Method of determining a seating arrangement

Patent metadata

Field	Value
Publication number	US-9783302-B2
Application number	US-201615202492-A
Country	US
Kind code	B2
Filing date	Jul 5, 2016
Priority date	May 15, 2014
Publication date	Oct 10, 2017
Grant date	Oct 10, 2017

Abstract

A method of determining a seating arrangement for an aircraft cabin includes entering configuration parameters into a processor including a cabin width, a quantity of aisles, a minimum aisle width, and a quantity of columns of seats, wherein each seat is movable between a seated configuration and a bed configuration. The method additionally includes entering seat parameters describing the taper in seat width from a main portion to a footrest, and entering configuration rules wherein in at least one column of an inboard column set and/or an outboard column set, the seats are reversed in direction and/or are staggered. The method further includes determining, using the processor, a seating arrangement including a column quantity in each column set, and a seat direction and/or a stagger for each column in the seating arrangement that results in a maximum seat width at a main portion of the seats.

First claim

What is claimed is:

1. A method of determining a seating arrangement for an aircraft cabin, comprising the steps of:
entering configuration parameters into a processor, including a cabin width, a quantity of aisles, a minimum aisle width, and a quantity of columns of seats, wherein each seat is movable between a seated configuration and a bed configuration having a seat width that tapers from a main portion to a footrest;
entering seat parameters describing a taper in seat width from the main portion to the footrest;
entering configuration rules into the processor, including:
in at least one column of at least one of an inboard column set and an outboard column set, the seats are at least one of reversed in direction and staggered; and

determining, using the processor, a seating arrangement including a column quantity in each column set, and at least one of a seat direction and a stagger for each column in the seating arrangement that results in a maximum seat width at a main portion of the seats.

2. The method of claim 1 , wherein the configuration rules further include:
the seats are arranged in at least one outboard column set containing at least one of three or more columns and at least one inboard column set containing five or more columns.

3. The method of claim 1 , further including:
entering into the processor a seat parameter of a maximum offset of the footrest from a seat centerline.

4. The method of claim 1 , wherein the configuration rules further include:
in at least one column of at least one of an inboard column set and an outboard column set, a maximum of two columns are staggered; and
in an inboard column set, if two columns are staggered, the columns are adjacent to one another.

5. The method of claim 1 , wherein the configuration parameters include zone parameters, the method further including:
entering zone parameters into the processor including a cabin length and a minimum path width between the seats in a same column; and
entering into the processor a seat parameter of a minimum seat length.

6. The method of claim 1 , wherein the configuration rules further include:
in at least one column of at least one of an inboard column set and an outboard column set, the seats are reversed in direction and are transversely aligned with the seats in at least one of an adjacent column and an across-aisle column.

7. The method of claim 1 , wherein the configuration rules further include:
in at least one column of at least one of an inboard column set and an outboard column set, the seats have a same direction and are staggered relative to the seats in at least one of an adjacent column and an across-aisle column.

8. The method of claim 1 , wherein the configuration rules further include:
in at least one column the seats are staggered such that the footrest of the seats in one column are located at an approximate midpoint of the seat in an adjacent column.

9. The method of claim 1 , wherein the configuration rules further include:
in at least one column the footrest of the seats are located adjacent to a seat bottom of a seat in an adjacent column.

10. The method of claim 1 , wherein the configuration rules further include:
the seating arrangement is non-symmetrical about a longitudinal centerline of the aircraft cabin.

11. The method of claim 1 , wherein:
each seat has a seat centerline oriented at a seat angle relative to a longitudinal axis of an aircraft cabin.

12. The method of claim 1 , wherein:
each seat has a seat centerline;
the seats are arranged in at least one column; and
the seat centerline of the seats in the at least one column are parallel to one another.

13. The method of claim 1 , wherein:
the seats are arranged in two or more columns; and
the footrest of a seat in one column faces the footrest of a seat of an adjacent column.

14. The method of claim 1 , wherein:
the seats are arranged in at least one outboard column set containing at least one of three or more columns and at least one inboard column set containing five or more columns.

15. The method of claim 1 , wherein:
the seating arrangement includes at least two aisles.

16. The method of claim 1 , wherein:
the seats in adjacent columns are staggered.

17. A method of determining a seating arrangement for an aircraft cabin, comprising the steps of:
entering configuration parameters into a processor, including a cabin width, a quantity of aisles, a minimum aisle width, and a quantity of columns of seats, wherein each seat is movable between a seated configuration and a bed configuration having a seat width that tapers from a main portion to a footrest, each seat having direct, unimpeded access to an aisle of the aircraft cabin when adjacent seats are in the bed configuration;
entering seat parameters describing a taper in seat width from the main portion to the footrest;
entering configuration rules into the processor, including:
in at least one column of at least one of an inboard column set and an outboard column set, the seats are at least one of reversed in direction and staggered; and

determining, using the processor, a seating arrangement including a column quantity in each column set, and at least one of a seat direction and a stagger for each column in the seating arrangement that results in a maximum seat width at a main portion of the seats.

18. The method of claim 1 , wherein:
the aircraft cabin has opposing sidewalls and a single aisle dividing the seats into an outboard column set containing two columns and an outboard column set containing three columns, each outboard column set has a sidewall column located immediately adjacent one of the sidewalls and an aisle column located immediately adjacent the aisle, the seats in each outboard column set are non-reversed;
each seat has a seat centerline oriented at a seat angle relative to a longitudinal axis of an aircraft cabin;
in each column, the seat centerline of the seats are parallel to one another;
in the outboard column set containing two columns:
the seats in the sidewall column are staggered relative to the seats in the aisle column;
the seat centerline of the seats in the sidewall column are non-parallel to the seat centerline of the seats in the aisle column; and

in the outboard column sets containing three columns:
the seats in the sidewall column are staggered relative to the seats in the column located between the sidewall column and the aisle column;
the seat centerline of the seats in the sidewall column are non-parallel to the seat centerline of the seats in the column located between the sidewall column and the aisle column;
the seats in the aisle column are generally longitudinally aligned with the seats in the column immediately adjacent; and
the seat centerline of the seats in the aisle column are parallel to the seat centerline of the seats in the column located between the sidewall column and the aisle column.

19. The method of claim 1 , wherein:
the aircraft cabin has opposing sidewalls and a single aisle dividing the seats into an outboard column set containing two columns and an outboard column set containing three columns, each outboard column set has a sidewall column located immediately adjacent one of the sidewalls and an aisle column located immediately adjacent the aisle, the seats in each outboard column set are non-reversed;
each seat has a seat centerline;
in each column, the seat centerline of the seats are parallel to one another;
in the outboard column set containing two columns:
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Assignees

• Boeing Co

Inventors

• Eakins Mark E

Classifications

• B64D11/06

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

• B64D11/0601 Primary

  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

• B60N2/34

  into a bed · CPC title

• B64F5/00

  Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for · CPC title

• B64D11/0606

  with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title