Passenger seat

Patent metadata

Field	Value
Publication number	US-9682643-B2
Application number	US-201314372553-A
Country	US
Kind code	B2
Filing date	Jan 17, 2013
Priority date	Jan 17, 2012
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

Described are passenger seat assemblies including spreaders ( 18 ) with a transitional region having a forward surface with a radius of curvature of about 3.5 to 3.7 inches and an aft surface with an angular profile configured so that the aft surface is located forward of a plane formed by a surface of the at least one seat back ( 12 ) in a fully upright position. The passenger seat assemblies also include leg assemblies ( 22 with a forward leg portion having a forward surface that is substantially aligned with a forward base frame tube, and an aft surface with an angular profile having a shape of an “r.”

First claim

That which is claimed is:

1. A passenger seat assembly comprising a plurality of passenger seats, wherein the passenger seat assembly comprises:
(a) a plurality of spreaders, each spreader comprising an upper portion and a lower portion separated by a transitional region;
(b) a plurality of seat backs, each seat back comprising a central panel and a pair of extensions coupled to a lower end of the central panel, wherein the pair of extensions are pivotally coupled to the upper portions of two of the plurality of spreaders;
(c) a base structure comprising a forward base frame tube and an aft base frame tube, wherein the forward base frame tube and the aft base frame tube pass through a pair of apertures in the lower portion of each spreader; and
(d) at least two leg assemblies, each leg assembly comprising a forward leg portion, wherein the forward base frame tube and the aft base frame tube pass through a pair of apertures in the forward leg portion;
wherein the spreaders, base frame tubes, and leg assemblies are constructed and joined together to provide the passenger seat assembly with sufficient structural integrity to remain attached to an airframe after application of a 16 g-force load;
wherein the transitional region of each spreader comprises a forward surface having a radius of curvature of about 3.5 to 3.7 inches and an aft surface having an angular profile configured so that the aft surface is located forward of a plane formed by a surface of each seat back in a fully upright position; and
wherein the forward base frame tube is located at a lower height than the aft base frame tube so that an upper end of the forward leg portion of each leg assembly has a downward pitch in a forward direction between the aft base frame tube and the forward base frame tube.

2. The passenger seat assembly of claim 1 , wherein each leg assembly further comprises a load-limiting strut.

3. The passenger seat assembly of claim 1 , wherein the forward surface of the forward leg portion is substantially aligned with a forward edge of the forward base frame tube, and the aft surface of the forward leg portion comprises an angular profile having a shape of an “r”.

4. The passenger seat assembly of claim 1 , further comprising a plurality of arm rests coupled to the upper portions of the plurality of spreaders, wherein each seat back is configured to pivot relative to two of the plurality of spreaders adjacent the location where each arm rest is coupled to the upper portion of each spreader.

5. The passenger seat assembly of claim 1 , further comprising a plurality of seat pans, each seat pan positioned over the forward base frame tube and the aft base frame tube.

6. The passenger seat assembly of claim 5 , wherein each seat pan comprises a deep contour located between two of the plurality of spreaders.

7. The passenger seat assembly of claim 5 , wherein each seat pan comprises a door that provides access to an In-Flight Entertainment equipment stowed below each seat pan.

8. A passenger seat assembly comprising a plurality of passenger seats, wherein the passenger seat assembly comprises:
(a) a plurality of spreaders, each spreader comprising an upper portion and a lower portion separated by a transitional region;
(b) a plurality of seat backs, each seat back comprising a central panel and a pair of extensions coupled to a lower end of the central panel, wherein the pair of extensions are pivotally coupled to the upper portions of two of the plurality of spreaders;
(c) a plurality of arm rests coupled to the upper portions of the plurality of spreaders, wherein each seat back is configured to pivot relative to two of the plurality of spreaders adjacent the location where each arm rest is coupled to the upper portion of each spreader;
(d) a base structure comprising a forward base frame tube and an aft base frame tube, wherein the forward base frame tube and the aft base frame tube pass through a pair of apertures in the lower portion of each spreader; and
(e) at least two leg assemblies, each leg assembly comprising a forward leg portion, wherein the forward base frame tube and the aft base frame tube pass through a pair of apertures in the forward leg portion;
wherein the spreaders, base frame tubes, and leg assemblies are constructed and joined together to provide the passenger seat assembly with sufficient structural integrity to remain attached to an airframe after application of a 16 g-force load;
wherein the forward base frame tube is located at a lower height than the aft base frame tube so that an upper end of the forward leg portion of each leg assembly has a downward pitch in a forward direction between the aft base frame tube and the forward base frame tube; and
wherein a forward surface of the forward leg portion is substantially aligned with a forward edge of the forward base frame tube, and an aft surface of the forward leg portion comprises an angular profile having a shape of an “r”.

9. The passenger seat assembly of claim 8 , wherein each leg assembly further comprises a load-limiting strut.

10. The passenger seat assembly of claim 8 , wherein the transitional region of each spreader comprises the forward surface having a radius of curvature of about 3.5 to 3.7 inches and the aft surface having an angular profile configured so that the aft surface is located forward of a plane formed by a surface of each seat back in a fully upright position.

11. The passenger seat assembly of claim 8 , further comprising a plurality of seat pans, each seat pan positioned over the forward base frame tube and the aft base frame tube.

12. The passenger seat assembly of claim 11 , wherein each seat pan comprises a deep contour located between two of the plurality of spreaders.

13. The passenger seat assembly of claim 11 , wherein each seat pan comprises a door that provides access to an In-Flight Entertainment equipment stowed below each seat pan.

14. A passenger seat assembly comprising a plurality of passenger seats, wherein the passenger seat assembly comprises:
(a) a plurality of spreaders, each spreader comprising an upper portion and a lower portion separated by a transitional region;
(b) a plurality of seat backs, each seat back comprising a central panel and a pair of extensions coupled to a lower end of the central panel, wherein the pair of extensions are pivotally coupled to the upper portions of two of the plurality of spreaders;
(c) a plurality of arm rests coupled to the upper portions of the plurality of spreaders, wherein each seat back is configured to pivot relative to two of the plurality of spreaders adjacent the location where each arm rest is coupled to the upper portion of each spreader;
(d) a base structure comprising a forward base frame tube and an aft base frame tube, wherein the forward base frame tube and the aft base frame tube pass through a pair of apertures in the lower portion of each spreader;
(e) at least two leg assemblies, each leg assembly comprising a forward leg portion, wherein the forward base frame tube and the aft base frame tube pass through a pair of apertures in the forward leg portion, wherein the spreaders, base frame tubes, and leg assemblies are constructed and joined together to provide the passenger seat assembly with sufficient structural integrity to remain attached to an airframe after application of a 16 g-force load, wherein the forward base frame tube is located at a lower height than the aft base frame tube so that an upper end of the forward leg portion of each leg assembly has a downward pitch in a forward direction between the aft base frame tube and the forward base frame tube; and
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Assignees

• Zodiac Seats Us Llc

Inventors

• Wegenka Jeffrey P
• Shirey Allen
• Krikorian Aram
• Krishna Shreyas

Classifications

• B60R7/043

  mounted on or under a seat · CPC title

• B64D11/0646

  Seats characterised by special features of stationary arms, foot or head rests · CPC title

• B64D11/064

  Adjustable inclination or position of seats · CPC title

• B60N2/42

  the seat constructed to protect the occupant from the effect of abnormal g-forces, e.g. crash or safety seats (for protecting children B60N2/26; arm-rests B60N2/75; head-rests B60N2/888) · CPC title

• B64D11/0696

  Means for fastening seats to floors, e.g. to floor rails · CPC title