Aircraft integrated child seat

Patent metadata

Field	Value
Publication number	US-9227535-B2
Application number	US-201314036358-A
Country	US
Kind code	B2
Filing date	Sep 25, 2013
Priority date	Sep 25, 2012
Publication date	Jan 5, 2016
Grant date	Jan 5, 2016

Abstract

The present invention generally relates to passenger aircraft seats. Some examples provide systems for integrating a child seat into a certified aircraft seat. Some examples include a passenger seat backrest having an integrated child seat. An integrated child seat base may be moved between a stowed position and a deployed position. When in the stowed position, the integrated child seat base may fit within a recessed surface of the seat backrest and the seat may then accommodate an adult passenger. When in a deployed position, the integrated child seat may then accommodate a child passenger. The integrated seat may include a harness system that extends through the seat backrest and couples with an internal support structure of seat backrest. In some embodiments the mounting points of the harness system may be reinforced with stiff brackets attached to the internal support structure.

First claim

What is claimed is:

1. A passenger airplane seat, comprising:
an internal frame structure having a plurality of routing channels, the plurality of routing channels comprising a first routing channel and a second routing channel;
a first reinforcing bracket coupled to the internal frame structure about one or more of the plurality of routing channels of the internal frame structure, the first reinforcing bracket attached to a back side of the internal frame structure;
aircraft seat spreaders coupled to each side of the internal frame structure of the passenger airplane seat;
a seat backrest supported by the internal frame structure, the seat backrest including an integrated seat on a front side of the internal frame structure opposite the back side of the internal frame structure;
the integrated seat comprising an integrated seat base, an integrated seat backrest, and an integrated seat harness; and
the integrated seat base moveable between a stowed position and a deployed position;
wherein the integrated seat harness includes one or more belts that route from the front side of the internal frame structure through the integrated seat backrest, through the first routing channel of the internal frame structure, and through the first reinforcing bracket on the back side of the internal frame structure, and routes from the back side of the internal frame structure through the second routing channel of the internal frame structure to the front side of the internal frame structure;
wherein the first and second routing channels extend through the first reinforcing bracket such that the first reinforcing bracket surrounds an opening of the first and second routing channels on the back side of the internal frame structure.

2. The passenger airplane seat of claim 1 , wherein the first and second routing channels include an anti-friction trim for harness routing, the anti-friction trim extending from a front side of the seat backrest through the first reinforcing bracket to the back side of the internal frame structure.

3. The passenger airplane seat of claim 1 , wherein the first reinforcing bracket is welded with the internal frame structure on the back side of the internal frame structure.

4. The passenger airplane seat of claim 1 , wherein the plurality of routing channels of the internal frame structure comprise two upper routing channels for receiving the integrated seat harness, the two upper routing channels disposed at a first height and in a horizontal orientation.

5. The passenger airplane seat of claim 4 , wherein the first and second routing channels of the internal frame structure comprise two lower routing channels for receiving the integrated seat harness, the two lower routing channels at a second height and in a vertical orientation, the second height being less than the first height.

6. The passenger airplane seat of claim 5 , wherein the plurality of routing channels of the internal frame structure further comprise two middle routing channels for receiving the integrated seat harness, the two middle routing channels disposed at a third height and in a horizontal orientation, the third height being less than the first height and greater than the second height.

7. The passenger airplane seat of claim 6 , further comprising an upper reinforcing bracket for reinforcing the two upper routing channels, the upper reinforcing bracket coupled with the back side of the internal frame structure at the first height, the upper reinforcing bracket disposed around the two upper routing channels such that the upper reinforcing bracket surrounds an opening of the two upper routing channels along the back side of the internal frame structure.

8. The passenger airplane seat of claim 7 , wherein the first reinforcing bracket comprises a lower bracket for reinforcing the two lower routing channels, the lower bracket coupled with the back side of the internal frame structure at the second height.

9. The passenger airplane seat of claim 8 , further comprising a middle reinforcing bracket for reinforcing the two middle routing channels, the middle reinforcing bracket coupled with the back side of the internal frame structure at the third height, the middle reinforcing bracket disposed around the two middle routing channels such that the middle reinforcing bracket surrounds an opening of the two middle routing channels along the back side of the internal frame structure.

10. The passenger airplane seat of claim 9 , wherein the integrated seat base is supported by an internal integrated seat base frame structure, and wherein the integrated seat harness routes through the integrated seat base and couples with the internal integrated seat base frame structure.

11. The passenger airplane seat of claim 10 , wherein the one or more belts of the integrated seat harness route horizontally between the two lower routing channels along the back side of the internal frame structure; and wherein the one or more belts of the integrated seat harness route vertically between one of the two upper routing channels and one of the two middle routing channels along the back side of the internal frame structure.

12. The passenger airplane seat of claim 1 , wherein the integrated seat comprises an antimicrobial material, an antibacterial material, a water-resistant material, and a stain-resistant material.

13. A passenger seat comprising:
a seat harness apparatus;
a seat backrest supported by an internal frame structure, the internal frame structure including a first routing channel and a second routing channel for coupling the seat harness apparatus;
aircraft seat spreaders coupled to each side of the internal frame structure of the passenger airplane seat;
a first reinforcing bracket disposed around the first routing channel and the second routing channel, the first reinforcing bracket coupled with the internal frame structure on a back side of the internal frame structure, the back side being opposite the seat harness apparatus; and
wherein a belt of the seat harness apparatus routes between the first routing channel and the second routing channel along the back side of the internal frame structure and over a back side of the first reinforcing bracket;
wherein the internal frame structure further comprises two upper routing channels for receiving the seat harness apparatus, the two upper routing channels disposed at a first height and in a horizontal orientation;
wherein the first and second routing channels of the internal frame structure comprise two lower routing channels for receiving the seat harness apparatus, the two lower routing channels at a second height and in a vertical orientation, the second height being less than the first height; and
wherein the internal frame structure further comprises two middle routing channels for receiving the seat harness apparatus, the two middle routing channels disposed at a third height and in a horizontal orientation, the third height being less than the first height and greater than the second height.

14. The passenger airplane seat of claim 13 , further comprising an upper bracket for reinforcing the two upper routing channels, the upper bracket coupled with the back side of the internal frame structure at the first height, the upper bracket disposed around the two upper routing channels such that the upper bracket surrounds an opening of the two upper routing channels along the back side of the internal frame structure.

15. The passenger airplane seat of claim 14 , wherein the first reinforcing bracket comprises a lower bracket for reinforcing the two lower routing channels, the lower bracket coupled w

Assignees

• Zodiac Seats Us Llc

Inventors

• Coman Sorin
• Romano Michael
• Jafri Aamir
• Sabo Dianna
• Westerink Rik
• Valdes Armando

Classifications

• Y02T50/46

  Cross-Sectional Technologies · mapped topic

• B60N2/265 Primary

  Adaptations for seat belts · CPC title

• B60R22/00

  Safety belts or body harnesses in vehicles (safety belts or body harnesses in general A62B35/00) · CPC title

• B64D11/0612

  specially adapted for children · CPC title

• B64D11/06

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title