An enclosed patient suite may include a plurality of suite walls, a patient bed positioned in a patient area defined within the plurality of suite walls, a plurality of medical systems with at least some of the plurality of medical systems mounted to the plurality of suite walls, a plurality of support members coupled to the plurality of suite walls, a plurality of wheels with a particular wheel of the plurality of wheels coupled to a corresponding support member of the plurality of support members, a rail brake configured to engage a floor-mounted rail in a floor of at least one of a cargo hold or a cabin of an aircraft, and a controller coupled to the plurality of medical systems and configured to receive data from and transmit data to the plurality of medical systems. The enclosed patient suite may be dimensioned to fit within the aircraft.

The invention provides aeromedical ambulance equipment. In some embodiments, the equipment includes a module base comprising a mount assembly having an unlocked configuration and a locked configuration. The mount assembly preferably can be adjusted between the unlocked and locked configurations by a tool-free operation. In addition, certain embodiments provide a module base having an advantageous system for releasably locking a stretcher onto the module base.

A vehicle includes a passenger cabin, a monument, a pet travel system, and a ventilation system. The pet travel system includes at least a portion of the monument and at least one pet storage module configured to be received in the portion of the monument. The ventilation system includes an inlet port defined in the at least one pet storage module, an exhaust port defined in the at least one pet storage module, and an exhaust duct. The inlet port is in flow communication with an air source outside of the pet travel system. The exhaust duct is in flow communication with the exhaust port. The pressure within the exhaust duct is lower than the pressure of the air source to cause air to flow from the air source through the at least one pet storage module from the inlet port to the exhaust port.

An aircraft passenger compartment suite may include at least one single passenger compartment including at least one single aircraft seat. The at least one single aircraft seat may be configured to seat a single passenger. The aircraft passenger compartment suite may include a combined divan passenger compartment with a combined divan aircraft seat. The combined divan aircraft seat may be configured to seat at least one passenger. The combined divan aircraft seat may have a width greater than a width of the at least one single aircraft seat. The combined divan passenger compartment may include a stowage compartment configured to stow large passenger amenities in a substantially vertical orientation. The aircraft passenger compartment suite may include a privacy divider separating the combined divan passenger compartment and the at least one single passenger compartment.

An isolation section assembly includes a section housing defining an interior space. The section housing includes a door with access to the interior space. The isolation section assembly includes an enclosure abutting the door. The airlock enclosure defines an interior airlock space. The interior airlock space is configured and adapted to be at a negative pressure relative to a cabin area. An air recirculation system in fluid communication with at least one of the interior space of the section housing or the interior airlock space.

An aircraft berth includes a bowed slat surface; the bowed slats provide a degree of cushioning apart from a foam mattress. The bowed slats are held in deformable brackets that allow the bowed slats to expand laterally as they are compressed vertically, and allow a degree of twisting of individual bowed slats. The bowed slats may be placed in a berth frame with greater or lesser density along the length of the berth frame to provide more or less support at particular locations. Alternatively, or in addition, bowed slats with greater cross-sectional thickness may be used were more support is desirable. The bowed slats may be organized in sub-frames that may be oriented to provide head and/or knee support.

An aircraft berth includes a bowed slat surface; the bowed slats provide a degree of cushioning apart from a foam mattress. The bowed slats are held in deformable brackets that allow the bowed slats to expand laterally as they are compressed vertically, and allow a degree of twisting of individual bowed slats. The bowed slats may be placed in a berth frame with greater or lesser density along the length of the berth frame to provide more or less support at particular locations. Alternatively, or in addition, bowed slats with greater cross-sectional thickness may be used were more support is desirable. The bowed slats may be organized in sub-frames that may be oriented to provide head and/or knee support.

The present invention generally relates to bed structures having an inflatable and/or collapsible/deflatable component. More particularly, it relates to bed construction configurations that can include multiple adaptations for enhanced safety in situations of rapid loss of aircraft cabin pressure to meet airflow requirements for emergency decompression events as well as to provide overall better airflow for in-cabin air filtration systems. The bed configurations can include cross-welded structures and bowing-prevention stabilizers to control bulging of the bed when inflated.

The invention provides aeromedical ambulance equipment. In some embodiments, the equipment includes a module base comprising a mount assembly having an unlocked configuration and a locked configuration. The mount assembly preferably can be adjusted between the unlocked and locked configurations by a tool-free operation. In addition, certain embodiments provide a module base having an advantageous system for releasably locking a stretcher onto the module base.

Disclosed is a modular seat for aircraft. The system has a frame that is able to be interconnected with other frames laterally. Since each lateral frame has the same pivot points (when viewed from the side), the linked seats rotate together. The seats also include buckle lugs which enable a particular seat to be used on either side of the aircraft.