a lower surface of each of the plurality of stringers and the deltoid filler,

wherein the plurality of stringers define walls which are vertical and perpendicular to both the upper facing sheet and the lower facing sheet,

wherein the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are integrally consolidated forming a unitary construction such that the upper facing sheet wraps around an upper half of a vertical back of each of the outermost stringers and the lower facing sheet wraps around a lower half of the vertical backs of the outermost stringers.

9. The front panel according to claim 8 , wherein the walls of each of the plurality of stringers define a pair of vertical backs corresponding to a pair of horizontal flanges extending substantially perpendicularly from opposing ends of the pair of vertical backs.

10. The floor panel according to claim 8 , wherein the pair of the plurality of stringers is disposed back-to-back.

11. The floor panel according to claim 10 , wherein each of the plurality of stringers has a vertical back and a pair of substantially horizontal flanges extending from respective opposing ends of the vertical back.

12. The floor panel according to claim 11 , wherein the horizontal flanges of adjacent stringers have adjoined edges.

13. The floor panel according to claim 8 , wherein the deltoid filler includes a plurality of thermoplastic sheets, consolidated and machined to a deltoid shape.

14. The floor panel according to claim 8 , wherein each of the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are fabricated from carbon and/or glass fibers with a thermoplastic polymer selected from the group consisting of Poly-Ether-Ether-Ketone (PEEK), Poly Ether-Ketone-Ketone (PEKK), polyether sulfide (PES), and polyphenylene sulfide (PPS) or similar materials.

15. The floor panel according to claim 8 , wherein the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are integrally consolidated via a compressive force.

16. The floor panel according to claim 15 , wherein the plurality of stringers, the deltoid filler, and the upper and lower facing sheets are integrally consolidated by being heated to a temperature between approximately 700° F. and approximately 800° F. while simultaneously undergoing the compressive force.