AIRCRAFT FOR THE TRANSPORT OF PASSENGERS HAVING LOWER DECK FACILITIES

Abstract

An aircraft includes a passenger cabin having a floor, a cargo compartment below the floor, a first access unit for accessing the cargo compartment from the passenger cabin, the first access unit being located on the floor and a utility space module arranged in the cargo. At least one part of the cargo compartment includes a first lateral half and a second lateral half in relation to a longitudinal axis of the aircraft; the lateral halves form the part of the cargo compartment. The utility space module includes a utility space cross-section in a direction normal to the longitudinal axis, which is dimensioned such that it conforms to a cross-section of one of the lateral halves of the cargo compartment. Further, the utility space module is placed exclusively in the first lateral half or the second lateral half of the cargo compartment directly below the first access unit.

Claims

1. An aircraft for the transport of passengers and/or cargo, the aircraft comprising: a passenger cabin having a cabin floor; a cargo compartment situated below the cabin floor; a first access unit to access the cargo compartment from the passenger cabin, the first access unit being located on the cabin floor; a utility space module arranged in the cargo compartment; wherein at least one part of the cargo compartment comprises a first lateral half and a second lateral half in relation to a longitudinal axis of the aircraft, which lateral halves together form the at least one part of the cargo compartment; wherein the utility space module comprises a utility space cross-section in a direction normal to the longitudinal axis, which utility space cross section is dimensioned such that it conforms a cross-section of one of the first lateral half and the second lateral half of the cargo compartment; and wherein the utility space module is placed exclusively in the first lateral half or the second lateral half of the cargo compartment directly below the access unit.

2. The aircraft of claim 1, wherein the utility space module comprises at least one access opening aligned with the access unit.

3. The aircraft of claim 1, wherein the passenger cabin comprises two aisles arranged parallel to the longitudinal axis and at a distance to each other.

4. The aircraft of claim 3, wherein the access unit is aligned with one of the two aisles in a lateral direction of the passenger cabin.

5. The aircraft of claim 1, wherein the access unit is arranged in a door region of the passenger cabin.

6. The aircraft of claim 1, wherein: the cabin floor comprises at least one dedicated monument zone comprising an aircraft adaptation providing increased structural stability or system connections; the at least one dedicated monument zone is equipped with at least one cabin monument; and the access unit is placed in the at least one dedicated monument zone.

7. The aircraft of claim 6, wherein the access unit is attached to or integrated into the at least one cabin monument.

8. The aircraft of claim 1, wherein the access unit comprises a housing having an access door.

9. The aircraft of claim 1, wherein the access unit comprises at least one of a stairs, an elevator and a ladder.

10. The aircraft of claim 1, wherein the utility space module comprises at least one crew rest compartment.

11. The aircraft of claim 10, wherein the at least one crew rest compartment comprises at least one bed arranged at an outer lateral wall of the at least one crew rest compartment.

12. The aircraft of claim 1, wherein the utility space module is located in a lateral half of the cargo compartment, which is opposite to a cargo door.

13. The aircraft of claim 12, wherein the utility space module is located in a backboard half of the cargo compartment.

14. A method of exclusively using one of a first lateral half and a second lateral half of a cargo compartment of an aircraft in relation to a longitudinal axis of the aircraft, which lateral halves together form at least one part of the cargo compartment, for receiving a utility space module in the cargo compartment directly below an access unit arranged in a passenger cabin of the aircraft, wherein the utility space module comprises a utility space cross-section in a direction normal to a longitudinal axis of the aircraft, which utility space cross section is dimensioned such that it conforms a cross-section of one of the first lateral half and the second lateral half of the cargo compartment.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0031] Further characteristics, advantages and application options of the present embodiment are disclosed in the following description of the exemplary embodiments in the figures. All the described and/or illustrated characteristics per se and in any combination form the subject of the embodiment, even irrespective of their composition in the individual claims or their interrelationships. Furthermore, identical or similar components in the figures have the same reference characters.

[0032] FIG. 1 shows a utility space module in a cargo compartment and a first access unit in a cabin of an aircraft in a three-dimensional view.

[0033] FIG. 2 shows the utility space module and cargo containers in two different lateral halves of the cargo compartment.

[0034] FIG. 3 shows an elevated view without any airframe structure of the cargo containers and the utility space module, exemplarily a crew rest compartment, without a top cover.

[0035] FIG. 4 shows the arrangement of FIG. 3 from another angle and with a top cover arranged on the utility space module, exemplarily a trolley stowage system.

[0036] FIG. 5 shows the utility space module and a further module in two different lateral halves of the cargo compartment.

[0037] FIG. 6 shows an aircraft comprising a cabin and a cargo compartment receiving the utility space module.

DETAILED DESCRIPTION

[0038] The following detailed description is merely exemplary in nature and is not intended to limit the disclosed embodiments or the application and uses thereof. Furthermore, there is no intention to be bound by any theory presented in the preceding background detailed description.

[0039] FIG. 1 shows a section of an aircraft showing a part of a passenger cabin 2 with a first access unit 4 arranged on a cabin floor 6, underneath of which a cargo compartment 8 is located. The first access unit 4 comprises a housing 10 with an access opening 12 closable by a door (not shown). Inside the housing 10, a horizontal access opening 14 reaching through the cabin floor 6 is present, through which the cargo compartment 8 may be reached by a person.

[0040] The cargo compartment 8 is separated into a first lateral half 16 and a second lateral half 18, wherein in the second lateral half 18, a utility space module 20 is located. The separation into the first and second lateral half 16 and 18 is created along a longitudinal axis 22, such that both lateral halves 16 and 18 comprise the same width.

[0041] In the depicted exemplary embodiment, the utility space module 20 has a longitudinal shape and comprises a crew rest compartment with several beds 24 arranged at a rearward portion, at a front portion and at lateral outboard portions of the utility space module 20. Access from the first access unit 4 is provided by means of a ladder 26 or stairs, through which an aisle 28 can be reached, which in turn allows access to the beds 24 placed in several sub-compartments 30, 32 and 34.

[0042] A lateral wall 36 located near the longitudinal axis 22 comprises a greater height than a more outboard located lateral wall 38, which adjoins an angled lateral wall 40 at a lower portion of the utility space module 20. The cross-sectional profile created by this design conforms the cross-sectional profile e.g. of an LD3 container and thus allows the integration into a common cargo compartment 8.

[0043] The utility space module 20 is preferably fixedly installed in the cargo compartment 8 using common installation equipment. Due to the longitudinal shape of the utility space module 20, the actual installation position is shiftable along the x-axis of the aircraft basically arbitrarily, depending on the available length of the cargo compartment 8. Hence, the location of the first access unit 4, which has to be chosen according to several constraints within the passenger cabin 2, may easily be adapted.

[0044] The aircraft fixed coordinate system shown in all figures indicates an x-direction, i.e. a longitudinal axis in the direction of flight, an y-axis, i.e. a lateral direction, as well as a z-axis, i.e. a vertical direction pointing downward.

[0045] FIG. 2 shows the integration of the utility space module 20 from a different angle. Here, the cross-sectional profile of the utility space module 20 given through the lateral walls 36 and 38 is more clearly shown. Exemplarily, a lower portion of the utility space module 20 at an outboard position comprises a step 42 instead of an angled surface 40 shown in FIG. 1. The actual design may differ in a variety of ways as the only requirement is to fit into the cargo compartment 8.

[0046] It is clear from the illustration in FIG. 2 that the utility space module 20 is exemplarily located in a backboard half of the cargo compartment 8, while the starboard half holds a row of several common cargo containers 44. These are introduced into the cargo compartment by a cargo door (not shown), which is located at the starboard half.

[0047] In FIG. 3, another exemplary embodiment of a utility space module 46 is demonstrated. Here, a possible setup of ten beds 24 is demonstrated. The interior of the utility space module 46 exemplarily comprises a separate access opening 48 just in front of a ladder 26 (or simple stairs) allows access to a separate closable sleeping compartment 50, which may exemplarily be used for a flight crew. In this example, the utility space module 46 has a length that exceeds the length of four common cargo containers arranged one behind the other in the starboard half of the cargo compartment 8.

[0048] In FIG. 4, the utility space module 46 is shown together with a row of cargo containers 44, wherein a cover 52 is disposed on top of the utility space module 46. The cover 52 may comprise at least one cover plate attached to the utility space module 46 and comprises an access opening 54, which is flush with the access opening 14 of the first access unit 4, when the utility space module 46 is installed at a predetermined location.

[0049] In FIG. 5, another combination is shown. Here, the utility space module 46 may be arranged adjacent to a second utility space module 56, which may also house a crew rest compartment or an automated trolley storage system, which may be combined with a waste management system (not shown). For simplifying the illustration of an arbitrarily designed second utility space module 56 it is shown as a block having a cover 58 including an access opening 60.

[0050] Finally, FIG. 6 shows an aircraft 62 exemplarily having a passenger cabin 64 with two decks arranged on top of each other as well as a cargo compartment 66 underneath the passenger cabin 64, which receives a utility space module according to the above description. The aircraft 62 exemplarily comprises at least two cargo doors 68 and 70 arranged at a starboard side, while the utility space module as discussed above may exemplarily be arranged at a backboard side. An exemplary door area 72 between two opposite cabin doors 74 is indicated. Here, a monument zone 76 may be arranged at a border of the door zone 72 for installing cabin monuments 78 as well as the first access unit 4.

[0051] In addition, it should be pointed out that comprising does not exclude other elements or steps, and a or an does not exclude a plural number. Furthermore, it should be pointed out that characteristics or steps which have been described with reference to one of the above exemplary embodiments can also be used in combination with other characteristics or steps of other exemplary embodiments described above. Reference characters in the claims are not to be interpreted as limitations.

[0052] While at least one exemplary embodiment has been presented in the foregoing detailed description, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the embodiment in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing an exemplary embodiment, it being understood that various changes may be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the embodiment as set forth in the appended claims and their legal equivalents.