Ultra lightweight seat for aircraft
The seat for an aircraft passenger is, in particular, very light. It consists principally of a structure ( 1 ), a back ( 2 ) and a base ( 3 ). The structure ( 1 ) is rigid and tubular. It may be obtained as a single piece by rotational moulding of a plastic or, alternatively, by extrusion-bending or bladder inflation moulding if the structure ( 1 ) consists of several tubes assembled with one another in rigid fashion. Application to civil aircraft seats, in particular in economy class.
1. A seat for aircraft passengers including:
a structure including a back section, a base portion, and feet adapted to be attached to a floor of an aircraft;
at least one back, and
at least one base,
wherein the at least one back is attached to the back section of the structure, the at least one base is attached to the base portion of the structure, and the feet are attached to the base portion of the structure,
wherein the back section and the base portion are formed of rigid plastic tubes attached to one another by joining parts comprising rigid bushings, at least one of the rigid bushings connecting at least two rigid plastic tubes together,
wherein a first of the at least two rigid plastic tubes comprises an end that terminates inside the at least one of the rigid bushings, and
wherein a second of the at least two rigid plastic tubes comprises a portion that extends inside and is encircled by the at least one of the rigid bushings.
2. The seat according to claim 1 , wherein the plastic is a thermoplastic polymer.
3. The seat according to claim 2 , wherein the structure is strengthened with fibres of a material selected from the group consisting of carbon, glass and plants.
4. The seat according to claim 2 , wherein the thermoplastic polymer comprises polyetherimide resin.
5. The seat according to claim 1 , wherein the plastic is a thermohardening polymer.
6. The seat according to claim 5 , wherein the structure is strengthened with fibres of a material selected from the group consisting of carbon, glass and plants.
7. The seat according to claim 5 , wherein the thermohardening polymer comprises epoxy resin.
8. The seat according to claim 1 , wherein the structure is strengthened with fibres of a material selected from the group consisting of carbon, glass and plants.
9. The seat according to claim 8 , wherein the structure is produced by bladder inflation moulding, and wherein the plastic is strengthened with fibres of a material selected from the group consisting of carbon, glass and plants.
10. The seat according to claim 9 , wherein the at least one back and the at least one base are overmoulded on to the structure.
11. The seat according to claim 8 , wherein the structure is produced by extrusion/bending.
12. The seat according to claim 11 , wherein the at least one back and the at least one base are overmoulded on to the structure.
13. The seat according to claim 1 , wherein the joining parts comprise metal bushings.
14. The seat according to claim 13 , wherein the metal bushings are produced by injection of metal.
15. The seat according to claim 1 , wherein the joining parts comprise bushings made of composite material.
16. The seat according to claim 15 , wherein the bushings made of composite material are produced by injection of a thermohardening matrix filled with fibres of a material selected from the group consisting of carbon, glass and plant fibres.
17. The seat according to claim 1 , wherein at least one of the at least one back and the at least one base are thin, of the order of one millimetre thick.
18. The seat according to claim 1 , wherein the feet are formed of rigid plastic tubes and are attached to the base portion by joining parts comprising rigid bushings surrounding at least an end of the tubes to be attached.