PASSENGER SEATBACK ASSEMBLY WITH THERMOPLASTIC ELEMENTS

Abstract

A thermoplastic seatback for a passenger seat includes a thermoplastic peripheral structural frame for attachment to a seat assembly and a thermoplastic diaphragm overmolded onto a forward face of the frame. An aircraft passenger seat and a method of constructing a passenger seatback is also disclosed.

Claims

1. A thermoplastic seatback for a passenger seat, comprising: (a) a thermoplastic peripheral structural frame for attachment to a seat assembly; and (b) a thermoplastic diaphragm overmolded onto a forward face of the frame.

2. A thermoplastic seatback for a passenger seat according to claim 1, wherein the thermoplastic material of the frame comprises carbon fiber reinforced polyether ether Ketone (PEEK).

3. A thermoplastic seatback for a passenger seat according to claim 1, wherein the thermoplastic material of the diaphragm comprises polyethylenimine (PEI) reinforced glass fiber.

4. A thermoplastic seatback for a passenger seat according to claim 1, wherein the thermoplastic material of the frame comprises carbon fiber reinforced polyether ether Ketone (PEEK) and the thermoplastic material of the diaphragm comprises polyethylenimine (PEI) reinforced glass fiber.

5. A thermoplastic seatback for a passenger seat according to claim 1, wherein the frame is formed of two injection-molded halves joined together to form a unitary frame structure.

6. A thermoplastic seatback for a passenger seat according to claim 5, wherein the injection-molded frame halves comprise an aft section and a forward section.

7. A thermoplastic seatback for a passenger seat according to claim 5, wherein the two injection-molded frame halves are joined together by friction-welding.

8. An aircraft passenger seat, comprising: (a) a seat base, a seat bottom carried on the seat base and at least one armrest; (b) a seatback mounted on the seat base aft of the seat bottom, and comprising: (i) a thermoplastic peripheral structural frame for attachment to a seat assembly; and (ii) a thermoplastic diaphragm overmolded onto a forward face of the frame.

9. An aircraft passenger seat according to claim 8, wherein the thermoplastic material of the frame comprises carbon fiber reinforced polyether ether Ketone (PEEK) and the thermoplastic material of the diaphragm comprises polyethylenimine (PEI) reinforced glass fiber.

10. An aircraft passenger seat according to claim 9, wherein the frame is formed of two injection-molded halves joined together to form a unitary frame structure.

11. An aircraft passenger seat according to claim 9, wherein the injection-molded frame halves comprise an aft section and a forward section.

12. An aircraft passenger seat according to claim 10, wherein the two injection-molded frame halves are joined together by friction-welding.

13. An aircraft passenger seat according to claim 8, wherein the thermoplastic material of the frame comprises carbon fiber reinforced polyether ether Ketone (PEEK) and the thermoplastic material of the diaphragm comprises polyethylenimine (PEI) reinforced glass fiber, the frame is formed of two injection-molded halves joined together to form a unitary frame structure, and the two injection-molded frame halves are joined together by friction-welding.

14. A method of constructing a seatback for a passenger seat, comprising the steps of: (a) forming a thermoplastic peripheral structural frame for attachment to a seat assembly; (b) thermoforming a thermoplastic diaphragm; and (c) overmolding the diaphragm onto a forward face of the frame.

15. A method according to claim 14, wherein step of forming the frame includes the steps of separately forming an aft frame section and a forward frame section and thereafter joining the aft frame section and forward frame section to form a unitary frame structure.

16. A method according to claim 15, wherein the step of joining the aft frame section and forward frame section comprises friction-welding.

Description

BRIEF DESCRIPTION OF THE DRAWING FIGURES

[0020] The present invention is best understood when the following detailed description of the invention is read with reference to the accompanying drawings, in which:

[0021] FIG. 1 is a front perspective view of a pair of aircraft passenger seats of the type in which a seatback according to the present invention may be used;

[0022] FIG. 2 is a fragmentary exploded rear perspective view of a seatback fabricated of thermoplastic elements in accordance with an embodiment of the invention;

[0023] FIG. 3 is a fragmentary side elevation of the seatback shown in FIG. 2;

[0024] FIG. 4 is a rear elevation of the seatback shown in FIG. 2;

[0025] FIG. 5 is a rear, perspective view of the seatback shown in FIG. 2; and

[0026] FIG. 6 is a front perspective view of the seatback shown in FIG. 2.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

[0027] Referring now specifically to the drawings wherein identical reference numerals denote the same elements within and among the various views, a typical seating arrangement incorporating a seatback assembly according to the present invention is illustrated in FIG. 1. A seating unit 10 is provided that includes two side adjacent seats 10A, 10B positioned on locking tracks 12 and secured by means of track fastener assemblies 14 mounted on the front end of the seat legs 16, 18. The seat 10A includes a base 20 that supports a seat bottom 22, including cushioning and a dress cover, an aisle armrest 24 and a center armrest 26 shared with seat 10B. A seatback 30, including cushioning and a dress cover, is conventionally-mounted aft of the seat bottom 22. Seat 10B includes the same elements.

[0028] Referring now to FIGS. 2-6, the seatback 30 is shown, and includes a peripheral structural frame 32 preferably formed of two part short fiber Carbon fiber reinforced Polyether ether Ketone (PEEK) thermoplastic material. The frame 32 is injection molded in two halves—an aft section 34 and a forward section 36, and is preferably friction-welded together to form the unitary structure shown in FIGS. 3-7. Friction-welding refers generally a solid-state welding process that generates heat through mechanical friction between workpieces in relative motion to one another, with the addition of a lateral “upset” force to plastically displace and fuse the materials. The process is particularly useful in fusing thermoplastics given the relatively low melting point of most thermoplastic materials. Of course, other known processes, for example sonic welding, may be used to join the frame halves. Alternatively, the frame 32 can be fabricated using other suitable techniques.

[0029] The diaphragm 40 is preferably fabricated of consolidated Polyethylenimine (PEI) reinforced glass fiber. The PEI diaphragm 40 is thermoformed and then overmolded onto the forward face of the forward frame section 36. Using this process avoids the need for a secondary attachment technique.

[0030] The use of an injection molding process and thermoplastic material have not heretofore been used for components as large as these seat components and that are as heavily loaded. The injection molding process provides overall final quality and reduced cost while maintaining similar structural performance. The process of overmolding PEEK and PEI has not been carried out before and the process carried out to produce the seatback 30 demonstrates that this new process achieves suitable results. The use of a friction-welding process also gives the feel of a ‘traditional’ seatback as well as giving a closed box section useful for maintaining structural integrity combined with light weight and a degree of flexibility. Another benefit of this process is that the wall thickness of the head pan is less than the thickness recommendations of the material supplier with no loss of structural integrity or other performance characteristics. When the seatback has reached the end of its useful life, the thermoplastic components can be recycled, further enhancing the cost-effectiveness of the process and resulting product.

[0031] A thermoplastic seatback, a seat having a thermoplastic seatback, and a method of fabricating a thermoplastic seatback according to preferred embodiments of the invention have been described with reference to specific embodiments and examples. Various details of the invention may be changed without departing from the scope of the invention. Furthermore, the foregoing description of the preferred embodiments of the invention and best mode for practicing the invention are provided for the purpose of illustration only and not for the purpose of limitation, the invention being defined by the claims.