Method for boarding and unloading of passengers of an aircraft with reduced immobilization time of the aircraft, aircraft and air terminal for its implementation
AssigneeAirbus Operations GmbH
InventorYann-Henri Laudrain
Life of this patent
Estimating the term…
Abstract
Methods for transferring a payload such as passengers and/or luggage and/or freight between an airport and a cabin of an aircraft are provided. Air terminals, aircraft and removable cabin modules suitable for implementing these methods are also provided. An aircraft is provided which includes a removable cabin module. A docking module is also provided for transferring a removable cabin module between an aircraft and an airport. A method for modifying the internal configuration of the cabin of such an aircraft by replacing a removable cabin module of the aircraft is also provided.
Claims19
An aircraft comprising:
- a removable cabin module, comprising a floor, an upper aircraft fuselage portion connected to the floor, and a first and a second end wall, wherein the first and second end walls, the floor and the upper aircraft fuselage portion form a cabin for transport of passengers, luggage, freight or combinations thereof;
- a reception space for receiving the removable cabin module;
- a nose cone comprising a cockpit and a transverse wall;
- a tail cone comprising a tail unit and a transverse wall;
- a lower structure comprising a lower fuselage portion truncated in a horizontal plane, wherein the reception space is delimited between the transverse wall of the nose cone and the transverse wall of the tail cone, and above the horizontal plane of the lower structure;
- a centring device for centring the removable cabin module in the reception space;
- and
- a retaining device for retaining the removable cabin module in the reception space, wherein the retaining device comprises a first docking device for securely coupling the floor of the removable cabin module to the horizontal plane of the lower structure, wherein the first docking device comprises a first element forming a hook which is coupled securely to the floor of the removable cabin module, and a second element forming a hook coupled securely to the horizontal plane of the lower structure, wherein the retaining device comprises a second docking device for securely coupling the first or second end wall of the removable cabin module to the transverse wall of the nose cone or the transverse wall of the tail cone, wherein the second docking device comprises a lengthways rod retractably housed in a bore in the transverse wall of the nose cone, the transverse wall of the tail cone, or both.
A removable cabin module for an aircraft comprising:
- a floor;
- an upper aircraft fuselage portion connected to the floor;
- a first and a second end wall;
- a centring device;
- and
- a retaining device, wherein the retaining device comprises a first docking device for securely coupling the floor of the removable cabin module to a reception space of the aircraft, wherein the first docking device comprises a first element forming a hook which is coupled securely to the floor of the removable cabin module, and a second element forming a hook coupled securely to a horizontal plane of a lower structure of the aircraft, wherein the retaining device comprises a second docking device for securely coupling the first or second end wall of the removable cabin module to the reception space of the aircraft, wherein the second docking device comprises a lengthways rod retractably housed in a bore of at least one transverse wall of the aircraft;
- wherein the first and second end walls, the floor and the upper aircraft fuselage portion form a cabin for transport of passengers, luggage, freight or combinations thereof;
- wherein the removable cabin module is receivable in the reception space of the aircraft;
- wherein the centring device centers the removable cabin module in the reception space of the aircraft;
- and
- wherein the retaining device retains the removable cabin module in the reception space of the aircraft.
Dependencies are inferred from the claim text.