In a cargo hold module for an aircraft, in particular a passenger aircraft, with exterior dimensions that are adjusted to a respective cargo hold of the aircraft, and suitable for securing the cargo hold module in a predetermined position in a cargo hold of the aircraft, the cargo hold module has an accessway, via which it can be accessed from a cabin of the aircraft. The cargo hold module can be hooked up to onboard electrical systems of the aircraft for power, water and/or air supply. The cargo hold module has a massage facility with at least one massage table for treating passengers or crew.

A cabin arrangement for a vehicle includes a first lateral segment module having a first main extension axis, a second lateral segment module having a second main extension axis, and an aisle. The main extension axes run parallel to each other, wherein the first lateral segment module and the second lateral segment module are distanced from each other in a direction perpendicular to the main extension axes and enclose the aisle between each other. The aisle runs parallel to the main extension axes, and the first lateral segment module has a receiving space that receives serving trolleys. The receiving space has an opening that faces into the aisle. The receiving space is designed to receive serving trolleys arranged transverse to the first main extension axis and staggered parallel to the first main extension axis.

A multifunctional container system for producing a container for a cargo compartment of an aircraft includes a first lateral container component, which forms a first lateral surface of the container that is at least partially beveled, a first lower resting surface having first fastening devices and a first top side, a second lateral container component, which forms a second lateral surface of the container that is at least partially beveled, a second lower resting surface having second fastening devices and a second top side, and a floor cladding. The cladding is selectively positionable between the first resting surface and the second resting surface, which enclose a continuous gap to each other and comprise a predetermined distance to each other and to create a protrusion that faces away from the first and second top side. The protrusion extends into a recess of a floor in a cargo compartment.

Arrangements for safety and comfort in vehicles.

A transportation system that includes one or more pods that include an interior space configured to house one or more travelers. The pods can be attached to and transported by multiple different vehicles. The different vehicles can provide for different modes of transportation. The pods are configured to supply one or more utility functions to the interior space. One or more of the utility functions to be supplied from the vehicles to the pods when the pods are attached to the vehicles.

A transportation system that includes one or more pods that each includes an interior space configured to house travelers and objects. The pods can be attached to and transported by multiple different vehicles. The different vehicles can provide for different modes of transportation depending upon the plans of the travelers. Different modes include but are not limited to ground travel, air travel, water travel, and rail travel.

A method of installing interior modules to support structures in an aircraft fuselage comprises attaching fixed ends of a plurality of tie rods to the support structures; and determining installation length of the tie rods, installation spacing between free ends of the tie rods, and installation orientation of the tie rods prior to positioning the interior module for installation. The method further comprises securing tie rod holding fixtures to the tie rods to hold the spacing and orientation at or near final configuration to facilitate installation of the interior modules.

A sub-structure for an aircraft cabin monument is disclosed. The sub-structure includes a plurality of mounting attachment points for supporting a mount to engage with a corresponding mounting attachment point on a lattice structure of a load carrying partition wall. The aircraft cabin monument is supported by the load carrying partition wall through the sub-structure, supporting a substantial weight of the monument, and relieving the cabin floor from supporting the load and weight of the aircraft cabin monument.

A set of consolidated electronics packages for staggered aircraft seats may include a first consolidated electronics package and a second consolidated electronics package. The first consolidated electronics package and a second consolidated electronics package may be installed within a primary passenger compartment. The first consolidated electronics package and the second consolidated electronics package may be configured to provide electrical connectivity to the primary passenger compartment and an auxiliary passenger compartment including an auxiliary aircraft seat. A primary aircraft seat and the auxiliary aircraft seat may be installed in a staggered configuration within an aircraft cabin including the primary passenger compartment and the auxiliary passenger compartment.

An ultra light weight aircraft composite galley architecture system and method comprises composite construction of a partially molded aircraft monument structure based on embedded load bearing hoops and beams used in conjunction with pre formed composite flat panel construction. An upper L shaped structural section mates with a lower inverted L shaped structural section forming a structure upon which additional panels are joined to form the complete composite galley. This system and method of construction produces a high strength aircraft monument capable of maintaining aircraft structural flight and crash load requirements without external monument extrusions for support. This galley architecture system and method of construction creates an aircraft monument with desirable reduction in weight with no loss of required structural strength.