Aircraft galley configuration
Embodiments of the present invention provide improved layouts that can increase space on-board aircraft and other passenger transport vehicles. The improved layouts may include two galley sections installed on an aircraft having a centerline and curved outer sidewalls. The first galley section can be positioned so that its longitudinal axis generally aligns with one of the outer sidewalls of the aircraft, and the second galley section can be positioned so that its longitudinal axis generally aligns with the longitudinal axis of the first galley. This can create a space along a rear side of the second galley section. The created space may be used for any number of options.
1. A galley layout for a vehicle, the vehicle having a centerline and vehicle sidewalls, the galley layout comprising:
at least two galley sections, each of the galley sections having a longitudinal axis, wherein the at least two galley sections are positioned so that longitudinal axes of the at least two galley sections are not aligned with the vehicle centerline, wherein a triangular compartment comprising upper and lower crew rest levels is created along a rear wall of one of the at least two galley sections, the triangular compartment defined at least in part by (a) the galley section rear wall that faces one of the vehicle sidewalls and (b) a sidewall of the vehicle.
2. The galley layout of claim 1 , wherein the upper and lower crew rest levels are configured for use as a storage area, a closet, for housing aircraft electronics or other equipment, for storing safety equipment, or any combination thereof.
3. The galley layout of claim 1 , wherein the at least two galley sections are both rotated or angled to one side of the centerline.
4. A galley layout for an aircraft, comprising:
(a) first and second galley sections, each of the first and second galley sections having a longitudinal axis,
(b) the aircraft having (i) a center plane that divides the aircraft into left and right hand sides and (ii) outer sidewalls defining planes that angle outwardly from the center plane,
(c) the first and second galley sections each further comprising rear walls that face the outer sidewalls of the aircraft,
wherein the first galley section is positioned so that the longitudinal axis of the first galley section is parallel with one of the outer sidewall planes and wherein the first and second galley sections are angled to one side of the center plane, wherein an enclosed triangular compartment is created along a side of the second galley section, the triangular compartment defined at least in part by the rear wall of the second galley section, the outer sidewall of the aircraft, and a privacy curtain or closeable door.
5. The galley layout of claim 4 , wherein the second galley section is positioned so that the longitudinal axis of the second galley section is generally parallel with the longitudinal axis of the first galley section.
6. The galley layout of claim 4 , wherein the longitudinal axes of the first and second galley sections are generally parallel to one another, but are not parallel to the aircraft center plane.
7. The galley layout of claim 6 , wherein the enclosed triangular compartment is configured for use as a crew rest space.
8. The galley layout of claim 6 , wherein the enclosed triangular compartment is configured for use as a lavatory.
9. The galley layout of claim 6 , wherein the enclosed triangular compartment is configured for use as a storage area, for housing a vending machine, a closet, for housing aircraft electronics or other equipment, for storing safety equipment, or any combination thereof.
10. The galley layout of claim 4 , wherein the first and second galley sections are both rotated to one side of the center plane.
11. A galley layout for an aircraft, the aircraft having a centerline and curved outer sidewalls, the galley layout comprising:
first and second galley sections, each of the first and second galley sections having a longitudinal axis and rear walls, wherein the first galley section is positioned so that the longitudinal axis of the first galley section is parallel to one of the aircraft curved outer sidewalls, and wherein the second galley section is positioned so that the longitudinal axis of the second galley section is parallel to the longitudinal axis of the first galley section but not parallel to the outer sidewall such that the first and second galley sections are not aligned with the centerline of the aircraft, wherein a pie-shaped compartment is created along a rear side of the second galley section, the compartment defined at least in part by (a) the second galley section rear wall that faces the aircraft curved outer sidewall and (b) the curved outer sidewall of the aircraft.
12. The galley layout of claim 11 , wherein the pie-shaped compartment is configured for use as a crew rest space.
13. The galley layout of claim 11 , wherein the pie-shaped compartment is configured for use as a lavatory.
14. The galley layout of claim 11 , wherein the pie-shaped compartment is configured for use as a storage area, for housing a vending machine, a closet, for housing aircraft electronics or other equipment, for storing safety equipment, or any combination thereof.
15. The galley layout of claim 11 , wherein the first and second galley sections are both rotated to one side of the center plane.
16. The galley layout of claim 1 , wherein the longitudinal axes of the at least two galley sections are parallel to one another.
17. The galley layout of claim 1 , further comprising a privacy curtain or closeable door for the compartment comprising two crew rest levels.