A system and method according to which goods and services are provided during vehicular travel. In an exemplary embodiment, the vehicle is an airplane operated by a commercial airline.

Passenger seat assemblies including thermoelectric devices are described herein. An example passenger seat assembly may include a seat shell configured to receive a passenger seat. The seat shell (20) may include a plurality of surfaces. The passenger seat assembly may also include a thermoelectric device (78) disposed below or within at least one of the surfaces to define a thermal zone. The thermoelectric device may include a first side and a second side. The first side may be adjacent to the at least one surface. The thermoelectric device may be configured such that application of a first current having a first polarity causes a temperature of the thermal zone to increase, and application of a second current having a second polarity causes the temperature of the thermal zone to decrease.

Described is an aircraft suite having an aircraft seat for use by a passenger, the aircraft suite also having a controller, for controlling a number of output states of the aircraft suite, the controller having a logic condition receiver for receiving a logic condition input, and distance measurement equipment for measuring a distance between a first location within the suite and a second location within the suite, and providing a distance input to a distance receiver of the controller, wherein, in use, the controller controls at least one of the output states of the aircraft suite based upon both the logic condition input and the distance input. The invention also provides a method of controlling an environment within an aircraft suite.

Methods, systems, and apparatuses for temporarily increasing, on demand, the relative humidity of an area located proximate to a user in environments having lower than ambient relative humidity are provided by integrating a personal humidification circuit into a water delivery circuit to provide a diverted flow of water, and provide a flow of water vapor to a user, and returning the relative humidity-enhanced environment to a predetermined relative humidity by purging the environment.

The germ protection system for vehicles, hospitals, restaurants, schools, nursing homes, lifts and the like uses: a) A system that prevents germs: bacteria, protozoa, viruses or parasites from being breathed in vehicles or closed premises, lifts or the like, blowing or sucking air, b) An independent air installation that applies air conditioning, fed with turbofan engines, to the individual air blowing nozzles in the ceiling or backrest of the compartments of each passenger, c) An independent air installation using compressors that extracts and compresses the outside air, and apply it to the individual air blowing nozzles in the ceiling or backrest of the compartments of each passenger, d) A system that uses an individual installation to replace oxygen system in case of emergency, e) A system that is valid simultaneously for protection against germs and for breathing in case of emergency. The air is filtered, disinfected, its pressure, temperature and humidity regulated, and through some ducts it is applied to the masks, helmets, hoods, their ducts or nasal cannulas. f), A system that is coupled to the individual air supply nozzle of the passengers, using for this purpose at the end of the duct of the mask, face mask screen, diving suit or helmet.

A vehicle seat includes a seat frame including a pan frame (12), a blower, and a bracket (50) configured to attach the blower to the pan frame (12). The bracket (50) is provided with a first engagement portion (110) protruding toward the pan frame (12), and the pan frame (12) is provided with a first engagement hole (12A) in which the first engagement portion (110) is engageable. The first engagement portion (110) includes a first stopper portion (112) configured to be locked to the pan frame (12) when the first engagement portion (110) is engaged in the first engagement hole (12A), and a first elastically deformable portion (113) configured to deform elastically to allow the first stopper portion (112) to pass through the first engagement hole (12A) when the first engagement portion (110) is inserted into the first engagement hole (12A).

Two-stage vortex tube assemblies including an internal vortex generation chamber for generating a main vortex and a compressed air inlet having a tangential outlet port for creating a pre-vortex in an inflow of compressed air in a direction of flow of the main vortex. The two-stage vortex assemblies may be utilized in low pressure and low flow applications such as seat climatization, local heating or cooling, etc. Further disclosed are seat constructions and seat climatization systems utilizing a two-stage vortex tube as a single source for heating or cooling.

Provided is an aircraft seat that enhances passenger comfort and reduces the burden on cabin attendants. The aircraft seat includes a base with a relatively movable seat portion and a backrest portion; an actuator for relatively moving the seat portion and the backrest portion; a biometric sensor installed on the base and configured to obtain biometric information of a passenger; a plurality of elastic members installed on the base; a modification device configured to change an elastic force of at least one elastic member, and a control device, wherein the control device operates the actuator or the modification device in response to a signal from the biometric sensor.

A seat assembly includes an external structure, at least one seating support surface, a valve, and at least one air distribution passageway. The external structure has a cavity therein. The at least one seating support surface is configured for contact with an occupant. The valve is disposed within the cavity and is in fluid communication with an external air supply. The at least one air distribution passageway is in fluid communication with the valve and is interposed between the valve and the at least one seating support surface. Air from the external air supply is directed to the seating support surface via the valve and the at least one passageway.

The present invention achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present invention includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.