Seat unit and lower structure thereof

Patent metadata

Field	Value
Publication number	US-11753168-B2
Application number	US-201716498528-A
Country	US
Kind code	B2
Filing date	Dec 18, 2017
Priority date	Apr 3, 2017
Publication date	Sep 12, 2023
Grant date	Sep 12, 2023

Abstract

A seat unit and a lower structure thereof that are not restricted in their positional relationship with seat tracks provided in advance in the airframe. One representative seat unit of the present invention and the lower structure thereof includes a hollow structure integrally formed using a composite member. The hollow structure is hollow in a front direction of the seat unit. The hollow structure has a quadrilateral shape in the front direction of the seat unit. In addition, a partition plate is disposed in the hollow structure. Furthermore, the lower structure includes attachment points to an aircraft at three locations on its bottom. In addition, a block is embedded in the composite member at the attachment point, and a thickness of the composite member around a bracket coupled to the block is less than thickness at other locations.

First claim

The invention claimed is:

1. A lower structure of a seat unit comprising:
a hollow box structure integrally formed of a composite member for supporting a seat;
wherein the hollow box structure includes and is defined by a bottom surface for attaching the hollow box structure to a floor, at least two side wall surfaces extending in an upward direction from the bottom surface, and a top surface for supporting a seat,
wherein the top surface is substantially parallel to the bottom surface and is coupled to the at least two side wall surfaces,
wherein the lower structure includes brackets and fitting portions configured to attach the lower structure to seat rails in an aircraft at three attachment points on the bottom surface.

2. The lower structure of the seat unit according to claim 1 , wherein the hollow box structure has an opening in a front direction of the lower structure of a seat unit.

3. The lower structure of the seat unit according to claim 2 , wherein the opening of the hollow box structure has a quadrilateral shape.

4. The lower structure of the seat unit according to claim 1 , wherein a partition plate is disposed in the hollow box structure to separate the hollow box structure into smaller sections.

5. The lower structure of the seat unit according to claim 1 , wherein a block is embedded in the composite member at each of the attachment points, and one of the brackets is coupled to each block,
wherein a thickness of the composite member at an area where each bracket is coupled to each block is less than a thickness at an area of the composite member other than the area where each bracket is coupled to each block.

6. The lower structure of the seat unit according to claim 5 , wherein a lower surface of the composite member at the area where each bracket is coupled to each block has a recess, and
an upper surface of the composite member at the area where each bracket is coupled to each block is flat.

7. A seat unit comprising:
a lower structure comprising a hollow box structure integrally formed of a composite member for supporting a seat; and
an upper shell formed above the lower structure,
wherein the hollow box structure includes and is defined by a bottom surface for attaching the hollow box structure to a floor, at least two side wall surfaces extending in an upward direction from the bottom surface, and a top surface for supporting a seat,
wherein the top surface is substantially parallel to the bottom surface and is coupled to the at least two side wall surfaces, and
wherein the lower structure includes brackets and fitting portions configured to attach the lower structure to seat rails in an aircraft at three attachment points on the bottom surface.

8. The seat unit according to claim 7 , wherein:
the hollow box structure has an opening in a front direction of the seat unit;
the opening of the hollow box structure has a quadrilateral shape;
a partition plate is disposed in the hollow box structure to separate the hollow box structure into smaller sections;
the lower structure includes attachment points for attaching the lower structure to an aircraft at three places on the bottom surface;
a block is embedded in the composite member at each of the attachment points, and one of the brackets is coupled to each block,
wherein a thickness of the composite member at an area where each bracket is coupled to each block is less than a thickness at an area of the composite member other than the area where each bracket is coupled to each block; and
a lower surface of the composite member at the area where each bracket is coupled to each block has a recess, and
an upper surface of the composite member at the area where each bracket is coupled to each block is flat.

9. A seat unit comprising:
a lower structure comprising a hollow box structure integrally formed of a composite member; and
a multi-person seat unit disposed above and supported by the lower structure,
wherein the hollow box structure includes and is defined by a bottom surface for attaching the hollow box structure to a floor, at least two side wall surfaces extending in an upward direction from the bottom surface, and a top surface for supporting a seat,
wherein the top surface is substantially parallel to the bottom surface and is coupled to the at least two side wall surfaces, and
wherein the lower structure includes brackets and fitting portions configured to attach the lower structure to seat rails in an aircraft at three attachment points on the bottom surface.

10. The seat unit according to claim 9 , wherein:
the hollow box structure has an opening in a front direction of the seat unit;
the opening of the hollow box structure has a quadrilateral shape;
a partition plate is disposed in the hollow box structure to separate the hollow box structure into smaller sections;
the lower structure includes attachment points for attaching the lower structure to an aircraft at three places on the bottom surface;
a block is embedded in the composite member at each of the attachment points, and one of the brackets is coupled to each block,
wherein a thickness of the composite member at an area where each bracket is coupled to each block is less than a thickness at an area of the composite member other than the area where each bracket is coupled to each block; and
a lower surface of the composite member at the area where each bracket is coupled to each block has a recess, and
an upper surface of the composite member at the area where each bracket is coupled to each block is flat.

Assignees

• Jamco Corp

Inventors

• Ozaki Masaji
• Suzuki Michihito

Classifications

• B64D11/0648 Primary

  Lower frame constructions · CPC title

• B64D11/0627 Primary

  Seats combined with storage means · CPC title

• B64D11/0649

  Seats characterised by special features for reducing weight · CPC title

• B64D11/0696

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

• B60N2/686

  Panel like structures · CPC title