초록 ▼

A module for an aircraft is provided for the accommodation of crew members. The module includes, but is not limited to a trough-shaped floor region having an external contour that corresponds to the contour of further stowage bins installed in the aircraft. The storage space created in this way in t

A module for an aircraft is provided for the accommodation of crew members. The module includes, but is not limited to a trough-shaped floor region having an external contour that corresponds to the contour of further stowage bins installed in the aircraft. The storage space created in this way in the interior of the module is accessible from the interior of the module. In this way the stability of the module may be enhanced and the installation expenditure may be reduced. Furthermore, comfort may be enhanced, in particular as a result of more space being available for the crew.

대표청구항 ▼

1. A module in an aircraft for an accommodation of crew members, comprising: an interior;a floor region comprising a module stowage bin of the aircraft integrated therein; andan access to the module stowage bin from the interior;wherein the module is designed for installation in a ceiling region of

1. A module in an aircraft for an accommodation of crew members, comprising: an interior;a floor region comprising a module stowage bin of the aircraft integrated therein; andan access to the module stowage bin from the interior;wherein the module is designed for installation in a ceiling region of a passenger cabin of the aircraft; andwherein the floor region and said module stowage bin comprise an external contour that corresponds to a hatrack contour of a hatrack chain in the aircraft. 2. The module of claim 1, wherein the exterior contour is closed so that the module stowage bin is exclusively accessible from the interior of the module. 3. The module of claim 1, wherein the module stowage bin comprises an inward-directed opening with a closing arrangement that is adapted to be opened and closed. 4. The module of claim 3, wherein the closing arrangement is designed as a trap door. 5. The module of claim 3, wherein the closing arrangement is designed as a bed that can be hinged up sideways and arranged on the module stowage bin. 6. The module of claim 3, wherein the closing arrangement is designed as a sliding door and a rubber net. 7. The module of claim 3, wherein the closing arrangement is designed as rubber net. 8. The module of claim 1, further comprising an ascent unit for the crew members to climb up from a level of the passenger cabin into the interior of the module. 9. The module of claim 1, further comprising a rest region for the crew members wherein the rest region comprises a bed. 10. The module of claim 1, further comprising a work area, wherein the floor region comprises a stowage bin storage space of the aircraft, wherein the stowage bin storage space is accessible from the interior of the module, and wherein the work area is in part arranged in the stowage bin storage space. 11. The module of claim 10, wherein the work area comprises a chair and a table. 12. The module of claim 1, wherein the module stowage bin is integrated in the module. 13. The module of claim 1, wherein the module stowage bin is accessible both from the passenger cabin and from the interior of the module. 14. The module of claim 13, wherein the module stowage bin comprises a locking mechanism, wherein the locking mechanism is designed such that the module stowage bin is accessible from the passenger cabin only to selected users. 15. The module of claim 14, wherein the locking mechanism comprises a lock. 16. The module of claim 13, wherein the module stowage bin is designed to be lowered when opened from the passenger cabin. 17. The module of claim 13, wherein the module stowage bin is designed to form part of a bottom region of the module and is thus immovable when opening. 18. The module of claim 13, wherein the module stowage bin comprises a hinged lid. 19. An aircraft, comprising: a fuselage; anda module for an accommodation of a crew member, the module arranged within the fuselage, the module comprising: an interior;a floor region comprising a module stowage bin of the aircraft integrated therein; andan access to the module stowage bin from the interior,wherein the module is designed for installation in a ceiling region of a passenger cabin of the aircraft; andwherein the floor region and said module stowage bin comprise an external contour that corresponds to a hatrack contour of a hatrack chain in the aircraft.