Aircraft seat kit, and aircraft seat and cabin arrangement with different types of seat rail adapters

Patent metadata

Field	Value
Publication number	US-11136128-B2
Application number	US-201715805251-A
Country	US
Kind code	B2
Filing date	Nov 7, 2017
Priority date	Nov 16, 2016
Publication date	Oct 5, 2021
Grant date	Oct 5, 2021

Abstract

An aircraft seat kit with one aircraft seat, and an aircraft seat and cabin arrangement with at least two aircraft seats for being mounted one after the other onto a seat rail are described. The seat rail provides a grid with a pre-determined grid pitch for mounting the at least two aircraft seats. Each of the at least two aircraft seats includes: a seating structure, a support for supporting the seating structure, and one of two types of seat rail adapters for mounting the support onto the seat rail. The two types of seat rail adapters differ from each other in that they configure at least one aircraft seat with a different distance in a longitudinal direction between a seat reference point and a reference mounting position, respectively.

First claim

The invention claimed is:

1. An aircraft seat arrangement comprising at least a first and a second aircraft seat for being mounted directly one after the other onto a seat rail which extends along a longitudinal direction of an aircraft cabin, the seat rail providing a grid of reference mounting positions with a pre-determined grid pitch for mounting at least the first and the second aircraft seat,
wherein each of the first and the second aircraft seat comprises:
a seating structure having a seating area and a backrest extending upwards from the seating area wherein a seat reference point is defined at the connection between the seating area and the backrest;
a support supporting the seating structure; and

one of a first and a second seat rail adapter connected on the support, the first and the second seat rail adapter configured to mount the support at a reference mounting position onto the seat rail,
wherein the first aircraft seat comprises the first seat rail adapter and the second aircraft seat comprises the second seat rail adapter, wherein the first seat rail adapter comprises a first front seat rail adapter part and a first back seat rail adapter part and the second seat rail adapter comprises a second front seat rail adapter part and a second back seat rail adapter part, wherein the second seat rail adapter is structurally different than the first seat adapter,
wherein the first seat rail adapter is configured such that the seat reference point of the first aircraft seat is spaced in the longitudinal direction from the reference mounting position at which the first seat rail adapter is connected, by a first distance;
wherein the second seat rail adapter is configured such that the seat reference point of the second aircraft seat is spaced in the longitudinal direction from the reference mounting position at which the second seat rail adapter is connected, by a second distance; and
wherein the first distance differs from the second distance
such that at least the first and the second aircraft seats, when mounted in the grid onto the seat rail, have a spacing between the respective seat reference points which is not an integer multiple of the grid pitch of the seat rail.

2. The aircraft seat arrangement according to claim 1 , wherein each of the first and second seat rail adapters comprises at least one stud for engaging the seat rail in the grid, and a foremost of the at least one stud defines the respective reference mounting position.

3. The aircraft seat arrangement according to claim 1 , wherein
the support of each of the first and the second aircraft seat comprises a first connector assembly defining a connecting point which has a distance in the longitudinal direction to the seat reference point, this distance being the same for each of the first and the second aircraft seat, and
each of the first and second seat rail adapter of the first and second aircraft seat comprises a second connector assembly connectable at the connection point to the first connector assembly for connecting the respective one of the first and the second seat rail adapters on the support.

4. The aircraft seat arrangement according to claim 1 , wherein
the support of the first and second aircraft seat comprises a front strut and a back strut, and
each of the first and second seat rail adapters comprises a front and a back seat rail adapter part that are connected to a front and a back strut on the support, respectively,
wherein the reference mounting position is where the front seat rail adapter part of each of the first and second seat rail adapter is configured to mount the support onto the seat rail.

5. The aircraft seat arrangement according to claim 1 , wherein the spacing in the longitudinal direction is an integer multiple plus half of the grid pitch of the seat rail.

6. The aircraft seat arrangement according to claim 1 , further comprising:
a third aircraft seat for being mounted directly after the second aircraft seat onto the seat rail, the third aircraft seat comprises:
a seating structure having a seating area and a backrest extending upwards from the seating area wherein a seat reference point is defined at the connection between the seating area and the backrest,
a support supporting the seating structure, and
a third seat rail adapter connected on the support, the third seat rail adapter configured to mount the support at a reference mounting position onto the seat rail,

wherein the third seat rail adapter of the third aircraft seat is of a same type as the first seat rail adapter and of a different type as the second seat rail adapter.

7. An aircraft cabin arrangement comprising a seat rail and at least a first and a second aircraft seat that are mounted directly one after the other onto the seat rail which extends along a longitudinal direction of an aircraft cabin, the seat rail providing a grid of reference mounting position with a pre-determined grid pitch for mounting at least the first and second aircraft seat,
wherein each of the first and second aircraft seat comprises:
a seating structure having a seating area and a backrest extending upwards from the seating area wherein a seat reference point is defined at the connection between the seating area and the backrest,
a support supporting the seating structure, and
one of a first and a second seat rail adapter mounted on the support, the first and the second seat rail adapter being configured to connect the support at a reference mounting position onto the seat rail,

wherein the first aircraft seat comprises the first seat rail adapter and the second aircraft seat comprises the second seat rail adapter, wherein the first seat rail adapter comprises a first front seat rail adapter part and a first back seat rail adapter part and the second seat rail adapter comprises a second front seat rail adapter part and a second back seat rail adapter part, wherein the second seat rail adapter is structurally different than the first seat rail adapter;
wherein the first seat rail adapter is configured such that the seat reference point of the first aircraft seat is spaced in the longitudinal direction from the reference mounting position at which the first seat rail adapter is connected, by a first distance;
wherein the second seat rail adapter is configured such that the seat reference point of the second aircraft seat is spaced in the longitudinal direction from the reference mounting position at which the second seat rail adapter is connected, by a second distance; and
wherein the first distance differs from the second distance such that at least the first and the second aircraft seats, when mounted in the grid onto the seat rail, have a spacing between the respective seat reference points which is not an integer multiple of the grid pitch of the seat rail.

8. The aircraft cabin arrangement according to claim 7 , wherein each of the first and second seat rail adapters comprises at least one stud for engaging the seat rail in the grid, and a foremost of the at least one stud defines the respective reference mounting position.

9. The aircraft cabin arrangement according to claim 7 , wherein the support of each of the first and the second aircraft seat comprises a first connector assembly defining a connecting point which has a distance in the longitudinal direction to the seat reference point, this distance being the same for each of the first and the second aircraft seat, and
each of the first and second seat rail adapter of the first and second aircraft seat comprises a second connector assembly connectable at the connection point to the first connector assembly for connecting the respective one of the first and the second seat rail adapters on the support.

Assignees

• Airbus Operations Gmbh

Inventors

• Weifenbach Jörg

Classifications

• B64D11/0696 Primary

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

• B64D11/0601

  Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight · CPC title

• B60N2/01

  Arrangement of seats relative to one another · CPC title

• B60N2/01558

  with key and slot · CPC title